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| author | Anton Babushkin <anton.babushkin@me.com> | 2014-05-17 23:31:14 +0200 |
|---|---|---|
| committer | Anton Babushkin <anton.babushkin@me.com> | 2014-05-17 23:31:14 +0200 |
| commit | cb18b8e06485e1426471e7b41fba621747574ec0 (patch) | |
| tree | 0055217fe8f505aeb040faa16dd94d6b8e67a5c9 | |
| parent | a8701ed3084fdf7f495baee843af4d636eb1aa0b (diff) | |
| parent | 98f05ea5c127acd3d8ff0ebcba109f9e326a129b (diff) | |
| download | px4-firmware-cb18b8e06485e1426471e7b41fba621747574ec0.tar.gz px4-firmware-cb18b8e06485e1426471e7b41fba621747574ec0.tar.bz2 px4-firmware-cb18b8e06485e1426471e7b41fba621747574ec0.zip | |
Merge branch 'master' into mpc_auto_gain
532 files changed, 23525 insertions, 10526 deletions
diff --git a/.gitignore b/.gitignore index 71326517f..afd63e06a 100644 --- a/.gitignore +++ b/.gitignore @@ -34,5 +34,8 @@ mavlink/include/mavlink/v0.9/ /Documentation/html/ /Documentation/doxygen*objdb*tmp .tags +tags .tags_sorted_by_file .pydevproject +.ropeproject +*.orig diff --git a/.ycm_extra_conf.py b/.ycm_extra_conf.py new file mode 100644 index 000000000..fed5cd28a --- /dev/null +++ b/.ycm_extra_conf.py @@ -0,0 +1,173 @@ +# This file is NOT licensed under the GPLv3, which is the license for the rest +# of YouCompleteMe. +# +# Here's the license text for this file: +# +# This is free and unencumbered software released into the public domain. +# +# Anyone is free to copy, modify, publish, use, compile, sell, or +# distribute this software, either in source code form or as a compiled +# binary, for any purpose, commercial or non-commercial, and by any +# means. +# +# In jurisdictions that recognize copyright laws, the author or authors +# of this software dedicate any and all copyright interest in the +# software to the public domain. We make this dedication for the benefit +# of the public at large and to the detriment of our heirs and +# successors. We intend this dedication to be an overt act of +# relinquishment in perpetuity of all present and future rights to this +# software under copyright law. +# +# THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, +# EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF +# MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT. +# IN NO EVENT SHALL THE AUTHORS BE LIABLE FOR ANY CLAIM, DAMAGES OR +# OTHER LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, +# ARISING FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR +# OTHER DEALINGS IN THE SOFTWARE. +# +# For more information, please refer to <http://unlicense.org/> + +import os +import ycm_core + +# These are the compilation flags that will be used in case there's no +# compilation database set (by default, one is not set). +# CHANGE THIS LIST OF FLAGS. YES, THIS IS THE DROID YOU HAVE BEEN LOOKING FOR. +flags = [ +'-Wall', +'-Wextra', +'-Werror', +#'-Wc++98-compat', +'-Wno-long-long', +'-Wno-variadic-macros', +'-fexceptions', +'-DNDEBUG', +# You 100% do NOT need -DUSE_CLANG_COMPLETER in your flags; only the YCM +# source code needs it. +#'-DUSE_CLANG_COMPLETER', +# THIS IS IMPORTANT! Without a "-std=<something>" flag, clang won't know which +# language to use when compiling headers. So it will guess. Badly. So C++ +# headers will be compiled as C headers. You don't want that so ALWAYS specify +# a "-std=<something>". +# For a C project, you would set this to something like 'c99' instead of +# 'c++11'. +'-std=c++11', +# ...and the same thing goes for the magic -x option which specifies the +# language that the files to be compiled are written in. This is mostly +# relevant for c++ headers. +# For a C project, you would set this to 'c' instead of 'c++'. +'-x', +'c++', +'-undef', # get rid of standard definitions to allow us to include arm math header +'-I', os.path.join(os.path.expanduser("~"),'gcc-arm-none-eabi-4_7-2013q3/arm-none-eabi/include'), +'-I', 'Build/px4io-v1_default.build/nuttx-export/include/', +'-I', 'Build/px4io-v2_default.build/nuttx-export/include/', +'-I', './NuttX/nuttx/arch/arm/include', +'-include', './src/include/visibility.h', +'-I', './src', +'-I', './src/modules', +'-I', './src/include', +'-I', './src/lib', +'-I', './NuttX', +] + + +# Set this to the absolute path to the folder (NOT the file!) containing the +# compile_commands.json file to use that instead of 'flags'. See here for +# more details: http://clang.llvm.org/docs/JSONCompilationDatabase.html +# +# Most projects will NOT need to set this to anything; you can just change the +# 'flags' list of compilation flags. Notice that YCM itself uses that approach. +compilation_database_folder = '' + +if os.path.exists( compilation_database_folder ): + database = ycm_core.CompilationDatabase( compilation_database_folder ) +else: + database = None + +SOURCE_EXTENSIONS = [ '.cpp', '.cxx', '.cc', '.c', '.m', '.mm' ] + +def DirectoryOfThisScript(): + return os.path.dirname( os.path.abspath( __file__ ) ) + + +def MakeRelativePathsInFlagsAbsolute( flags, working_directory ): + if not working_directory: + return list( flags ) + new_flags = [] + make_next_absolute = False + path_flags = [ '-isystem', '-I', '-iquote', '--sysroot=' ] + for flag in flags: + new_flag = flag + + if make_next_absolute: + make_next_absolute = False + if not flag.startswith( '/' ): + new_flag = os.path.join( working_directory, flag ) + + for path_flag in path_flags: + if flag == path_flag: + make_next_absolute = True + break + + if flag.startswith( path_flag ): + path = flag[ len( path_flag ): ] + new_flag = path_flag + os.path.join( working_directory, path ) + break + + if new_flag: + new_flags.append( new_flag ) + return new_flags + + +def IsHeaderFile( filename ): + extension = os.path.splitext( filename )[ 1 ] + return extension in [ '.h', '.hxx', '.hpp', '.hh' ] + + +def GetCompilationInfoForFile( filename ): + # The compilation_commands.json file generated by CMake does not have entries + # for header files. So we do our best by asking the db for flags for a + # corresponding source file, if any. If one exists, the flags for that file + # should be good enough. + if IsHeaderFile( filename ): + basename = os.path.splitext( filename )[ 0 ] + for extension in SOURCE_EXTENSIONS: + replacement_file = basename + extension + if os.path.exists( replacement_file ): + compilation_info = database.GetCompilationInfoForFile( + replacement_file ) + if compilation_info.compiler_flags_: + return compilation_info + return None + return database.GetCompilationInfoForFile( filename ) + + +def FlagsForFile( filename, **kwargs ): + if database: + # Bear in mind that compilation_info.compiler_flags_ does NOT return a + # python list, but a "list-like" StringVec object + compilation_info = GetCompilationInfoForFile( filename ) + if not compilation_info: + return None + + final_flags = MakeRelativePathsInFlagsAbsolute( + compilation_info.compiler_flags_, + compilation_info.compiler_working_dir_ ) + + # NOTE: This is just for YouCompleteMe; it's highly likely that your project + # does NOT need to remove the stdlib flag. DO NOT USE THIS IN YOUR + # ycm_extra_conf IF YOU'RE NOT 100% SURE YOU NEED IT. + #try: + # final_flags.remove( '-stdlib=libc++' ) + #except ValueError: + # pass + else: + relative_to = DirectoryOfThisScript() + final_flags = MakeRelativePathsInFlagsAbsolute( flags, relative_to ) + + return { + 'flags': final_flags, + 'do_cache': True + } diff --git a/Debug/NuttX b/Debug/NuttX index 3b95e96b2..d34e9f5b4 100644 --- a/Debug/NuttX +++ b/Debug/NuttX @@ -34,10 +34,10 @@ define _showheap else set $MM_ALLOC_BIT = 0x80000000 end - printf "HEAP %d %p - %p\n", $index, g_heapstart[$index], g_heapend[$index] + printf "HEAP %d %p - %p\n", $index, g_mmheap.mm_heapstart[$index], g_mmheap.mm_heapend[$index] printf "ptr size\n" - set $node = (char *)g_heapstart[$index] + sizeof(struct mm_allocnode_s) - while $node < g_heapend[$index] + set $node = (char *)g_mmheap.mm_heapstart[$index] + sizeof(struct mm_allocnode_s) + while $node < g_mmheap.mm_heapend[$index] printf " %p", $node set $nodestruct = (struct mm_allocnode_s *)$node printf " %u", $nodestruct->size @@ -47,7 +47,7 @@ define _showheap else set $used = $used + $nodestruct->size end - if ($nodestruct->size > g_heapsize) || (($node + $nodestruct->size) > g_heapend[$index]) + if ($nodestruct->size > g_mmheap.mm_heapsize) || (($node + $nodestruct->size) > g_mmheap.mm_heapend[$index]) printf " (BAD SIZE)" end printf "\n" @@ -59,7 +59,7 @@ define _showheap end define showheap - set $nheaps = sizeof(g_heapstart) / sizeof(g_heapstart[0]) + set $nheaps = sizeof(g_mmheap.mm_heapstart) / sizeof(g_mmheap.mm_heapstart[0]) printf "Printing %d heaps\n", $nheaps set $heapindex = (int)0 while $heapindex < $nheaps diff --git a/Debug/Nuttx.py b/Debug/Nuttx.py index 093edd0e0..7cc21b99f 100644 --- a/Debug/Nuttx.py +++ b/Debug/Nuttx.py @@ -306,12 +306,15 @@ class NX_show_heap (gdb.Command): def __init__(self): super(NX_show_heap, self).__init__('show heap', gdb.COMMAND_USER) - if gdb.lookup_type('struct mm_allocnode_s').sizeof == 8: - self._allocflag = 0x80000000 - self._allocnodesize = 8 - else: + struct_mm_allocnode_s = gdb.lookup_type('struct mm_allocnode_s') + preceding_size = struct_mm_allocnode_s['preceding'].type.sizeof + if preceding_size == 2: self._allocflag = 0x8000 - self._allocnodesize = 4 + elif preceding_size == 4: + self._allocflag = 0x80000000 + else: + raise gdb.GdbError('invalid mm_allocnode_s.preceding size %u' % preceding_size) + self._allocnodesize = struct_mm_allocnode_s.sizeof def _node_allocated(self, allocnode): if allocnode['preceding'] & self._allocflag: @@ -333,7 +336,8 @@ class NX_show_heap (gdb.Command): state = '' else: state = '(free)' - print ' {} {} {}'.format(allocnode.address + 8, self._node_size(allocnode), state) + print ' {} {} {}'.format(allocnode.address + self._allocnodesize, + self._node_size(allocnode), state) cursor += self._node_size(allocnode) / self._allocnodesize def invoke(self, args, from_tty): diff --git a/Documentation/rc_mode_switch.odg b/Documentation/rc_mode_switch.odg Binary files differindex 29d738c39..682c63e47 100644 --- a/Documentation/rc_mode_switch.odg +++ b/Documentation/rc_mode_switch.odg diff --git a/Documentation/rc_mode_switch.pdf b/Documentation/rc_mode_switch.pdf Binary files differindex 856dd55c5..e795f4870 100644 --- a/Documentation/rc_mode_switch.pdf +++ b/Documentation/rc_mode_switch.pdf diff --git a/Images/aerocore.prototype b/Images/aerocore.prototype new file mode 100644 index 000000000..8502a0864 --- /dev/null +++ b/Images/aerocore.prototype @@ -0,0 +1,12 @@ +{ + "board_id": 19, + "magic": "AeroCore", + "description": "Firmware for the Gumstix AeroCore board", + "image": "", + "build_time": 0, + "summary": "AEROCORE", + "version": "0.1", + "image_size": 0, + "git_identity": "", + "board_revision": 0 +} diff --git a/ROMFS/px4fmu_common/init.d/1000_rc_fw_easystar.hil b/ROMFS/px4fmu_common/init.d/1000_rc_fw_easystar.hil index 36194ad68..d114fe21a 100644 --- a/ROMFS/px4fmu_common/init.d/1000_rc_fw_easystar.hil +++ b/ROMFS/px4fmu_common/init.d/1000_rc_fw_easystar.hil @@ -7,7 +7,7 @@ sh /etc/init.d/rc.fw_defaults -echo "HIL Rascal 110 starting.." +echo "X Plane HIL starting.." set HIL yes diff --git a/ROMFS/px4fmu_common/init.d/10017_steadidrone_qu4d b/ROMFS/px4fmu_common/init.d/10017_steadidrone_qu4d new file mode 100644 index 000000000..6179855f6 --- /dev/null +++ b/ROMFS/px4fmu_common/init.d/10017_steadidrone_qu4d @@ -0,0 +1,35 @@ +#!nsh +# +# Steadidrone QU4D +# +# Thomas Gubler <thomasgubler@gmail.com> +# Lorenz Meier <lm@inf.ethz.ch> +# + +sh /etc/init.d/rc.mc_defaults + +if [ $DO_AUTOCONFIG == yes ] +then + # TODO tune roll/pitch separately + param set MC_ROLL_P 7.0 + param set MC_ROLLRATE_P 0.13 + param set MC_ROLLRATE_I 0.0 + param set MC_ROLLRATE_D 0.004 + param set MC_PITCH_P 7.0 + param set MC_PITCHRATE_P 0.13 + param set MC_PITCHRATE_I 0.0 + param set MC_PITCHRATE_D 0.004 + param set MC_YAW_P 0.5 + param set MC_YAWRATE_P 0.2 + param set MC_YAWRATE_I 0.0 + param set MC_YAWRATE_D 0.0 + + param set BAT_N_CELLS 4 +fi + +set MIXER FMU_quad_w + +set PWM_MIN 1210 +set PWM_MAX 2100 + +set PWM_OUTPUTS 1234 diff --git a/ROMFS/px4fmu_common/init.d/11001_hexa_cox b/ROMFS/px4fmu_common/init.d/11001_hexa_cox index 38e65435b..df2e609bc 100644 --- a/ROMFS/px4fmu_common/init.d/11001_hexa_cox +++ b/ROMFS/px4fmu_common/init.d/11001_hexa_cox @@ -9,7 +9,7 @@ sh /etc/init.d/rc.mc_defaults -set MIXER hexa_cox +set MIXER FMU_hexa_cox # We only can run one channel group with one rate, so set all 8 channels set PWM_OUTPUTS 12345678 diff --git a/ROMFS/px4fmu_common/init.d/12001_octo_cox b/ROMFS/px4fmu_common/init.d/12001_octo_cox index 99f902a6d..8703f5f2f 100644 --- a/ROMFS/px4fmu_common/init.d/12001_octo_cox +++ b/ROMFS/px4fmu_common/init.d/12001_octo_cox @@ -7,6 +7,6 @@ sh /etc/init.d/rc.mc_defaults -set MIXER octo_cox +set MIXER FMU_octo_cox set PWM_OUTPUTS 12345678 diff --git a/ROMFS/px4fmu_common/init.d/2100_mpx_easystar b/ROMFS/px4fmu_common/init.d/2100_mpx_easystar index 465a22c53..db0e40fc2 100644 --- a/ROMFS/px4fmu_common/init.d/2100_mpx_easystar +++ b/ROMFS/px4fmu_common/init.d/2100_mpx_easystar @@ -5,4 +5,4 @@ sh /etc/init.d/rc.fw_defaults -set MIXER FMU_RET +set MIXER easystar.mix diff --git a/ROMFS/px4fmu_common/init.d/2103_skyhunter_1800 b/ROMFS/px4fmu_common/init.d/2103_skyhunter_1800 new file mode 100644 index 000000000..9bc0262d8 --- /dev/null +++ b/ROMFS/px4fmu_common/init.d/2103_skyhunter_1800 @@ -0,0 +1,5 @@ +#!nsh + +sh /etc/init.d/rc.fw_defaults + +set MIXER FMU_AET diff --git a/ROMFS/px4fmu_common/init.d/3031_phantom b/ROMFS/px4fmu_common/init.d/3031_phantom index 6cbd23643..24372bddc 100644 --- a/ROMFS/px4fmu_common/init.d/3031_phantom +++ b/ROMFS/px4fmu_common/init.d/3031_phantom @@ -10,8 +10,8 @@ sh /etc/init.d/rc.fw_defaults if [ $DO_AUTOCONFIG == yes ] then param set FW_AIRSPD_MIN 13 - param set FW_AIRSPD_TRIM 18 - param set FW_AIRSPD_MAX 40 + param set FW_AIRSPD_TRIM 15 + param set FW_AIRSPD_MAX 25 param set FW_ATT_TC 0.3 param set FW_L1_DAMPING 0.75 param set FW_L1_PERIOD 15 @@ -23,12 +23,12 @@ then param set FW_P_LIM_MIN -50 param set FW_P_RMAX_NEG 0 param set FW_P_RMAX_POS 0 - param set FW_P_ROLLFF 0 + param set FW_P_ROLLFF 1 param set FW_RR_FF 0.5 param set FW_RR_I 0.02 param set FW_RR_IMAX 0.2 param set FW_RR_P 0.08 - param set FW_R_LIM 70 + param set FW_R_LIM 50 param set FW_R_RMAX 0 param set FW_T_HRATE_P 0.01 param set FW_T_RLL2THR 15 diff --git a/ROMFS/px4fmu_common/init.d/3032_skywalker_x5 b/ROMFS/px4fmu_common/init.d/3032_skywalker_x5 index bf5a87068..465166f25 100644 --- a/ROMFS/px4fmu_common/init.d/3032_skywalker_x5 +++ b/ROMFS/px4fmu_common/init.d/3032_skywalker_x5 @@ -23,7 +23,7 @@ then param set FW_P_LIM_MIN -45 param set FW_P_RMAX_NEG 0 param set FW_P_RMAX_POS 0 - param set FW_P_ROLLFF 0 + param set FW_P_ROLLFF 1 param set FW_RR_FF 0.3 param set FW_RR_I 0 param set FW_RR_IMAX 0.2 diff --git a/ROMFS/px4fmu_common/init.d/3033_wingwing b/ROMFS/px4fmu_common/init.d/3033_wingwing index 7ff381d97..fff4b58df 100644 --- a/ROMFS/px4fmu_common/init.d/3033_wingwing +++ b/ROMFS/px4fmu_common/init.d/3033_wingwing @@ -27,9 +27,12 @@ then param set FW_PR_IMAX 0.2 param set FW_PR_P 0.06 param set FW_RR_FF 0.6 - param set FW_RR_IMA 0.2 + param set FW_RR_IMAX 0.2 param set FW_RR_P 0.09 param set FW_THR_CRUISE 0.65 fi set MIXER FMU_Q +# Provide ESC a constant 1000 us pulse +set PWM_OUTPUTS 4 +set PWM_DISARMED 1000 diff --git a/ROMFS/px4fmu_common/init.d/rc.autostart b/ROMFS/px4fmu_common/init.d/rc.autostart index 4ae6a2794..b365bd642 100644 --- a/ROMFS/px4fmu_common/init.d/rc.autostart +++ b/ROMFS/px4fmu_common/init.d/rc.autostart @@ -68,6 +68,12 @@ then set MODE custom fi +if param compare SYS_AUTOSTART 2103 103 +then + sh /etc/init.d/2103_skyhunter_1800 + set MODE custom +fi + # # Flying wing # @@ -189,6 +195,11 @@ then sh /etc/init.d/10016_3dr_iris fi +if param compare SYS_AUTOSTART 10017 +then + sh /etc/init.d/10017_steadidrone_qu4d +fi + # # Hexa Coaxial # diff --git a/ROMFS/px4fmu_common/init.d/rc.fw_apps b/ROMFS/px4fmu_common/init.d/rc.fw_apps index 72327c554..9aca3fc5f 100644 --- a/ROMFS/px4fmu_common/init.d/rc.fw_apps +++ b/ROMFS/px4fmu_common/init.d/rc.fw_apps @@ -3,6 +3,13 @@ # Standard apps for fixed wing # -att_pos_estimator_ekf start +# +# Start the attitude and position estimator +# +ekf_att_pos_estimator start + +# +# Start attitude controller +# fw_att_control start fw_pos_control_l1 start diff --git a/ROMFS/px4fmu_common/init.d/rc.fw_defaults b/ROMFS/px4fmu_common/init.d/rc.fw_defaults index 4cd73e23f..3a50fcf56 100644 --- a/ROMFS/px4fmu_common/init.d/rc.fw_defaults +++ b/ROMFS/px4fmu_common/init.d/rc.fw_defaults @@ -11,6 +11,4 @@ then param set NAV_RTL_ALT 100 param set NAV_RTL_LAND_T -1 param set NAV_ACCEPT_RAD 50 - param set RC_SCALE_ROLL 1 - param set RC_SCALE_PITCH 1 fi
\ No newline at end of file diff --git a/ROMFS/px4fmu_common/init.d/rc.io b/ROMFS/px4fmu_common/init.d/rc.io index 6e8fdbc0f..e23aebd87 100644 --- a/ROMFS/px4fmu_common/init.d/rc.io +++ b/ROMFS/px4fmu_common/init.d/rc.io @@ -11,7 +11,7 @@ px4io recovery # Adjust PX4IO update rate limit # set PX4IO_LIMIT 400 -if hw_ver compare PX4FMU_V1 +if ver hwcmp PX4FMU_V1 then set PX4IO_LIMIT 200 fi diff --git a/ROMFS/px4fmu_common/init.d/rc.logging b/ROMFS/px4fmu_common/init.d/rc.logging index c5aef8273..517e073af 100644 --- a/ROMFS/px4fmu_common/init.d/rc.logging +++ b/ROMFS/px4fmu_common/init.d/rc.logging @@ -5,10 +5,10 @@ if [ -d /fs/microsd ] then - if hw_ver compare PX4FMU_V1 + if ver hwcmp PX4FMU_V1 then echo "Start sdlog2 at 50Hz" - sdlog2 start -r 50 -a -b 8 -t + sdlog2 start -r 50 -a -b 4 -t else echo "Start sdlog2 at 200Hz" sdlog2 start -r 200 -a -b 16 -t diff --git a/ROMFS/px4fmu_common/init.d/rc.mc_apps b/ROMFS/px4fmu_common/init.d/rc.mc_apps index ed3939757..268eb9bba 100644 --- a/ROMFS/px4fmu_common/init.d/rc.mc_apps +++ b/ROMFS/px4fmu_common/init.d/rc.mc_apps @@ -5,6 +5,7 @@ # attitude_estimator_ekf start +#ekf_att_pos_estimator start position_estimator_inav start mc_att_control start diff --git a/ROMFS/px4fmu_common/init.d/rc.mc_defaults b/ROMFS/px4fmu_common/init.d/rc.mc_defaults index 4db62607a..b6b0a5b4e 100644 --- a/ROMFS/px4fmu_common/init.d/rc.mc_defaults +++ b/ROMFS/px4fmu_common/init.d/rc.mc_defaults @@ -32,9 +32,15 @@ then param set MPC_Z_VEL_D 0.0 param set MPC_Z_VEL_MAX 3 param set MPC_Z_FF 0.5 - param set MPC_TILT_MAX 1.0 + param set MPC_TILTMAX_AIR 45.0 + param set MPC_TILTMAX_LND 15.0 param set MPC_LAND_SPEED 1.0 - param set MPC_LAND_TILT 0.3 + + param set PE_VELNE_NOISE 0.5 + param set PE_VELNE_NOISE 0.7 + param set PE_POSNE_NOISE 0.5 + param set PE_POSD_NOISE 1.0 + fi set PWM_RATE 400 diff --git a/ROMFS/px4fmu_common/init.d/rc.sensors b/ROMFS/px4fmu_common/init.d/rc.sensors index 235be2431..1e14930fe 100644 --- a/ROMFS/px4fmu_common/init.d/rc.sensors +++ b/ROMFS/px4fmu_common/init.d/rc.sensors @@ -22,7 +22,7 @@ then echo "[init] Using L3GD20(H)" fi -if hw_ver compare PX4FMU_V2 +if ver hwcmp PX4FMU_V2 then if lsm303d start then diff --git a/ROMFS/px4fmu_common/init.d/rc.usb b/ROMFS/px4fmu_common/init.d/rc.usb index 2aeea5cbe..76593881d 100644 --- a/ROMFS/px4fmu_common/init.d/rc.usb +++ b/ROMFS/px4fmu_common/init.d/rc.usb @@ -3,13 +3,20 @@ # USB MAVLink start # -echo "Starting MAVLink on this USB console" - mavlink start -r 10000 -d /dev/ttyACM0 # Enable a number of interesting streams we want via USB mavlink stream -d /dev/ttyACM0 -s NAMED_VALUE_FLOAT -r 10 +usleep 100000 mavlink stream -d /dev/ttyACM0 -s OPTICAL_FLOW -r 10 +usleep 100000 +mavlink stream -d /dev/ttyACM0 -s VFR_HUD -r 20 +usleep 100000 +mavlink stream -d /dev/ttyACM0 -s ATTITUDE -r 20 +usleep 100000 mavlink stream -d /dev/ttyACM0 -s ATTITUDE_CONTROLS -r 30 +usleep 100000 +mavlink stream -d /dev/ttyACM0 -s SERVO_OUTPUT_RAW_0 -r 20 +usleep 100000 # Exit shell to make it available to MAVLink -exit +exit diff --git a/ROMFS/px4fmu_common/init.d/rcS b/ROMFS/px4fmu_common/init.d/rcS index 503dbb83e..8c413e087 100644 --- a/ROMFS/px4fmu_common/init.d/rcS +++ b/ROMFS/px4fmu_common/init.d/rcS @@ -20,7 +20,7 @@ echo "[init] Looking for microSD..." if mount -t vfat /dev/mmcsd0 /fs/microsd then set LOG_FILE /fs/microsd/bootlog.txt - echo "[init] microSD card mounted at /fs/microsd" + echo "[init] microSD mounted: /fs/microsd" # Start playing the startup tune tone_alarm start else @@ -83,9 +83,9 @@ then param select $PARAM_FILE if param load then - echo "[init] Parameters loaded: $PARAM_FILE" + echo "[init] Params loaded: $PARAM_FILE" else - echo "[init] ERROR: Parameters loading failed: $PARAM_FILE" + echo "[init] ERROR: Params loading failed: $PARAM_FILE" fi # @@ -120,6 +120,8 @@ then set EXIT_ON_END no set MAV_TYPE none set LOAD_DEFAULT_APPS yes + set GPS yes + set GPS_FAKE no # # Set DO_AUTOCONFIG flag to use it in AUTOSTART scripts @@ -146,7 +148,7 @@ then # if param compare SYS_AUTOSTART 0 then - echo "[init] Don't try to find autostart script" + echo "[init] No autostart" else sh /etc/init.d/rc.autostart fi @@ -156,10 +158,10 @@ then # if [ -f $CONFIG_FILE ] then - echo "[init] Reading config: $CONFIG_FILE" + echo "[init] Config: $CONFIG_FILE" sh $CONFIG_FILE else - echo "[init] Config file not found: $CONFIG_FILE" + echo "[init] Config not found: $CONFIG_FILE" fi # @@ -246,7 +248,7 @@ then echo "[init] ERROR: PX4IO not found, disabling output" # Avoid using ttyS0 for MAVLink on FMUv1 - if hw_ver compare PX4FMU_V1 + if ver hwcmp PX4FMU_V1 then set FMU_MODE serial fi @@ -260,14 +262,14 @@ then if [ $HIL == yes ] then set OUTPUT_MODE hil - if hw_ver compare PX4FMU_V1 + if ver hwcmp PX4FMU_V1 then set FMU_MODE serial fi - else - # Try to get an USB console if not in HIL mode - nshterm /dev/ttyACM0 & fi + + # Try to get an USB console + nshterm /dev/ttyACM0 & # # Start the Commander (needs to be this early for in-air-restarts) @@ -294,6 +296,7 @@ then tone_alarm $TUNE_OUT_ERROR fi fi + if [ $OUTPUT_MODE == fmu -o $OUTPUT_MODE == ardrone ] then echo "[init] Use FMU as primary output" @@ -305,7 +308,7 @@ then tone_alarm $TUNE_OUT_ERROR fi - if hw_ver compare PX4FMU_V1 + if ver hwcmp PX4FMU_V1 then if [ $FMU_MODE == pwm -o $FMU_MODE == gpio ] then @@ -317,6 +320,7 @@ then fi fi fi + if [ $OUTPUT_MODE == mkblctrl ] then echo "[init] Use MKBLCTRL as primary output" @@ -338,7 +342,8 @@ then tone_alarm $TUNE_OUT_ERROR fi - fi + fi + if [ $OUTPUT_MODE == hil ] then echo "[init] Use HIL as primary output" @@ -378,7 +383,7 @@ then tone_alarm $TUNE_OUT_ERROR fi - if hw_ver compare PX4FMU_V1 + if ver hwcmp PX4FMU_V1 then if [ $FMU_MODE == pwm -o $FMU_MODE == gpio ] then @@ -396,60 +401,47 @@ then # # MAVLink # - if [ $MAVLINK_FLAGS == default ] then - if [ $HIL == yes ] + # Normal mode, use baudrate 57600 (default) and data rate 1000 bytes/s + if [ $TTYS1_BUSY == yes ] then - sleep 1 - set MAVLINK_FLAGS "-r 10000 -d /dev/ttyACM0" - usleep 5000 + # Start MAVLink on ttyS0, because FMU ttyS1 pins configured as something else + set MAVLINK_FLAGS "-r 1000 -d /dev/ttyS0" + + # Exit from nsh to free port for mavlink + set EXIT_ON_END yes else - # Normal mode, use baudrate 57600 (default) and data rate 1000 bytes/s - if [ $TTYS1_BUSY == yes ] - then - # Start MAVLink on ttyS0, because FMU ttyS1 pins configured as something else - set MAVLINK_FLAGS "-r 1000 -d /dev/ttyS0" - usleep 5000 - - # Exit from nsh to free port for mavlink - set EXIT_ON_END yes - else - # Start MAVLink on default port: ttyS1 - set MAVLINK_FLAGS "-r 1000" - usleep 5000 - fi + # Start MAVLink on default port: ttyS1 + set MAVLINK_FLAGS "-r 1000" fi fi mavlink start $MAVLINK_FLAGS - usleep 5000 - - # - # Start the datamanager - # - dataman start - - # - # Start the navigator - # - navigator start # # Sensors, Logging, GPS # - echo "[init] Start sensors" sh /etc/init.d/rc.sensors if [ $HIL == no ] then echo "[init] Start logging" sh /etc/init.d/rc.logging - - echo "[init] Start GPS" - gps start fi + if [ $GPS == yes ] + then + echo "[init] Start GPS" + if [ $GPS_FAKE == yes ] + then + echo "[init] Faking GPS" + gps start -f + else + gps start + fi + fi + # # Start up ARDrone Motor interface # @@ -516,7 +508,7 @@ then then set MAV_TYPE 13 fi - if [ $MIXER == hexa_cox ] + if [ $MIXER == FMU_hexa_cox ] then set MAV_TYPE 13 fi @@ -549,6 +541,16 @@ then fi # + # Start the datamanager + # + dataman start + + # + # Start the navigator + # + navigator start + + # # Generic setup (autostart ID not found) # if [ $VEHICLE_TYPE == none ] @@ -563,7 +565,7 @@ then echo "[init] Starting addons script: $EXTRAS_FILE" sh $EXTRAS_FILE else - echo "[init] Addons script not found: $EXTRAS_FILE" + echo "[init] No addons script: $EXTRAS_FILE" fi if [ $EXIT_ON_END == yes ] diff --git a/ROMFS/px4fmu_common/mixers/hexa_cox.mix b/ROMFS/px4fmu_common/mixers/FMU_hexa_cox.mix index 497786feb..497786feb 100644 --- a/ROMFS/px4fmu_common/mixers/hexa_cox.mix +++ b/ROMFS/px4fmu_common/mixers/FMU_hexa_cox.mix diff --git a/ROMFS/px4fmu_common/mixers/easystar.mix b/ROMFS/px4fmu_common/mixers/easystar.mix new file mode 100644 index 000000000..0051ffdbb --- /dev/null +++ b/ROMFS/px4fmu_common/mixers/easystar.mix @@ -0,0 +1,31 @@ +EASYSTAR / EASYSTAR II MIXER +============================ + +Aileron mixer +------------- +One output - would be easy to add support for 2 servos + +M: 1 +O: 10000 10000 0 -10000 10000 +S: 0 0 10000 10000 0 -10000 10000 + +Elevator mixer +------------ + +M: 1 +O: 10000 10000 0 -10000 10000 +S: 0 1 -10000 -10000 0 -10000 10000 + +Rudder mixer +------------ + +M: 1 +O: 10000 10000 0 -10000 10000 +S: 0 2 -10000 -10000 0 -10000 10000 + +Motor speed mixer +----------------- + +M: 1 +O: 10000 10000 0 -10000 10000 +S: 0 3 0 20000 -10000 -10000 10000 diff --git a/Tools/.gitignore b/Tools/.gitignore new file mode 100644 index 000000000..7628bda82 --- /dev/null +++ b/Tools/.gitignore @@ -0,0 +1,2 @@ +parameters.wiki +parameters.xml diff --git a/Tools/fix_code_style.sh b/Tools/fix_code_style.sh index 0b6743013..5995d428e 100755 --- a/Tools/fix_code_style.sh +++ b/Tools/fix_code_style.sh @@ -16,5 +16,6 @@ astyle \ --ignore-exclude-errors-x \ --lineend=linux \ --exclude=EASTL \ - --add-brackets \ + --add-brackets \ + --max-code-length=120 \ $* diff --git a/Tools/px4params/.gitignore b/Tools/px4params/.gitignore deleted file mode 100644 index d78b71a6e..000000000 --- a/Tools/px4params/.gitignore +++ /dev/null @@ -1,4 +0,0 @@ -parameters.wiki -parameters.xml -parameters.wikirpc.xml -cookies.txt
\ No newline at end of file diff --git a/Tools/px4params/README.md b/Tools/px4params/README.md index a23b44799..50dcd2e29 100644 --- a/Tools/px4params/README.md +++ b/Tools/px4params/README.md @@ -1,9 +1 @@ -h1. PX4 Parameters Processor - -It's designed to scan PX4 source codes, find declarations of tunable parameters, -and generate the list in various formats. - -Currently supported formats are: - -* XML for the parametric UI generator -* Human-readable description in DokuWiki format +This folder contains a python library used by px_process_params.py diff --git a/Tools/px4params/__init__.py b/Tools/px4params/__init__.py new file mode 100644 index 000000000..3a9f1e2c6 --- /dev/null +++ b/Tools/px4params/__init__.py @@ -0,0 +1 @@ +__all__ = ["srcscanner", "srcparser", "xmlout", "dokuwikiout", "dokuwikirpc"]
\ No newline at end of file diff --git a/Tools/px4params/dokuwikiout.py b/Tools/px4params/dokuwikiout.py new file mode 100644 index 000000000..77e0ef53d --- /dev/null +++ b/Tools/px4params/dokuwikiout.py @@ -0,0 +1,44 @@ +from xml.sax.saxutils import escape +import codecs + +class DokuWikiTablesOutput(): + def __init__(self, groups): + result = ("====== Parameter Reference ======\n" + "<note>**This list is auto-generated from the source code** and contains the most recent parameter documentation.</note>\n" + "\n") + for group in groups: + result += "==== %s ====\n\n" % group.GetName() + result += "|< 100% 25% 45% 10% 10% 10% >|\n" + result += "^ Name ^ Description ^ Min ^ Max ^ Default ^\n" + result += "^ ::: ^ Comment ^^^^\n" + for param in group.GetParams(): + code = param.GetFieldValue("code") + name = param.GetFieldValue("short_desc") + min_val = param.GetFieldValue("min") + max_val = param.GetFieldValue("max") + def_val = param.GetFieldValue("default") + long_desc = param.GetFieldValue("long_desc") + + if name == code: + name = "" + else: + name = name.replace("\n", " ") + name = name.replace("|", "%%|%%") + name = name.replace("^", "%%^%%") + + result += "| **%s** |" % code + result += " %s |" % name + result += " %s |" % (min_val or "") + result += " %s |" % (max_val or "") + result += " %s |" % (def_val or "") + result += "\n" + + if long_desc is not None: + result += "| ::: | <div>%s</div> ||||\n" % long_desc + + result += "\n" + self.output = result; + + def Save(self, filename): + with codecs.open(filename, 'w', 'utf-8') as f: + f.write(self.output) diff --git a/Tools/px4params/dokuwikirpc.py b/Tools/px4params/dokuwikirpc.py new file mode 100644 index 000000000..407d306fd --- /dev/null +++ b/Tools/px4params/dokuwikirpc.py @@ -0,0 +1,16 @@ +try: + import xmlrpclib +except ImportError: + import xmlrpc.client as xmlrpclib + +# See https://www.dokuwiki.org/devel:xmlrpc for a list of available functions! +# Usage example: +# xmlrpc = dokuwikirpc.get_xmlrpc(url, username, password) +# print(xmlrpc.dokuwiki.getVersion()) + +def get_xmlrpc(url, username, password): + #proto, url = url.split("://") + #url = proto + "://" + username + ":" + password + "@" + url + "/lib/exe/xmlrpc.php" + url += "/lib/exe/xmlrpc.php?u=" + username + "&p=" + password + + return xmlrpclib.ServerProxy(url) diff --git a/Tools/px4params/output_dokuwiki_listings.py b/Tools/px4params/output_dokuwiki_listings.py deleted file mode 100644 index 83c50ae15..000000000 --- a/Tools/px4params/output_dokuwiki_listings.py +++ /dev/null @@ -1,31 +0,0 @@ -import codecs - -class DokuWikiListingsOutput(): - def __init__(self, groups): - result = "" - for group in groups: - result += "==== %s ====\n\n" % group.GetName() - for param in group.GetParams(): - code = param.GetFieldValue("code") - name = param.GetFieldValue("short_desc") - if code != name: - name = "%s (%s)" % (name, code) - result += "=== %s ===\n\n" % name - long_desc = param.GetFieldValue("long_desc") - if long_desc is not None: - result += "%s\n\n" % long_desc - min_val = param.GetFieldValue("min") - if min_val is not None: - result += "* Minimal value: %s\n" % min_val - max_val = param.GetFieldValue("max") - if max_val is not None: - result += "* Maximal value: %s\n" % max_val - def_val = param.GetFieldValue("default") - if def_val is not None: - result += "* Default value: %s\n" % def_val - result += "\n" - self.output = result - - def Save(self, filename): - with codecs.open(filename, 'w', 'utf-8') as f: - f.write(self.output) diff --git a/Tools/px4params/output_dokuwiki_tables.py b/Tools/px4params/output_dokuwiki_tables.py deleted file mode 100644 index aa04304df..000000000 --- a/Tools/px4params/output_dokuwiki_tables.py +++ /dev/null @@ -1,76 +0,0 @@ -from xml.sax.saxutils import escape -import codecs - -class DokuWikiTablesOutput(): - def __init__(self, groups): - result = "====== Parameter Reference ======\nThis list is auto-generated every few minutes and contains the most recent parameter names and default values.\n\n" - for group in groups: - result += "==== %s ====\n\n" % group.GetName() - result += "|< 100% 20% 20% 10% 10% 10% 30%>|\n" - result += "^ Name ^ Description ^ Min ^ Max ^ Default ^ Comment ^\n" - for param in group.GetParams(): - code = param.GetFieldValue("code") - name = param.GetFieldValue("short_desc") - min_val = param.GetFieldValue("min") - max_val = param.GetFieldValue("max") - def_val = param.GetFieldValue("default") - long_desc = param.GetFieldValue("long_desc") - - name = name.replace("\n", " ") - result += "| %s | %s |" % (code, name) - - if min_val is not None: - result += " %s |" % min_val - else: - result += " |" - - if max_val is not None: - result += " %s |" % max_val - else: - result += " |" - - if def_val is not None: - result += " %s |" % def_val - else: - result += " |" - - if long_desc is not None: - long_desc = long_desc.replace("\n", " ") - result += " %s |" % long_desc - else: - result += " |" - - result += "\n" - result += "\n" - self.output = result; - - def Save(self, filename): - with codecs.open(filename, 'w', 'utf-8') as f: - f.write(self.output) - - def SaveRpc(self, filename): - with codecs.open(filename, 'w', 'utf-8') as f: - f.write("""<?xml version='1.0'?> -<methodCall> - <methodName>wiki.putPage</methodName> - <params> - <param> - <value> - <string>:firmware:parameters</string> - </value> - </param> - <param> - <value> - <string>""") - f.write(escape(self.output)) - f.write("""</string> - </value> - </param> - <param> - <value> - <name>sum</name> - <string>Updated parameters automagically from code.</string> - </value> - </param> - </params> -</methodCall>""") diff --git a/Tools/px4params/srcparser.py b/Tools/px4params/srcparser.py index 1b2d30110..0a4d21d26 100644 --- a/Tools/px4params/srcparser.py +++ b/Tools/px4params/srcparser.py @@ -44,6 +44,7 @@ class Parameter(object): "default": 6, "min": 5, "max": 4, + "unit": 3, # all others == 0 (sorted alphabetically) } @@ -71,7 +72,7 @@ class Parameter(object): """ return self.fields.get(code) -class Parser(object): +class SourceParser(object): """ Parses provided data and stores all found parameters internally. """ @@ -86,7 +87,7 @@ class Parser(object): re_is_a_number = re.compile(r'^-?[0-9\.]') re_remove_dots = re.compile(r'\.+$') - valid_tags = set(["min", "max", "group"]) + valid_tags = set(["group", "min", "max", "unit"]) # Order of parameter groups priority = { diff --git a/Tools/px4params/scanner.py b/Tools/px4params/srcscanner.py index 8779b7bbf..d7eca72d7 100644 --- a/Tools/px4params/scanner.py +++ b/Tools/px4params/srcscanner.py @@ -2,26 +2,21 @@ import os import re import codecs -class Scanner(object): +class SourceScanner(object): """ Traverses directory tree, reads all source files, and passes their contents to the Parser. """ - re_file_extension = re.compile(r'\.([^\.]+)$') - def ScanDir(self, srcdir, parser): """ Scans provided path and passes all found contents to the parser using parser.Parse method. """ - extensions = set(parser.GetSupportedExtensions()) + extensions = tuple(parser.GetSupportedExtensions()) for dirname, dirnames, filenames in os.walk(srcdir): for filename in filenames: - m = self.re_file_extension.search(filename) - if m: - ext = m.group(1) - if ext in extensions: + if filename.endswith(extensions): path = os.path.join(dirname, filename) self.ScanFile(path, parser) diff --git a/Tools/px4params/output_xml.py b/Tools/px4params/xmlout.py index e845cd1b1..e845cd1b1 100644 --- a/Tools/px4params/output_xml.py +++ b/Tools/px4params/xmlout.py diff --git a/Tools/px4params/xmlrpc.sh b/Tools/px4params/xmlrpc.sh deleted file mode 100644 index efd177f46..000000000 --- a/Tools/px4params/xmlrpc.sh +++ /dev/null @@ -1,5 +0,0 @@ -python px_process_params.py - -rm cookies.txt -curl --cookie cookies.txt --cookie-jar cookies.txt --user-agent Mozilla/4.0 --data "u=$XMLRPCUSER&p=$XMLRPCPASS" https://pixhawk.org/start?do=login -curl -k --cookie cookies.txt -H "Content-Type: application/xml" -X POST --data-binary @parameters.wikirpc.xml "https://pixhawk.org/lib/exe/xmlrpc.php" diff --git a/Tools/px_process_params.py b/Tools/px_process_params.py new file mode 100644 index 000000000..12128a997 --- /dev/null +++ b/Tools/px_process_params.py @@ -0,0 +1,140 @@ +#!/usr/bin/env python +############################################################################ +# +# Copyright (C) 2013-2014 PX4 Development Team. All rights reserved. +# +# Redistribution and use in source and binary forms, with or without +# modification, are permitted provided that the following conditions +# are met: +# +# 1. Redistributions of source code must retain the above copyright +# notice, this list of conditions and the following disclaimer. +# 2. Redistributions in binary form must reproduce the above copyright +# notice, this list of conditions and the following disclaimer in +# the documentation and/or other materials provided with the +# distribution. +# 3. Neither the name PX4 nor the names of its contributors may be +# used to endorse or promote products derived from this software +# without specific prior written permission. +# +# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS +# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT +# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS +# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE +# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, +# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, +# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS +# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED +# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT +# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN +# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE +# POSSIBILITY OF SUCH DAMAGE. +# +############################################################################ + +# +# PX4 paramers processor (main executable file) +# +# This tool scans the PX4 source code for declarations of tunable parameters +# and outputs the list in various formats. +# +# Currently supported formats are: +# * XML for the parametric UI generator +# * Human-readable description in DokuWiki page format +# +# This tool also allows to automatically upload the human-readable version +# to the DokuWiki installation via XML-RPC. +# + +from __future__ import print_function +import sys +import os +import argparse +from px4params import srcscanner, srcparser, xmlout, dokuwikiout, dokuwikirpc + +def main(): + # Parse command line arguments + parser = argparse.ArgumentParser(description="Process parameter documentation.") + parser.add_argument("-s", "--src-path", + default="../src", + metavar="PATH", + help="path to source files to scan for parameters") + parser.add_argument("-x", "--xml", + nargs='?', + const="parameters.xml", + metavar="FILENAME", + help="Create XML file" + " (default FILENAME: parameters.xml)") + parser.add_argument("-w", "--wiki", + nargs='?', + const="parameters.wiki", + metavar="FILENAME", + help="Create DokuWiki file" + " (default FILENAME: parameters.wiki)") + parser.add_argument("-u", "--wiki-update", + nargs='?', + const="firmware:parameters", + metavar="PAGENAME", + help="Update DokuWiki page" + " (default PAGENAME: firmware:parameters)") + parser.add_argument("--wiki-url", + default="https://pixhawk.org", + metavar="URL", + help="DokuWiki URL" + " (default: https://pixhawk.org)") + parser.add_argument("--wiki-user", + default=os.environ.get('XMLRPCUSER', None), + metavar="USERNAME", + help="DokuWiki XML-RPC user name" + " (default: $XMLRPCUSER environment variable)") + parser.add_argument("--wiki-pass", + default=os.environ.get('XMLRPCPASS', None), + metavar="PASSWORD", + help="DokuWiki XML-RPC user password" + " (default: $XMLRPCUSER environment variable)") + parser.add_argument("--wiki-summary", + metavar="SUMMARY", + default="Automagically updated parameter documentation from code.", + help="DokuWiki page edit summary") + args = parser.parse_args() + + # Check for valid command + if not (args.xml or args.wiki or args.wiki_update): + print("Error: You need to specify at least one output method!\n") + parser.print_usage() + sys.exit(1) + + # Initialize source scanner and parser + scanner = srcscanner.SourceScanner() + parser = srcparser.SourceParser() + + # Scan directories, and parse the files + print("Scanning source path " + args.src_path) + scanner.ScanDir(args.src_path, parser) + param_groups = parser.GetParamGroups() + + # Output to XML file + if args.xml: + print("Creating XML file " + args.xml) + out = xmlout.XMLOutput(param_groups) + out.Save(args.xml) + + # Output to DokuWiki tables + if args.wiki or args.wiki_update: + out = dokuwikiout.DokuWikiTablesOutput(param_groups) + if args.wiki: + print("Creating wiki file " + args.wiki) + out.Save(args.wiki) + if args.wiki_update: + if args.wiki_user and args.wiki_pass: + print("Updating wiki page " + args.wiki_update) + xmlrpc = dokuwikirpc.get_xmlrpc(args.wiki_url, args.wiki_user, args.wiki_pass) + xmlrpc.wiki.putPage(args.wiki_update, out.output, {'sum': args.wiki_summary}) + else: + print("Error: You need to specify DokuWiki XML-RPC username and password!") + + print("All done!") + + +if __name__ == "__main__": + main() diff --git a/Tools/px_romfs_pruner.py b/Tools/px_romfs_pruner.py index ceef9f9be..fcc40b09e 100644 --- a/Tools/px_romfs_pruner.py +++ b/Tools/px_romfs_pruner.py @@ -43,29 +43,30 @@ from __future__ import print_function import argparse import os + def main(): - + # Parse commandline arguments parser = argparse.ArgumentParser(description="ROMFS pruner.") parser.add_argument('--folder', action="store", help="ROMFS scratch folder.") args = parser.parse_args() - + print("Pruning ROMFS files.") - - # go through + + # go through for (root, dirs, files) in os.walk(args.folder): for file in files: # only prune text files - if ".zip" in file or ".bin" in file: + if ".zip" in file or ".bin" in file or ".swp" in file: continue - - file_path = os.path.join(root, file) - + + file_path = os.path.join(root, file) + # read file line by line pruned_content = "" with open(file_path, "r") as f: - for line in f: - + for line in f: + # handle mixer files differently than startup files if file_path.endswith(".mix"): if line.startswith(("Z:", "M:", "R: ", "O:", "S:")): @@ -73,11 +74,11 @@ def main(): else: if not line.isspace() and not line.strip().startswith("#"): pruned_content += line - + # overwrite old scratch file with open(file_path, "w") as f: f.write(pruned_content) - - + + if __name__ == '__main__': - main()
\ No newline at end of file + main() diff --git a/Tools/px_update_wiki.sh b/Tools/px_update_wiki.sh new file mode 100644 index 000000000..d66bb9e10 --- /dev/null +++ b/Tools/px_update_wiki.sh @@ -0,0 +1,2 @@ +# Remember to set the XMLRPCUSER and XMLRPCPASS environment variables +python px_process_params.py --wiki-update diff --git a/Tools/px_uploader.py b/Tools/px_uploader.py index e4a8b3c05..985e6ffd9 100755 --- a/Tools/px_uploader.py +++ b/Tools/px_uploader.py @@ -389,18 +389,22 @@ class uploader(object): self.otp_pid = self.otp[12:8:-1] self.otp_coa = self.otp[32:160] # show user: - print("type: " + self.otp_id.decode('Latin-1')) - print("idtype: " + binascii.b2a_qp(self.otp_idtype).decode('Latin-1')) - print("vid: " + binascii.hexlify(self.otp_vid).decode('Latin-1')) - print("pid: "+ binascii.hexlify(self.otp_pid).decode('Latin-1')) - print("coa: "+ binascii.b2a_base64(self.otp_coa).decode('Latin-1')) - print("sn: ", end='') - for byte in range(0,12,4): - x = self.__getSN(byte) - x = x[::-1] # reverse the bytes - self.sn = self.sn + x - print(binascii.hexlify(x).decode('Latin-1'), end='') # show user - print('') + try: + print("type: " + self.otp_id.decode('Latin-1')) + print("idtype: " + binascii.b2a_qp(self.otp_idtype).decode('Latin-1')) + print("vid: " + binascii.hexlify(self.otp_vid).decode('Latin-1')) + print("pid: "+ binascii.hexlify(self.otp_pid).decode('Latin-1')) + print("coa: "+ binascii.b2a_base64(self.otp_coa).decode('Latin-1')) + print("sn: ", end='') + for byte in range(0,12,4): + x = self.__getSN(byte) + x = x[::-1] # reverse the bytes + self.sn = self.sn + x + print(binascii.hexlify(x).decode('Latin-1'), end='') # show user + print('') + except Exception: + # ignore bad character encodings + pass print("erase...") self.__erase() diff --git a/Tools/tests-host/.gitignore b/Tools/tests-host/.gitignore index 61e091551..87b314c61 100644 --- a/Tools/tests-host/.gitignore +++ b/Tools/tests-host/.gitignore @@ -1,2 +1,4 @@ ./obj/* mixer_test +sbus2_test +autodeclination_test diff --git a/Tools/tests-host/Makefile b/Tools/tests-host/Makefile index 7ab1454f0..f0737ef88 100644 --- a/Tools/tests-host/Makefile +++ b/Tools/tests-host/Makefile @@ -1,47 +1,39 @@ CC=g++ -CFLAGS=-I. -I../../src/modules -I ../../src/include -I../../src/drivers -I../../src -D__EXPORT="" -Dnullptr="0" +CFLAGS=-I. -I../../src/modules -I ../../src/include -I../../src/drivers \ + -I../../src -I../../src/lib -D__EXPORT="" -Dnullptr="0" -lm -ODIR=obj -LDIR =../lib +all: mixer_test sbus2_test autodeclination_test -LIBS=-lm +MIXER_FILES=../../src/systemcmds/tests/test_mixer.cpp \ + ../../src/systemcmds/tests/test_conv.cpp \ + ../../src/modules/systemlib/mixer/mixer_simple.cpp \ + ../../src/modules/systemlib/mixer/mixer_multirotor.cpp \ + ../../src/modules/systemlib/mixer/mixer.cpp \ + ../../src/modules/systemlib/mixer/mixer_group.cpp \ + ../../src/modules/systemlib/mixer/mixer_load.c \ + ../../src/modules/systemlib/pwm_limit/pwm_limit.c \ + hrt.cpp \ + mixer_test.cpp -#_DEPS = test.h -#DEPS = $(patsubst %,$(IDIR)/%,$(_DEPS)) +SBUS2_FILES=../../src/modules/px4iofirmware/sbus.c \ + hrt.cpp \ + sbus2_test.cpp -_OBJ = mixer_test.o test_mixer.o mixer_simple.o mixer_multirotor.o \ - mixer.o mixer_group.o mixer_load.o test_conv.o pwm_limit.o hrt.o -OBJ = $(patsubst %,$(ODIR)/%,$(_OBJ)) +AUTODECLINATION_FILES= ../../src/lib/geo/geo_mag_declination.c \ + hrt.cpp \ + autodeclination_test.cpp -#$(DEPS) -$(ODIR)/%.o: %.cpp - mkdir -p obj - $(CC) -c -o $@ $< $(CFLAGS) +mixer_test: $(MIXER_FILES) + $(CC) -o mixer_test $(MIXER_FILES) $(CFLAGS) -$(ODIR)/%.o: ../../src/systemcmds/tests/%.cpp - $(CC) -c -o $@ $< $(CFLAGS) +sbus2_test: $(SBUS2_FILES) + $(CC) -o sbus2_test $(SBUS2_FILES) $(CFLAGS) -$(ODIR)/%.o: ../../src/modules/systemlib/%.cpp - $(CC) -c -o $@ $< $(CFLAGS) - -$(ODIR)/%.o: ../../src/modules/systemlib/mixer/%.cpp - $(CC) -c -o $@ $< $(CFLAGS) - -$(ODIR)/%.o: ../../src/modules/systemlib/pwm_limit/%.cpp - $(CC) -c -o $@ $< $(CFLAGS) - -$(ODIR)/%.o: ../../src/modules/systemlib/pwm_limit/%.c - $(CC) -c -o $@ $< $(CFLAGS) - -$(ODIR)/%.o: ../../src/modules/systemlib/mixer/%.c - $(CC) -c -o $@ $< $(CFLAGS) - -# -mixer_test: $(OBJ) - g++ -o $@ $^ $(CFLAGS) $(LIBS) +autodeclination_test: $(SBUS2_FILES) + $(CC) -o autodeclination_test $(AUTODECLINATION_FILES) $(CFLAGS) .PHONY: clean clean: - rm -f $(ODIR)/*.o *~ core $(INCDIR)/*~
\ No newline at end of file + rm -f $(ODIR)/*.o *~ core $(INCDIR)/*~ mixer_test sbus2_test autodeclination_test
\ No newline at end of file diff --git a/Tools/tests-host/autodeclination_test.cpp b/Tools/tests-host/autodeclination_test.cpp new file mode 100644 index 000000000..93bc340bb --- /dev/null +++ b/Tools/tests-host/autodeclination_test.cpp @@ -0,0 +1,28 @@ + +#include <stdio.h> +#include <stdlib.h> +#include <unistd.h> +#include <string.h> +#include <systemlib/mixer/mixer.h> +#include <systemlib/err.h> +#include <drivers/drv_hrt.h> +#include <px4iofirmware/px4io.h> +#include "../../src/systemcmds/tests/tests.h" +#include <geo/geo.h> + +int main(int argc, char *argv[]) { + warnx("autodeclination test started"); + + if (argc < 3) + errx(1, "Need lat/lon!"); + + char* p_end; + + float lat = strtod(argv[1], &p_end); + float lon = strtod(argv[2], &p_end); + + float declination = get_mag_declination(lat, lon); + + printf("lat: %f lon: %f, dec: %f\n", lat, lon, declination); + +} diff --git a/Tools/tests-host/board_config.h b/Tools/tests-host/board_config.h new file mode 100644 index 000000000..e69de29bb --- /dev/null +++ b/Tools/tests-host/board_config.h diff --git a/Tools/tests-host/debug.h b/Tools/tests-host/debug.h new file mode 100644 index 000000000..9824d13fc --- /dev/null +++ b/Tools/tests-host/debug.h @@ -0,0 +1,5 @@ + +#pragma once + +#include <systemlib/err.h> +#define lowsyslog warnx
\ No newline at end of file diff --git a/Tools/tests-host/mixer_test.cpp b/Tools/tests-host/mixer_test.cpp index e311617f9..06499afd0 100644 --- a/Tools/tests-host/mixer_test.cpp +++ b/Tools/tests-host/mixer_test.cpp @@ -11,4 +11,4 @@ int main(int argc, char *argv[]) { test_mixer(3, args); test_conv(1, args); -}
\ No newline at end of file +} diff --git a/Tools/tests-host/run_tests.sh b/Tools/tests-host/run_tests.sh new file mode 100755 index 000000000..ff5ee509a --- /dev/null +++ b/Tools/tests-host/run_tests.sh @@ -0,0 +1,6 @@ +#!/bin/sh + +make clean +make all +./mixer_test +./sbus2_test ../../../../data/sbus2/sbus2_r7008SB_gps_baro_tx_off.txt
\ No newline at end of file diff --git a/Tools/tests-host/sbus2_test.cpp b/Tools/tests-host/sbus2_test.cpp new file mode 100644 index 000000000..d8fcb695d --- /dev/null +++ b/Tools/tests-host/sbus2_test.cpp @@ -0,0 +1,75 @@ + +#include <stdio.h> +#include <unistd.h> +#include <string.h> +#include <systemlib/mixer/mixer.h> +#include <systemlib/err.h> +#include <drivers/drv_hrt.h> +#include <px4iofirmware/px4io.h> +#include "../../src/systemcmds/tests/tests.h" + +int main(int argc, char *argv[]) { + warnx("SBUS2 test started"); + + if (argc < 2) + errx(1, "Need a filename for the input file"); + + warnx("loading data from: %s", argv[1]); + + FILE *fp; + + fp = fopen(argv[1],"rt"); + + if (!fp) + errx(1, "failed opening file"); + + float f; + unsigned x; + int ret; + + // Trash the first 20 lines + for (unsigned i = 0; i < 20; i++) { + (void)fscanf(fp, "%f,%x,,", &f, &x); + } + + // Init the parser + uint8_t frame[30]; + unsigned partial_frame_count = 0; + uint16_t rc_values[18]; + uint16_t num_values; + bool sbus_failsafe; + bool sbus_frame_drop; + uint16_t max_channels = sizeof(rc_values) / sizeof(rc_values[0]); + + float last_time = 0; + + while (EOF != (ret = fscanf(fp, "%f,%x,,", &f, &x))) { + if (((f - last_time) * 1000 * 1000) > 3000) { + partial_frame_count = 0; + warnx("FRAME RESET\n\n"); + } + + frame[partial_frame_count] = x; + partial_frame_count++; + + //warnx("%f: 0x%02x, first: 0x%02x, last: 0x%02x, pcount: %u", (double)f, x, frame[0], frame[24], partial_frame_count); + + if (partial_frame_count == sizeof(frame)) + partial_frame_count = 0; + + last_time = f; + + // Pipe the data into the parser + hrt_abstime now = hrt_absolute_time(); + + //if (partial_frame_count % 25 == 0) + //sbus_parse(now, frame, &partial_frame_count, rc_values, &num_values, &sbus_failsafe, &sbus_frame_drop, max_channels); + } + + if (ret == EOF) { + warnx("Test finished, reached end of file"); + } else { + warnx("Test aborted, errno: %d", ret); + } + +} diff --git a/makefiles/board_aerocore.mk b/makefiles/board_aerocore.mk new file mode 100644 index 000000000..6f4b93266 --- /dev/null +++ b/makefiles/board_aerocore.mk @@ -0,0 +1,11 @@ +# +# Board-specific definitions for the Gumstix AeroCore +# + +# +# Configure the toolchain +# +CONFIG_ARCH = CORTEXM4F +CONFIG_BOARD = AEROCORE + +include $(PX4_MK_DIR)/toolchain_gnu-arm-eabi.mk diff --git a/makefiles/config_aerocore_default.mk b/makefiles/config_aerocore_default.mk new file mode 100644 index 000000000..d6902c4ee --- /dev/null +++ b/makefiles/config_aerocore_default.mk @@ -0,0 +1,125 @@ +# +# Makefile for the AeroCore *default* configuration +# + +# +# Use the configuration's ROMFS. +# +ROMFS_ROOT = $(PX4_BASE)/ROMFS/px4fmu_common + +# +# Board support modules +# +MODULES += drivers/device +MODULES += drivers/stm32 +MODULES += drivers/stm32/adc +MODULES += drivers/stm32/tone_alarm +MODULES += drivers/led +MODULES += drivers/px4fmu +MODULES += drivers/boards/aerocore +MODULES += drivers/lsm303d +MODULES += drivers/l3gd20 +MODULES += drivers/ms5611 +MODULES += drivers/gps +MODULES += drivers/hil +MODULES += modules/sensors + +# +# System commands +# +MODULES += systemcmds/boardinfo +MODULES += systemcmds/mixer +MODULES += systemcmds/param +MODULES += systemcmds/perf +MODULES += systemcmds/preflight_check +MODULES += systemcmds/pwm +MODULES += systemcmds/esc_calib +MODULES += systemcmds/reboot +MODULES += systemcmds/top +MODULES += systemcmds/config +MODULES += systemcmds/nshterm +MODULES += systemcmds/mtd +MODULES += systemcmds/dumpfile + +# +# General system control +# +MODULES += modules/commander +MODULES += modules/navigator +MODULES += modules/mavlink + +# +# Estimation modules (EKF/ SO3 / other filters) +# +MODULES += modules/attitude_estimator_ekf +MODULES += modules/attitude_estimator_so3 +MODULES += modules/ekf_att_pos_estimator +MODULES += modules/position_estimator_inav + +# +# Vehicle Control +# +MODULES += modules/fw_pos_control_l1 +MODULES += modules/fw_att_control +MODULES += modules/mc_att_control +MODULES += modules/mc_pos_control + +# +# Library modules +# +MODULES += modules/systemlib +MODULES += modules/systemlib/mixer +MODULES += modules/controllib +MODULES += modules/uORB +MODULES += modules/dataman + +# +# Libraries +# +LIBRARIES += lib/mathlib/CMSIS +MODULES += lib/mathlib +MODULES += lib/mathlib/math/filter +MODULES += lib/ecl +MODULES += lib/external_lgpl +MODULES += lib/geo +MODULES += lib/conversion +MODULES += lib/launchdetection + +# +# Demo apps +# +#MODULES += examples/math_demo +# Tutorial code from +# https://pixhawk.ethz.ch/px4/dev/hello_sky +MODULES += examples/px4_simple_app + +# Tutorial code from +# https://pixhawk.ethz.ch/px4/dev/daemon +#MODULES += examples/px4_daemon_app + +# Tutorial code from +# https://pixhawk.ethz.ch/px4/dev/debug_values +#MODULES += examples/px4_mavlink_debug + +# Tutorial code from +# https://pixhawk.ethz.ch/px4/dev/example_fixedwing_control +#MODULES += examples/fixedwing_control + +# Hardware test +#MODULES += examples/hwtest + +# +# Transitional support - add commands from the NuttX export archive. +# +# In general, these should move to modules over time. +# +# Each entry here is <command>.<priority>.<stacksize>.<entrypoint> but we use a helper macro +# to make the table a bit more readable. +# +define _B + $(strip $1).$(or $(strip $2),SCHED_PRIORITY_DEFAULT).$(or $(strip $3),CONFIG_PTHREAD_STACK_DEFAULT).$(strip $4) +endef + +BUILTIN_COMMANDS := \ + $(call _B, hello, , 2048, hello_main) \ + $(call _B, i2c, , 2048, i2c_main) diff --git a/makefiles/config_px4fmu-v1_default.mk b/makefiles/config_px4fmu-v1_default.mk index 651c2ac38..810e008ae 100644 --- a/makefiles/config_px4fmu-v1_default.mk +++ b/makefiles/config_px4fmu-v1_default.mk @@ -55,8 +55,8 @@ MODULES += systemcmds/top MODULES += systemcmds/tests MODULES += systemcmds/config MODULES += systemcmds/nshterm -MODULES += systemcmds/hw_ver MODULES += systemcmds/dumpfile +MODULES += systemcmds/ver # # General system control @@ -70,7 +70,7 @@ MODULES += modules/gpio_led # Estimation modules (EKF/ SO3 / other filters) # MODULES += modules/attitude_estimator_ekf -MODULES += modules/att_pos_estimator_ekf +MODULES += modules/ekf_att_pos_estimator MODULES += modules/position_estimator_inav #MODULES += examples/flow_position_estimator diff --git a/makefiles/config_px4fmu-v2_default.mk b/makefiles/config_px4fmu-v2_default.mk index 5bed190d9..d6e88859c 100644 --- a/makefiles/config_px4fmu-v2_default.mk +++ b/makefiles/config_px4fmu-v2_default.mk @@ -63,8 +63,8 @@ MODULES += systemcmds/tests MODULES += systemcmds/config MODULES += systemcmds/nshterm MODULES += systemcmds/mtd -MODULES += systemcmds/hw_ver MODULES += systemcmds/dumpfile +MODULES += systemcmds/ver # # General system control @@ -79,7 +79,7 @@ MODULES += modules/gpio_led # MODULES += modules/attitude_estimator_ekf MODULES += modules/attitude_estimator_so3 -MODULES += modules/att_pos_estimator_ekf +MODULES += modules/ekf_att_pos_estimator MODULES += modules/position_estimator_inav MODULES += examples/flow_position_estimator diff --git a/makefiles/config_px4fmu-v2_test.mk b/makefiles/config_px4fmu-v2_test.mk index 79922374d..84274bf75 100644 --- a/makefiles/config_px4fmu-v2_test.mk +++ b/makefiles/config_px4fmu-v2_test.mk @@ -29,7 +29,7 @@ MODULES += systemcmds/reboot MODULES += systemcmds/tests MODULES += systemcmds/nshterm MODULES += systemcmds/mtd -MODULES += systemcmds/hw_ver +MODULES += systemcmds/ver # # Library modules diff --git a/makefiles/firmware.mk b/makefiles/firmware.mk index 1b646d9e0..60602e76f 100644 --- a/makefiles/firmware.mk +++ b/makefiles/firmware.mk @@ -113,7 +113,7 @@ endif $(info % GIT_DESC = $(GIT_DESC)) # -# Set a default target so that included makefiles or errors here don't +# Set a default target so that included makefiles or errors here don't # cause confusion. # # XXX We could do something cute here with $(DEFAULT_GOAL) if it's not one @@ -177,7 +177,7 @@ GLOBAL_DEPS += $(MAKEFILE_LIST) # # Extra things we should clean # -EXTRA_CLEANS = +EXTRA_CLEANS = # @@ -371,6 +371,8 @@ $(ROMFS_IMG): $(ROMFS_SCRATCH) $(ROMFS_DEPS) $(GLOBAL_DEPS) $(ROMFS_SCRATCH): $(ROMFS_DEPS) $(GLOBAL_DEPS) $(Q) $(MKDIR) -p $(ROMFS_SCRATCH) $(Q) $(COPYDIR) $(ROMFS_ROOT)/* $(ROMFS_SCRATCH) +# delete all files in ROMFS_SCRATCH which start with a . or end with a ~ + $(Q) $(RM) $(ROMFS_SCRATCH)/*/.[!.]* $(ROMFS_SCRATCH)/*/*~ ifneq ($(ROMFS_EXTRA_FILES),) $(Q) $(MKDIR) -p $(ROMFS_SCRATCH)/extras $(Q) $(COPY) $(ROMFS_EXTRA_FILES) $(ROMFS_SCRATCH)/extras diff --git a/makefiles/toolchain_gnu-arm-eabi.mk b/makefiles/toolchain_gnu-arm-eabi.mk index bb729e103..b519e0e7a 100644 --- a/makefiles/toolchain_gnu-arm-eabi.mk +++ b/makefiles/toolchain_gnu-arm-eabi.mk @@ -1,5 +1,5 @@ # -# Copyright (C) 2012 PX4 Development Team. All rights reserved. +# Copyright (C) 2012-2014 PX4 Development Team. All rights reserved. # # Redistribution and use in source and binary forms, with or without # modification, are permitted provided that the following conditions @@ -125,7 +125,11 @@ ARCHWARNINGS = -Wall \ -Wlogical-op \ -Wmissing-declarations \ -Wpacked \ - -Wno-unused-parameter + -Wno-unused-parameter \ + -Werror=format-security \ + -Werror=array-bounds \ + -Wfatal-errors \ + -Wformat=1 # -Wcast-qual - generates spurious noreturn attribute warnings, try again later # -Wconversion - would be nice, but too many "risky-but-safe" conversions in the code # -Wcast-align - would help catch bad casts in some cases, but generates too many false positives @@ -142,7 +146,8 @@ ARCHCWARNINGS = $(ARCHWARNINGS) \ # C++-specific warnings # -ARCHWARNINGSXX = $(ARCHWARNINGS) +ARCHWARNINGSXX = $(ARCHWARNINGS) \ + -Wno-missing-field-initializers # pull in *just* libm from the toolchain ... this is grody LIBM := $(shell $(CC) $(ARCHCPUFLAGS) -print-file-name=libm.a) diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/ardupilotmega.h b/mavlink/include/mavlink/v1.0/ardupilotmega/ardupilotmega.h index 2acb7965c..c887dc68a 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/ardupilotmega.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/ardupilotmega.h @@ -12,15 +12,15 @@ extern "C" { // MESSAGE LENGTHS AND CRCS #ifndef MAVLINK_MESSAGE_LENGTHS -#define MAVLINK_MESSAGE_LENGTHS {9, 31, 12, 0, 14, 28, 3, 32, 0, 0, 0, 6, 0, 0, 0, 0, 0, 0, 0, 0, 20, 2, 25, 23, 30, 101, 22, 26, 16, 14, 28, 32, 28, 28, 22, 22, 21, 6, 6, 37, 4, 4, 2, 2, 4, 2, 2, 3, 13, 12, 19, 17, 15, 15, 27, 25, 18, 18, 20, 20, 9, 34, 26, 46, 36, 0, 6, 4, 0, 11, 18, 0, 0, 0, 20, 0, 33, 3, 0, 0, 20, 22, 0, 0, 0, 0, 0, 0, 0, 28, 56, 42, 33, 0, 0, 0, 0, 0, 0, 0, 26, 32, 32, 20, 32, 62, 54, 64, 84, 9, 254, 249, 9, 36, 26, 64, 22, 6, 14, 12, 97, 2, 2, 113, 35, 0, 0, 0, 0, 0, 13, 255, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 24, 33, 25, 42, 8, 4, 12, 15, 13, 6, 15, 14, 0, 12, 3, 8, 28, 44, 3, 9, 22, 12, 18, 34, 66, 98, 8, 48, 19, 3, 0, 24, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 30, 18, 18, 51, 9, 0} +#define MAVLINK_MESSAGE_LENGTHS {9, 31, 12, 0, 14, 28, 3, 32, 0, 0, 0, 6, 0, 0, 0, 0, 0, 0, 0, 0, 20, 2, 25, 23, 30, 101, 22, 26, 16, 14, 28, 32, 28, 28, 22, 22, 21, 6, 6, 37, 4, 4, 2, 2, 4, 2, 2, 3, 13, 12, 19, 17, 15, 15, 27, 25, 18, 18, 20, 20, 9, 34, 26, 46, 36, 42, 6, 4, 0, 11, 18, 0, 0, 0, 20, 0, 33, 3, 0, 0, 20, 22, 0, 0, 0, 0, 0, 0, 0, 28, 56, 42, 33, 0, 0, 0, 0, 0, 0, 0, 26, 32, 32, 20, 32, 62, 54, 64, 84, 9, 254, 249, 9, 36, 26, 64, 22, 6, 14, 12, 97, 2, 2, 113, 35, 6, 79, 0, 0, 0, 13, 255, 14, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 24, 33, 25, 42, 8, 4, 12, 15, 13, 6, 15, 14, 0, 12, 3, 8, 28, 44, 3, 9, 22, 12, 18, 34, 66, 98, 8, 48, 19, 3, 20, 24, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 30, 18, 18, 51, 9, 0} #endif #ifndef MAVLINK_MESSAGE_CRCS -#define MAVLINK_MESSAGE_CRCS {50, 124, 137, 0, 237, 217, 104, 119, 0, 0, 0, 89, 0, 0, 0, 0, 0, 0, 0, 0, 214, 159, 220, 168, 24, 23, 170, 144, 67, 115, 39, 246, 185, 104, 237, 244, 222, 212, 9, 254, 230, 28, 28, 132, 221, 232, 11, 153, 41, 39, 214, 223, 141, 33, 15, 3, 100, 24, 239, 238, 30, 240, 183, 130, 130, 0, 148, 21, 0, 243, 124, 0, 0, 0, 20, 0, 152, 143, 0, 0, 127, 106, 0, 0, 0, 0, 0, 0, 0, 231, 183, 63, 54, 0, 0, 0, 0, 0, 0, 0, 175, 102, 158, 208, 56, 93, 211, 108, 32, 185, 235, 93, 124, 124, 119, 4, 76, 128, 56, 116, 134, 237, 203, 250, 87, 0, 0, 0, 0, 0, 29, 223, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 177, 241, 15, 134, 219, 208, 188, 84, 22, 19, 21, 134, 0, 78, 68, 189, 127, 154, 21, 21, 144, 1, 234, 73, 181, 22, 83, 167, 138, 234, 0, 47, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 204, 49, 170, 44, 83, 46, 0} +#define MAVLINK_MESSAGE_CRCS {50, 124, 137, 0, 237, 217, 104, 119, 0, 0, 0, 89, 0, 0, 0, 0, 0, 0, 0, 0, 214, 159, 220, 168, 24, 23, 170, 144, 67, 115, 39, 246, 185, 104, 237, 244, 222, 212, 9, 254, 230, 28, 28, 132, 221, 232, 11, 153, 41, 39, 214, 223, 141, 33, 15, 3, 100, 24, 239, 238, 30, 240, 183, 130, 130, 118, 148, 21, 0, 243, 124, 0, 0, 0, 20, 0, 152, 143, 0, 0, 127, 106, 0, 0, 0, 0, 0, 0, 0, 231, 183, 63, 54, 0, 0, 0, 0, 0, 0, 0, 175, 102, 158, 208, 56, 93, 211, 108, 32, 185, 235, 93, 124, 124, 119, 4, 76, 128, 56, 116, 134, 237, 203, 250, 87, 203, 220, 0, 0, 0, 29, 223, 85, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 177, 241, 15, 134, 219, 208, 188, 84, 22, 19, 21, 134, 0, 78, 68, 189, 127, 154, 21, 21, 144, 1, 234, 73, 181, 22, 83, 167, 138, 234, 240, 47, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 204, 49, 170, 44, 83, 46, 0} #endif #ifndef MAVLINK_MESSAGE_INFO -#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_MODE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_ATTITUDE_QUATERNION, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_WRITE_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_ITEM, MAVLINK_MESSAGE_INFO_MISSION_REQUEST, MAVLINK_MESSAGE_INFO_MISSION_SET_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_LIST, MAVLINK_MESSAGE_INFO_MISSION_COUNT, MAVLINK_MESSAGE_INFO_MISSION_CLEAR_ALL, MAVLINK_MESSAGE_INFO_MISSION_ITEM_REACHED, MAVLINK_MESSAGE_INFO_MISSION_ACK, MAVLINK_MESSAGE_INFO_SET_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_SET_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SET_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_MOTORS_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_DATA_STREAM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_VFR_HUD, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_COMMAND_LONG, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_MANUAL_SETPOINT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_HIL_RC_INPUTS_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_GLOBAL_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_SPEED_ESTIMATE, MAVLINK_MESSAGE_INFO_VICON_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_HIGHRES_IMU, MAVLINK_MESSAGE_INFO_OMNIDIRECTIONAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_SENSOR, MAVLINK_MESSAGE_INFO_SIM_STATE, MAVLINK_MESSAGE_INFO_RADIO_STATUS, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_START, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_DIR_LIST, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_RES, MAVLINK_MESSAGE_INFO_HIL_GPS, MAVLINK_MESSAGE_INFO_HIL_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION, MAVLINK_MESSAGE_INFO_SCALED_IMU2, MAVLINK_MESSAGE_INFO_LOG_REQUEST_LIST, MAVLINK_MESSAGE_INFO_LOG_ENTRY, MAVLINK_MESSAGE_INFO_LOG_REQUEST_DATA, MAVLINK_MESSAGE_INFO_LOG_DATA, MAVLINK_MESSAGE_INFO_LOG_ERASE, MAVLINK_MESSAGE_INFO_LOG_REQUEST_END, MAVLINK_MESSAGE_INFO_GPS_INJECT_DATA, MAVLINK_MESSAGE_INFO_GPS2_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_DATA_TRANSMISSION_HANDSHAKE, MAVLINK_MESSAGE_INFO_ENCAPSULATED_DATA, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_BATTERY_STATUS, MAVLINK_MESSAGE_INFO_SETPOINT_8DOF, MAVLINK_MESSAGE_INFO_SETPOINT_6DOF, MAVLINK_MESSAGE_INFO_SENSOR_OFFSETS, MAVLINK_MESSAGE_INFO_SET_MAG_OFFSETS, MAVLINK_MESSAGE_INFO_MEMINFO, MAVLINK_MESSAGE_INFO_AP_ADC, MAVLINK_MESSAGE_INFO_DIGICAM_CONFIGURE, MAVLINK_MESSAGE_INFO_DIGICAM_CONTROL, MAVLINK_MESSAGE_INFO_MOUNT_CONFIGURE, MAVLINK_MESSAGE_INFO_MOUNT_CONTROL, MAVLINK_MESSAGE_INFO_MOUNT_STATUS, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_FENCE_POINT, MAVLINK_MESSAGE_INFO_FENCE_FETCH_POINT, MAVLINK_MESSAGE_INFO_FENCE_STATUS, MAVLINK_MESSAGE_INFO_AHRS, MAVLINK_MESSAGE_INFO_SIMSTATE, MAVLINK_MESSAGE_INFO_HWSTATUS, MAVLINK_MESSAGE_INFO_RADIO, MAVLINK_MESSAGE_INFO_LIMITS_STATUS, MAVLINK_MESSAGE_INFO_WIND, MAVLINK_MESSAGE_INFO_DATA16, MAVLINK_MESSAGE_INFO_DATA32, MAVLINK_MESSAGE_INFO_DATA64, MAVLINK_MESSAGE_INFO_DATA96, MAVLINK_MESSAGE_INFO_RANGEFINDER, MAVLINK_MESSAGE_INFO_AIRSPEED_AUTOCAL, MAVLINK_MESSAGE_INFO_RALLY_POINT, MAVLINK_MESSAGE_INFO_RALLY_FETCH_POINT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_AHRS2, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MEMORY_VECT, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}} +#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_MODE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_ATTITUDE_QUATERNION, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_WRITE_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_ITEM, MAVLINK_MESSAGE_INFO_MISSION_REQUEST, MAVLINK_MESSAGE_INFO_MISSION_SET_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_LIST, MAVLINK_MESSAGE_INFO_MISSION_COUNT, MAVLINK_MESSAGE_INFO_MISSION_CLEAR_ALL, MAVLINK_MESSAGE_INFO_MISSION_ITEM_REACHED, MAVLINK_MESSAGE_INFO_MISSION_ACK, MAVLINK_MESSAGE_INFO_SET_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_SET_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SET_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_MOTORS_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, MAVLINK_MESSAGE_INFO_RC_CHANNELS, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_DATA_STREAM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_VFR_HUD, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_COMMAND_LONG, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_MANUAL_SETPOINT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_HIL_RC_INPUTS_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_GLOBAL_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_SPEED_ESTIMATE, MAVLINK_MESSAGE_INFO_VICON_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_HIGHRES_IMU, MAVLINK_MESSAGE_INFO_OMNIDIRECTIONAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_SENSOR, MAVLINK_MESSAGE_INFO_SIM_STATE, MAVLINK_MESSAGE_INFO_RADIO_STATUS, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_START, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_DIR_LIST, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_RES, MAVLINK_MESSAGE_INFO_HIL_GPS, MAVLINK_MESSAGE_INFO_HIL_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION, MAVLINK_MESSAGE_INFO_SCALED_IMU2, MAVLINK_MESSAGE_INFO_LOG_REQUEST_LIST, MAVLINK_MESSAGE_INFO_LOG_ENTRY, MAVLINK_MESSAGE_INFO_LOG_REQUEST_DATA, MAVLINK_MESSAGE_INFO_LOG_DATA, MAVLINK_MESSAGE_INFO_LOG_ERASE, MAVLINK_MESSAGE_INFO_LOG_REQUEST_END, MAVLINK_MESSAGE_INFO_GPS_INJECT_DATA, MAVLINK_MESSAGE_INFO_GPS2_RAW, MAVLINK_MESSAGE_INFO_POWER_STATUS, MAVLINK_MESSAGE_INFO_SERIAL_CONTROL, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_DATA_TRANSMISSION_HANDSHAKE, MAVLINK_MESSAGE_INFO_ENCAPSULATED_DATA, MAVLINK_MESSAGE_INFO_DISTANCE_SENSOR, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_BATTERY_STATUS, MAVLINK_MESSAGE_INFO_SETPOINT_8DOF, MAVLINK_MESSAGE_INFO_SETPOINT_6DOF, MAVLINK_MESSAGE_INFO_SENSOR_OFFSETS, MAVLINK_MESSAGE_INFO_SET_MAG_OFFSETS, MAVLINK_MESSAGE_INFO_MEMINFO, MAVLINK_MESSAGE_INFO_AP_ADC, MAVLINK_MESSAGE_INFO_DIGICAM_CONFIGURE, MAVLINK_MESSAGE_INFO_DIGICAM_CONTROL, MAVLINK_MESSAGE_INFO_MOUNT_CONFIGURE, MAVLINK_MESSAGE_INFO_MOUNT_CONTROL, MAVLINK_MESSAGE_INFO_MOUNT_STATUS, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_FENCE_POINT, MAVLINK_MESSAGE_INFO_FENCE_FETCH_POINT, MAVLINK_MESSAGE_INFO_FENCE_STATUS, MAVLINK_MESSAGE_INFO_AHRS, MAVLINK_MESSAGE_INFO_SIMSTATE, MAVLINK_MESSAGE_INFO_HWSTATUS, MAVLINK_MESSAGE_INFO_RADIO, MAVLINK_MESSAGE_INFO_LIMITS_STATUS, MAVLINK_MESSAGE_INFO_WIND, MAVLINK_MESSAGE_INFO_DATA16, MAVLINK_MESSAGE_INFO_DATA32, MAVLINK_MESSAGE_INFO_DATA64, MAVLINK_MESSAGE_INFO_DATA96, MAVLINK_MESSAGE_INFO_RANGEFINDER, MAVLINK_MESSAGE_INFO_AIRSPEED_AUTOCAL, MAVLINK_MESSAGE_INFO_RALLY_POINT, MAVLINK_MESSAGE_INFO_RALLY_FETCH_POINT, MAVLINK_MESSAGE_INFO_COMPASSMOT_STATUS, MAVLINK_MESSAGE_INFO_AHRS2, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, 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{"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MEMORY_VECT, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}} #endif #include "../protocol.h" @@ -30,95 +30,6 @@ extern "C" { // ENUM DEFINITIONS -/** @brief Enumeration of possible mount operation modes */ -#ifndef HAVE_ENUM_MAV_MOUNT_MODE -#define HAVE_ENUM_MAV_MOUNT_MODE -enum MAV_MOUNT_MODE -{ - MAV_MOUNT_MODE_RETRACT=0, /* Load and keep safe position (Roll,Pitch,Yaw) from EEPROM and stop stabilization | */ - MAV_MOUNT_MODE_NEUTRAL=1, /* Load and keep neutral position (Roll,Pitch,Yaw) from EEPROM. | */ - MAV_MOUNT_MODE_MAVLINK_TARGETING=2, /* Load neutral position and start MAVLink Roll,Pitch,Yaw control with stabilization | */ - MAV_MOUNT_MODE_RC_TARGETING=3, /* Load neutral position and start RC Roll,Pitch,Yaw control with stabilization | */ - MAV_MOUNT_MODE_GPS_POINT=4, /* Load neutral position and start to point to Lat,Lon,Alt | */ - MAV_MOUNT_MODE_ENUM_END=5, /* | */ -}; -#endif - -/** @brief */ -#ifndef HAVE_ENUM_MAV_CMD -#define HAVE_ENUM_MAV_CMD -enum MAV_CMD -{ - MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing)| Latitude| Longitude| Altitude| */ - MAV_CMD_NAV_LOITER_UNLIM=17, /* Loiter around this MISSION an unlimited amount of time |Empty| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */ - MAV_CMD_NAV_LOITER_TURNS=18, /* Loiter around this MISSION for X turns |Turns| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */ - MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this MISSION for X seconds |Seconds (decimal)| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */ - MAV_CMD_NAV_RETURN_TO_LAUNCH=20, /* Return to launch location |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_NAV_LAND=21, /* Land at location |Empty| Empty| Empty| Desired yaw angle.| Latitude| Longitude| Altitude| */ - MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer| Latitude| Longitude| Altitude| */ - MAV_CMD_NAV_ROI=80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */ - MAV_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */ - MAV_CMD_NAV_LAST=95, /* NOP - This command is only used to mark the upper limit of the NAV/ACTION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_CONDITION_DELAY=112, /* Delay mission state machine. |Delay in seconds (decimal)| Empty| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_CONDITION_CHANGE_ALT=113, /* Ascend/descend at rate. Delay mission state machine until desired altitude reached. |Descent / Ascend rate (m/s)| Empty| Empty| Empty| Empty| Empty| Finish Altitude| */ - MAV_CMD_CONDITION_DISTANCE=114, /* Delay mission state machine until within desired distance of next NAV point. |Distance (meters)| Empty| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_CONDITION_YAW=115, /* Reach a certain target angle. |target angle: [0-360], 0 is north| speed during yaw change:[deg per second]| direction: negative: counter clockwise, positive: clockwise [-1,1]| relative offset or absolute angle: [ 1,0]| Empty| Empty| Empty| */ - MAV_CMD_CONDITION_LAST=159, /* NOP - This command is only used to mark the upper limit of the CONDITION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_DO_SET_MODE=176, /* Set system mode. |Mode, as defined by ENUM MAV_MODE| Empty| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_DO_JUMP=177, /* Jump to the desired command in the mission list. Repeat this action only the specified number of times |Sequence number| Repeat count| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_DO_CHANGE_SPEED=178, /* Change speed and/or throttle set points. |Speed type (0=Airspeed, 1=Ground Speed)| Speed (m/s, -1 indicates no change)| Throttle ( Percent, -1 indicates no change)| Empty| Empty| Empty| Empty| */ - MAV_CMD_DO_SET_HOME=179, /* Changes the home location either to the current location or a specified location. |Use current (1=use current location, 0=use specified location)| Empty| Empty| Empty| Latitude| Longitude| Altitude| */ - MAV_CMD_DO_SET_PARAMETER=180, /* Set a system parameter. Caution! Use of this command requires knowledge of the numeric enumeration value of the parameter. |Parameter number| Parameter value| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_DO_SET_RELAY=181, /* Set a relay to a condition. |Relay number| Setting (1=on, 0=off, others possible depending on system hardware)| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_DO_REPEAT_RELAY=182, /* Cycle a relay on and off for a desired number of cyles with a desired period. |Relay number| Cycle count| Cycle time (seconds, decimal)| Empty| Empty| Empty| Empty| */ - MAV_CMD_DO_SET_SERVO=183, /* Set a servo to a desired PWM value. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_DO_REPEAT_SERVO=184, /* Cycle a between its nominal setting and a desired PWM for a desired number of cycles with a desired period. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Cycle count| Cycle time (seconds)| Empty| Empty| Empty| */ - MAV_CMD_DO_CONTROL_VIDEO=200, /* Control onboard camera system. |Camera ID (-1 for all)| Transmission: 0: disabled, 1: enabled compressed, 2: enabled raw| Transmission mode: 0: video stream, >0: single images every n seconds (decimal)| Recording: 0: disabled, 1: enabled compressed, 2: enabled raw| Empty| Empty| Empty| */ - MAV_CMD_DO_SET_ROI=201, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */ - MAV_CMD_DO_DIGICAM_CONFIGURE=202, /* Mission command to configure an on-board camera controller system. |Modes: P, TV, AV, M, Etc| Shutter speed: Divisor number for one second| Aperture: F stop number| ISO number e.g. 80, 100, 200, Etc| Exposure type enumerator| Command Identity| Main engine cut-off time before camera trigger in seconds/10 (0 means no cut-off)| */ - MAV_CMD_DO_DIGICAM_CONTROL=203, /* Mission command to control an on-board camera controller system. |Session control e.g. show/hide lens| Zoom's absolute position| Zooming step value to offset zoom from the current position| Focus Locking, Unlocking or Re-locking| Shooting Command| Command Identity| Empty| */ - MAV_CMD_DO_MOUNT_CONFIGURE=204, /* Mission command to configure a camera or antenna mount |Mount operation mode (see MAV_MOUNT_MODE enum)| stabilize roll? (1 = yes, 0 = no)| stabilize pitch? (1 = yes, 0 = no)| stabilize yaw? (1 = yes, 0 = no)| Empty| Empty| Empty| */ - MAV_CMD_DO_MOUNT_CONTROL=205, /* Mission command to control a camera or antenna mount |pitch(deg*100) or lat, depending on mount mode.| roll(deg*100) or lon depending on mount mode| yaw(deg*100) or alt (in cm) depending on mount mode| Empty| Empty| Empty| Empty| */ - MAV_CMD_DO_SET_CAM_TRIGG_DIST=206, /* Mission command to set CAM_TRIGG_DIST for this flight |Camera trigger distance (meters)| Empty| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_PREFLIGHT_CALIBRATION=241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Empty| Empty| */ - MAV_CMD_PREFLIGHT_SET_SENSOR_OFFSETS=242, /* Set sensor offsets. This command will be only accepted if in pre-flight mode. |Sensor to adjust the offsets for: 0: gyros, 1: accelerometer, 2: magnetometer, 3: barometer, 4: optical flow| X axis offset (or generic dimension 1), in the sensor's raw units| Y axis offset (or generic dimension 2), in the sensor's raw units| Z axis offset (or generic dimension 3), in the sensor's raw units| Generic dimension 4, in the sensor's raw units| Generic dimension 5, in the sensor's raw units| Generic dimension 6, in the sensor's raw units| */ - MAV_CMD_PREFLIGHT_STORAGE=245, /* Request storage of different parameter values and logs. This command will be only accepted if in pre-flight mode. |Parameter storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Mission storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Reserved| Reserved| Empty| Empty| Empty| */ - MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN=246, /* Request the reboot or shutdown of system components. |0: Do nothing for autopilot, 1: Reboot autopilot, 2: Shutdown autopilot.| 0: Do nothing for onboard computer, 1: Reboot onboard computer, 2: Shutdown onboard computer.| Reserved| Reserved| Empty| Empty| Empty| */ - MAV_CMD_OVERRIDE_GOTO=252, /* Hold / continue the current action |MAV_GOTO_DO_HOLD: hold MAV_GOTO_DO_CONTINUE: continue with next item in mission plan| MAV_GOTO_HOLD_AT_CURRENT_POSITION: Hold at current position MAV_GOTO_HOLD_AT_SPECIFIED_POSITION: hold at specified position| MAV_FRAME coordinate frame of hold point| Desired yaw angle in degrees| Latitude / X position| Longitude / Y position| Altitude / Z position| */ - MAV_CMD_MISSION_START=300, /* start running a mission |first_item: the first mission item to run| last_item: the last mission item to run (after this item is run, the mission ends)| */ - MAV_CMD_COMPONENT_ARM_DISARM=400, /* Arms / Disarms a component |1 to arm, 0 to disarm| */ - MAV_CMD_START_RX_PAIR=500, /* Starts receiver pairing |0:Spektrum| 0:Spektrum DSM2, 1:Spektrum DSMX| */ - MAV_CMD_ENUM_END=501, /* | */ -}; -#endif - -/** @brief */ -#ifndef HAVE_ENUM_FENCE_ACTION -#define HAVE_ENUM_FENCE_ACTION -enum FENCE_ACTION -{ - FENCE_ACTION_NONE=0, /* Disable fenced mode | */ - FENCE_ACTION_GUIDED=1, /* Switched to guided mode to return point (fence point 0) | */ - FENCE_ACTION_REPORT=2, /* Report fence breach, but don't take action | */ - FENCE_ACTION_GUIDED_THR_PASS=3, /* Switched to guided mode to return point (fence point 0) with manual throttle control | */ - FENCE_ACTION_ENUM_END=4, /* | */ -}; -#endif - -/** @brief */ -#ifndef HAVE_ENUM_FENCE_BREACH -#define HAVE_ENUM_FENCE_BREACH -enum FENCE_BREACH -{ - FENCE_BREACH_NONE=0, /* No last fence breach | */ - FENCE_BREACH_MINALT=1, /* Breached minimum altitude | */ - FENCE_BREACH_MAXALT=2, /* Breached maximum altitude | */ - FENCE_BREACH_BOUNDARY=3, /* Breached fence boundary | */ - FENCE_BREACH_ENUM_END=4, /* | */ -}; -#endif - /** @brief */ #ifndef HAVE_ENUM_LIMITS_STATE #define HAVE_ENUM_LIMITS_STATE @@ -157,6 +68,18 @@ enum RALLY_FLAGS }; #endif +/** @brief */ +#ifndef HAVE_ENUM_PARACHUTE_ACTION +#define HAVE_ENUM_PARACHUTE_ACTION +enum PARACHUTE_ACTION +{ + PARACHUTE_DISABLE=0, /* Disable parachute release | */ + PARACHUTE_ENABLE=1, /* Enable parachute release | */ + PARACHUTE_RELEASE=2, /* Release parachute | */ + PARACHUTE_ACTION_ENUM_END=3, /* | */ +}; +#endif + #include "../common/common.h" // MAVLINK VERSION @@ -197,6 +120,7 @@ enum RALLY_FLAGS #include "./mavlink_msg_airspeed_autocal.h" #include "./mavlink_msg_rally_point.h" #include "./mavlink_msg_rally_fetch_point.h" +#include "./mavlink_msg_compassmot_status.h" #include "./mavlink_msg_ahrs2.h" #ifdef __cplusplus diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_ahrs.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_ahrs.h index c3ead1140..50ddc79e5 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_ahrs.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_ahrs.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_ahrs_send(mavlink_channel_t chan, float omegaIx, #endif } +#if MAVLINK_MSG_ID_AHRS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_ahrs_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float omegaIx, float omegaIy, float omegaIz, float accel_weight, float renorm_val, float error_rp, float error_yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, omegaIx); + _mav_put_float(buf, 4, omegaIy); + _mav_put_float(buf, 8, omegaIz); + _mav_put_float(buf, 12, accel_weight); + _mav_put_float(buf, 16, renorm_val); + _mav_put_float(buf, 20, error_rp); + _mav_put_float(buf, 24, error_yaw); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AHRS, buf, MAVLINK_MSG_ID_AHRS_LEN, MAVLINK_MSG_ID_AHRS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AHRS, buf, MAVLINK_MSG_ID_AHRS_LEN); +#endif +#else + mavlink_ahrs_t *packet = (mavlink_ahrs_t *)msgbuf; + packet->omegaIx = omegaIx; + packet->omegaIy = omegaIy; + packet->omegaIz = omegaIz; + packet->accel_weight = accel_weight; + packet->renorm_val = renorm_val; + packet->error_rp = error_rp; + packet->error_yaw = error_yaw; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AHRS, (const char *)packet, MAVLINK_MSG_ID_AHRS_LEN, MAVLINK_MSG_ID_AHRS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AHRS, (const char *)packet, MAVLINK_MSG_ID_AHRS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE AHRS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_ahrs2.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_ahrs2.h index f6fde9590..33e006688 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_ahrs2.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_ahrs2.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_ahrs2_send(mavlink_channel_t chan, float roll, fl #endif } +#if MAVLINK_MSG_ID_AHRS2_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_ahrs2_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float roll, float pitch, float yaw, float altitude, int32_t lat, int32_t lng) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, roll); + _mav_put_float(buf, 4, pitch); + _mav_put_float(buf, 8, yaw); + _mav_put_float(buf, 12, altitude); + _mav_put_int32_t(buf, 16, lat); + _mav_put_int32_t(buf, 20, lng); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AHRS2, buf, MAVLINK_MSG_ID_AHRS2_LEN, MAVLINK_MSG_ID_AHRS2_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AHRS2, buf, MAVLINK_MSG_ID_AHRS2_LEN); +#endif +#else + mavlink_ahrs2_t *packet = (mavlink_ahrs2_t *)msgbuf; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + packet->altitude = altitude; + packet->lat = lat; + packet->lng = lng; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AHRS2, (const char *)packet, MAVLINK_MSG_ID_AHRS2_LEN, MAVLINK_MSG_ID_AHRS2_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AHRS2, (const char *)packet, MAVLINK_MSG_ID_AHRS2_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE AHRS2 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h index d046f2ad0..521831c8f 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_airspeed_autocal.h @@ -267,6 +267,60 @@ static inline void mavlink_msg_airspeed_autocal_send(mavlink_channel_t chan, flo #endif } +#if MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_airspeed_autocal_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float vx, float vy, float vz, float diff_pressure, float EAS2TAS, float ratio, float state_x, float state_y, float state_z, float Pax, float Pby, float Pcz) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, vx); + _mav_put_float(buf, 4, vy); + _mav_put_float(buf, 8, vz); + _mav_put_float(buf, 12, diff_pressure); + _mav_put_float(buf, 16, EAS2TAS); + _mav_put_float(buf, 20, ratio); + _mav_put_float(buf, 24, state_x); + _mav_put_float(buf, 28, state_y); + _mav_put_float(buf, 32, state_z); + _mav_put_float(buf, 36, Pax); + _mav_put_float(buf, 40, Pby); + _mav_put_float(buf, 44, Pcz); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, buf, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); +#endif +#else + mavlink_airspeed_autocal_t *packet = (mavlink_airspeed_autocal_t *)msgbuf; + packet->vx = vx; + packet->vy = vy; + packet->vz = vz; + packet->diff_pressure = diff_pressure; + packet->EAS2TAS = EAS2TAS; + packet->ratio = ratio; + packet->state_x = state_x; + packet->state_y = state_y; + packet->state_z = state_z; + packet->Pax = Pax; + packet->Pby = Pby; + packet->Pcz = Pcz; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, (const char *)packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL, (const char *)packet, MAVLINK_MSG_ID_AIRSPEED_AUTOCAL_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE AIRSPEED_AUTOCAL UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_ap_adc.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_ap_adc.h index 821ce73e4..3c18e644e 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_ap_adc.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_ap_adc.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_ap_adc_send(mavlink_channel_t chan, uint16_t adc1 #endif } +#if MAVLINK_MSG_ID_AP_ADC_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_ap_adc_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t adc1, uint16_t adc2, uint16_t adc3, uint16_t adc4, uint16_t adc5, uint16_t adc6) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, adc1); + _mav_put_uint16_t(buf, 2, adc2); + _mav_put_uint16_t(buf, 4, adc3); + _mav_put_uint16_t(buf, 6, adc4); + _mav_put_uint16_t(buf, 8, adc5); + _mav_put_uint16_t(buf, 10, adc6); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AP_ADC, buf, MAVLINK_MSG_ID_AP_ADC_LEN, MAVLINK_MSG_ID_AP_ADC_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AP_ADC, buf, MAVLINK_MSG_ID_AP_ADC_LEN); +#endif +#else + mavlink_ap_adc_t *packet = (mavlink_ap_adc_t *)msgbuf; + packet->adc1 = adc1; + packet->adc2 = adc2; + packet->adc3 = adc3; + packet->adc4 = adc4; + packet->adc5 = adc5; + packet->adc6 = adc6; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AP_ADC, (const char *)packet, MAVLINK_MSG_ID_AP_ADC_LEN, MAVLINK_MSG_ID_AP_ADC_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AP_ADC, (const char *)packet, MAVLINK_MSG_ID_AP_ADC_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE AP_ADC UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_compassmot_status.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_compassmot_status.h new file mode 100644 index 000000000..965545988 --- /dev/null +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_compassmot_status.h @@ -0,0 +1,329 @@ +// MESSAGE COMPASSMOT_STATUS PACKING + +#define MAVLINK_MSG_ID_COMPASSMOT_STATUS 177 + +typedef struct __mavlink_compassmot_status_t +{ + float current; ///< current (amps) + float CompensationX; ///< Motor Compensation X + float CompensationY; ///< Motor Compensation Y + float CompensationZ; ///< Motor Compensation Z + uint16_t throttle; ///< throttle (percent*10) + uint16_t interference; ///< interference (percent) +} mavlink_compassmot_status_t; + +#define MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN 20 +#define MAVLINK_MSG_ID_177_LEN 20 + +#define MAVLINK_MSG_ID_COMPASSMOT_STATUS_CRC 240 +#define MAVLINK_MSG_ID_177_CRC 240 + + + +#define MAVLINK_MESSAGE_INFO_COMPASSMOT_STATUS { \ + "COMPASSMOT_STATUS", \ + 6, \ + { { "current", NULL, MAVLINK_TYPE_FLOAT, 0, 0, offsetof(mavlink_compassmot_status_t, current) }, \ + { "CompensationX", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_compassmot_status_t, CompensationX) }, \ + { "CompensationY", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_compassmot_status_t, CompensationY) }, \ + { "CompensationZ", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_compassmot_status_t, CompensationZ) }, \ + { "throttle", NULL, MAVLINK_TYPE_UINT16_T, 0, 16, offsetof(mavlink_compassmot_status_t, throttle) }, \ + { "interference", NULL, MAVLINK_TYPE_UINT16_T, 0, 18, offsetof(mavlink_compassmot_status_t, interference) }, \ + } \ +} + + +/** + * @brief Pack a compassmot_status message + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param msg The MAVLink message to compress the data into + * + * @param throttle throttle (percent*10) + * @param current current (amps) + * @param interference interference (percent) + * @param CompensationX Motor Compensation X + * @param CompensationY Motor Compensation Y + * @param CompensationZ Motor Compensation Z + * @return length of the message in bytes (excluding serial stream start sign) + */ +static inline uint16_t mavlink_msg_compassmot_status_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, + uint16_t throttle, float current, uint16_t interference, float CompensationX, float CompensationY, float CompensationZ) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN]; + _mav_put_float(buf, 0, current); + _mav_put_float(buf, 4, CompensationX); + _mav_put_float(buf, 8, CompensationY); + _mav_put_float(buf, 12, CompensationZ); + _mav_put_uint16_t(buf, 16, throttle); + _mav_put_uint16_t(buf, 18, interference); + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN); +#else + mavlink_compassmot_status_t packet; + packet.current = current; + packet.CompensationX = CompensationX; + packet.CompensationY = CompensationY; + packet.CompensationZ = CompensationZ; + packet.throttle = throttle; + packet.interference = interference; + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN); +#endif + + msg->msgid = MAVLINK_MSG_ID_COMPASSMOT_STATUS; +#if MAVLINK_CRC_EXTRA + return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN, MAVLINK_MSG_ID_COMPASSMOT_STATUS_CRC); +#else + return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN); +#endif +} + +/** + * @brief Pack a compassmot_status message on a channel + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param chan The MAVLink channel this message will be sent over + * @param msg The MAVLink message to compress the data into + * @param throttle throttle (percent*10) + * @param current current (amps) + * @param interference interference (percent) + * @param CompensationX Motor Compensation X + * @param CompensationY Motor Compensation Y + * @param CompensationZ Motor Compensation Z + * @return length of the message in bytes (excluding serial stream start sign) + */ +static inline uint16_t mavlink_msg_compassmot_status_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, + mavlink_message_t* msg, + uint16_t throttle,float current,uint16_t interference,float CompensationX,float CompensationY,float CompensationZ) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN]; + _mav_put_float(buf, 0, current); + _mav_put_float(buf, 4, CompensationX); + _mav_put_float(buf, 8, CompensationY); + _mav_put_float(buf, 12, CompensationZ); + _mav_put_uint16_t(buf, 16, throttle); + _mav_put_uint16_t(buf, 18, interference); + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN); +#else + mavlink_compassmot_status_t packet; + packet.current = current; + packet.CompensationX = CompensationX; + packet.CompensationY = CompensationY; + packet.CompensationZ = CompensationZ; + packet.throttle = throttle; + packet.interference = interference; + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN); +#endif + + msg->msgid = MAVLINK_MSG_ID_COMPASSMOT_STATUS; +#if MAVLINK_CRC_EXTRA + return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN, MAVLINK_MSG_ID_COMPASSMOT_STATUS_CRC); +#else + return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN); +#endif +} + +/** + * @brief Encode a compassmot_status struct + * + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param msg The MAVLink message to compress the data into + * @param compassmot_status C-struct to read the message contents from + */ +static inline uint16_t mavlink_msg_compassmot_status_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_compassmot_status_t* compassmot_status) +{ + return mavlink_msg_compassmot_status_pack(system_id, component_id, msg, compassmot_status->throttle, compassmot_status->current, compassmot_status->interference, compassmot_status->CompensationX, compassmot_status->CompensationY, compassmot_status->CompensationZ); +} + +/** + * @brief Encode a compassmot_status struct on a channel + * + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param chan The MAVLink channel this message will be sent over + * @param msg The MAVLink message to compress the data into + * @param compassmot_status C-struct to read the message contents from + */ +static inline uint16_t mavlink_msg_compassmot_status_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_compassmot_status_t* compassmot_status) +{ + return mavlink_msg_compassmot_status_pack_chan(system_id, component_id, chan, msg, compassmot_status->throttle, compassmot_status->current, compassmot_status->interference, compassmot_status->CompensationX, compassmot_status->CompensationY, compassmot_status->CompensationZ); +} + +/** + * @brief Send a compassmot_status message + * @param chan MAVLink channel to send the message + * + * @param throttle throttle (percent*10) + * @param current current (amps) + * @param interference interference (percent) + * @param CompensationX Motor Compensation X + * @param CompensationY Motor Compensation Y + * @param CompensationZ Motor Compensation Z + */ +#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS + +static inline void mavlink_msg_compassmot_status_send(mavlink_channel_t chan, uint16_t throttle, float current, uint16_t interference, float CompensationX, float CompensationY, float CompensationZ) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN]; + _mav_put_float(buf, 0, current); + _mav_put_float(buf, 4, CompensationX); + _mav_put_float(buf, 8, CompensationY); + _mav_put_float(buf, 12, CompensationZ); + _mav_put_uint16_t(buf, 16, throttle); + _mav_put_uint16_t(buf, 18, interference); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMPASSMOT_STATUS, buf, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN, MAVLINK_MSG_ID_COMPASSMOT_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMPASSMOT_STATUS, buf, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN); +#endif +#else + mavlink_compassmot_status_t packet; + packet.current = current; + packet.CompensationX = CompensationX; + packet.CompensationY = CompensationY; + packet.CompensationZ = CompensationZ; + packet.throttle = throttle; + packet.interference = interference; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMPASSMOT_STATUS, (const char *)&packet, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN, MAVLINK_MSG_ID_COMPASSMOT_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMPASSMOT_STATUS, (const char *)&packet, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN); +#endif +#endif +} + +#if MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_compassmot_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t throttle, float current, uint16_t interference, float CompensationX, float CompensationY, float CompensationZ) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, current); + _mav_put_float(buf, 4, CompensationX); + _mav_put_float(buf, 8, CompensationY); + _mav_put_float(buf, 12, CompensationZ); + _mav_put_uint16_t(buf, 16, throttle); + _mav_put_uint16_t(buf, 18, interference); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMPASSMOT_STATUS, buf, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN, MAVLINK_MSG_ID_COMPASSMOT_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMPASSMOT_STATUS, buf, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN); +#endif +#else + mavlink_compassmot_status_t *packet = (mavlink_compassmot_status_t *)msgbuf; + packet->current = current; + packet->CompensationX = CompensationX; + packet->CompensationY = CompensationY; + packet->CompensationZ = CompensationZ; + packet->throttle = throttle; + packet->interference = interference; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMPASSMOT_STATUS, (const char *)packet, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN, MAVLINK_MSG_ID_COMPASSMOT_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMPASSMOT_STATUS, (const char *)packet, MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN); +#endif +#endif +} +#endif + +#endif + +// MESSAGE COMPASSMOT_STATUS UNPACKING + + +/** + * @brief Get field throttle from compassmot_status message + * + * @return throttle (percent*10) + */ +static inline uint16_t mavlink_msg_compassmot_status_get_throttle(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 16); +} + +/** + * @brief Get field current from compassmot_status message + * + * @return current (amps) + */ +static inline float mavlink_msg_compassmot_status_get_current(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 0); +} + +/** + * @brief Get field interference from compassmot_status message + * + * @return interference (percent) + */ +static inline uint16_t mavlink_msg_compassmot_status_get_interference(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 18); +} + +/** + * @brief Get field CompensationX from compassmot_status message + * + * @return Motor Compensation X + */ +static inline float mavlink_msg_compassmot_status_get_CompensationX(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 4); +} + +/** + * @brief Get field CompensationY from compassmot_status message + * + * @return Motor Compensation Y + */ +static inline float mavlink_msg_compassmot_status_get_CompensationY(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 8); +} + +/** + * @brief Get field CompensationZ from compassmot_status message + * + * @return Motor Compensation Z + */ +static inline float mavlink_msg_compassmot_status_get_CompensationZ(const mavlink_message_t* msg) +{ + return _MAV_RETURN_float(msg, 12); +} + +/** + * @brief Decode a compassmot_status message into a struct + * + * @param msg The message to decode + * @param compassmot_status C-struct to decode the message contents into + */ +static inline void mavlink_msg_compassmot_status_decode(const mavlink_message_t* msg, mavlink_compassmot_status_t* compassmot_status) +{ +#if MAVLINK_NEED_BYTE_SWAP + compassmot_status->current = mavlink_msg_compassmot_status_get_current(msg); + compassmot_status->CompensationX = mavlink_msg_compassmot_status_get_CompensationX(msg); + compassmot_status->CompensationY = mavlink_msg_compassmot_status_get_CompensationY(msg); + compassmot_status->CompensationZ = mavlink_msg_compassmot_status_get_CompensationZ(msg); + compassmot_status->throttle = mavlink_msg_compassmot_status_get_throttle(msg); + compassmot_status->interference = mavlink_msg_compassmot_status_get_interference(msg); +#else + memcpy(compassmot_status, _MAV_PAYLOAD(msg), MAVLINK_MSG_ID_COMPASSMOT_STATUS_LEN); +#endif +} diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data16.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data16.h index 9200eefa0..7bad1b23d 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data16.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data16.h @@ -162,6 +162,40 @@ static inline void mavlink_msg_data16_send(mavlink_channel_t chan, uint8_t type, #endif } +#if MAVLINK_MSG_ID_DATA16_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_data16_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t type, uint8_t len, const uint8_t *data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, type); + _mav_put_uint8_t(buf, 1, len); + _mav_put_uint8_t_array(buf, 2, data, 16); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA16, buf, MAVLINK_MSG_ID_DATA16_LEN, MAVLINK_MSG_ID_DATA16_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA16, buf, MAVLINK_MSG_ID_DATA16_LEN); +#endif +#else + mavlink_data16_t *packet = (mavlink_data16_t *)msgbuf; + packet->type = type; + packet->len = len; + mav_array_memcpy(packet->data, data, sizeof(uint8_t)*16); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA16, (const char *)packet, MAVLINK_MSG_ID_DATA16_LEN, MAVLINK_MSG_ID_DATA16_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA16, (const char *)packet, MAVLINK_MSG_ID_DATA16_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE DATA16 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data32.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data32.h index 3afedb787..df7a2ec80 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data32.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data32.h @@ -162,6 +162,40 @@ static inline void mavlink_msg_data32_send(mavlink_channel_t chan, uint8_t type, #endif } +#if MAVLINK_MSG_ID_DATA32_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_data32_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t type, uint8_t len, const uint8_t *data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, type); + _mav_put_uint8_t(buf, 1, len); + _mav_put_uint8_t_array(buf, 2, data, 32); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA32, buf, MAVLINK_MSG_ID_DATA32_LEN, MAVLINK_MSG_ID_DATA32_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA32, buf, MAVLINK_MSG_ID_DATA32_LEN); +#endif +#else + mavlink_data32_t *packet = (mavlink_data32_t *)msgbuf; + packet->type = type; + packet->len = len; + mav_array_memcpy(packet->data, data, sizeof(uint8_t)*32); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA32, (const char *)packet, MAVLINK_MSG_ID_DATA32_LEN, MAVLINK_MSG_ID_DATA32_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA32, (const char *)packet, MAVLINK_MSG_ID_DATA32_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE DATA32 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data64.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data64.h index 6931ada16..c354f8908 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data64.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data64.h @@ -162,6 +162,40 @@ static inline void mavlink_msg_data64_send(mavlink_channel_t chan, uint8_t type, #endif } +#if MAVLINK_MSG_ID_DATA64_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_data64_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t type, uint8_t len, const uint8_t *data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, type); + _mav_put_uint8_t(buf, 1, len); + _mav_put_uint8_t_array(buf, 2, data, 64); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA64, buf, MAVLINK_MSG_ID_DATA64_LEN, MAVLINK_MSG_ID_DATA64_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA64, buf, MAVLINK_MSG_ID_DATA64_LEN); +#endif +#else + mavlink_data64_t *packet = (mavlink_data64_t *)msgbuf; + packet->type = type; + packet->len = len; + mav_array_memcpy(packet->data, data, sizeof(uint8_t)*64); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA64, (const char *)packet, MAVLINK_MSG_ID_DATA64_LEN, MAVLINK_MSG_ID_DATA64_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA64, (const char *)packet, MAVLINK_MSG_ID_DATA64_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE DATA64 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data96.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data96.h index cffc7d7e7..634e3f81d 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data96.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_data96.h @@ -162,6 +162,40 @@ static inline void mavlink_msg_data96_send(mavlink_channel_t chan, uint8_t type, #endif } +#if MAVLINK_MSG_ID_DATA96_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_data96_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t type, uint8_t len, const uint8_t *data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, type); + _mav_put_uint8_t(buf, 1, len); + _mav_put_uint8_t_array(buf, 2, data, 96); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA96, buf, MAVLINK_MSG_ID_DATA96_LEN, MAVLINK_MSG_ID_DATA96_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA96, buf, MAVLINK_MSG_ID_DATA96_LEN); +#endif +#else + mavlink_data96_t *packet = (mavlink_data96_t *)msgbuf; + packet->type = type; + packet->len = len; + mav_array_memcpy(packet->data, data, sizeof(uint8_t)*96); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA96, (const char *)packet, MAVLINK_MSG_ID_DATA96_LEN, MAVLINK_MSG_ID_DATA96_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA96, (const char *)packet, MAVLINK_MSG_ID_DATA96_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE DATA96 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_digicam_configure.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_digicam_configure.h index c6518c419..d5f9e7132 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_digicam_configure.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_digicam_configure.h @@ -256,6 +256,58 @@ static inline void mavlink_msg_digicam_configure_send(mavlink_channel_t chan, ui #endif } +#if MAVLINK_MSG_ID_DIGICAM_CONFIGURE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_digicam_configure_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t mode, uint16_t shutter_speed, uint8_t aperture, uint8_t iso, uint8_t exposure_type, uint8_t command_id, uint8_t engine_cut_off, uint8_t extra_param, float extra_value) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, extra_value); + _mav_put_uint16_t(buf, 4, shutter_speed); + _mav_put_uint8_t(buf, 6, target_system); + _mav_put_uint8_t(buf, 7, target_component); + _mav_put_uint8_t(buf, 8, mode); + _mav_put_uint8_t(buf, 9, aperture); + _mav_put_uint8_t(buf, 10, iso); + _mav_put_uint8_t(buf, 11, exposure_type); + _mav_put_uint8_t(buf, 12, command_id); + _mav_put_uint8_t(buf, 13, engine_cut_off); + _mav_put_uint8_t(buf, 14, extra_param); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DIGICAM_CONFIGURE, buf, MAVLINK_MSG_ID_DIGICAM_CONFIGURE_LEN, MAVLINK_MSG_ID_DIGICAM_CONFIGURE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DIGICAM_CONFIGURE, buf, MAVLINK_MSG_ID_DIGICAM_CONFIGURE_LEN); +#endif +#else + mavlink_digicam_configure_t *packet = (mavlink_digicam_configure_t *)msgbuf; + packet->extra_value = extra_value; + packet->shutter_speed = shutter_speed; + packet->target_system = target_system; + packet->target_component = target_component; + packet->mode = mode; + packet->aperture = aperture; + packet->iso = iso; + packet->exposure_type = exposure_type; + packet->command_id = command_id; + packet->engine_cut_off = engine_cut_off; + packet->extra_param = extra_param; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DIGICAM_CONFIGURE, (const char *)packet, MAVLINK_MSG_ID_DIGICAM_CONFIGURE_LEN, MAVLINK_MSG_ID_DIGICAM_CONFIGURE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DIGICAM_CONFIGURE, (const char *)packet, MAVLINK_MSG_ID_DIGICAM_CONFIGURE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE DIGICAM_CONFIGURE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_digicam_control.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_digicam_control.h index bfa5414a3..68484f7b8 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_digicam_control.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_digicam_control.h @@ -245,6 +245,56 @@ static inline void mavlink_msg_digicam_control_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_DIGICAM_CONTROL_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_digicam_control_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t session, uint8_t zoom_pos, int8_t zoom_step, uint8_t focus_lock, uint8_t shot, uint8_t command_id, uint8_t extra_param, float extra_value) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, extra_value); + _mav_put_uint8_t(buf, 4, target_system); + _mav_put_uint8_t(buf, 5, target_component); + _mav_put_uint8_t(buf, 6, session); + _mav_put_uint8_t(buf, 7, zoom_pos); + _mav_put_int8_t(buf, 8, zoom_step); + _mav_put_uint8_t(buf, 9, focus_lock); + _mav_put_uint8_t(buf, 10, shot); + _mav_put_uint8_t(buf, 11, command_id); + _mav_put_uint8_t(buf, 12, extra_param); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DIGICAM_CONTROL, buf, MAVLINK_MSG_ID_DIGICAM_CONTROL_LEN, MAVLINK_MSG_ID_DIGICAM_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DIGICAM_CONTROL, buf, MAVLINK_MSG_ID_DIGICAM_CONTROL_LEN); +#endif +#else + mavlink_digicam_control_t *packet = (mavlink_digicam_control_t *)msgbuf; + packet->extra_value = extra_value; + packet->target_system = target_system; + packet->target_component = target_component; + packet->session = session; + packet->zoom_pos = zoom_pos; + packet->zoom_step = zoom_step; + packet->focus_lock = focus_lock; + packet->shot = shot; + packet->command_id = command_id; + packet->extra_param = extra_param; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DIGICAM_CONTROL, (const char *)packet, MAVLINK_MSG_ID_DIGICAM_CONTROL_LEN, MAVLINK_MSG_ID_DIGICAM_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DIGICAM_CONTROL, (const char *)packet, MAVLINK_MSG_ID_DIGICAM_CONTROL_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE DIGICAM_CONTROL UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_fence_fetch_point.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_fence_fetch_point.h index fe3677d53..4021c7a09 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_fence_fetch_point.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_fence_fetch_point.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_fence_fetch_point_send(mavlink_channel_t chan, ui #endif } +#if MAVLINK_MSG_ID_FENCE_FETCH_POINT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_fence_fetch_point_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t idx) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + _mav_put_uint8_t(buf, 2, idx); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FENCE_FETCH_POINT, buf, MAVLINK_MSG_ID_FENCE_FETCH_POINT_LEN, MAVLINK_MSG_ID_FENCE_FETCH_POINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FENCE_FETCH_POINT, buf, MAVLINK_MSG_ID_FENCE_FETCH_POINT_LEN); +#endif +#else + mavlink_fence_fetch_point_t *packet = (mavlink_fence_fetch_point_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + packet->idx = idx; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FENCE_FETCH_POINT, (const char *)packet, MAVLINK_MSG_ID_FENCE_FETCH_POINT_LEN, MAVLINK_MSG_ID_FENCE_FETCH_POINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FENCE_FETCH_POINT, (const char *)packet, MAVLINK_MSG_ID_FENCE_FETCH_POINT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FENCE_FETCH_POINT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_fence_point.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_fence_point.h index febda6cdc..6fc2c83fc 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_fence_point.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_fence_point.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_fence_point_send(mavlink_channel_t chan, uint8_t #endif } +#if MAVLINK_MSG_ID_FENCE_POINT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_fence_point_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t idx, uint8_t count, float lat, float lng) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, lat); + _mav_put_float(buf, 4, lng); + _mav_put_uint8_t(buf, 8, target_system); + _mav_put_uint8_t(buf, 9, target_component); + _mav_put_uint8_t(buf, 10, idx); + _mav_put_uint8_t(buf, 11, count); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FENCE_POINT, buf, MAVLINK_MSG_ID_FENCE_POINT_LEN, MAVLINK_MSG_ID_FENCE_POINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FENCE_POINT, buf, MAVLINK_MSG_ID_FENCE_POINT_LEN); +#endif +#else + mavlink_fence_point_t *packet = (mavlink_fence_point_t *)msgbuf; + packet->lat = lat; + packet->lng = lng; + packet->target_system = target_system; + packet->target_component = target_component; + packet->idx = idx; + packet->count = count; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FENCE_POINT, (const char *)packet, MAVLINK_MSG_ID_FENCE_POINT_LEN, MAVLINK_MSG_ID_FENCE_POINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FENCE_POINT, (const char *)packet, MAVLINK_MSG_ID_FENCE_POINT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FENCE_POINT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_fence_status.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_fence_status.h index 612090406..c50d37724 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_fence_status.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_fence_status.h @@ -179,6 +179,44 @@ static inline void mavlink_msg_fence_status_send(mavlink_channel_t chan, uint8_t #endif } +#if MAVLINK_MSG_ID_FENCE_STATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_fence_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t breach_status, uint16_t breach_count, uint8_t breach_type, uint32_t breach_time) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, breach_time); + _mav_put_uint16_t(buf, 4, breach_count); + _mav_put_uint8_t(buf, 6, breach_status); + _mav_put_uint8_t(buf, 7, breach_type); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FENCE_STATUS, buf, MAVLINK_MSG_ID_FENCE_STATUS_LEN, MAVLINK_MSG_ID_FENCE_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FENCE_STATUS, buf, MAVLINK_MSG_ID_FENCE_STATUS_LEN); +#endif +#else + mavlink_fence_status_t *packet = (mavlink_fence_status_t *)msgbuf; + packet->breach_time = breach_time; + packet->breach_count = breach_count; + packet->breach_status = breach_status; + packet->breach_type = breach_type; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FENCE_STATUS, (const char *)packet, MAVLINK_MSG_ID_FENCE_STATUS_LEN, MAVLINK_MSG_ID_FENCE_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FENCE_STATUS, (const char *)packet, MAVLINK_MSG_ID_FENCE_STATUS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FENCE_STATUS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_hwstatus.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_hwstatus.h index 2f5dea513..acf031f62 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_hwstatus.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_hwstatus.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_hwstatus_send(mavlink_channel_t chan, uint16_t Vc #endif } +#if MAVLINK_MSG_ID_HWSTATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_hwstatus_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t Vcc, uint8_t I2Cerr) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, Vcc); + _mav_put_uint8_t(buf, 2, I2Cerr); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HWSTATUS, buf, MAVLINK_MSG_ID_HWSTATUS_LEN, MAVLINK_MSG_ID_HWSTATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HWSTATUS, buf, MAVLINK_MSG_ID_HWSTATUS_LEN); +#endif +#else + mavlink_hwstatus_t *packet = (mavlink_hwstatus_t *)msgbuf; + packet->Vcc = Vcc; + packet->I2Cerr = I2Cerr; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HWSTATUS, (const char *)packet, MAVLINK_MSG_ID_HWSTATUS_LEN, MAVLINK_MSG_ID_HWSTATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HWSTATUS, (const char *)packet, MAVLINK_MSG_ID_HWSTATUS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE HWSTATUS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_limits_status.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_limits_status.h index 34743fd02..5fef93718 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_limits_status.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_limits_status.h @@ -234,6 +234,54 @@ static inline void mavlink_msg_limits_status_send(mavlink_channel_t chan, uint8_ #endif } +#if MAVLINK_MSG_ID_LIMITS_STATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_limits_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t limits_state, uint32_t last_trigger, uint32_t last_action, uint32_t last_recovery, uint32_t last_clear, uint16_t breach_count, uint8_t mods_enabled, uint8_t mods_required, uint8_t mods_triggered) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, last_trigger); + _mav_put_uint32_t(buf, 4, last_action); + _mav_put_uint32_t(buf, 8, last_recovery); + _mav_put_uint32_t(buf, 12, last_clear); + _mav_put_uint16_t(buf, 16, breach_count); + _mav_put_uint8_t(buf, 18, limits_state); + _mav_put_uint8_t(buf, 19, mods_enabled); + _mav_put_uint8_t(buf, 20, mods_required); + _mav_put_uint8_t(buf, 21, mods_triggered); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LIMITS_STATUS, buf, MAVLINK_MSG_ID_LIMITS_STATUS_LEN, MAVLINK_MSG_ID_LIMITS_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LIMITS_STATUS, buf, MAVLINK_MSG_ID_LIMITS_STATUS_LEN); +#endif +#else + mavlink_limits_status_t *packet = (mavlink_limits_status_t *)msgbuf; + packet->last_trigger = last_trigger; + packet->last_action = last_action; + packet->last_recovery = last_recovery; + packet->last_clear = last_clear; + packet->breach_count = breach_count; + packet->limits_state = limits_state; + packet->mods_enabled = mods_enabled; + packet->mods_required = mods_required; + packet->mods_triggered = mods_triggered; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LIMITS_STATUS, (const char *)packet, MAVLINK_MSG_ID_LIMITS_STATUS_LEN, MAVLINK_MSG_ID_LIMITS_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LIMITS_STATUS, (const char *)packet, MAVLINK_MSG_ID_LIMITS_STATUS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE LIMITS_STATUS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_meminfo.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_meminfo.h index 55f772bbc..c64b2e937 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_meminfo.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_meminfo.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_meminfo_send(mavlink_channel_t chan, uint16_t brk #endif } +#if MAVLINK_MSG_ID_MEMINFO_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_meminfo_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t brkval, uint16_t freemem) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, brkval); + _mav_put_uint16_t(buf, 2, freemem); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEMINFO, buf, MAVLINK_MSG_ID_MEMINFO_LEN, MAVLINK_MSG_ID_MEMINFO_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEMINFO, buf, MAVLINK_MSG_ID_MEMINFO_LEN); +#endif +#else + mavlink_meminfo_t *packet = (mavlink_meminfo_t *)msgbuf; + packet->brkval = brkval; + packet->freemem = freemem; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEMINFO, (const char *)packet, MAVLINK_MSG_ID_MEMINFO_LEN, MAVLINK_MSG_ID_MEMINFO_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEMINFO, (const char *)packet, MAVLINK_MSG_ID_MEMINFO_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MEMINFO UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_mount_configure.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_mount_configure.h index de717dfa4..350bb0b78 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_mount_configure.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_mount_configure.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_mount_configure_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_MOUNT_CONFIGURE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mount_configure_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t mount_mode, uint8_t stab_roll, uint8_t stab_pitch, uint8_t stab_yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + _mav_put_uint8_t(buf, 2, mount_mode); + _mav_put_uint8_t(buf, 3, stab_roll); + _mav_put_uint8_t(buf, 4, stab_pitch); + _mav_put_uint8_t(buf, 5, stab_yaw); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOUNT_CONFIGURE, buf, MAVLINK_MSG_ID_MOUNT_CONFIGURE_LEN, MAVLINK_MSG_ID_MOUNT_CONFIGURE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOUNT_CONFIGURE, buf, MAVLINK_MSG_ID_MOUNT_CONFIGURE_LEN); +#endif +#else + mavlink_mount_configure_t *packet = (mavlink_mount_configure_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + packet->mount_mode = mount_mode; + packet->stab_roll = stab_roll; + packet->stab_pitch = stab_pitch; + packet->stab_yaw = stab_yaw; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOUNT_CONFIGURE, (const char *)packet, MAVLINK_MSG_ID_MOUNT_CONFIGURE_LEN, MAVLINK_MSG_ID_MOUNT_CONFIGURE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOUNT_CONFIGURE, (const char *)packet, MAVLINK_MSG_ID_MOUNT_CONFIGURE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MOUNT_CONFIGURE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_mount_control.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_mount_control.h index 44416353e..72d6e2419 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_mount_control.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_mount_control.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_mount_control_send(mavlink_channel_t chan, uint8_ #endif } +#if MAVLINK_MSG_ID_MOUNT_CONTROL_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mount_control_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, int32_t input_a, int32_t input_b, int32_t input_c, uint8_t save_position) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, input_a); + _mav_put_int32_t(buf, 4, input_b); + _mav_put_int32_t(buf, 8, input_c); + _mav_put_uint8_t(buf, 12, target_system); + _mav_put_uint8_t(buf, 13, target_component); + _mav_put_uint8_t(buf, 14, save_position); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOUNT_CONTROL, buf, MAVLINK_MSG_ID_MOUNT_CONTROL_LEN, MAVLINK_MSG_ID_MOUNT_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOUNT_CONTROL, buf, MAVLINK_MSG_ID_MOUNT_CONTROL_LEN); +#endif +#else + mavlink_mount_control_t *packet = (mavlink_mount_control_t *)msgbuf; + packet->input_a = input_a; + packet->input_b = input_b; + packet->input_c = input_c; + packet->target_system = target_system; + packet->target_component = target_component; + packet->save_position = save_position; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOUNT_CONTROL, (const char *)packet, MAVLINK_MSG_ID_MOUNT_CONTROL_LEN, MAVLINK_MSG_ID_MOUNT_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOUNT_CONTROL, (const char *)packet, MAVLINK_MSG_ID_MOUNT_CONTROL_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MOUNT_CONTROL UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_mount_status.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_mount_status.h index 4905905dc..c140dd2c7 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_mount_status.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_mount_status.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_mount_status_send(mavlink_channel_t chan, uint8_t #endif } +#if MAVLINK_MSG_ID_MOUNT_STATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mount_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, int32_t pointing_a, int32_t pointing_b, int32_t pointing_c) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, pointing_a); + _mav_put_int32_t(buf, 4, pointing_b); + _mav_put_int32_t(buf, 8, pointing_c); + _mav_put_uint8_t(buf, 12, target_system); + _mav_put_uint8_t(buf, 13, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOUNT_STATUS, buf, MAVLINK_MSG_ID_MOUNT_STATUS_LEN, MAVLINK_MSG_ID_MOUNT_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOUNT_STATUS, buf, MAVLINK_MSG_ID_MOUNT_STATUS_LEN); +#endif +#else + mavlink_mount_status_t *packet = (mavlink_mount_status_t *)msgbuf; + packet->pointing_a = pointing_a; + packet->pointing_b = pointing_b; + packet->pointing_c = pointing_c; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOUNT_STATUS, (const char *)packet, MAVLINK_MSG_ID_MOUNT_STATUS_LEN, MAVLINK_MSG_ID_MOUNT_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOUNT_STATUS, (const char *)packet, MAVLINK_MSG_ID_MOUNT_STATUS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MOUNT_STATUS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_radio.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_radio.h index 8e9740e82..830eb4639 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_radio.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_radio.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_radio_send(mavlink_channel_t chan, uint8_t rssi, #endif } +#if MAVLINK_MSG_ID_RADIO_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_radio_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t rssi, uint8_t remrssi, uint8_t txbuf, uint8_t noise, uint8_t remnoise, uint16_t rxerrors, uint16_t fixed) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, rxerrors); + _mav_put_uint16_t(buf, 2, fixed); + _mav_put_uint8_t(buf, 4, rssi); + _mav_put_uint8_t(buf, 5, remrssi); + _mav_put_uint8_t(buf, 6, txbuf); + _mav_put_uint8_t(buf, 7, noise); + _mav_put_uint8_t(buf, 8, remnoise); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO, buf, MAVLINK_MSG_ID_RADIO_LEN, MAVLINK_MSG_ID_RADIO_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO, buf, MAVLINK_MSG_ID_RADIO_LEN); +#endif +#else + mavlink_radio_t *packet = (mavlink_radio_t *)msgbuf; + packet->rxerrors = rxerrors; + packet->fixed = fixed; + packet->rssi = rssi; + packet->remrssi = remrssi; + packet->txbuf = txbuf; + packet->noise = noise; + packet->remnoise = remnoise; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO, (const char *)packet, MAVLINK_MSG_ID_RADIO_LEN, MAVLINK_MSG_ID_RADIO_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO, (const char *)packet, MAVLINK_MSG_ID_RADIO_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE RADIO UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_rally_fetch_point.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_rally_fetch_point.h index f057e3c33..4598251fe 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_rally_fetch_point.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_rally_fetch_point.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_rally_fetch_point_send(mavlink_channel_t chan, ui #endif } +#if MAVLINK_MSG_ID_RALLY_FETCH_POINT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_rally_fetch_point_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t idx) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + _mav_put_uint8_t(buf, 2, idx); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RALLY_FETCH_POINT, buf, MAVLINK_MSG_ID_RALLY_FETCH_POINT_LEN, MAVLINK_MSG_ID_RALLY_FETCH_POINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RALLY_FETCH_POINT, buf, MAVLINK_MSG_ID_RALLY_FETCH_POINT_LEN); +#endif +#else + mavlink_rally_fetch_point_t *packet = (mavlink_rally_fetch_point_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + packet->idx = idx; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RALLY_FETCH_POINT, (const char *)packet, MAVLINK_MSG_ID_RALLY_FETCH_POINT_LEN, MAVLINK_MSG_ID_RALLY_FETCH_POINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RALLY_FETCH_POINT, (const char *)packet, MAVLINK_MSG_ID_RALLY_FETCH_POINT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE RALLY_FETCH_POINT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_rally_point.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_rally_point.h index 2c21db4c0..b44e764a9 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_rally_point.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_rally_point.h @@ -245,6 +245,56 @@ static inline void mavlink_msg_rally_point_send(mavlink_channel_t chan, uint8_t #endif } +#if MAVLINK_MSG_ID_RALLY_POINT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_rally_point_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t idx, uint8_t count, int32_t lat, int32_t lng, int16_t alt, int16_t break_alt, uint16_t land_dir, uint8_t flags) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, lat); + _mav_put_int32_t(buf, 4, lng); + _mav_put_int16_t(buf, 8, alt); + _mav_put_int16_t(buf, 10, break_alt); + _mav_put_uint16_t(buf, 12, land_dir); + _mav_put_uint8_t(buf, 14, target_system); + _mav_put_uint8_t(buf, 15, target_component); + _mav_put_uint8_t(buf, 16, idx); + _mav_put_uint8_t(buf, 17, count); + _mav_put_uint8_t(buf, 18, flags); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RALLY_POINT, buf, MAVLINK_MSG_ID_RALLY_POINT_LEN, MAVLINK_MSG_ID_RALLY_POINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RALLY_POINT, buf, MAVLINK_MSG_ID_RALLY_POINT_LEN); +#endif +#else + mavlink_rally_point_t *packet = (mavlink_rally_point_t *)msgbuf; + packet->lat = lat; + packet->lng = lng; + packet->alt = alt; + packet->break_alt = break_alt; + packet->land_dir = land_dir; + packet->target_system = target_system; + packet->target_component = target_component; + packet->idx = idx; + packet->count = count; + packet->flags = flags; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RALLY_POINT, (const char *)packet, MAVLINK_MSG_ID_RALLY_POINT_LEN, MAVLINK_MSG_ID_RALLY_POINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RALLY_POINT, (const char *)packet, MAVLINK_MSG_ID_RALLY_POINT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE RALLY_POINT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_rangefinder.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_rangefinder.h index c476447a8..464ce8a47 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_rangefinder.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_rangefinder.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_rangefinder_send(mavlink_channel_t chan, float di #endif } +#if MAVLINK_MSG_ID_RANGEFINDER_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_rangefinder_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float distance, float voltage) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, distance); + _mav_put_float(buf, 4, voltage); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RANGEFINDER, buf, MAVLINK_MSG_ID_RANGEFINDER_LEN, MAVLINK_MSG_ID_RANGEFINDER_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RANGEFINDER, buf, MAVLINK_MSG_ID_RANGEFINDER_LEN); +#endif +#else + mavlink_rangefinder_t *packet = (mavlink_rangefinder_t *)msgbuf; + packet->distance = distance; + packet->voltage = voltage; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RANGEFINDER, (const char *)packet, MAVLINK_MSG_ID_RANGEFINDER_LEN, MAVLINK_MSG_ID_RANGEFINDER_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RANGEFINDER, (const char *)packet, MAVLINK_MSG_ID_RANGEFINDER_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE RANGEFINDER UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_sensor_offsets.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_sensor_offsets.h index 31b7d989d..d18f31c95 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_sensor_offsets.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_sensor_offsets.h @@ -267,6 +267,60 @@ static inline void mavlink_msg_sensor_offsets_send(mavlink_channel_t chan, int16 #endif } +#if MAVLINK_MSG_ID_SENSOR_OFFSETS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_sensor_offsets_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, int16_t mag_ofs_x, int16_t mag_ofs_y, int16_t mag_ofs_z, float mag_declination, int32_t raw_press, int32_t raw_temp, float gyro_cal_x, float gyro_cal_y, float gyro_cal_z, float accel_cal_x, float accel_cal_y, float accel_cal_z) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, mag_declination); + _mav_put_int32_t(buf, 4, raw_press); + _mav_put_int32_t(buf, 8, raw_temp); + _mav_put_float(buf, 12, gyro_cal_x); + _mav_put_float(buf, 16, gyro_cal_y); + _mav_put_float(buf, 20, gyro_cal_z); + _mav_put_float(buf, 24, accel_cal_x); + _mav_put_float(buf, 28, accel_cal_y); + _mav_put_float(buf, 32, accel_cal_z); + _mav_put_int16_t(buf, 36, mag_ofs_x); + _mav_put_int16_t(buf, 38, mag_ofs_y); + _mav_put_int16_t(buf, 40, mag_ofs_z); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SENSOR_OFFSETS, buf, MAVLINK_MSG_ID_SENSOR_OFFSETS_LEN, MAVLINK_MSG_ID_SENSOR_OFFSETS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SENSOR_OFFSETS, buf, MAVLINK_MSG_ID_SENSOR_OFFSETS_LEN); +#endif +#else + mavlink_sensor_offsets_t *packet = (mavlink_sensor_offsets_t *)msgbuf; + packet->mag_declination = mag_declination; + packet->raw_press = raw_press; + packet->raw_temp = raw_temp; + packet->gyro_cal_x = gyro_cal_x; + packet->gyro_cal_y = gyro_cal_y; + packet->gyro_cal_z = gyro_cal_z; + packet->accel_cal_x = accel_cal_x; + packet->accel_cal_y = accel_cal_y; + packet->accel_cal_z = accel_cal_z; + packet->mag_ofs_x = mag_ofs_x; + packet->mag_ofs_y = mag_ofs_y; + packet->mag_ofs_z = mag_ofs_z; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SENSOR_OFFSETS, (const char *)packet, MAVLINK_MSG_ID_SENSOR_OFFSETS_LEN, MAVLINK_MSG_ID_SENSOR_OFFSETS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SENSOR_OFFSETS, (const char *)packet, MAVLINK_MSG_ID_SENSOR_OFFSETS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SENSOR_OFFSETS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_set_mag_offsets.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_set_mag_offsets.h index b2c629c39..fc6aa71e0 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_set_mag_offsets.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_set_mag_offsets.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_set_mag_offsets_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_SET_MAG_OFFSETS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_set_mag_offsets_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, int16_t mag_ofs_x, int16_t mag_ofs_y, int16_t mag_ofs_z) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int16_t(buf, 0, mag_ofs_x); + _mav_put_int16_t(buf, 2, mag_ofs_y); + _mav_put_int16_t(buf, 4, mag_ofs_z); + _mav_put_uint8_t(buf, 6, target_system); + _mav_put_uint8_t(buf, 7, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_MAG_OFFSETS, buf, MAVLINK_MSG_ID_SET_MAG_OFFSETS_LEN, MAVLINK_MSG_ID_SET_MAG_OFFSETS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_MAG_OFFSETS, buf, MAVLINK_MSG_ID_SET_MAG_OFFSETS_LEN); +#endif +#else + mavlink_set_mag_offsets_t *packet = (mavlink_set_mag_offsets_t *)msgbuf; + packet->mag_ofs_x = mag_ofs_x; + packet->mag_ofs_y = mag_ofs_y; + packet->mag_ofs_z = mag_ofs_z; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_MAG_OFFSETS, (const char *)packet, MAVLINK_MSG_ID_SET_MAG_OFFSETS_LEN, MAVLINK_MSG_ID_SET_MAG_OFFSETS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_MAG_OFFSETS, (const char *)packet, MAVLINK_MSG_ID_SET_MAG_OFFSETS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SET_MAG_OFFSETS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_simstate.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_simstate.h index 8ef44f76d..48cfb6ffd 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_simstate.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_simstate.h @@ -256,6 +256,58 @@ static inline void mavlink_msg_simstate_send(mavlink_channel_t chan, float roll, #endif } +#if MAVLINK_MSG_ID_SIMSTATE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_simstate_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float roll, float pitch, float yaw, float xacc, float yacc, float zacc, float xgyro, float ygyro, float zgyro, int32_t lat, int32_t lng) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, roll); + _mav_put_float(buf, 4, pitch); + _mav_put_float(buf, 8, yaw); + _mav_put_float(buf, 12, xacc); + _mav_put_float(buf, 16, yacc); + _mav_put_float(buf, 20, zacc); + _mav_put_float(buf, 24, xgyro); + _mav_put_float(buf, 28, ygyro); + _mav_put_float(buf, 32, zgyro); + _mav_put_int32_t(buf, 36, lat); + _mav_put_int32_t(buf, 40, lng); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SIMSTATE, buf, MAVLINK_MSG_ID_SIMSTATE_LEN, MAVLINK_MSG_ID_SIMSTATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SIMSTATE, buf, MAVLINK_MSG_ID_SIMSTATE_LEN); +#endif +#else + mavlink_simstate_t *packet = (mavlink_simstate_t *)msgbuf; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + packet->xacc = xacc; + packet->yacc = yacc; + packet->zacc = zacc; + packet->xgyro = xgyro; + packet->ygyro = ygyro; + packet->zgyro = zgyro; + packet->lat = lat; + packet->lng = lng; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SIMSTATE, (const char *)packet, MAVLINK_MSG_ID_SIMSTATE_LEN, MAVLINK_MSG_ID_SIMSTATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SIMSTATE, (const char *)packet, MAVLINK_MSG_ID_SIMSTATE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SIMSTATE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_wind.h b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_wind.h index 7608a7bd1..5d5edc4cc 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_wind.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/mavlink_msg_wind.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_wind_send(mavlink_channel_t chan, float direction #endif } +#if MAVLINK_MSG_ID_WIND_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_wind_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float direction, float speed, float speed_z) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, direction); + _mav_put_float(buf, 4, speed); + _mav_put_float(buf, 8, speed_z); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WIND, buf, MAVLINK_MSG_ID_WIND_LEN, MAVLINK_MSG_ID_WIND_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WIND, buf, MAVLINK_MSG_ID_WIND_LEN); +#endif +#else + mavlink_wind_t *packet = (mavlink_wind_t *)msgbuf; + packet->direction = direction; + packet->speed = speed; + packet->speed_z = speed_z; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WIND, (const char *)packet, MAVLINK_MSG_ID_WIND_LEN, MAVLINK_MSG_ID_WIND_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WIND, (const char *)packet, MAVLINK_MSG_ID_WIND_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE WIND UNPACKING diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/testsuite.h b/mavlink/include/mavlink/v1.0/ardupilotmega/testsuite.h index b2496334f..489553ea4 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/testsuite.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/testsuite.h @@ -1398,6 +1398,59 @@ static void mavlink_test_rally_fetch_point(uint8_t system_id, uint8_t component_ MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); } +static void mavlink_test_compassmot_status(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg) +{ + mavlink_message_t msg; + uint8_t buffer[MAVLINK_MAX_PACKET_LEN]; + uint16_t i; + mavlink_compassmot_status_t packet_in = { + 17.0, + }45.0, + }73.0, + }101.0, + }18067, + }18171, + }; + mavlink_compassmot_status_t packet1, packet2; + memset(&packet1, 0, sizeof(packet1)); + packet1.current = packet_in.current; + packet1.CompensationX = packet_in.CompensationX; + packet1.CompensationY = packet_in.CompensationY; + packet1.CompensationZ = packet_in.CompensationZ; + packet1.throttle = packet_in.throttle; + packet1.interference = packet_in.interference; + + + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_compassmot_status_encode(system_id, component_id, &msg, &packet1); + mavlink_msg_compassmot_status_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_compassmot_status_pack(system_id, component_id, &msg , packet1.throttle , packet1.current , packet1.interference , packet1.CompensationX , packet1.CompensationY , packet1.CompensationZ ); + mavlink_msg_compassmot_status_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_compassmot_status_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.throttle , packet1.current , packet1.interference , packet1.CompensationX , packet1.CompensationY , packet1.CompensationZ ); + mavlink_msg_compassmot_status_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_to_send_buffer(buffer, &msg); + for (i=0; i<mavlink_msg_get_send_buffer_length(&msg); i++) { + comm_send_ch(MAVLINK_COMM_0, buffer[i]); + } + mavlink_msg_compassmot_status_decode(last_msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_compassmot_status_send(MAVLINK_COMM_1 , packet1.throttle , packet1.current , packet1.interference , packet1.CompensationX , packet1.CompensationY , packet1.CompensationZ ); + mavlink_msg_compassmot_status_decode(last_msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); +} + static void mavlink_test_ahrs2(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg) { mavlink_message_t msg; @@ -1479,6 +1532,7 @@ static void mavlink_test_ardupilotmega(uint8_t system_id, uint8_t component_id, mavlink_test_airspeed_autocal(system_id, component_id, last_msg); mavlink_test_rally_point(system_id, component_id, last_msg); mavlink_test_rally_fetch_point(system_id, component_id, last_msg); + mavlink_test_compassmot_status(system_id, component_id, last_msg); mavlink_test_ahrs2(system_id, component_id, last_msg); } diff --git a/mavlink/include/mavlink/v1.0/ardupilotmega/version.h b/mavlink/include/mavlink/v1.0/ardupilotmega/version.h index 983237eb5..1892fffb3 100644 --- a/mavlink/include/mavlink/v1.0/ardupilotmega/version.h +++ b/mavlink/include/mavlink/v1.0/ardupilotmega/version.h @@ -5,7 +5,7 @@ #ifndef MAVLINK_VERSION_H #define MAVLINK_VERSION_H -#define MAVLINK_BUILD_DATE "Tue Feb 4 15:27:33 2014" +#define MAVLINK_BUILD_DATE "Sun Apr 13 09:37:48 2014" #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0" #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255 diff --git a/mavlink/include/mavlink/v1.0/autoquad/autoquad.h b/mavlink/include/mavlink/v1.0/autoquad/autoquad.h index b4dde669f..93e868dc3 100644 --- a/mavlink/include/mavlink/v1.0/autoquad/autoquad.h +++ b/mavlink/include/mavlink/v1.0/autoquad/autoquad.h @@ -12,15 +12,15 @@ extern "C" { // MESSAGE LENGTHS AND CRCS #ifndef MAVLINK_MESSAGE_LENGTHS -#define MAVLINK_MESSAGE_LENGTHS {9, 31, 12, 0, 14, 28, 3, 32, 0, 0, 0, 6, 0, 0, 0, 0, 0, 0, 0, 0, 20, 2, 25, 23, 30, 101, 22, 26, 16, 14, 28, 32, 28, 28, 22, 22, 21, 6, 6, 37, 4, 4, 2, 2, 4, 2, 2, 3, 13, 12, 19, 17, 15, 15, 27, 25, 18, 18, 20, 20, 9, 34, 26, 46, 36, 0, 6, 4, 0, 11, 18, 0, 0, 0, 20, 0, 33, 3, 0, 0, 20, 22, 0, 0, 0, 0, 0, 0, 0, 28, 56, 42, 33, 0, 0, 0, 0, 0, 0, 0, 26, 32, 32, 20, 32, 62, 54, 64, 84, 9, 254, 249, 9, 36, 26, 64, 22, 6, 14, 12, 97, 2, 2, 113, 35, 0, 0, 0, 0, 0, 13, 255, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 24, 33, 25, 82, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 30, 18, 18, 51, 9, 0} +#define MAVLINK_MESSAGE_LENGTHS {9, 31, 12, 0, 14, 28, 3, 32, 0, 0, 0, 6, 0, 0, 0, 0, 0, 0, 0, 0, 20, 2, 25, 23, 30, 101, 22, 26, 16, 14, 28, 32, 28, 28, 22, 22, 21, 6, 6, 37, 4, 4, 2, 2, 4, 2, 2, 3, 13, 12, 19, 17, 15, 15, 27, 25, 18, 18, 20, 20, 9, 34, 26, 46, 36, 42, 6, 4, 0, 11, 18, 0, 0, 0, 20, 0, 33, 3, 0, 0, 20, 22, 0, 0, 0, 0, 0, 0, 0, 28, 56, 42, 33, 0, 0, 0, 0, 0, 0, 0, 26, 32, 32, 20, 32, 62, 54, 64, 84, 9, 254, 249, 9, 36, 26, 64, 22, 6, 14, 12, 97, 2, 2, 113, 35, 6, 79, 0, 0, 0, 13, 255, 14, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 24, 33, 25, 82, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 30, 18, 18, 51, 9, 0} #endif #ifndef MAVLINK_MESSAGE_CRCS -#define MAVLINK_MESSAGE_CRCS {50, 124, 137, 0, 237, 217, 104, 119, 0, 0, 0, 89, 0, 0, 0, 0, 0, 0, 0, 0, 214, 159, 220, 168, 24, 23, 170, 144, 67, 115, 39, 246, 185, 104, 237, 244, 222, 212, 9, 254, 230, 28, 28, 132, 221, 232, 11, 153, 41, 39, 214, 223, 141, 33, 15, 3, 100, 24, 239, 238, 30, 240, 183, 130, 130, 0, 148, 21, 0, 243, 124, 0, 0, 0, 20, 0, 152, 143, 0, 0, 127, 106, 0, 0, 0, 0, 0, 0, 0, 231, 183, 63, 54, 0, 0, 0, 0, 0, 0, 0, 175, 102, 158, 208, 56, 93, 211, 108, 32, 185, 235, 93, 124, 124, 119, 4, 76, 128, 56, 116, 134, 237, 203, 250, 87, 0, 0, 0, 0, 0, 29, 223, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 177, 241, 15, 241, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 204, 49, 170, 44, 83, 46, 0} +#define MAVLINK_MESSAGE_CRCS {50, 124, 137, 0, 237, 217, 104, 119, 0, 0, 0, 89, 0, 0, 0, 0, 0, 0, 0, 0, 214, 159, 220, 168, 24, 23, 170, 144, 67, 115, 39, 246, 185, 104, 237, 244, 222, 212, 9, 254, 230, 28, 28, 132, 221, 232, 11, 153, 41, 39, 214, 223, 141, 33, 15, 3, 100, 24, 239, 238, 30, 240, 183, 130, 130, 118, 148, 21, 0, 243, 124, 0, 0, 0, 20, 0, 152, 143, 0, 0, 127, 106, 0, 0, 0, 0, 0, 0, 0, 231, 183, 63, 54, 0, 0, 0, 0, 0, 0, 0, 175, 102, 158, 208, 56, 93, 211, 108, 32, 185, 235, 93, 124, 124, 119, 4, 76, 128, 56, 116, 134, 237, 203, 250, 87, 203, 220, 0, 0, 0, 29, 223, 85, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 177, 241, 15, 241, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 204, 49, 170, 44, 83, 46, 0} #endif #ifndef MAVLINK_MESSAGE_INFO -#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_MODE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_ATTITUDE_QUATERNION, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_WRITE_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_ITEM, MAVLINK_MESSAGE_INFO_MISSION_REQUEST, MAVLINK_MESSAGE_INFO_MISSION_SET_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_LIST, MAVLINK_MESSAGE_INFO_MISSION_COUNT, MAVLINK_MESSAGE_INFO_MISSION_CLEAR_ALL, MAVLINK_MESSAGE_INFO_MISSION_ITEM_REACHED, MAVLINK_MESSAGE_INFO_MISSION_ACK, MAVLINK_MESSAGE_INFO_SET_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_SET_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SET_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_MOTORS_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_DATA_STREAM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_VFR_HUD, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_COMMAND_LONG, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_MANUAL_SETPOINT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_HIL_RC_INPUTS_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_GLOBAL_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_SPEED_ESTIMATE, MAVLINK_MESSAGE_INFO_VICON_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_HIGHRES_IMU, MAVLINK_MESSAGE_INFO_OMNIDIRECTIONAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_SENSOR, MAVLINK_MESSAGE_INFO_SIM_STATE, MAVLINK_MESSAGE_INFO_RADIO_STATUS, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_START, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_DIR_LIST, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_RES, MAVLINK_MESSAGE_INFO_HIL_GPS, MAVLINK_MESSAGE_INFO_HIL_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION, MAVLINK_MESSAGE_INFO_SCALED_IMU2, MAVLINK_MESSAGE_INFO_LOG_REQUEST_LIST, MAVLINK_MESSAGE_INFO_LOG_ENTRY, MAVLINK_MESSAGE_INFO_LOG_REQUEST_DATA, MAVLINK_MESSAGE_INFO_LOG_DATA, MAVLINK_MESSAGE_INFO_LOG_ERASE, MAVLINK_MESSAGE_INFO_LOG_REQUEST_END, MAVLINK_MESSAGE_INFO_GPS_INJECT_DATA, MAVLINK_MESSAGE_INFO_GPS2_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_DATA_TRANSMISSION_HANDSHAKE, MAVLINK_MESSAGE_INFO_ENCAPSULATED_DATA, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_BATTERY_STATUS, MAVLINK_MESSAGE_INFO_SETPOINT_8DOF, MAVLINK_MESSAGE_INFO_SETPOINT_6DOF, MAVLINK_MESSAGE_INFO_AQ_TELEMETRY_F, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MEMORY_VECT, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}} +#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_MODE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_ATTITUDE_QUATERNION, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_WRITE_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_ITEM, MAVLINK_MESSAGE_INFO_MISSION_REQUEST, MAVLINK_MESSAGE_INFO_MISSION_SET_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_LIST, MAVLINK_MESSAGE_INFO_MISSION_COUNT, MAVLINK_MESSAGE_INFO_MISSION_CLEAR_ALL, MAVLINK_MESSAGE_INFO_MISSION_ITEM_REACHED, MAVLINK_MESSAGE_INFO_MISSION_ACK, MAVLINK_MESSAGE_INFO_SET_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_SET_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SET_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_MOTORS_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, MAVLINK_MESSAGE_INFO_RC_CHANNELS, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_DATA_STREAM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_VFR_HUD, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_COMMAND_LONG, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_MANUAL_SETPOINT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_HIL_RC_INPUTS_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_GLOBAL_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_SPEED_ESTIMATE, MAVLINK_MESSAGE_INFO_VICON_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_HIGHRES_IMU, MAVLINK_MESSAGE_INFO_OMNIDIRECTIONAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_SENSOR, MAVLINK_MESSAGE_INFO_SIM_STATE, MAVLINK_MESSAGE_INFO_RADIO_STATUS, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_START, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_DIR_LIST, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_RES, MAVLINK_MESSAGE_INFO_HIL_GPS, MAVLINK_MESSAGE_INFO_HIL_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION, MAVLINK_MESSAGE_INFO_SCALED_IMU2, MAVLINK_MESSAGE_INFO_LOG_REQUEST_LIST, MAVLINK_MESSAGE_INFO_LOG_ENTRY, MAVLINK_MESSAGE_INFO_LOG_REQUEST_DATA, MAVLINK_MESSAGE_INFO_LOG_DATA, MAVLINK_MESSAGE_INFO_LOG_ERASE, MAVLINK_MESSAGE_INFO_LOG_REQUEST_END, MAVLINK_MESSAGE_INFO_GPS_INJECT_DATA, MAVLINK_MESSAGE_INFO_GPS2_RAW, MAVLINK_MESSAGE_INFO_POWER_STATUS, MAVLINK_MESSAGE_INFO_SERIAL_CONTROL, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_DATA_TRANSMISSION_HANDSHAKE, MAVLINK_MESSAGE_INFO_ENCAPSULATED_DATA, MAVLINK_MESSAGE_INFO_DISTANCE_SENSOR, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, 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{"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MEMORY_VECT, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}} #endif #include "../protocol.h" @@ -71,6 +71,7 @@ enum MAV_CMD MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer| Latitude| Longitude| Altitude| */ MAV_CMD_NAV_ROI=80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */ MAV_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */ + MAV_CMD_NAV_SPLINE_WAYPOINT=82, /* Navigate to MISSION using a spline path. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Empty| Empty| Empty| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */ MAV_CMD_NAV_LAST=95, /* NOP - This command is only used to mark the upper limit of the NAV/ACTION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ MAV_CMD_CONDITION_DELAY=112, /* Delay mission state machine. |Delay in seconds (decimal)| Empty| Empty| Empty| Empty| Empty| Empty| */ MAV_CMD_CONDITION_CHANGE_ALT=113, /* Ascend/descend at rate. Delay mission state machine until desired altitude reached. |Descent / Ascend rate (m/s)| Empty| Empty| Empty| Empty| Empty| Finish Altitude| */ @@ -88,8 +89,16 @@ enum MAV_CMD MAV_CMD_DO_REPEAT_SERVO=184, /* Cycle a between its nominal setting and a desired PWM for a desired number of cycles with a desired period. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Cycle count| Cycle time (seconds)| Empty| Empty| Empty| */ MAV_CMD_DO_CONTROL_VIDEO=200, /* Control onboard camera system. |Camera ID (-1 for all)| Transmission: 0: disabled, 1: enabled compressed, 2: enabled raw| Transmission mode: 0: video stream, >0: single images every n seconds (decimal)| Recording: 0: disabled, 1: enabled compressed, 2: enabled raw| Empty| Empty| Empty| */ MAV_CMD_DO_SET_ROI=201, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */ + MAV_CMD_DO_DIGICAM_CONFIGURE=202, /* Mission command to configure an on-board camera controller system. |Modes: P, TV, AV, M, Etc| Shutter speed: Divisor number for one second| Aperture: F stop number| ISO number e.g. 80, 100, 200, Etc| Exposure type enumerator| Command Identity| Main engine cut-off time before camera trigger in seconds/10 (0 means no cut-off)| */ + MAV_CMD_DO_DIGICAM_CONTROL=203, /* Mission command to control an on-board camera controller system. |Session control e.g. show/hide lens| Zoom's absolute position| Zooming step value to offset zoom from the current position| Focus Locking, Unlocking or Re-locking| Shooting Command| Command Identity| Empty| */ + MAV_CMD_DO_MOUNT_CONFIGURE=204, /* Mission command to configure a camera or antenna mount |Mount operation mode (see MAV_MOUNT_MODE enum)| stabilize roll? (1 = yes, 0 = no)| stabilize pitch? (1 = yes, 0 = no)| stabilize yaw? (1 = yes, 0 = no)| Empty| Empty| Empty| */ + MAV_CMD_DO_MOUNT_CONTROL=205, /* Mission command to control a camera or antenna mount |pitch or lat in degrees, depending on mount mode.| roll or lon in degrees depending on mount mode| yaw or alt (in meters) depending on mount mode| reserved| reserved| reserved| MAV_MOUNT_MODE enum value| */ + MAV_CMD_DO_SET_CAM_TRIGG_DIST=206, /* Mission command to set CAM_TRIGG_DIST for this flight |Camera trigger distance (meters)| Empty| Empty| Empty| Empty| Empty| Empty| */ + MAV_CMD_DO_FENCE_ENABLE=207, /* Mission command to enable the geofence |enable? (0=disable, 1=enable)| Empty| Empty| Empty| Empty| Empty| Empty| */ + MAV_CMD_DO_PARACHUTE=208, /* Mission command to trigger a parachute |action (0=disable, 1=enable, 2=release, for some systems see PARACHUTE_ACTION enum, not in general message set.)| Empty| Empty| Empty| Empty| Empty| Empty| */ + MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1| q2 - quaternion param #2| q3 - quaternion param #3| q4 - quaternion param #4| Empty| Empty| Empty| */ MAV_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_PREFLIGHT_CALIBRATION=241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Empty| Empty| */ + MAV_CMD_PREFLIGHT_CALIBRATION=241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Compass/Motor interference calibration: 0: no, 1: yes| Empty| */ MAV_CMD_PREFLIGHT_SET_SENSOR_OFFSETS=242, /* Set sensor offsets. This command will be only accepted if in pre-flight mode. |Sensor to adjust the offsets for: 0: gyros, 1: accelerometer, 2: magnetometer, 3: barometer, 4: optical flow| X axis offset (or generic dimension 1), in the sensor's raw units| Y axis offset (or generic dimension 2), in the sensor's raw units| Z axis offset (or generic dimension 3), in the sensor's raw units| Generic dimension 4, in the sensor's raw units| Generic dimension 5, in the sensor's raw units| Generic dimension 6, in the sensor's raw units| */ MAV_CMD_PREFLIGHT_STORAGE=245, /* Request storage of different parameter values and logs. This command will be only accepted if in pre-flight mode. |Parameter storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Mission storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Reserved| Reserved| Empty| Empty| Empty| */ MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN=246, /* Request the reboot or shutdown of system components. |0: Do nothing for autopilot, 1: Reboot autopilot, 2: Shutdown autopilot.| 0: Do nothing for onboard computer, 1: Reboot onboard computer, 2: Shutdown onboard computer.| Reserved| Reserved| Empty| Empty| Empty| */ diff --git a/mavlink/include/mavlink/v1.0/autoquad/mavlink_msg_aq_telemetry_f.h b/mavlink/include/mavlink/v1.0/autoquad/mavlink_msg_aq_telemetry_f.h index ed7c86bcb..e78d5687a 100644 --- a/mavlink/include/mavlink/v1.0/autoquad/mavlink_msg_aq_telemetry_f.h +++ b/mavlink/include/mavlink/v1.0/autoquad/mavlink_msg_aq_telemetry_f.h @@ -366,6 +366,78 @@ static inline void mavlink_msg_aq_telemetry_f_send(mavlink_channel_t chan, uint1 #endif } +#if MAVLINK_MSG_ID_AQ_TELEMETRY_F_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_aq_telemetry_f_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t Index, float value1, float value2, float value3, float value4, float value5, float value6, float value7, float value8, float value9, float value10, float value11, float value12, float value13, float value14, float value15, float value16, float value17, float value18, float value19, float value20) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, value1); + _mav_put_float(buf, 4, value2); + _mav_put_float(buf, 8, value3); + _mav_put_float(buf, 12, value4); + _mav_put_float(buf, 16, value5); + _mav_put_float(buf, 20, value6); + _mav_put_float(buf, 24, value7); + _mav_put_float(buf, 28, value8); + _mav_put_float(buf, 32, value9); + _mav_put_float(buf, 36, value10); + _mav_put_float(buf, 40, value11); + _mav_put_float(buf, 44, value12); + _mav_put_float(buf, 48, value13); + _mav_put_float(buf, 52, value14); + _mav_put_float(buf, 56, value15); + _mav_put_float(buf, 60, value16); + _mav_put_float(buf, 64, value17); + _mav_put_float(buf, 68, value18); + _mav_put_float(buf, 72, value19); + _mav_put_float(buf, 76, value20); + _mav_put_uint16_t(buf, 80, Index); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AQ_TELEMETRY_F, buf, MAVLINK_MSG_ID_AQ_TELEMETRY_F_LEN, MAVLINK_MSG_ID_AQ_TELEMETRY_F_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AQ_TELEMETRY_F, buf, MAVLINK_MSG_ID_AQ_TELEMETRY_F_LEN); +#endif +#else + mavlink_aq_telemetry_f_t *packet = (mavlink_aq_telemetry_f_t *)msgbuf; + packet->value1 = value1; + packet->value2 = value2; + packet->value3 = value3; + packet->value4 = value4; + packet->value5 = value5; + packet->value6 = value6; + packet->value7 = value7; + packet->value8 = value8; + packet->value9 = value9; + packet->value10 = value10; + packet->value11 = value11; + packet->value12 = value12; + packet->value13 = value13; + packet->value14 = value14; + packet->value15 = value15; + packet->value16 = value16; + packet->value17 = value17; + packet->value18 = value18; + packet->value19 = value19; + packet->value20 = value20; + packet->Index = Index; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AQ_TELEMETRY_F, (const char *)packet, MAVLINK_MSG_ID_AQ_TELEMETRY_F_LEN, MAVLINK_MSG_ID_AQ_TELEMETRY_F_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AQ_TELEMETRY_F, (const char *)packet, MAVLINK_MSG_ID_AQ_TELEMETRY_F_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE AQ_TELEMETRY_F UNPACKING diff --git a/mavlink/include/mavlink/v1.0/autoquad/version.h b/mavlink/include/mavlink/v1.0/autoquad/version.h index d125e92b1..5d2f33b60 100644 --- a/mavlink/include/mavlink/v1.0/autoquad/version.h +++ b/mavlink/include/mavlink/v1.0/autoquad/version.h @@ -5,7 +5,7 @@ #ifndef MAVLINK_VERSION_H #define MAVLINK_VERSION_H -#define MAVLINK_BUILD_DATE "Tue Feb 4 15:27:43 2014" +#define MAVLINK_BUILD_DATE "Sun Apr 13 09:38:19 2014" #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0" #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255 diff --git a/mavlink/include/mavlink/v1.0/common/common.h b/mavlink/include/mavlink/v1.0/common/common.h index 7e1cf765b..020211d40 100644 --- a/mavlink/include/mavlink/v1.0/common/common.h +++ b/mavlink/include/mavlink/v1.0/common/common.h @@ -12,15 +12,15 @@ extern "C" { // MESSAGE LENGTHS AND CRCS #ifndef MAVLINK_MESSAGE_LENGTHS -#define MAVLINK_MESSAGE_LENGTHS {9, 31, 12, 0, 14, 28, 3, 32, 0, 0, 0, 6, 0, 0, 0, 0, 0, 0, 0, 0, 20, 2, 25, 23, 30, 101, 22, 26, 16, 14, 28, 32, 28, 28, 22, 22, 21, 6, 6, 37, 4, 4, 2, 2, 4, 2, 2, 3, 13, 12, 19, 17, 15, 15, 27, 25, 18, 18, 20, 20, 9, 34, 26, 46, 36, 0, 6, 4, 0, 11, 18, 0, 0, 0, 20, 0, 33, 3, 0, 0, 20, 22, 0, 0, 0, 0, 0, 0, 0, 28, 56, 42, 33, 0, 0, 0, 0, 0, 0, 0, 26, 32, 32, 20, 32, 62, 54, 64, 84, 9, 254, 249, 9, 36, 26, 64, 22, 6, 14, 12, 97, 2, 2, 113, 35, 0, 0, 0, 0, 0, 13, 255, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 24, 33, 25, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 30, 18, 18, 51, 9, 0} +#define MAVLINK_MESSAGE_LENGTHS {9, 31, 12, 0, 14, 28, 3, 32, 0, 0, 0, 6, 0, 0, 0, 0, 0, 0, 0, 0, 20, 2, 25, 23, 30, 101, 22, 26, 16, 14, 28, 32, 28, 28, 22, 22, 21, 6, 6, 37, 4, 4, 2, 2, 4, 2, 2, 3, 13, 12, 19, 17, 15, 15, 27, 25, 18, 18, 20, 20, 9, 34, 26, 46, 36, 42, 6, 4, 0, 11, 18, 0, 0, 0, 20, 0, 33, 3, 0, 0, 20, 22, 0, 0, 0, 0, 0, 0, 0, 28, 56, 42, 33, 0, 0, 0, 0, 0, 0, 0, 26, 32, 32, 20, 32, 62, 54, 64, 84, 9, 254, 249, 9, 36, 26, 64, 22, 6, 14, 12, 97, 2, 2, 113, 35, 6, 79, 0, 0, 0, 13, 255, 14, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 24, 33, 25, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 30, 18, 18, 51, 9, 0} #endif #ifndef MAVLINK_MESSAGE_CRCS -#define MAVLINK_MESSAGE_CRCS {50, 124, 137, 0, 237, 217, 104, 119, 0, 0, 0, 89, 0, 0, 0, 0, 0, 0, 0, 0, 214, 159, 220, 168, 24, 23, 170, 144, 67, 115, 39, 246, 185, 104, 237, 244, 222, 212, 9, 254, 230, 28, 28, 132, 221, 232, 11, 153, 41, 39, 214, 223, 141, 33, 15, 3, 100, 24, 239, 238, 30, 240, 183, 130, 130, 0, 148, 21, 0, 243, 124, 0, 0, 0, 20, 0, 152, 143, 0, 0, 127, 106, 0, 0, 0, 0, 0, 0, 0, 231, 183, 63, 54, 0, 0, 0, 0, 0, 0, 0, 175, 102, 158, 208, 56, 93, 211, 108, 32, 185, 235, 93, 124, 124, 119, 4, 76, 128, 56, 116, 134, 237, 203, 250, 87, 0, 0, 0, 0, 0, 29, 223, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 177, 241, 15, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 204, 49, 170, 44, 83, 46, 0} +#define MAVLINK_MESSAGE_CRCS {50, 124, 137, 0, 237, 217, 104, 119, 0, 0, 0, 89, 0, 0, 0, 0, 0, 0, 0, 0, 214, 159, 220, 168, 24, 23, 170, 144, 67, 115, 39, 246, 185, 104, 237, 244, 222, 212, 9, 254, 230, 28, 28, 132, 221, 232, 11, 153, 41, 39, 214, 223, 141, 33, 15, 3, 100, 24, 239, 238, 30, 240, 183, 130, 130, 118, 148, 21, 0, 243, 124, 0, 0, 0, 20, 0, 152, 143, 0, 0, 127, 106, 0, 0, 0, 0, 0, 0, 0, 231, 183, 63, 54, 0, 0, 0, 0, 0, 0, 0, 175, 102, 158, 208, 56, 93, 211, 108, 32, 185, 235, 93, 124, 124, 119, 4, 76, 128, 56, 116, 134, 237, 203, 250, 87, 203, 220, 0, 0, 0, 29, 223, 85, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 177, 241, 15, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 204, 49, 170, 44, 83, 46, 0} #endif #ifndef MAVLINK_MESSAGE_INFO -#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_MODE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_ATTITUDE_QUATERNION, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_WRITE_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_ITEM, MAVLINK_MESSAGE_INFO_MISSION_REQUEST, MAVLINK_MESSAGE_INFO_MISSION_SET_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_LIST, MAVLINK_MESSAGE_INFO_MISSION_COUNT, MAVLINK_MESSAGE_INFO_MISSION_CLEAR_ALL, MAVLINK_MESSAGE_INFO_MISSION_ITEM_REACHED, MAVLINK_MESSAGE_INFO_MISSION_ACK, MAVLINK_MESSAGE_INFO_SET_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_SET_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SET_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_MOTORS_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_DATA_STREAM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_VFR_HUD, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_COMMAND_LONG, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, 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MAVLINK_MESSAGE_INFO_VISION_SPEED_ESTIMATE, MAVLINK_MESSAGE_INFO_VICON_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_HIGHRES_IMU, MAVLINK_MESSAGE_INFO_OMNIDIRECTIONAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_SENSOR, MAVLINK_MESSAGE_INFO_SIM_STATE, MAVLINK_MESSAGE_INFO_RADIO_STATUS, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_START, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_DIR_LIST, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_RES, MAVLINK_MESSAGE_INFO_HIL_GPS, MAVLINK_MESSAGE_INFO_HIL_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION, MAVLINK_MESSAGE_INFO_SCALED_IMU2, MAVLINK_MESSAGE_INFO_LOG_REQUEST_LIST, MAVLINK_MESSAGE_INFO_LOG_ENTRY, MAVLINK_MESSAGE_INFO_LOG_REQUEST_DATA, MAVLINK_MESSAGE_INFO_LOG_DATA, MAVLINK_MESSAGE_INFO_LOG_ERASE, MAVLINK_MESSAGE_INFO_LOG_REQUEST_END, MAVLINK_MESSAGE_INFO_GPS_INJECT_DATA, MAVLINK_MESSAGE_INFO_GPS2_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_DATA_TRANSMISSION_HANDSHAKE, MAVLINK_MESSAGE_INFO_ENCAPSULATED_DATA, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_BATTERY_STATUS, MAVLINK_MESSAGE_INFO_SETPOINT_8DOF, MAVLINK_MESSAGE_INFO_SETPOINT_6DOF, 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{"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MEMORY_VECT, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}} +#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_MODE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_ATTITUDE_QUATERNION, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_WRITE_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_ITEM, MAVLINK_MESSAGE_INFO_MISSION_REQUEST, MAVLINK_MESSAGE_INFO_MISSION_SET_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_LIST, MAVLINK_MESSAGE_INFO_MISSION_COUNT, MAVLINK_MESSAGE_INFO_MISSION_CLEAR_ALL, MAVLINK_MESSAGE_INFO_MISSION_ITEM_REACHED, MAVLINK_MESSAGE_INFO_MISSION_ACK, MAVLINK_MESSAGE_INFO_SET_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_SET_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SET_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_MOTORS_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, MAVLINK_MESSAGE_INFO_RC_CHANNELS, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_DATA_STREAM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_VFR_HUD, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_COMMAND_LONG, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_MANUAL_SETPOINT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_HIL_RC_INPUTS_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_GLOBAL_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_SPEED_ESTIMATE, MAVLINK_MESSAGE_INFO_VICON_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_HIGHRES_IMU, MAVLINK_MESSAGE_INFO_OMNIDIRECTIONAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_SENSOR, MAVLINK_MESSAGE_INFO_SIM_STATE, MAVLINK_MESSAGE_INFO_RADIO_STATUS, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_START, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_DIR_LIST, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_RES, MAVLINK_MESSAGE_INFO_HIL_GPS, MAVLINK_MESSAGE_INFO_HIL_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION, MAVLINK_MESSAGE_INFO_SCALED_IMU2, MAVLINK_MESSAGE_INFO_LOG_REQUEST_LIST, MAVLINK_MESSAGE_INFO_LOG_ENTRY, MAVLINK_MESSAGE_INFO_LOG_REQUEST_DATA, MAVLINK_MESSAGE_INFO_LOG_DATA, MAVLINK_MESSAGE_INFO_LOG_ERASE, MAVLINK_MESSAGE_INFO_LOG_REQUEST_END, MAVLINK_MESSAGE_INFO_GPS_INJECT_DATA, MAVLINK_MESSAGE_INFO_GPS2_RAW, MAVLINK_MESSAGE_INFO_POWER_STATUS, MAVLINK_MESSAGE_INFO_SERIAL_CONTROL, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_DATA_TRANSMISSION_HANDSHAKE, MAVLINK_MESSAGE_INFO_ENCAPSULATED_DATA, MAVLINK_MESSAGE_INFO_DISTANCE_SENSOR, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_BATTERY_STATUS, MAVLINK_MESSAGE_INFO_SETPOINT_8DOF, MAVLINK_MESSAGE_INFO_SETPOINT_6DOF, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MEMORY_VECT, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}} #endif #include "../protocol.h" @@ -79,7 +79,8 @@ enum MAV_TYPE MAV_TYPE_TRICOPTER=15, /* Octorotor | */ MAV_TYPE_FLAPPING_WING=16, /* Flapping wing | */ MAV_TYPE_KITE=17, /* Flapping wing | */ - MAV_TYPE_ENUM_END=18, /* | */ + MAV_TYPE_ONBOARD_CONTROLLER=18, /* Onboard companion controller | */ + MAV_TYPE_ENUM_END=19, /* | */ }; #endif @@ -228,7 +229,8 @@ enum MAV_SYS_STATUS_SENSOR MAV_SYS_STATUS_SENSOR_3D_GYRO2=131072, /* 0x20000 2nd 3D gyro | */ MAV_SYS_STATUS_SENSOR_3D_ACCEL2=262144, /* 0x40000 2nd 3D accelerometer | */ MAV_SYS_STATUS_SENSOR_3D_MAG2=524288, /* 0x80000 2nd 3D magnetometer | */ - MAV_SYS_STATUS_SENSOR_ENUM_END=524289, /* | */ + MAV_SYS_STATUS_GEOFENCE=1048576, /* 0x100000 geofence | */ + MAV_SYS_STATUS_SENSOR_ENUM_END=1048577, /* | */ }; #endif @@ -242,7 +244,9 @@ enum MAV_FRAME MAV_FRAME_MISSION=2, /* NOT a coordinate frame, indicates a mission command. | */ MAV_FRAME_GLOBAL_RELATIVE_ALT=3, /* Global coordinate frame, WGS84 coordinate system, relative altitude over ground with respect to the home position. First value / x: latitude, second value / y: longitude, third value / z: positive altitude with 0 being at the altitude of the home location. | */ MAV_FRAME_LOCAL_ENU=4, /* Local coordinate frame, Z-down (x: east, y: north, z: up) | */ - MAV_FRAME_ENUM_END=5, /* | */ + MAV_FRAME_GLOBAL_INT=5, /* Global coordinate frame with some fields as scaled integers, WGS84 coordinate system. First value / x: latitude, second value / y: longitude, third value / z: positive altitude over mean sea level (MSL). Lat / Lon are scaled * 1E7 to avoid floating point accuracy limitations. | */ + MAV_FRAME_GLOBAL_RELATIVE_ALT_INT=6, /* Global coordinate frame with some fields as scaled integers, WGS84 coordinate system, relative altitude over ground with respect to the home position. First value / x: latitude, second value / y: longitude, third value / z: positive altitude with 0 being at the altitude of the home location. Lat / Lon are scaled * 1E7 to avoid floating point accuracy limitations. | */ + MAV_FRAME_ENUM_END=7, /* | */ }; #endif @@ -261,6 +265,57 @@ enum MAVLINK_DATA_STREAM_TYPE }; #endif +/** @brief */ +#ifndef HAVE_ENUM_FENCE_ACTION +#define HAVE_ENUM_FENCE_ACTION +enum FENCE_ACTION +{ + FENCE_ACTION_NONE=0, /* Disable fenced mode | */ + FENCE_ACTION_GUIDED=1, /* Switched to guided mode to return point (fence point 0) | */ + FENCE_ACTION_REPORT=2, /* Report fence breach, but don't take action | */ + FENCE_ACTION_GUIDED_THR_PASS=3, /* Switched to guided mode to return point (fence point 0) with manual throttle control | */ + FENCE_ACTION_ENUM_END=4, /* | */ +}; +#endif + +/** @brief */ +#ifndef HAVE_ENUM_FENCE_BREACH +#define HAVE_ENUM_FENCE_BREACH +enum FENCE_BREACH +{ + FENCE_BREACH_NONE=0, /* No last fence breach | */ + FENCE_BREACH_MINALT=1, /* Breached minimum altitude | */ + FENCE_BREACH_MAXALT=2, /* Breached maximum altitude | */ + FENCE_BREACH_BOUNDARY=3, /* Breached fence boundary | */ + FENCE_BREACH_ENUM_END=4, /* | */ +}; +#endif + +/** @brief Enumeration of possible mount operation modes */ +#ifndef HAVE_ENUM_MAV_MOUNT_MODE +#define HAVE_ENUM_MAV_MOUNT_MODE +enum MAV_MOUNT_MODE +{ + MAV_MOUNT_MODE_RETRACT=0, /* Load and keep safe position (Roll,Pitch,Yaw) from permant memory and stop stabilization | */ + MAV_MOUNT_MODE_NEUTRAL=1, /* Load and keep neutral position (Roll,Pitch,Yaw) from permanent memory. | */ + MAV_MOUNT_MODE_MAVLINK_TARGETING=2, /* Load neutral position and start MAVLink Roll,Pitch,Yaw control with stabilization | */ + MAV_MOUNT_MODE_RC_TARGETING=3, /* Load neutral position and start RC Roll,Pitch,Yaw control with stabilization | */ + MAV_MOUNT_MODE_GPS_POINT=4, /* Load neutral position and start to point to Lat,Lon,Alt | */ + MAV_MOUNT_MODE_ENUM_END=5, /* | */ +}; +#endif + +/** @brief Enumeration of distance sensor types */ +#ifndef HAVE_ENUM_MAV_DISTANCE_SENSOR +#define HAVE_ENUM_MAV_DISTANCE_SENSOR +enum MAV_DISTANCE_SENSOR +{ + MAV_DISTANCE_SENSOR_LASER=0, /* Laser altimeter, e.g. LightWare SF02/F or PulsedLight units | */ + MAV_DISTANCE_SENSOR_ULTRASOUND=1, /* Laser altimeter, e.g. MaxBotix units | */ + MAV_DISTANCE_SENSOR_ENUM_END=2, /* | */ +}; +#endif + /** @brief Commands to be executed by the MAV. They can be executed on user request, or as part of a mission script. If the action is used in a mission, the parameter mapping to the waypoint/mission message is as follows: Param 1, Param 2, Param 3, Param 4, X: Param 5, Y:Param 6, Z:Param 7. This command list is similar what ARINC 424 is for commercial aircraft: A data format how to interpret waypoint/mission data. */ #ifndef HAVE_ENUM_MAV_CMD #define HAVE_ENUM_MAV_CMD @@ -275,6 +330,7 @@ enum MAV_CMD MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer| Latitude| Longitude| Altitude| */ MAV_CMD_NAV_ROI=80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */ MAV_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */ + MAV_CMD_NAV_SPLINE_WAYPOINT=82, /* Navigate to MISSION using a spline path. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Empty| Empty| Empty| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */ MAV_CMD_NAV_LAST=95, /* NOP - This command is only used to mark the upper limit of the NAV/ACTION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ MAV_CMD_CONDITION_DELAY=112, /* Delay mission state machine. |Delay in seconds (decimal)| Empty| Empty| Empty| Empty| Empty| Empty| */ MAV_CMD_CONDITION_CHANGE_ALT=113, /* Ascend/descend at rate. Delay mission state machine until desired altitude reached. |Descent / Ascend rate (m/s)| Empty| Empty| Empty| Empty| Empty| Finish Altitude| */ @@ -292,8 +348,16 @@ enum MAV_CMD MAV_CMD_DO_REPEAT_SERVO=184, /* Cycle a between its nominal setting and a desired PWM for a desired number of cycles with a desired period. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Cycle count| Cycle time (seconds)| Empty| Empty| Empty| */ MAV_CMD_DO_CONTROL_VIDEO=200, /* Control onboard camera system. |Camera ID (-1 for all)| Transmission: 0: disabled, 1: enabled compressed, 2: enabled raw| Transmission mode: 0: video stream, >0: single images every n seconds (decimal)| Recording: 0: disabled, 1: enabled compressed, 2: enabled raw| Empty| Empty| Empty| */ MAV_CMD_DO_SET_ROI=201, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */ + MAV_CMD_DO_DIGICAM_CONFIGURE=202, /* Mission command to configure an on-board camera controller system. |Modes: P, TV, AV, M, Etc| Shutter speed: Divisor number for one second| Aperture: F stop number| ISO number e.g. 80, 100, 200, Etc| Exposure type enumerator| Command Identity| Main engine cut-off time before camera trigger in seconds/10 (0 means no cut-off)| */ + MAV_CMD_DO_DIGICAM_CONTROL=203, /* Mission command to control an on-board camera controller system. |Session control e.g. show/hide lens| Zoom's absolute position| Zooming step value to offset zoom from the current position| Focus Locking, Unlocking or Re-locking| Shooting Command| Command Identity| Empty| */ + MAV_CMD_DO_MOUNT_CONFIGURE=204, /* Mission command to configure a camera or antenna mount |Mount operation mode (see MAV_MOUNT_MODE enum)| stabilize roll? (1 = yes, 0 = no)| stabilize pitch? (1 = yes, 0 = no)| stabilize yaw? (1 = yes, 0 = no)| Empty| Empty| Empty| */ + MAV_CMD_DO_MOUNT_CONTROL=205, /* Mission command to control a camera or antenna mount |pitch or lat in degrees, depending on mount mode.| roll or lon in degrees depending on mount mode| yaw or alt (in meters) depending on mount mode| reserved| reserved| reserved| MAV_MOUNT_MODE enum value| */ + MAV_CMD_DO_SET_CAM_TRIGG_DIST=206, /* Mission command to set CAM_TRIGG_DIST for this flight |Camera trigger distance (meters)| Empty| Empty| Empty| Empty| Empty| Empty| */ + MAV_CMD_DO_FENCE_ENABLE=207, /* Mission command to enable the geofence |enable? (0=disable, 1=enable)| Empty| Empty| Empty| Empty| Empty| Empty| */ + MAV_CMD_DO_PARACHUTE=208, /* Mission command to trigger a parachute |action (0=disable, 1=enable, 2=release, for some systems see PARACHUTE_ACTION enum, not in general message set.)| Empty| Empty| Empty| Empty| Empty| Empty| */ + MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1| q2 - quaternion param #2| q3 - quaternion param #3| q4 - quaternion param #4| Empty| Empty| Empty| */ MAV_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_PREFLIGHT_CALIBRATION=241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Empty| Empty| */ + MAV_CMD_PREFLIGHT_CALIBRATION=241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Compass/Motor interference calibration: 0: no, 1: yes| Empty| */ MAV_CMD_PREFLIGHT_SET_SENSOR_OFFSETS=242, /* Set sensor offsets. This command will be only accepted if in pre-flight mode. |Sensor to adjust the offsets for: 0: gyros, 1: accelerometer, 2: magnetometer, 3: barometer, 4: optical flow| X axis offset (or generic dimension 1), in the sensor's raw units| Y axis offset (or generic dimension 2), in the sensor's raw units| Z axis offset (or generic dimension 3), in the sensor's raw units| Generic dimension 4, in the sensor's raw units| Generic dimension 5, in the sensor's raw units| Generic dimension 6, in the sensor's raw units| */ MAV_CMD_PREFLIGHT_STORAGE=245, /* Request storage of different parameter values and logs. This command will be only accepted if in pre-flight mode. |Parameter storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Mission storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Reserved| Reserved| Empty| Empty| Empty| */ MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN=246, /* Request the reboot or shutdown of system components. |0: Do nothing for autopilot, 1: Reboot autopilot, 2: Shutdown autopilot.| 0: Do nothing for onboard computer, 1: Reboot onboard computer, 2: Shutdown onboard computer.| Reserved| Reserved| Empty| Empty| Empty| */ @@ -433,6 +497,48 @@ enum MAV_SEVERITY }; #endif +/** @brief Power supply status flags (bitmask) */ +#ifndef HAVE_ENUM_MAV_POWER_STATUS +#define HAVE_ENUM_MAV_POWER_STATUS +enum MAV_POWER_STATUS +{ + MAV_POWER_STATUS_BRICK_VALID=1, /* main brick power supply valid | */ + MAV_POWER_STATUS_SERVO_VALID=2, /* main servo power supply valid for FMU | */ + MAV_POWER_STATUS_USB_CONNECTED=4, /* USB power is connected | */ + MAV_POWER_STATUS_PERIPH_OVERCURRENT=8, /* peripheral supply is in over-current state | */ + MAV_POWER_STATUS_PERIPH_HIPOWER_OVERCURRENT=16, /* hi-power peripheral supply is in over-current state | */ + MAV_POWER_STATUS_CHANGED=32, /* Power status has changed since boot | */ + MAV_POWER_STATUS_ENUM_END=33, /* | */ +}; +#endif + +/** @brief SERIAL_CONTROL device types */ +#ifndef HAVE_ENUM_SERIAL_CONTROL_DEV +#define HAVE_ENUM_SERIAL_CONTROL_DEV +enum SERIAL_CONTROL_DEV +{ + SERIAL_CONTROL_DEV_TELEM1=0, /* First telemetry port | */ + SERIAL_CONTROL_DEV_TELEM2=1, /* Second telemetry port | */ + SERIAL_CONTROL_DEV_GPS1=2, /* First GPS port | */ + SERIAL_CONTROL_DEV_GPS2=3, /* Second GPS port | */ + SERIAL_CONTROL_DEV_ENUM_END=4, /* | */ +}; +#endif + +/** @brief SERIAL_CONTROL flags (bitmask) */ +#ifndef HAVE_ENUM_SERIAL_CONTROL_FLAG +#define HAVE_ENUM_SERIAL_CONTROL_FLAG +enum SERIAL_CONTROL_FLAG +{ + SERIAL_CONTROL_FLAG_REPLY=1, /* Set if this is a reply | */ + SERIAL_CONTROL_FLAG_RESPOND=2, /* Set if the sender wants the receiver to send a response as another SERIAL_CONTROL message | */ + SERIAL_CONTROL_FLAG_EXCLUSIVE=4, /* Set if access to the serial port should be removed from whatever driver is currently using it, giving exclusive access to the SERIAL_CONTROL protocol. The port can be handed back by sending a request without this flag set | */ + SERIAL_CONTROL_FLAG_BLOCKING=8, /* Block on writes to the serial port | */ + SERIAL_CONTROL_FLAG_MULTI=16, /* Send multiple replies until port is drained | */ + SERIAL_CONTROL_FLAG_ENUM_END=17, /* | */ +}; +#endif + // MAVLINK VERSION @@ -500,6 +606,7 @@ enum MAV_SEVERITY #include "./mavlink_msg_nav_controller_output.h" #include "./mavlink_msg_set_quad_swarm_led_roll_pitch_yaw_thrust.h" #include "./mavlink_msg_state_correction.h" +#include "./mavlink_msg_rc_channels.h" #include "./mavlink_msg_request_data_stream.h" #include "./mavlink_msg_data_stream.h" #include "./mavlink_msg_manual_control.h" @@ -538,8 +645,11 @@ enum MAV_SEVERITY #include "./mavlink_msg_log_request_end.h" #include "./mavlink_msg_gps_inject_data.h" #include "./mavlink_msg_gps2_raw.h" +#include "./mavlink_msg_power_status.h" +#include "./mavlink_msg_serial_control.h" #include "./mavlink_msg_data_transmission_handshake.h" #include "./mavlink_msg_encapsulated_data.h" +#include "./mavlink_msg_distance_sensor.h" #include "./mavlink_msg_battery_status.h" #include "./mavlink_msg_setpoint_8dof.h" #include "./mavlink_msg_setpoint_6dof.h" diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_attitude.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_attitude.h index 8ddf5bf09..ff2f104d4 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_attitude.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_attitude.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_attitude_send(mavlink_channel_t chan, uint32_t ti #endif } +#if MAVLINK_MSG_ID_ATTITUDE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_attitude_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, float roll, float pitch, float yaw, float rollspeed, float pitchspeed, float yawspeed) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_float(buf, 4, roll); + _mav_put_float(buf, 8, pitch); + _mav_put_float(buf, 12, yaw); + _mav_put_float(buf, 16, rollspeed); + _mav_put_float(buf, 20, pitchspeed); + _mav_put_float(buf, 24, yawspeed); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ATTITUDE, buf, MAVLINK_MSG_ID_ATTITUDE_LEN, MAVLINK_MSG_ID_ATTITUDE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ATTITUDE, buf, MAVLINK_MSG_ID_ATTITUDE_LEN); +#endif +#else + mavlink_attitude_t *packet = (mavlink_attitude_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + packet->rollspeed = rollspeed; + packet->pitchspeed = pitchspeed; + packet->yawspeed = yawspeed; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ATTITUDE, (const char *)packet, MAVLINK_MSG_ID_ATTITUDE_LEN, MAVLINK_MSG_ID_ATTITUDE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ATTITUDE, (const char *)packet, MAVLINK_MSG_ID_ATTITUDE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE ATTITUDE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_attitude_quaternion.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_attitude_quaternion.h index 9f8d58759..3b97b40d0 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_attitude_quaternion.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_attitude_quaternion.h @@ -223,6 +223,52 @@ static inline void mavlink_msg_attitude_quaternion_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_ATTITUDE_QUATERNION_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_attitude_quaternion_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, float q1, float q2, float q3, float q4, float rollspeed, float pitchspeed, float yawspeed) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_float(buf, 4, q1); + _mav_put_float(buf, 8, q2); + _mav_put_float(buf, 12, q3); + _mav_put_float(buf, 16, q4); + _mav_put_float(buf, 20, rollspeed); + _mav_put_float(buf, 24, pitchspeed); + _mav_put_float(buf, 28, yawspeed); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ATTITUDE_QUATERNION, buf, MAVLINK_MSG_ID_ATTITUDE_QUATERNION_LEN, MAVLINK_MSG_ID_ATTITUDE_QUATERNION_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ATTITUDE_QUATERNION, buf, MAVLINK_MSG_ID_ATTITUDE_QUATERNION_LEN); +#endif +#else + mavlink_attitude_quaternion_t *packet = (mavlink_attitude_quaternion_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->q1 = q1; + packet->q2 = q2; + packet->q3 = q3; + packet->q4 = q4; + packet->rollspeed = rollspeed; + packet->pitchspeed = pitchspeed; + packet->yawspeed = yawspeed; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ATTITUDE_QUATERNION, (const char *)packet, MAVLINK_MSG_ID_ATTITUDE_QUATERNION_LEN, MAVLINK_MSG_ID_ATTITUDE_QUATERNION_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ATTITUDE_QUATERNION, (const char *)packet, MAVLINK_MSG_ID_ATTITUDE_QUATERNION_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE ATTITUDE_QUATERNION UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_auth_key.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_auth_key.h index 5703a5987..f31b6bbf4 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_auth_key.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_auth_key.h @@ -146,6 +146,38 @@ static inline void mavlink_msg_auth_key_send(mavlink_channel_t chan, const char #endif } +#if MAVLINK_MSG_ID_AUTH_KEY_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_auth_key_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, const char *key) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + + _mav_put_char_array(buf, 0, key, 32); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AUTH_KEY, buf, MAVLINK_MSG_ID_AUTH_KEY_LEN, MAVLINK_MSG_ID_AUTH_KEY_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AUTH_KEY, buf, MAVLINK_MSG_ID_AUTH_KEY_LEN); +#endif +#else + mavlink_auth_key_t *packet = (mavlink_auth_key_t *)msgbuf; + + mav_array_memcpy(packet->key, key, sizeof(char)*32); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AUTH_KEY, (const char *)packet, MAVLINK_MSG_ID_AUTH_KEY_LEN, MAVLINK_MSG_ID_AUTH_KEY_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AUTH_KEY, (const char *)packet, MAVLINK_MSG_ID_AUTH_KEY_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE AUTH_KEY UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_battery_status.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_battery_status.h index 03e4d569e..faaabf9f7 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_battery_status.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_battery_status.h @@ -256,6 +256,58 @@ static inline void mavlink_msg_battery_status_send(mavlink_channel_t chan, uint8 #endif } +#if MAVLINK_MSG_ID_BATTERY_STATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_battery_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t accu_id, uint16_t voltage_cell_1, uint16_t voltage_cell_2, uint16_t voltage_cell_3, uint16_t voltage_cell_4, uint16_t voltage_cell_5, uint16_t voltage_cell_6, int16_t current_battery, int32_t current_consumed, int32_t energy_consumed, int8_t battery_remaining) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, current_consumed); + _mav_put_int32_t(buf, 4, energy_consumed); + _mav_put_uint16_t(buf, 8, voltage_cell_1); + _mav_put_uint16_t(buf, 10, voltage_cell_2); + _mav_put_uint16_t(buf, 12, voltage_cell_3); + _mav_put_uint16_t(buf, 14, voltage_cell_4); + _mav_put_uint16_t(buf, 16, voltage_cell_5); + _mav_put_uint16_t(buf, 18, voltage_cell_6); + _mav_put_int16_t(buf, 20, current_battery); + _mav_put_uint8_t(buf, 22, accu_id); + _mav_put_int8_t(buf, 23, battery_remaining); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_BATTERY_STATUS, buf, MAVLINK_MSG_ID_BATTERY_STATUS_LEN, MAVLINK_MSG_ID_BATTERY_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_BATTERY_STATUS, buf, MAVLINK_MSG_ID_BATTERY_STATUS_LEN); +#endif +#else + mavlink_battery_status_t *packet = (mavlink_battery_status_t *)msgbuf; + packet->current_consumed = current_consumed; + packet->energy_consumed = energy_consumed; + packet->voltage_cell_1 = voltage_cell_1; + packet->voltage_cell_2 = voltage_cell_2; + packet->voltage_cell_3 = voltage_cell_3; + packet->voltage_cell_4 = voltage_cell_4; + packet->voltage_cell_5 = voltage_cell_5; + packet->voltage_cell_6 = voltage_cell_6; + packet->current_battery = current_battery; + packet->accu_id = accu_id; + packet->battery_remaining = battery_remaining; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_BATTERY_STATUS, (const char *)packet, MAVLINK_MSG_ID_BATTERY_STATUS_LEN, MAVLINK_MSG_ID_BATTERY_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_BATTERY_STATUS, (const char *)packet, MAVLINK_MSG_ID_BATTERY_STATUS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE BATTERY_STATUS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_change_operator_control.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_change_operator_control.h index 0b6de930d..3f0987f10 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_change_operator_control.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_change_operator_control.h @@ -173,6 +173,42 @@ static inline void mavlink_msg_change_operator_control_send(mavlink_channel_t ch #endif } +#if MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_change_operator_control_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t control_request, uint8_t version, const char *passkey) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, control_request); + _mav_put_uint8_t(buf, 2, version); + _mav_put_char_array(buf, 3, passkey, 25); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL, buf, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_LEN, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL, buf, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_LEN); +#endif +#else + mavlink_change_operator_control_t *packet = (mavlink_change_operator_control_t *)msgbuf; + packet->target_system = target_system; + packet->control_request = control_request; + packet->version = version; + mav_array_memcpy(packet->passkey, passkey, sizeof(char)*25); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL, (const char *)packet, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_LEN, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL, (const char *)packet, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE CHANGE_OPERATOR_CONTROL UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_change_operator_control_ack.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_change_operator_control_ack.h index c6f6a28e4..768e7ed5c 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_change_operator_control_ack.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_change_operator_control_ack.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_change_operator_control_ack_send(mavlink_channel_ #endif } +#if MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_change_operator_control_ack_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t gcs_system_id, uint8_t control_request, uint8_t ack) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, gcs_system_id); + _mav_put_uint8_t(buf, 1, control_request); + _mav_put_uint8_t(buf, 2, ack); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK, buf, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK_LEN, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK, buf, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK_LEN); +#endif +#else + mavlink_change_operator_control_ack_t *packet = (mavlink_change_operator_control_ack_t *)msgbuf; + packet->gcs_system_id = gcs_system_id; + packet->control_request = control_request; + packet->ack = ack; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK, (const char *)packet, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK_LEN, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK, (const char *)packet, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE CHANGE_OPERATOR_CONTROL_ACK UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_command_ack.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_command_ack.h index dca2fe681..d3d163041 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_command_ack.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_command_ack.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_command_ack_send(mavlink_channel_t chan, uint16_t #endif } +#if MAVLINK_MSG_ID_COMMAND_ACK_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_command_ack_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t command, uint8_t result) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, command); + _mav_put_uint8_t(buf, 2, result); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMMAND_ACK, buf, MAVLINK_MSG_ID_COMMAND_ACK_LEN, MAVLINK_MSG_ID_COMMAND_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMMAND_ACK, buf, MAVLINK_MSG_ID_COMMAND_ACK_LEN); +#endif +#else + mavlink_command_ack_t *packet = (mavlink_command_ack_t *)msgbuf; + packet->command = command; + packet->result = result; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMMAND_ACK, (const char *)packet, MAVLINK_MSG_ID_COMMAND_ACK_LEN, MAVLINK_MSG_ID_COMMAND_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMMAND_ACK, (const char *)packet, MAVLINK_MSG_ID_COMMAND_ACK_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE COMMAND_ACK UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_command_long.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_command_long.h index 8f705c0dd..161896b97 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_command_long.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_command_long.h @@ -256,6 +256,58 @@ static inline void mavlink_msg_command_long_send(mavlink_channel_t chan, uint8_t #endif } +#if MAVLINK_MSG_ID_COMMAND_LONG_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_command_long_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint16_t command, uint8_t confirmation, float param1, float param2, float param3, float param4, float param5, float param6, float param7) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, param1); + _mav_put_float(buf, 4, param2); + _mav_put_float(buf, 8, param3); + _mav_put_float(buf, 12, param4); + _mav_put_float(buf, 16, param5); + _mav_put_float(buf, 20, param6); + _mav_put_float(buf, 24, param7); + _mav_put_uint16_t(buf, 28, command); + _mav_put_uint8_t(buf, 30, target_system); + _mav_put_uint8_t(buf, 31, target_component); + _mav_put_uint8_t(buf, 32, confirmation); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMMAND_LONG, buf, MAVLINK_MSG_ID_COMMAND_LONG_LEN, MAVLINK_MSG_ID_COMMAND_LONG_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMMAND_LONG, buf, MAVLINK_MSG_ID_COMMAND_LONG_LEN); +#endif +#else + mavlink_command_long_t *packet = (mavlink_command_long_t *)msgbuf; + packet->param1 = param1; + packet->param2 = param2; + packet->param3 = param3; + packet->param4 = param4; + packet->param5 = param5; + packet->param6 = param6; + packet->param7 = param7; + packet->command = command; + packet->target_system = target_system; + packet->target_component = target_component; + packet->confirmation = confirmation; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMMAND_LONG, (const char *)packet, MAVLINK_MSG_ID_COMMAND_LONG_LEN, MAVLINK_MSG_ID_COMMAND_LONG_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_COMMAND_LONG, (const char *)packet, MAVLINK_MSG_ID_COMMAND_LONG_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE COMMAND_LONG UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_data_stream.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_data_stream.h index dc0768e12..640ffebf4 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_data_stream.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_data_stream.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_data_stream_send(mavlink_channel_t chan, uint8_t #endif } +#if MAVLINK_MSG_ID_DATA_STREAM_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_data_stream_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t stream_id, uint16_t message_rate, uint8_t on_off) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, message_rate); + _mav_put_uint8_t(buf, 2, stream_id); + _mav_put_uint8_t(buf, 3, on_off); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA_STREAM, buf, MAVLINK_MSG_ID_DATA_STREAM_LEN, MAVLINK_MSG_ID_DATA_STREAM_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA_STREAM, buf, MAVLINK_MSG_ID_DATA_STREAM_LEN); +#endif +#else + mavlink_data_stream_t *packet = (mavlink_data_stream_t *)msgbuf; + packet->message_rate = message_rate; + packet->stream_id = stream_id; + packet->on_off = on_off; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA_STREAM, (const char *)packet, MAVLINK_MSG_ID_DATA_STREAM_LEN, MAVLINK_MSG_ID_DATA_STREAM_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA_STREAM, (const char *)packet, MAVLINK_MSG_ID_DATA_STREAM_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE DATA_STREAM UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_data_transmission_handshake.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_data_transmission_handshake.h index fdd8fddd8..d84a73709 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_data_transmission_handshake.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_data_transmission_handshake.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_data_transmission_handshake_send(mavlink_channel_ #endif } +#if MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_data_transmission_handshake_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t type, uint32_t size, uint16_t width, uint16_t height, uint16_t packets, uint8_t payload, uint8_t jpg_quality) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, size); + _mav_put_uint16_t(buf, 4, width); + _mav_put_uint16_t(buf, 6, height); + _mav_put_uint16_t(buf, 8, packets); + _mav_put_uint8_t(buf, 10, type); + _mav_put_uint8_t(buf, 11, payload); + _mav_put_uint8_t(buf, 12, jpg_quality); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE, buf, MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE_LEN, MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE, buf, MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE_LEN); +#endif +#else + mavlink_data_transmission_handshake_t *packet = (mavlink_data_transmission_handshake_t *)msgbuf; + packet->size = size; + packet->width = width; + packet->height = height; + packet->packets = packets; + packet->type = type; + packet->payload = payload; + packet->jpg_quality = jpg_quality; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE, (const char *)packet, MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE_LEN, MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE, (const char *)packet, MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE DATA_TRANSMISSION_HANDSHAKE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_debug.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_debug.h index 9a6ed87ee..2102af862 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_debug.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_debug.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_debug_send(mavlink_channel_t chan, uint32_t time_ #endif } +#if MAVLINK_MSG_ID_DEBUG_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_debug_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, uint8_t ind, float value) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_float(buf, 4, value); + _mav_put_uint8_t(buf, 8, ind); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DEBUG, buf, MAVLINK_MSG_ID_DEBUG_LEN, MAVLINK_MSG_ID_DEBUG_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DEBUG, buf, MAVLINK_MSG_ID_DEBUG_LEN); +#endif +#else + mavlink_debug_t *packet = (mavlink_debug_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->value = value; + packet->ind = ind; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DEBUG, (const char *)packet, MAVLINK_MSG_ID_DEBUG_LEN, MAVLINK_MSG_ID_DEBUG_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DEBUG, (const char *)packet, MAVLINK_MSG_ID_DEBUG_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE DEBUG UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_debug_vect.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_debug_vect.h index 6cfc75212..67c339e89 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_debug_vect.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_debug_vect.h @@ -184,6 +184,44 @@ static inline void mavlink_msg_debug_vect_send(mavlink_channel_t chan, const cha #endif } +#if MAVLINK_MSG_ID_DEBUG_VECT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_debug_vect_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, const char *name, uint64_t time_usec, float x, float y, float z) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_float(buf, 8, x); + _mav_put_float(buf, 12, y); + _mav_put_float(buf, 16, z); + _mav_put_char_array(buf, 20, name, 10); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DEBUG_VECT, buf, MAVLINK_MSG_ID_DEBUG_VECT_LEN, MAVLINK_MSG_ID_DEBUG_VECT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DEBUG_VECT, buf, MAVLINK_MSG_ID_DEBUG_VECT_LEN); +#endif +#else + mavlink_debug_vect_t *packet = (mavlink_debug_vect_t *)msgbuf; + packet->time_usec = time_usec; + packet->x = x; + packet->y = y; + packet->z = z; + mav_array_memcpy(packet->name, name, sizeof(char)*10); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DEBUG_VECT, (const char *)packet, MAVLINK_MSG_ID_DEBUG_VECT_LEN, MAVLINK_MSG_ID_DEBUG_VECT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DEBUG_VECT, (const char *)packet, MAVLINK_MSG_ID_DEBUG_VECT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE DEBUG_VECT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_distance_sensor.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_distance_sensor.h new file mode 100644 index 000000000..39b384396 --- /dev/null +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_distance_sensor.h @@ -0,0 +1,377 @@ +// MESSAGE DISTANCE_SENSOR PACKING + +#define MAVLINK_MSG_ID_DISTANCE_SENSOR 132 + +typedef struct __mavlink_distance_sensor_t +{ + uint32_t time_boot_ms; ///< Time since system boot + uint16_t min_distance; ///< Minimum distance the sensor can measure in centimeters + uint16_t max_distance; ///< Maximum distance the sensor can measure in centimeters + uint16_t current_distance; ///< Current distance reading + uint8_t type; ///< Type from MAV_DISTANCE_SENSOR enum. + uint8_t id; ///< Onboard ID of the sensor + uint8_t orientation; ///< Direction the sensor faces from FIXME enum. + uint8_t covariance; ///< Measurement covariance in centimeters, 0 for unknown / invalid readings +} mavlink_distance_sensor_t; + +#define MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN 14 +#define MAVLINK_MSG_ID_132_LEN 14 + +#define MAVLINK_MSG_ID_DISTANCE_SENSOR_CRC 85 +#define MAVLINK_MSG_ID_132_CRC 85 + + + +#define MAVLINK_MESSAGE_INFO_DISTANCE_SENSOR { \ + "DISTANCE_SENSOR", \ + 8, \ + { { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_distance_sensor_t, time_boot_ms) }, \ + { "min_distance", NULL, MAVLINK_TYPE_UINT16_T, 0, 4, offsetof(mavlink_distance_sensor_t, min_distance) }, \ + { "max_distance", NULL, MAVLINK_TYPE_UINT16_T, 0, 6, offsetof(mavlink_distance_sensor_t, max_distance) }, \ + { "current_distance", NULL, MAVLINK_TYPE_UINT16_T, 0, 8, offsetof(mavlink_distance_sensor_t, current_distance) }, \ + { "type", NULL, MAVLINK_TYPE_UINT8_T, 0, 10, offsetof(mavlink_distance_sensor_t, type) }, \ + { "id", NULL, MAVLINK_TYPE_UINT8_T, 0, 11, offsetof(mavlink_distance_sensor_t, id) }, \ + { "orientation", NULL, MAVLINK_TYPE_UINT8_T, 0, 12, offsetof(mavlink_distance_sensor_t, orientation) }, \ + { "covariance", NULL, MAVLINK_TYPE_UINT8_T, 0, 13, offsetof(mavlink_distance_sensor_t, covariance) }, \ + } \ +} + + +/** + * @brief Pack a distance_sensor message + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param msg The MAVLink message to compress the data into + * + * @param time_boot_ms Time since system boot + * @param type Type from MAV_DISTANCE_SENSOR enum. + * @param id Onboard ID of the sensor + * @param orientation Direction the sensor faces from FIXME enum. + * @param min_distance Minimum distance the sensor can measure in centimeters + * @param max_distance Maximum distance the sensor can measure in centimeters + * @param current_distance Current distance reading + * @param covariance Measurement covariance in centimeters, 0 for unknown / invalid readings + * @return length of the message in bytes (excluding serial stream start sign) + */ +static inline uint16_t mavlink_msg_distance_sensor_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, + uint32_t time_boot_ms, uint8_t type, uint8_t id, uint8_t orientation, uint16_t min_distance, uint16_t max_distance, uint16_t current_distance, uint8_t covariance) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN]; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_uint16_t(buf, 4, min_distance); + _mav_put_uint16_t(buf, 6, max_distance); + _mav_put_uint16_t(buf, 8, current_distance); + _mav_put_uint8_t(buf, 10, type); + _mav_put_uint8_t(buf, 11, id); + _mav_put_uint8_t(buf, 12, orientation); + _mav_put_uint8_t(buf, 13, covariance); + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN); +#else + mavlink_distance_sensor_t packet; + packet.time_boot_ms = time_boot_ms; + packet.min_distance = min_distance; + packet.max_distance = max_distance; + packet.current_distance = current_distance; + packet.type = type; + packet.id = id; + packet.orientation = orientation; + packet.covariance = covariance; + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN); +#endif + + msg->msgid = MAVLINK_MSG_ID_DISTANCE_SENSOR; +#if MAVLINK_CRC_EXTRA + return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN, MAVLINK_MSG_ID_DISTANCE_SENSOR_CRC); +#else + return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN); +#endif +} + +/** + * @brief Pack a distance_sensor message on a channel + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param chan The MAVLink channel this message will be sent over + * @param msg The MAVLink message to compress the data into + * @param time_boot_ms Time since system boot + * @param type Type from MAV_DISTANCE_SENSOR enum. + * @param id Onboard ID of the sensor + * @param orientation Direction the sensor faces from FIXME enum. + * @param min_distance Minimum distance the sensor can measure in centimeters + * @param max_distance Maximum distance the sensor can measure in centimeters + * @param current_distance Current distance reading + * @param covariance Measurement covariance in centimeters, 0 for unknown / invalid readings + * @return length of the message in bytes (excluding serial stream start sign) + */ +static inline uint16_t mavlink_msg_distance_sensor_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, + mavlink_message_t* msg, + uint32_t time_boot_ms,uint8_t type,uint8_t id,uint8_t orientation,uint16_t min_distance,uint16_t max_distance,uint16_t current_distance,uint8_t covariance) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN]; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_uint16_t(buf, 4, min_distance); + _mav_put_uint16_t(buf, 6, max_distance); + _mav_put_uint16_t(buf, 8, current_distance); + _mav_put_uint8_t(buf, 10, type); + _mav_put_uint8_t(buf, 11, id); + _mav_put_uint8_t(buf, 12, orientation); + _mav_put_uint8_t(buf, 13, covariance); + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN); +#else + mavlink_distance_sensor_t packet; + packet.time_boot_ms = time_boot_ms; + packet.min_distance = min_distance; + packet.max_distance = max_distance; + packet.current_distance = current_distance; + packet.type = type; + packet.id = id; + packet.orientation = orientation; + packet.covariance = covariance; + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN); +#endif + + msg->msgid = MAVLINK_MSG_ID_DISTANCE_SENSOR; +#if MAVLINK_CRC_EXTRA + return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN, MAVLINK_MSG_ID_DISTANCE_SENSOR_CRC); +#else + return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN); +#endif +} + +/** + * @brief Encode a distance_sensor struct + * + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param msg The MAVLink message to compress the data into + * @param distance_sensor C-struct to read the message contents from + */ +static inline uint16_t mavlink_msg_distance_sensor_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_distance_sensor_t* distance_sensor) +{ + return mavlink_msg_distance_sensor_pack(system_id, component_id, msg, distance_sensor->time_boot_ms, distance_sensor->type, distance_sensor->id, distance_sensor->orientation, distance_sensor->min_distance, distance_sensor->max_distance, distance_sensor->current_distance, distance_sensor->covariance); +} + +/** + * @brief Encode a distance_sensor struct on a channel + * + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param chan The MAVLink channel this message will be sent over + * @param msg The MAVLink message to compress the data into + * @param distance_sensor C-struct to read the message contents from + */ +static inline uint16_t mavlink_msg_distance_sensor_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_distance_sensor_t* distance_sensor) +{ + return mavlink_msg_distance_sensor_pack_chan(system_id, component_id, chan, msg, distance_sensor->time_boot_ms, distance_sensor->type, distance_sensor->id, distance_sensor->orientation, distance_sensor->min_distance, distance_sensor->max_distance, distance_sensor->current_distance, distance_sensor->covariance); +} + +/** + * @brief Send a distance_sensor message + * @param chan MAVLink channel to send the message + * + * @param time_boot_ms Time since system boot + * @param type Type from MAV_DISTANCE_SENSOR enum. + * @param id Onboard ID of the sensor + * @param orientation Direction the sensor faces from FIXME enum. + * @param min_distance Minimum distance the sensor can measure in centimeters + * @param max_distance Maximum distance the sensor can measure in centimeters + * @param current_distance Current distance reading + * @param covariance Measurement covariance in centimeters, 0 for unknown / invalid readings + */ +#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS + +static inline void mavlink_msg_distance_sensor_send(mavlink_channel_t chan, uint32_t time_boot_ms, uint8_t type, uint8_t id, uint8_t orientation, uint16_t min_distance, uint16_t max_distance, uint16_t current_distance, uint8_t covariance) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN]; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_uint16_t(buf, 4, min_distance); + _mav_put_uint16_t(buf, 6, max_distance); + _mav_put_uint16_t(buf, 8, current_distance); + _mav_put_uint8_t(buf, 10, type); + _mav_put_uint8_t(buf, 11, id); + _mav_put_uint8_t(buf, 12, orientation); + _mav_put_uint8_t(buf, 13, covariance); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DISTANCE_SENSOR, buf, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN, MAVLINK_MSG_ID_DISTANCE_SENSOR_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DISTANCE_SENSOR, buf, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN); +#endif +#else + mavlink_distance_sensor_t packet; + packet.time_boot_ms = time_boot_ms; + packet.min_distance = min_distance; + packet.max_distance = max_distance; + packet.current_distance = current_distance; + packet.type = type; + packet.id = id; + packet.orientation = orientation; + packet.covariance = covariance; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DISTANCE_SENSOR, (const char *)&packet, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN, MAVLINK_MSG_ID_DISTANCE_SENSOR_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DISTANCE_SENSOR, (const char *)&packet, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN); +#endif +#endif +} + +#if MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_distance_sensor_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, uint8_t type, uint8_t id, uint8_t orientation, uint16_t min_distance, uint16_t max_distance, uint16_t current_distance, uint8_t covariance) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_uint16_t(buf, 4, min_distance); + _mav_put_uint16_t(buf, 6, max_distance); + _mav_put_uint16_t(buf, 8, current_distance); + _mav_put_uint8_t(buf, 10, type); + _mav_put_uint8_t(buf, 11, id); + _mav_put_uint8_t(buf, 12, orientation); + _mav_put_uint8_t(buf, 13, covariance); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DISTANCE_SENSOR, buf, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN, MAVLINK_MSG_ID_DISTANCE_SENSOR_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DISTANCE_SENSOR, buf, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN); +#endif +#else + mavlink_distance_sensor_t *packet = (mavlink_distance_sensor_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->min_distance = min_distance; + packet->max_distance = max_distance; + packet->current_distance = current_distance; + packet->type = type; + packet->id = id; + packet->orientation = orientation; + packet->covariance = covariance; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DISTANCE_SENSOR, (const char *)packet, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN, MAVLINK_MSG_ID_DISTANCE_SENSOR_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_DISTANCE_SENSOR, (const char *)packet, MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN); +#endif +#endif +} +#endif + +#endif + +// MESSAGE DISTANCE_SENSOR UNPACKING + + +/** + * @brief Get field time_boot_ms from distance_sensor message + * + * @return Time since system boot + */ +static inline uint32_t mavlink_msg_distance_sensor_get_time_boot_ms(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint32_t(msg, 0); +} + +/** + * @brief Get field type from distance_sensor message + * + * @return Type from MAV_DISTANCE_SENSOR enum. + */ +static inline uint8_t mavlink_msg_distance_sensor_get_type(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint8_t(msg, 10); +} + +/** + * @brief Get field id from distance_sensor message + * + * @return Onboard ID of the sensor + */ +static inline uint8_t mavlink_msg_distance_sensor_get_id(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint8_t(msg, 11); +} + +/** + * @brief Get field orientation from distance_sensor message + * + * @return Direction the sensor faces from FIXME enum. + */ +static inline uint8_t mavlink_msg_distance_sensor_get_orientation(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint8_t(msg, 12); +} + +/** + * @brief Get field min_distance from distance_sensor message + * + * @return Minimum distance the sensor can measure in centimeters + */ +static inline uint16_t mavlink_msg_distance_sensor_get_min_distance(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 4); +} + +/** + * @brief Get field max_distance from distance_sensor message + * + * @return Maximum distance the sensor can measure in centimeters + */ +static inline uint16_t mavlink_msg_distance_sensor_get_max_distance(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 6); +} + +/** + * @brief Get field current_distance from distance_sensor message + * + * @return Current distance reading + */ +static inline uint16_t mavlink_msg_distance_sensor_get_current_distance(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 8); +} + +/** + * @brief Get field covariance from distance_sensor message + * + * @return Measurement covariance in centimeters, 0 for unknown / invalid readings + */ +static inline uint8_t mavlink_msg_distance_sensor_get_covariance(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint8_t(msg, 13); +} + +/** + * @brief Decode a distance_sensor message into a struct + * + * @param msg The message to decode + * @param distance_sensor C-struct to decode the message contents into + */ +static inline void mavlink_msg_distance_sensor_decode(const mavlink_message_t* msg, mavlink_distance_sensor_t* distance_sensor) +{ +#if MAVLINK_NEED_BYTE_SWAP + distance_sensor->time_boot_ms = mavlink_msg_distance_sensor_get_time_boot_ms(msg); + distance_sensor->min_distance = mavlink_msg_distance_sensor_get_min_distance(msg); + distance_sensor->max_distance = mavlink_msg_distance_sensor_get_max_distance(msg); + distance_sensor->current_distance = mavlink_msg_distance_sensor_get_current_distance(msg); + distance_sensor->type = mavlink_msg_distance_sensor_get_type(msg); + distance_sensor->id = mavlink_msg_distance_sensor_get_id(msg); + distance_sensor->orientation = mavlink_msg_distance_sensor_get_orientation(msg); + distance_sensor->covariance = mavlink_msg_distance_sensor_get_covariance(msg); +#else + memcpy(distance_sensor, _MAV_PAYLOAD(msg), MAVLINK_MSG_ID_DISTANCE_SENSOR_LEN); +#endif +} diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_encapsulated_data.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_encapsulated_data.h index 5900ea838..dacd7c9f4 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_encapsulated_data.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_encapsulated_data.h @@ -151,6 +151,38 @@ static inline void mavlink_msg_encapsulated_data_send(mavlink_channel_t chan, ui #endif } +#if MAVLINK_MSG_ID_ENCAPSULATED_DATA_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_encapsulated_data_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t seqnr, const uint8_t *data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, seqnr); + _mav_put_uint8_t_array(buf, 2, data, 253); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ENCAPSULATED_DATA, buf, MAVLINK_MSG_ID_ENCAPSULATED_DATA_LEN, MAVLINK_MSG_ID_ENCAPSULATED_DATA_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ENCAPSULATED_DATA, buf, MAVLINK_MSG_ID_ENCAPSULATED_DATA_LEN); +#endif +#else + mavlink_encapsulated_data_t *packet = (mavlink_encapsulated_data_t *)msgbuf; + packet->seqnr = seqnr; + mav_array_memcpy(packet->data, data, sizeof(uint8_t)*253); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ENCAPSULATED_DATA, (const char *)packet, MAVLINK_MSG_ID_ENCAPSULATED_DATA_LEN, MAVLINK_MSG_ID_ENCAPSULATED_DATA_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ENCAPSULATED_DATA, (const char *)packet, MAVLINK_MSG_ID_ENCAPSULATED_DATA_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE ENCAPSULATED_DATA UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_file_transfer_dir_list.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_file_transfer_dir_list.h index 4f31698d5..81c7031ce 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_file_transfer_dir_list.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_file_transfer_dir_list.h @@ -162,6 +162,40 @@ static inline void mavlink_msg_file_transfer_dir_list_send(mavlink_channel_t cha #endif } +#if MAVLINK_MSG_ID_FILE_TRANSFER_DIR_LIST_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_file_transfer_dir_list_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t transfer_uid, const char *dir_path, uint8_t flags) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, transfer_uid); + _mav_put_uint8_t(buf, 248, flags); + _mav_put_char_array(buf, 8, dir_path, 240); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILE_TRANSFER_DIR_LIST, buf, MAVLINK_MSG_ID_FILE_TRANSFER_DIR_LIST_LEN, MAVLINK_MSG_ID_FILE_TRANSFER_DIR_LIST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILE_TRANSFER_DIR_LIST, buf, MAVLINK_MSG_ID_FILE_TRANSFER_DIR_LIST_LEN); +#endif +#else + mavlink_file_transfer_dir_list_t *packet = (mavlink_file_transfer_dir_list_t *)msgbuf; + packet->transfer_uid = transfer_uid; + packet->flags = flags; + mav_array_memcpy(packet->dir_path, dir_path, sizeof(char)*240); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILE_TRANSFER_DIR_LIST, (const char *)packet, MAVLINK_MSG_ID_FILE_TRANSFER_DIR_LIST_LEN, MAVLINK_MSG_ID_FILE_TRANSFER_DIR_LIST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILE_TRANSFER_DIR_LIST, (const char *)packet, MAVLINK_MSG_ID_FILE_TRANSFER_DIR_LIST_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FILE_TRANSFER_DIR_LIST UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_file_transfer_res.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_file_transfer_res.h index fc6247fac..04981fa85 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_file_transfer_res.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_file_transfer_res.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_file_transfer_res_send(mavlink_channel_t chan, ui #endif } +#if MAVLINK_MSG_ID_FILE_TRANSFER_RES_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_file_transfer_res_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t transfer_uid, uint8_t result) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, transfer_uid); + _mav_put_uint8_t(buf, 8, result); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILE_TRANSFER_RES, buf, MAVLINK_MSG_ID_FILE_TRANSFER_RES_LEN, MAVLINK_MSG_ID_FILE_TRANSFER_RES_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILE_TRANSFER_RES, buf, MAVLINK_MSG_ID_FILE_TRANSFER_RES_LEN); +#endif +#else + mavlink_file_transfer_res_t *packet = (mavlink_file_transfer_res_t *)msgbuf; + packet->transfer_uid = transfer_uid; + packet->result = result; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILE_TRANSFER_RES, (const char *)packet, MAVLINK_MSG_ID_FILE_TRANSFER_RES_LEN, MAVLINK_MSG_ID_FILE_TRANSFER_RES_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILE_TRANSFER_RES, (const char *)packet, MAVLINK_MSG_ID_FILE_TRANSFER_RES_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FILE_TRANSFER_RES UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_file_transfer_start.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_file_transfer_start.h index 05be77339..7b1fba519 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_file_transfer_start.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_file_transfer_start.h @@ -184,6 +184,44 @@ static inline void mavlink_msg_file_transfer_start_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_FILE_TRANSFER_START_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_file_transfer_start_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t transfer_uid, const char *dest_path, uint8_t direction, uint32_t file_size, uint8_t flags) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, transfer_uid); + _mav_put_uint32_t(buf, 8, file_size); + _mav_put_uint8_t(buf, 252, direction); + _mav_put_uint8_t(buf, 253, flags); + _mav_put_char_array(buf, 12, dest_path, 240); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILE_TRANSFER_START, buf, MAVLINK_MSG_ID_FILE_TRANSFER_START_LEN, MAVLINK_MSG_ID_FILE_TRANSFER_START_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILE_TRANSFER_START, buf, MAVLINK_MSG_ID_FILE_TRANSFER_START_LEN); +#endif +#else + mavlink_file_transfer_start_t *packet = (mavlink_file_transfer_start_t *)msgbuf; + packet->transfer_uid = transfer_uid; + packet->file_size = file_size; + packet->direction = direction; + packet->flags = flags; + mav_array_memcpy(packet->dest_path, dest_path, sizeof(char)*240); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILE_TRANSFER_START, (const char *)packet, MAVLINK_MSG_ID_FILE_TRANSFER_START_LEN, MAVLINK_MSG_ID_FILE_TRANSFER_START_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILE_TRANSFER_START, (const char *)packet, MAVLINK_MSG_ID_FILE_TRANSFER_START_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FILE_TRANSFER_START UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_global_position_int.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_global_position_int.h index 7ed3d2a63..ba15bf365 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_global_position_int.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_global_position_int.h @@ -234,6 +234,54 @@ static inline void mavlink_msg_global_position_int_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_GLOBAL_POSITION_INT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_global_position_int_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, int32_t lat, int32_t lon, int32_t alt, int32_t relative_alt, int16_t vx, int16_t vy, int16_t vz, uint16_t hdg) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_int32_t(buf, 4, lat); + _mav_put_int32_t(buf, 8, lon); + _mav_put_int32_t(buf, 12, alt); + _mav_put_int32_t(buf, 16, relative_alt); + _mav_put_int16_t(buf, 20, vx); + _mav_put_int16_t(buf, 22, vy); + _mav_put_int16_t(buf, 24, vz); + _mav_put_uint16_t(buf, 26, hdg); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GLOBAL_POSITION_INT, buf, MAVLINK_MSG_ID_GLOBAL_POSITION_INT_LEN, MAVLINK_MSG_ID_GLOBAL_POSITION_INT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GLOBAL_POSITION_INT, buf, MAVLINK_MSG_ID_GLOBAL_POSITION_INT_LEN); +#endif +#else + mavlink_global_position_int_t *packet = (mavlink_global_position_int_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->lat = lat; + packet->lon = lon; + packet->alt = alt; + packet->relative_alt = relative_alt; + packet->vx = vx; + packet->vy = vy; + packet->vz = vz; + packet->hdg = hdg; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GLOBAL_POSITION_INT, (const char *)packet, MAVLINK_MSG_ID_GLOBAL_POSITION_INT_LEN, MAVLINK_MSG_ID_GLOBAL_POSITION_INT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GLOBAL_POSITION_INT, (const char *)packet, MAVLINK_MSG_ID_GLOBAL_POSITION_INT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE GLOBAL_POSITION_INT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_global_position_setpoint_int.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_global_position_setpoint_int.h index 1a1c97199..77d735cf4 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_global_position_setpoint_int.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_global_position_setpoint_int.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_global_position_setpoint_int_send(mavlink_channel #endif } +#if MAVLINK_MSG_ID_GLOBAL_POSITION_SETPOINT_INT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_global_position_setpoint_int_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t coordinate_frame, int32_t latitude, int32_t longitude, int32_t altitude, int16_t yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, latitude); + _mav_put_int32_t(buf, 4, longitude); + _mav_put_int32_t(buf, 8, altitude); + _mav_put_int16_t(buf, 12, yaw); + _mav_put_uint8_t(buf, 14, coordinate_frame); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GLOBAL_POSITION_SETPOINT_INT, buf, MAVLINK_MSG_ID_GLOBAL_POSITION_SETPOINT_INT_LEN, MAVLINK_MSG_ID_GLOBAL_POSITION_SETPOINT_INT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GLOBAL_POSITION_SETPOINT_INT, buf, MAVLINK_MSG_ID_GLOBAL_POSITION_SETPOINT_INT_LEN); +#endif +#else + mavlink_global_position_setpoint_int_t *packet = (mavlink_global_position_setpoint_int_t *)msgbuf; + packet->latitude = latitude; + packet->longitude = longitude; + packet->altitude = altitude; + packet->yaw = yaw; + packet->coordinate_frame = coordinate_frame; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GLOBAL_POSITION_SETPOINT_INT, (const char *)packet, MAVLINK_MSG_ID_GLOBAL_POSITION_SETPOINT_INT_LEN, MAVLINK_MSG_ID_GLOBAL_POSITION_SETPOINT_INT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GLOBAL_POSITION_SETPOINT_INT, (const char *)packet, MAVLINK_MSG_ID_GLOBAL_POSITION_SETPOINT_INT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE GLOBAL_POSITION_SETPOINT_INT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_global_vision_position_estimate.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_global_vision_position_estimate.h index f7be74c91..b2b75d7ef 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_global_vision_position_estimate.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_global_vision_position_estimate.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_global_vision_position_estimate_send(mavlink_chan #endif } +#if MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_global_vision_position_estimate_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t usec, float x, float y, float z, float roll, float pitch, float yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, usec); + _mav_put_float(buf, 8, x); + _mav_put_float(buf, 12, y); + _mav_put_float(buf, 16, z); + _mav_put_float(buf, 20, roll); + _mav_put_float(buf, 24, pitch); + _mav_put_float(buf, 28, yaw); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE, buf, MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE_LEN, MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE, buf, MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE_LEN); +#endif +#else + mavlink_global_vision_position_estimate_t *packet = (mavlink_global_vision_position_estimate_t *)msgbuf; + packet->usec = usec; + packet->x = x; + packet->y = y; + packet->z = z; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE, (const char *)packet, MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE_LEN, MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE, (const char *)packet, MAVLINK_MSG_ID_GLOBAL_VISION_POSITION_ESTIMATE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE GLOBAL_VISION_POSITION_ESTIMATE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps2_raw.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps2_raw.h index 17e5bd002..b184e7c9c 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps2_raw.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps2_raw.h @@ -267,6 +267,60 @@ static inline void mavlink_msg_gps2_raw_send(mavlink_channel_t chan, uint64_t ti #endif } +#if MAVLINK_MSG_ID_GPS2_RAW_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_gps2_raw_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, uint8_t fix_type, int32_t lat, int32_t lon, int32_t alt, uint16_t eph, uint16_t epv, uint16_t vel, uint16_t cog, uint8_t satellites_visible, uint8_t dgps_numch, uint32_t dgps_age) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_int32_t(buf, 8, lat); + _mav_put_int32_t(buf, 12, lon); + _mav_put_int32_t(buf, 16, alt); + _mav_put_uint32_t(buf, 20, dgps_age); + _mav_put_uint16_t(buf, 24, eph); + _mav_put_uint16_t(buf, 26, epv); + _mav_put_uint16_t(buf, 28, vel); + _mav_put_uint16_t(buf, 30, cog); + _mav_put_uint8_t(buf, 32, fix_type); + _mav_put_uint8_t(buf, 33, satellites_visible); + _mav_put_uint8_t(buf, 34, dgps_numch); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS2_RAW, buf, MAVLINK_MSG_ID_GPS2_RAW_LEN, MAVLINK_MSG_ID_GPS2_RAW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS2_RAW, buf, MAVLINK_MSG_ID_GPS2_RAW_LEN); +#endif +#else + mavlink_gps2_raw_t *packet = (mavlink_gps2_raw_t *)msgbuf; + packet->time_usec = time_usec; + packet->lat = lat; + packet->lon = lon; + packet->alt = alt; + packet->dgps_age = dgps_age; + packet->eph = eph; + packet->epv = epv; + packet->vel = vel; + packet->cog = cog; + packet->fix_type = fix_type; + packet->satellites_visible = satellites_visible; + packet->dgps_numch = dgps_numch; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS2_RAW, (const char *)packet, MAVLINK_MSG_ID_GPS2_RAW_LEN, MAVLINK_MSG_ID_GPS2_RAW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS2_RAW, (const char *)packet, MAVLINK_MSG_ID_GPS2_RAW_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE GPS2_RAW UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_global_origin.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_global_origin.h index 016e9cb0e..1589c8ca5 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_global_origin.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_global_origin.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_gps_global_origin_send(mavlink_channel_t chan, in #endif } +#if MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_gps_global_origin_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, int32_t latitude, int32_t longitude, int32_t altitude) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, latitude); + _mav_put_int32_t(buf, 4, longitude); + _mav_put_int32_t(buf, 8, altitude); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN, buf, MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN_LEN, MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN, buf, MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN_LEN); +#endif +#else + mavlink_gps_global_origin_t *packet = (mavlink_gps_global_origin_t *)msgbuf; + packet->latitude = latitude; + packet->longitude = longitude; + packet->altitude = altitude; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN, (const char *)packet, MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN_LEN, MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN, (const char *)packet, MAVLINK_MSG_ID_GPS_GLOBAL_ORIGIN_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE GPS_GLOBAL_ORIGIN UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_inject_data.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_inject_data.h index 485d8a4af..362e2d7b9 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_inject_data.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_inject_data.h @@ -173,6 +173,42 @@ static inline void mavlink_msg_gps_inject_data_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_GPS_INJECT_DATA_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_gps_inject_data_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t len, const uint8_t *data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + _mav_put_uint8_t(buf, 2, len); + _mav_put_uint8_t_array(buf, 3, data, 110); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_INJECT_DATA, buf, MAVLINK_MSG_ID_GPS_INJECT_DATA_LEN, MAVLINK_MSG_ID_GPS_INJECT_DATA_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_INJECT_DATA, buf, MAVLINK_MSG_ID_GPS_INJECT_DATA_LEN); +#endif +#else + mavlink_gps_inject_data_t *packet = (mavlink_gps_inject_data_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + packet->len = len; + mav_array_memcpy(packet->data, data, sizeof(uint8_t)*110); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_INJECT_DATA, (const char *)packet, MAVLINK_MSG_ID_GPS_INJECT_DATA_LEN, MAVLINK_MSG_ID_GPS_INJECT_DATA_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_INJECT_DATA, (const char *)packet, MAVLINK_MSG_ID_GPS_INJECT_DATA_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE GPS_INJECT_DATA UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_raw_int.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_raw_int.h index a105f8cda..b53996206 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_raw_int.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_raw_int.h @@ -245,6 +245,56 @@ static inline void mavlink_msg_gps_raw_int_send(mavlink_channel_t chan, uint64_t #endif } +#if MAVLINK_MSG_ID_GPS_RAW_INT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_gps_raw_int_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, uint8_t fix_type, int32_t lat, int32_t lon, int32_t alt, uint16_t eph, uint16_t epv, uint16_t vel, uint16_t cog, uint8_t satellites_visible) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_int32_t(buf, 8, lat); + _mav_put_int32_t(buf, 12, lon); + _mav_put_int32_t(buf, 16, alt); + _mav_put_uint16_t(buf, 20, eph); + _mav_put_uint16_t(buf, 22, epv); + _mav_put_uint16_t(buf, 24, vel); + _mav_put_uint16_t(buf, 26, cog); + _mav_put_uint8_t(buf, 28, fix_type); + _mav_put_uint8_t(buf, 29, satellites_visible); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_RAW_INT, buf, MAVLINK_MSG_ID_GPS_RAW_INT_LEN, MAVLINK_MSG_ID_GPS_RAW_INT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_RAW_INT, buf, MAVLINK_MSG_ID_GPS_RAW_INT_LEN); +#endif +#else + mavlink_gps_raw_int_t *packet = (mavlink_gps_raw_int_t *)msgbuf; + packet->time_usec = time_usec; + packet->lat = lat; + packet->lon = lon; + packet->alt = alt; + packet->eph = eph; + packet->epv = epv; + packet->vel = vel; + packet->cog = cog; + packet->fix_type = fix_type; + packet->satellites_visible = satellites_visible; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_RAW_INT, (const char *)packet, MAVLINK_MSG_ID_GPS_RAW_INT_LEN, MAVLINK_MSG_ID_GPS_RAW_INT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_RAW_INT, (const char *)packet, MAVLINK_MSG_ID_GPS_RAW_INT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE GPS_RAW_INT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_status.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_status.h index 28d6b57d1..10659d0dd 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_status.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_gps_status.h @@ -199,6 +199,46 @@ static inline void mavlink_msg_gps_status_send(mavlink_channel_t chan, uint8_t s #endif } +#if MAVLINK_MSG_ID_GPS_STATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_gps_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t satellites_visible, const uint8_t *satellite_prn, const uint8_t *satellite_used, const uint8_t *satellite_elevation, const uint8_t *satellite_azimuth, const uint8_t *satellite_snr) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, satellites_visible); + _mav_put_uint8_t_array(buf, 1, satellite_prn, 20); + _mav_put_uint8_t_array(buf, 21, satellite_used, 20); + _mav_put_uint8_t_array(buf, 41, satellite_elevation, 20); + _mav_put_uint8_t_array(buf, 61, satellite_azimuth, 20); + _mav_put_uint8_t_array(buf, 81, satellite_snr, 20); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_STATUS, buf, MAVLINK_MSG_ID_GPS_STATUS_LEN, MAVLINK_MSG_ID_GPS_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_STATUS, buf, MAVLINK_MSG_ID_GPS_STATUS_LEN); +#endif +#else + mavlink_gps_status_t *packet = (mavlink_gps_status_t *)msgbuf; + packet->satellites_visible = satellites_visible; + mav_array_memcpy(packet->satellite_prn, satellite_prn, sizeof(uint8_t)*20); + mav_array_memcpy(packet->satellite_used, satellite_used, sizeof(uint8_t)*20); + mav_array_memcpy(packet->satellite_elevation, satellite_elevation, sizeof(uint8_t)*20); + mav_array_memcpy(packet->satellite_azimuth, satellite_azimuth, sizeof(uint8_t)*20); + mav_array_memcpy(packet->satellite_snr, satellite_snr, sizeof(uint8_t)*20); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_STATUS, (const char *)packet, MAVLINK_MSG_ID_GPS_STATUS_LEN, MAVLINK_MSG_ID_GPS_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GPS_STATUS, (const char *)packet, MAVLINK_MSG_ID_GPS_STATUS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE GPS_STATUS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_heartbeat.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_heartbeat.h index 826138fad..902e381ca 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_heartbeat.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_heartbeat.h @@ -198,6 +198,48 @@ static inline void mavlink_msg_heartbeat_send(mavlink_channel_t chan, uint8_t ty #endif } +#if MAVLINK_MSG_ID_HEARTBEAT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_heartbeat_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t type, uint8_t autopilot, uint8_t base_mode, uint32_t custom_mode, uint8_t system_status) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, custom_mode); + _mav_put_uint8_t(buf, 4, type); + _mav_put_uint8_t(buf, 5, autopilot); + _mav_put_uint8_t(buf, 6, base_mode); + _mav_put_uint8_t(buf, 7, system_status); + _mav_put_uint8_t(buf, 8, 3); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HEARTBEAT, buf, MAVLINK_MSG_ID_HEARTBEAT_LEN, MAVLINK_MSG_ID_HEARTBEAT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HEARTBEAT, buf, MAVLINK_MSG_ID_HEARTBEAT_LEN); +#endif +#else + mavlink_heartbeat_t *packet = (mavlink_heartbeat_t *)msgbuf; + packet->custom_mode = custom_mode; + packet->type = type; + packet->autopilot = autopilot; + packet->base_mode = base_mode; + packet->system_status = system_status; + packet->mavlink_version = 3; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HEARTBEAT, (const char *)packet, MAVLINK_MSG_ID_HEARTBEAT_LEN, MAVLINK_MSG_ID_HEARTBEAT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HEARTBEAT, (const char *)packet, MAVLINK_MSG_ID_HEARTBEAT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE HEARTBEAT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_highres_imu.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_highres_imu.h index 0dcd95ed3..2749cb097 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_highres_imu.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_highres_imu.h @@ -300,6 +300,66 @@ static inline void mavlink_msg_highres_imu_send(mavlink_channel_t chan, uint64_t #endif } +#if MAVLINK_MSG_ID_HIGHRES_IMU_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_highres_imu_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, float xacc, float yacc, float zacc, float xgyro, float ygyro, float zgyro, float xmag, float ymag, float zmag, float abs_pressure, float diff_pressure, float pressure_alt, float temperature, uint16_t fields_updated) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_float(buf, 8, xacc); + _mav_put_float(buf, 12, yacc); + _mav_put_float(buf, 16, zacc); + _mav_put_float(buf, 20, xgyro); + _mav_put_float(buf, 24, ygyro); + _mav_put_float(buf, 28, zgyro); + _mav_put_float(buf, 32, xmag); + _mav_put_float(buf, 36, ymag); + _mav_put_float(buf, 40, zmag); + _mav_put_float(buf, 44, abs_pressure); + _mav_put_float(buf, 48, diff_pressure); + _mav_put_float(buf, 52, pressure_alt); + _mav_put_float(buf, 56, temperature); + _mav_put_uint16_t(buf, 60, fields_updated); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIGHRES_IMU, buf, MAVLINK_MSG_ID_HIGHRES_IMU_LEN, MAVLINK_MSG_ID_HIGHRES_IMU_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIGHRES_IMU, buf, MAVLINK_MSG_ID_HIGHRES_IMU_LEN); +#endif +#else + mavlink_highres_imu_t *packet = (mavlink_highres_imu_t *)msgbuf; + packet->time_usec = time_usec; + packet->xacc = xacc; + packet->yacc = yacc; + packet->zacc = zacc; + packet->xgyro = xgyro; + packet->ygyro = ygyro; + packet->zgyro = zgyro; + packet->xmag = xmag; + packet->ymag = ymag; + packet->zmag = zmag; + packet->abs_pressure = abs_pressure; + packet->diff_pressure = diff_pressure; + packet->pressure_alt = pressure_alt; + packet->temperature = temperature; + packet->fields_updated = fields_updated; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIGHRES_IMU, (const char *)packet, MAVLINK_MSG_ID_HIGHRES_IMU_LEN, MAVLINK_MSG_ID_HIGHRES_IMU_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIGHRES_IMU, (const char *)packet, MAVLINK_MSG_ID_HIGHRES_IMU_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE HIGHRES_IMU UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_controls.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_controls.h index aed5108d0..f7507b1cf 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_controls.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_controls.h @@ -256,6 +256,58 @@ static inline void mavlink_msg_hil_controls_send(mavlink_channel_t chan, uint64_ #endif } +#if MAVLINK_MSG_ID_HIL_CONTROLS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_hil_controls_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, float roll_ailerons, float pitch_elevator, float yaw_rudder, float throttle, float aux1, float aux2, float aux3, float aux4, uint8_t mode, uint8_t nav_mode) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_float(buf, 8, roll_ailerons); + _mav_put_float(buf, 12, pitch_elevator); + _mav_put_float(buf, 16, yaw_rudder); + _mav_put_float(buf, 20, throttle); + _mav_put_float(buf, 24, aux1); + _mav_put_float(buf, 28, aux2); + _mav_put_float(buf, 32, aux3); + _mav_put_float(buf, 36, aux4); + _mav_put_uint8_t(buf, 40, mode); + _mav_put_uint8_t(buf, 41, nav_mode); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_CONTROLS, buf, MAVLINK_MSG_ID_HIL_CONTROLS_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_CONTROLS, buf, MAVLINK_MSG_ID_HIL_CONTROLS_LEN); +#endif +#else + mavlink_hil_controls_t *packet = (mavlink_hil_controls_t *)msgbuf; + packet->time_usec = time_usec; + packet->roll_ailerons = roll_ailerons; + packet->pitch_elevator = pitch_elevator; + packet->yaw_rudder = yaw_rudder; + packet->throttle = throttle; + packet->aux1 = aux1; + packet->aux2 = aux2; + packet->aux3 = aux3; + packet->aux4 = aux4; + packet->mode = mode; + packet->nav_mode = nav_mode; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_CONTROLS, (const char *)packet, MAVLINK_MSG_ID_HIL_CONTROLS_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_CONTROLS, (const char *)packet, MAVLINK_MSG_ID_HIL_CONTROLS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE HIL_CONTROLS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_gps.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_gps.h index 91aec5b08..a22c0472f 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_gps.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_gps.h @@ -278,6 +278,62 @@ static inline void mavlink_msg_hil_gps_send(mavlink_channel_t chan, uint64_t tim #endif } +#if MAVLINK_MSG_ID_HIL_GPS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_hil_gps_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, uint8_t fix_type, int32_t lat, int32_t lon, int32_t alt, uint16_t eph, uint16_t epv, uint16_t vel, int16_t vn, int16_t ve, int16_t vd, uint16_t cog, uint8_t satellites_visible) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_int32_t(buf, 8, lat); + _mav_put_int32_t(buf, 12, lon); + _mav_put_int32_t(buf, 16, alt); + _mav_put_uint16_t(buf, 20, eph); + _mav_put_uint16_t(buf, 22, epv); + _mav_put_uint16_t(buf, 24, vel); + _mav_put_int16_t(buf, 26, vn); + _mav_put_int16_t(buf, 28, ve); + _mav_put_int16_t(buf, 30, vd); + _mav_put_uint16_t(buf, 32, cog); + _mav_put_uint8_t(buf, 34, fix_type); + _mav_put_uint8_t(buf, 35, satellites_visible); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_GPS, buf, MAVLINK_MSG_ID_HIL_GPS_LEN, MAVLINK_MSG_ID_HIL_GPS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_GPS, buf, MAVLINK_MSG_ID_HIL_GPS_LEN); +#endif +#else + mavlink_hil_gps_t *packet = (mavlink_hil_gps_t *)msgbuf; + packet->time_usec = time_usec; + packet->lat = lat; + packet->lon = lon; + packet->alt = alt; + packet->eph = eph; + packet->epv = epv; + packet->vel = vel; + packet->vn = vn; + packet->ve = ve; + packet->vd = vd; + packet->cog = cog; + packet->fix_type = fix_type; + packet->satellites_visible = satellites_visible; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_GPS, (const char *)packet, MAVLINK_MSG_ID_HIL_GPS_LEN, MAVLINK_MSG_ID_HIL_GPS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_GPS, (const char *)packet, MAVLINK_MSG_ID_HIL_GPS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE HIL_GPS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_optical_flow.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_optical_flow.h index acb1392e1..eaadf2435 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_optical_flow.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_optical_flow.h @@ -223,6 +223,52 @@ static inline void mavlink_msg_hil_optical_flow_send(mavlink_channel_t chan, uin #endif } +#if MAVLINK_MSG_ID_HIL_OPTICAL_FLOW_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_hil_optical_flow_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, uint8_t sensor_id, int16_t flow_x, int16_t flow_y, float flow_comp_m_x, float flow_comp_m_y, uint8_t quality, float ground_distance) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_float(buf, 8, flow_comp_m_x); + _mav_put_float(buf, 12, flow_comp_m_y); + _mav_put_float(buf, 16, ground_distance); + _mav_put_int16_t(buf, 20, flow_x); + _mav_put_int16_t(buf, 22, flow_y); + _mav_put_uint8_t(buf, 24, sensor_id); + _mav_put_uint8_t(buf, 25, quality); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_OPTICAL_FLOW, buf, MAVLINK_MSG_ID_HIL_OPTICAL_FLOW_LEN, MAVLINK_MSG_ID_HIL_OPTICAL_FLOW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_OPTICAL_FLOW, buf, MAVLINK_MSG_ID_HIL_OPTICAL_FLOW_LEN); +#endif +#else + mavlink_hil_optical_flow_t *packet = (mavlink_hil_optical_flow_t *)msgbuf; + packet->time_usec = time_usec; + packet->flow_comp_m_x = flow_comp_m_x; + packet->flow_comp_m_y = flow_comp_m_y; + packet->ground_distance = ground_distance; + packet->flow_x = flow_x; + packet->flow_y = flow_y; + packet->sensor_id = sensor_id; + packet->quality = quality; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_OPTICAL_FLOW, (const char *)packet, MAVLINK_MSG_ID_HIL_OPTICAL_FLOW_LEN, MAVLINK_MSG_ID_HIL_OPTICAL_FLOW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_OPTICAL_FLOW, (const char *)packet, MAVLINK_MSG_ID_HIL_OPTICAL_FLOW_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE HIL_OPTICAL_FLOW UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_rc_inputs_raw.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_rc_inputs_raw.h index a42bde50b..227cd9d94 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_rc_inputs_raw.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_rc_inputs_raw.h @@ -289,6 +289,64 @@ static inline void mavlink_msg_hil_rc_inputs_raw_send(mavlink_channel_t chan, ui #endif } +#if MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_hil_rc_inputs_raw_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, uint16_t chan1_raw, uint16_t chan2_raw, uint16_t chan3_raw, uint16_t chan4_raw, uint16_t chan5_raw, uint16_t chan6_raw, uint16_t chan7_raw, uint16_t chan8_raw, uint16_t chan9_raw, uint16_t chan10_raw, uint16_t chan11_raw, uint16_t chan12_raw, uint8_t rssi) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_uint16_t(buf, 8, chan1_raw); + _mav_put_uint16_t(buf, 10, chan2_raw); + _mav_put_uint16_t(buf, 12, chan3_raw); + _mav_put_uint16_t(buf, 14, chan4_raw); + _mav_put_uint16_t(buf, 16, chan5_raw); + _mav_put_uint16_t(buf, 18, chan6_raw); + _mav_put_uint16_t(buf, 20, chan7_raw); + _mav_put_uint16_t(buf, 22, chan8_raw); + _mav_put_uint16_t(buf, 24, chan9_raw); + _mav_put_uint16_t(buf, 26, chan10_raw); + _mav_put_uint16_t(buf, 28, chan11_raw); + _mav_put_uint16_t(buf, 30, chan12_raw); + _mav_put_uint8_t(buf, 32, rssi); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW, buf, MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW_LEN, MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW, buf, MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW_LEN); +#endif +#else + mavlink_hil_rc_inputs_raw_t *packet = (mavlink_hil_rc_inputs_raw_t *)msgbuf; + packet->time_usec = time_usec; + packet->chan1_raw = chan1_raw; + packet->chan2_raw = chan2_raw; + packet->chan3_raw = chan3_raw; + packet->chan4_raw = chan4_raw; + packet->chan5_raw = chan5_raw; + packet->chan6_raw = chan6_raw; + packet->chan7_raw = chan7_raw; + packet->chan8_raw = chan8_raw; + packet->chan9_raw = chan9_raw; + packet->chan10_raw = chan10_raw; + packet->chan11_raw = chan11_raw; + packet->chan12_raw = chan12_raw; + packet->rssi = rssi; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW, (const char *)packet, MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW_LEN, MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW, (const char *)packet, MAVLINK_MSG_ID_HIL_RC_INPUTS_RAW_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE HIL_RC_INPUTS_RAW UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_sensor.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_sensor.h index 6c2667473..8672f8b8a 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_sensor.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_sensor.h @@ -300,6 +300,66 @@ static inline void mavlink_msg_hil_sensor_send(mavlink_channel_t chan, uint64_t #endif } +#if MAVLINK_MSG_ID_HIL_SENSOR_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_hil_sensor_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, float xacc, float yacc, float zacc, float xgyro, float ygyro, float zgyro, float xmag, float ymag, float zmag, float abs_pressure, float diff_pressure, float pressure_alt, float temperature, uint32_t fields_updated) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_float(buf, 8, xacc); + _mav_put_float(buf, 12, yacc); + _mav_put_float(buf, 16, zacc); + _mav_put_float(buf, 20, xgyro); + _mav_put_float(buf, 24, ygyro); + _mav_put_float(buf, 28, zgyro); + _mav_put_float(buf, 32, xmag); + _mav_put_float(buf, 36, ymag); + _mav_put_float(buf, 40, zmag); + _mav_put_float(buf, 44, abs_pressure); + _mav_put_float(buf, 48, diff_pressure); + _mav_put_float(buf, 52, pressure_alt); + _mav_put_float(buf, 56, temperature); + _mav_put_uint32_t(buf, 60, fields_updated); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_SENSOR, buf, MAVLINK_MSG_ID_HIL_SENSOR_LEN, MAVLINK_MSG_ID_HIL_SENSOR_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_SENSOR, buf, MAVLINK_MSG_ID_HIL_SENSOR_LEN); +#endif +#else + mavlink_hil_sensor_t *packet = (mavlink_hil_sensor_t *)msgbuf; + packet->time_usec = time_usec; + packet->xacc = xacc; + packet->yacc = yacc; + packet->zacc = zacc; + packet->xgyro = xgyro; + packet->ygyro = ygyro; + packet->zgyro = zgyro; + packet->xmag = xmag; + packet->ymag = ymag; + packet->zmag = zmag; + packet->abs_pressure = abs_pressure; + packet->diff_pressure = diff_pressure; + packet->pressure_alt = pressure_alt; + packet->temperature = temperature; + packet->fields_updated = fields_updated; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_SENSOR, (const char *)packet, MAVLINK_MSG_ID_HIL_SENSOR_LEN, MAVLINK_MSG_ID_HIL_SENSOR_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_SENSOR, (const char *)packet, MAVLINK_MSG_ID_HIL_SENSOR_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE HIL_SENSOR UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state.h index bcc857767..923ed60b9 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state.h @@ -311,6 +311,68 @@ static inline void mavlink_msg_hil_state_send(mavlink_channel_t chan, uint64_t t #endif } +#if MAVLINK_MSG_ID_HIL_STATE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_hil_state_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, float roll, float pitch, float yaw, float rollspeed, float pitchspeed, float yawspeed, int32_t lat, int32_t lon, int32_t alt, int16_t vx, int16_t vy, int16_t vz, int16_t xacc, int16_t yacc, int16_t zacc) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_float(buf, 8, roll); + _mav_put_float(buf, 12, pitch); + _mav_put_float(buf, 16, yaw); + _mav_put_float(buf, 20, rollspeed); + _mav_put_float(buf, 24, pitchspeed); + _mav_put_float(buf, 28, yawspeed); + _mav_put_int32_t(buf, 32, lat); + _mav_put_int32_t(buf, 36, lon); + _mav_put_int32_t(buf, 40, alt); + _mav_put_int16_t(buf, 44, vx); + _mav_put_int16_t(buf, 46, vy); + _mav_put_int16_t(buf, 48, vz); + _mav_put_int16_t(buf, 50, xacc); + _mav_put_int16_t(buf, 52, yacc); + _mav_put_int16_t(buf, 54, zacc); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE, buf, MAVLINK_MSG_ID_HIL_STATE_LEN, MAVLINK_MSG_ID_HIL_STATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE, buf, MAVLINK_MSG_ID_HIL_STATE_LEN); +#endif +#else + mavlink_hil_state_t *packet = (mavlink_hil_state_t *)msgbuf; + packet->time_usec = time_usec; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + packet->rollspeed = rollspeed; + packet->pitchspeed = pitchspeed; + packet->yawspeed = yawspeed; + packet->lat = lat; + packet->lon = lon; + packet->alt = alt; + packet->vx = vx; + packet->vy = vy; + packet->vz = vz; + packet->xacc = xacc; + packet->yacc = yacc; + packet->zacc = zacc; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE, (const char *)packet, MAVLINK_MSG_ID_HIL_STATE_LEN, MAVLINK_MSG_ID_HIL_STATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE, (const char *)packet, MAVLINK_MSG_ID_HIL_STATE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE HIL_STATE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state_quaternion.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state_quaternion.h index 732176193..1a028bdf9 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state_quaternion.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_state_quaternion.h @@ -305,6 +305,66 @@ static inline void mavlink_msg_hil_state_quaternion_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_hil_state_quaternion_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, const float *attitude_quaternion, float rollspeed, float pitchspeed, float yawspeed, int32_t lat, int32_t lon, int32_t alt, int16_t vx, int16_t vy, int16_t vz, uint16_t ind_airspeed, uint16_t true_airspeed, int16_t xacc, int16_t yacc, int16_t zacc) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_float(buf, 24, rollspeed); + _mav_put_float(buf, 28, pitchspeed); + _mav_put_float(buf, 32, yawspeed); + _mav_put_int32_t(buf, 36, lat); + _mav_put_int32_t(buf, 40, lon); + _mav_put_int32_t(buf, 44, alt); + _mav_put_int16_t(buf, 48, vx); + _mav_put_int16_t(buf, 50, vy); + _mav_put_int16_t(buf, 52, vz); + _mav_put_uint16_t(buf, 54, ind_airspeed); + _mav_put_uint16_t(buf, 56, true_airspeed); + _mav_put_int16_t(buf, 58, xacc); + _mav_put_int16_t(buf, 60, yacc); + _mav_put_int16_t(buf, 62, zacc); + _mav_put_float_array(buf, 8, attitude_quaternion, 4); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN); +#endif +#else + mavlink_hil_state_quaternion_t *packet = (mavlink_hil_state_quaternion_t *)msgbuf; + packet->time_usec = time_usec; + packet->rollspeed = rollspeed; + packet->pitchspeed = pitchspeed; + packet->yawspeed = yawspeed; + packet->lat = lat; + packet->lon = lon; + packet->alt = alt; + packet->vx = vx; + packet->vy = vy; + packet->vz = vz; + packet->ind_airspeed = ind_airspeed; + packet->true_airspeed = true_airspeed; + packet->xacc = xacc; + packet->yacc = yacc; + packet->zacc = zacc; + mav_array_memcpy(packet->attitude_quaternion, attitude_quaternion, sizeof(float)*4); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, (const char *)packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, (const char *)packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE HIL_STATE_QUATERNION UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_local_position_ned.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_local_position_ned.h index a0b72c0e1..e18a94869 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_local_position_ned.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_local_position_ned.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_local_position_ned_send(mavlink_channel_t chan, u #endif } +#if MAVLINK_MSG_ID_LOCAL_POSITION_NED_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_local_position_ned_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, float x, float y, float z, float vx, float vy, float vz) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_float(buf, 4, x); + _mav_put_float(buf, 8, y); + _mav_put_float(buf, 12, z); + _mav_put_float(buf, 16, vx); + _mav_put_float(buf, 20, vy); + _mav_put_float(buf, 24, vz); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOCAL_POSITION_NED, buf, MAVLINK_MSG_ID_LOCAL_POSITION_NED_LEN, MAVLINK_MSG_ID_LOCAL_POSITION_NED_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOCAL_POSITION_NED, buf, MAVLINK_MSG_ID_LOCAL_POSITION_NED_LEN); +#endif +#else + mavlink_local_position_ned_t *packet = (mavlink_local_position_ned_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->x = x; + packet->y = y; + packet->z = z; + packet->vx = vx; + packet->vy = vy; + packet->vz = vz; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOCAL_POSITION_NED, (const char *)packet, MAVLINK_MSG_ID_LOCAL_POSITION_NED_LEN, MAVLINK_MSG_ID_LOCAL_POSITION_NED_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOCAL_POSITION_NED, (const char *)packet, MAVLINK_MSG_ID_LOCAL_POSITION_NED_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE LOCAL_POSITION_NED UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_local_position_ned_system_global_offset.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_local_position_ned_system_global_offset.h index 8c4686202..af7d195b0 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_local_position_ned_system_global_offset.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_local_position_ned_system_global_offset.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_local_position_ned_system_global_offset_send(mavl #endif } +#if MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_local_position_ned_system_global_offset_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, float x, float y, float z, float roll, float pitch, float yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_float(buf, 4, x); + _mav_put_float(buf, 8, y); + _mav_put_float(buf, 12, z); + _mav_put_float(buf, 16, roll); + _mav_put_float(buf, 20, pitch); + _mav_put_float(buf, 24, yaw); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, buf, MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET_LEN, MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, buf, MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET_LEN); +#endif +#else + mavlink_local_position_ned_system_global_offset_t *packet = (mavlink_local_position_ned_system_global_offset_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->x = x; + packet->y = y; + packet->z = z; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, (const char *)packet, MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET_LEN, MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, (const char *)packet, MAVLINK_MSG_ID_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_local_position_setpoint.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_local_position_setpoint.h index 1794815f8..8dae721be 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_local_position_setpoint.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_local_position_setpoint.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_local_position_setpoint_send(mavlink_channel_t ch #endif } +#if MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_local_position_setpoint_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t coordinate_frame, float x, float y, float z, float yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, x); + _mav_put_float(buf, 4, y); + _mav_put_float(buf, 8, z); + _mav_put_float(buf, 12, yaw); + _mav_put_uint8_t(buf, 16, coordinate_frame); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT, buf, MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT_LEN, MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT, buf, MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT_LEN); +#endif +#else + mavlink_local_position_setpoint_t *packet = (mavlink_local_position_setpoint_t *)msgbuf; + packet->x = x; + packet->y = y; + packet->z = z; + packet->yaw = yaw; + packet->coordinate_frame = coordinate_frame; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT_LEN, MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE LOCAL_POSITION_SETPOINT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_data.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_data.h index 1cf5d15e4..48641f3eb 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_data.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_data.h @@ -173,6 +173,42 @@ static inline void mavlink_msg_log_data_send(mavlink_channel_t chan, uint16_t id #endif } +#if MAVLINK_MSG_ID_LOG_DATA_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_log_data_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t id, uint32_t ofs, uint8_t count, const uint8_t *data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, ofs); + _mav_put_uint16_t(buf, 4, id); + _mav_put_uint8_t(buf, 6, count); + _mav_put_uint8_t_array(buf, 7, data, 90); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_DATA, buf, MAVLINK_MSG_ID_LOG_DATA_LEN, MAVLINK_MSG_ID_LOG_DATA_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_DATA, buf, MAVLINK_MSG_ID_LOG_DATA_LEN); +#endif +#else + mavlink_log_data_t *packet = (mavlink_log_data_t *)msgbuf; + packet->ofs = ofs; + packet->id = id; + packet->count = count; + mav_array_memcpy(packet->data, data, sizeof(uint8_t)*90); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_DATA, (const char *)packet, MAVLINK_MSG_ID_LOG_DATA_LEN, MAVLINK_MSG_ID_LOG_DATA_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_DATA, (const char *)packet, MAVLINK_MSG_ID_LOG_DATA_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE LOG_DATA UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_entry.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_entry.h index 681d8f07c..8ecaec3ae 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_entry.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_entry.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_log_entry_send(mavlink_channel_t chan, uint16_t i #endif } +#if MAVLINK_MSG_ID_LOG_ENTRY_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_log_entry_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t id, uint16_t num_logs, uint16_t last_log_num, uint32_t time_utc, uint32_t size) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_utc); + _mav_put_uint32_t(buf, 4, size); + _mav_put_uint16_t(buf, 8, id); + _mav_put_uint16_t(buf, 10, num_logs); + _mav_put_uint16_t(buf, 12, last_log_num); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_ENTRY, buf, MAVLINK_MSG_ID_LOG_ENTRY_LEN, MAVLINK_MSG_ID_LOG_ENTRY_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_ENTRY, buf, MAVLINK_MSG_ID_LOG_ENTRY_LEN); +#endif +#else + mavlink_log_entry_t *packet = (mavlink_log_entry_t *)msgbuf; + packet->time_utc = time_utc; + packet->size = size; + packet->id = id; + packet->num_logs = num_logs; + packet->last_log_num = last_log_num; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_ENTRY, (const char *)packet, MAVLINK_MSG_ID_LOG_ENTRY_LEN, MAVLINK_MSG_ID_LOG_ENTRY_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_ENTRY, (const char *)packet, MAVLINK_MSG_ID_LOG_ENTRY_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE LOG_ENTRY UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_erase.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_erase.h index feafeaf16..957c4d4cc 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_erase.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_erase.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_log_erase_send(mavlink_channel_t chan, uint8_t ta #endif } +#if MAVLINK_MSG_ID_LOG_ERASE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_log_erase_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_ERASE, buf, MAVLINK_MSG_ID_LOG_ERASE_LEN, MAVLINK_MSG_ID_LOG_ERASE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_ERASE, buf, MAVLINK_MSG_ID_LOG_ERASE_LEN); +#endif +#else + mavlink_log_erase_t *packet = (mavlink_log_erase_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_ERASE, (const char *)packet, MAVLINK_MSG_ID_LOG_ERASE_LEN, MAVLINK_MSG_ID_LOG_ERASE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_ERASE, (const char *)packet, MAVLINK_MSG_ID_LOG_ERASE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE LOG_ERASE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_request_data.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_request_data.h index 5be9eea47..ef5cbb67c 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_request_data.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_request_data.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_log_request_data_send(mavlink_channel_t chan, uin #endif } +#if MAVLINK_MSG_ID_LOG_REQUEST_DATA_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_log_request_data_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint16_t id, uint32_t ofs, uint32_t count) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, ofs); + _mav_put_uint32_t(buf, 4, count); + _mav_put_uint16_t(buf, 8, id); + _mav_put_uint8_t(buf, 10, target_system); + _mav_put_uint8_t(buf, 11, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_REQUEST_DATA, buf, MAVLINK_MSG_ID_LOG_REQUEST_DATA_LEN, MAVLINK_MSG_ID_LOG_REQUEST_DATA_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_REQUEST_DATA, buf, MAVLINK_MSG_ID_LOG_REQUEST_DATA_LEN); +#endif +#else + mavlink_log_request_data_t *packet = (mavlink_log_request_data_t *)msgbuf; + packet->ofs = ofs; + packet->count = count; + packet->id = id; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_REQUEST_DATA, (const char *)packet, MAVLINK_MSG_ID_LOG_REQUEST_DATA_LEN, MAVLINK_MSG_ID_LOG_REQUEST_DATA_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_REQUEST_DATA, (const char *)packet, MAVLINK_MSG_ID_LOG_REQUEST_DATA_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE LOG_REQUEST_DATA UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_request_end.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_request_end.h index 48a5a03b4..23fcca29f 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_request_end.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_request_end.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_log_request_end_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_LOG_REQUEST_END_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_log_request_end_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_REQUEST_END, buf, MAVLINK_MSG_ID_LOG_REQUEST_END_LEN, MAVLINK_MSG_ID_LOG_REQUEST_END_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_REQUEST_END, buf, MAVLINK_MSG_ID_LOG_REQUEST_END_LEN); +#endif +#else + mavlink_log_request_end_t *packet = (mavlink_log_request_end_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_REQUEST_END, (const char *)packet, MAVLINK_MSG_ID_LOG_REQUEST_END_LEN, MAVLINK_MSG_ID_LOG_REQUEST_END_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_REQUEST_END, (const char *)packet, MAVLINK_MSG_ID_LOG_REQUEST_END_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE LOG_REQUEST_END UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_request_list.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_request_list.h index 7a5b25c17..e511b5312 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_request_list.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_log_request_list.h @@ -179,6 +179,44 @@ static inline void mavlink_msg_log_request_list_send(mavlink_channel_t chan, uin #endif } +#if MAVLINK_MSG_ID_LOG_REQUEST_LIST_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_log_request_list_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint16_t start, uint16_t end) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, start); + _mav_put_uint16_t(buf, 2, end); + _mav_put_uint8_t(buf, 4, target_system); + _mav_put_uint8_t(buf, 5, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_REQUEST_LIST, buf, MAVLINK_MSG_ID_LOG_REQUEST_LIST_LEN, MAVLINK_MSG_ID_LOG_REQUEST_LIST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_REQUEST_LIST, buf, MAVLINK_MSG_ID_LOG_REQUEST_LIST_LEN); +#endif +#else + mavlink_log_request_list_t *packet = (mavlink_log_request_list_t *)msgbuf; + packet->start = start; + packet->end = end; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_REQUEST_LIST, (const char *)packet, MAVLINK_MSG_ID_LOG_REQUEST_LIST_LEN, MAVLINK_MSG_ID_LOG_REQUEST_LIST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LOG_REQUEST_LIST, (const char *)packet, MAVLINK_MSG_ID_LOG_REQUEST_LIST_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE LOG_REQUEST_LIST UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_manual_control.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_manual_control.h index 6b6e9e148..e93b759d0 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_manual_control.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_manual_control.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_manual_control_send(mavlink_channel_t chan, uint8 #endif } +#if MAVLINK_MSG_ID_MANUAL_CONTROL_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_manual_control_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target, int16_t x, int16_t y, int16_t z, int16_t r, uint16_t buttons) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int16_t(buf, 0, x); + _mav_put_int16_t(buf, 2, y); + _mav_put_int16_t(buf, 4, z); + _mav_put_int16_t(buf, 6, r); + _mav_put_uint16_t(buf, 8, buttons); + _mav_put_uint8_t(buf, 10, target); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MANUAL_CONTROL, buf, MAVLINK_MSG_ID_MANUAL_CONTROL_LEN, MAVLINK_MSG_ID_MANUAL_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MANUAL_CONTROL, buf, MAVLINK_MSG_ID_MANUAL_CONTROL_LEN); +#endif +#else + mavlink_manual_control_t *packet = (mavlink_manual_control_t *)msgbuf; + packet->x = x; + packet->y = y; + packet->z = z; + packet->r = r; + packet->buttons = buttons; + packet->target = target; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MANUAL_CONTROL, (const char *)packet, MAVLINK_MSG_ID_MANUAL_CONTROL_LEN, MAVLINK_MSG_ID_MANUAL_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MANUAL_CONTROL, (const char *)packet, MAVLINK_MSG_ID_MANUAL_CONTROL_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MANUAL_CONTROL UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_manual_setpoint.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_manual_setpoint.h index a694947c1..b27626726 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_manual_setpoint.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_manual_setpoint.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_manual_setpoint_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_MANUAL_SETPOINT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_manual_setpoint_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, float roll, float pitch, float yaw, float thrust, uint8_t mode_switch, uint8_t manual_override_switch) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_float(buf, 4, roll); + _mav_put_float(buf, 8, pitch); + _mav_put_float(buf, 12, yaw); + _mav_put_float(buf, 16, thrust); + _mav_put_uint8_t(buf, 20, mode_switch); + _mav_put_uint8_t(buf, 21, manual_override_switch); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MANUAL_SETPOINT, buf, MAVLINK_MSG_ID_MANUAL_SETPOINT_LEN, MAVLINK_MSG_ID_MANUAL_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MANUAL_SETPOINT, buf, MAVLINK_MSG_ID_MANUAL_SETPOINT_LEN); +#endif +#else + mavlink_manual_setpoint_t *packet = (mavlink_manual_setpoint_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + packet->thrust = thrust; + packet->mode_switch = mode_switch; + packet->manual_override_switch = manual_override_switch; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MANUAL_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_MANUAL_SETPOINT_LEN, MAVLINK_MSG_ID_MANUAL_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MANUAL_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_MANUAL_SETPOINT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MANUAL_SETPOINT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_memory_vect.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_memory_vect.h index 5f79329c2..2eb60cc0e 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_memory_vect.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_memory_vect.h @@ -173,6 +173,42 @@ static inline void mavlink_msg_memory_vect_send(mavlink_channel_t chan, uint16_t #endif } +#if MAVLINK_MSG_ID_MEMORY_VECT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_memory_vect_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t address, uint8_t ver, uint8_t type, const int8_t *value) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, address); + _mav_put_uint8_t(buf, 2, ver); + _mav_put_uint8_t(buf, 3, type); + _mav_put_int8_t_array(buf, 4, value, 32); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEMORY_VECT, buf, MAVLINK_MSG_ID_MEMORY_VECT_LEN, MAVLINK_MSG_ID_MEMORY_VECT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEMORY_VECT, buf, MAVLINK_MSG_ID_MEMORY_VECT_LEN); +#endif +#else + mavlink_memory_vect_t *packet = (mavlink_memory_vect_t *)msgbuf; + packet->address = address; + packet->ver = ver; + packet->type = type; + mav_array_memcpy(packet->value, value, sizeof(int8_t)*32); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEMORY_VECT, (const char *)packet, MAVLINK_MSG_ID_MEMORY_VECT_LEN, MAVLINK_MSG_ID_MEMORY_VECT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEMORY_VECT, (const char *)packet, MAVLINK_MSG_ID_MEMORY_VECT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MEMORY_VECT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_ack.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_ack.h index 7421d8394..43afd00f7 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_ack.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_ack.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_mission_ack_send(mavlink_channel_t chan, uint8_t #endif } +#if MAVLINK_MSG_ID_MISSION_ACK_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mission_ack_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t type) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + _mav_put_uint8_t(buf, 2, type); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_ACK, buf, MAVLINK_MSG_ID_MISSION_ACK_LEN, MAVLINK_MSG_ID_MISSION_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_ACK, buf, MAVLINK_MSG_ID_MISSION_ACK_LEN); +#endif +#else + mavlink_mission_ack_t *packet = (mavlink_mission_ack_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + packet->type = type; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_ACK, (const char *)packet, MAVLINK_MSG_ID_MISSION_ACK_LEN, MAVLINK_MSG_ID_MISSION_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_ACK, (const char *)packet, MAVLINK_MSG_ID_MISSION_ACK_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MISSION_ACK UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_clear_all.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_clear_all.h index 8f441c8e5..120986873 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_clear_all.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_clear_all.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_mission_clear_all_send(mavlink_channel_t chan, ui #endif } +#if MAVLINK_MSG_ID_MISSION_CLEAR_ALL_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mission_clear_all_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_CLEAR_ALL, buf, MAVLINK_MSG_ID_MISSION_CLEAR_ALL_LEN, MAVLINK_MSG_ID_MISSION_CLEAR_ALL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_CLEAR_ALL, buf, MAVLINK_MSG_ID_MISSION_CLEAR_ALL_LEN); +#endif +#else + mavlink_mission_clear_all_t *packet = (mavlink_mission_clear_all_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_CLEAR_ALL, (const char *)packet, MAVLINK_MSG_ID_MISSION_CLEAR_ALL_LEN, MAVLINK_MSG_ID_MISSION_CLEAR_ALL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_CLEAR_ALL, (const char *)packet, MAVLINK_MSG_ID_MISSION_CLEAR_ALL_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MISSION_CLEAR_ALL UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_count.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_count.h index eac779306..7e4748eae 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_count.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_count.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_mission_count_send(mavlink_channel_t chan, uint8_ #endif } +#if MAVLINK_MSG_ID_MISSION_COUNT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mission_count_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint16_t count) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, count); + _mav_put_uint8_t(buf, 2, target_system); + _mav_put_uint8_t(buf, 3, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_COUNT, buf, MAVLINK_MSG_ID_MISSION_COUNT_LEN, MAVLINK_MSG_ID_MISSION_COUNT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_COUNT, buf, MAVLINK_MSG_ID_MISSION_COUNT_LEN); +#endif +#else + mavlink_mission_count_t *packet = (mavlink_mission_count_t *)msgbuf; + packet->count = count; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_COUNT, (const char *)packet, MAVLINK_MSG_ID_MISSION_COUNT_LEN, MAVLINK_MSG_ID_MISSION_COUNT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_COUNT, (const char *)packet, MAVLINK_MSG_ID_MISSION_COUNT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MISSION_COUNT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_current.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_current.h index dbcdbd3f9..201b7a6fb 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_current.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_current.h @@ -146,6 +146,38 @@ static inline void mavlink_msg_mission_current_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_MISSION_CURRENT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mission_current_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t seq) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, seq); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_CURRENT, buf, MAVLINK_MSG_ID_MISSION_CURRENT_LEN, MAVLINK_MSG_ID_MISSION_CURRENT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_CURRENT, buf, MAVLINK_MSG_ID_MISSION_CURRENT_LEN); +#endif +#else + mavlink_mission_current_t *packet = (mavlink_mission_current_t *)msgbuf; + packet->seq = seq; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_CURRENT, (const char *)packet, MAVLINK_MSG_ID_MISSION_CURRENT_LEN, MAVLINK_MSG_ID_MISSION_CURRENT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_CURRENT, (const char *)packet, MAVLINK_MSG_ID_MISSION_CURRENT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MISSION_CURRENT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_item.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_item.h index a8d60eca7..ef9394f00 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_item.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_item.h @@ -289,6 +289,64 @@ static inline void mavlink_msg_mission_item_send(mavlink_channel_t chan, uint8_t #endif } +#if MAVLINK_MSG_ID_MISSION_ITEM_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mission_item_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint16_t seq, uint8_t frame, uint16_t command, uint8_t current, uint8_t autocontinue, float param1, float param2, float param3, float param4, float x, float y, float z) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, param1); + _mav_put_float(buf, 4, param2); + _mav_put_float(buf, 8, param3); + _mav_put_float(buf, 12, param4); + _mav_put_float(buf, 16, x); + _mav_put_float(buf, 20, y); + _mav_put_float(buf, 24, z); + _mav_put_uint16_t(buf, 28, seq); + _mav_put_uint16_t(buf, 30, command); + _mav_put_uint8_t(buf, 32, target_system); + _mav_put_uint8_t(buf, 33, target_component); + _mav_put_uint8_t(buf, 34, frame); + _mav_put_uint8_t(buf, 35, current); + _mav_put_uint8_t(buf, 36, autocontinue); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_ITEM, buf, MAVLINK_MSG_ID_MISSION_ITEM_LEN, MAVLINK_MSG_ID_MISSION_ITEM_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_ITEM, buf, MAVLINK_MSG_ID_MISSION_ITEM_LEN); +#endif +#else + mavlink_mission_item_t *packet = (mavlink_mission_item_t *)msgbuf; + packet->param1 = param1; + packet->param2 = param2; + packet->param3 = param3; + packet->param4 = param4; + packet->x = x; + packet->y = y; + packet->z = z; + packet->seq = seq; + packet->command = command; + packet->target_system = target_system; + packet->target_component = target_component; + packet->frame = frame; + packet->current = current; + packet->autocontinue = autocontinue; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_ITEM, (const char *)packet, MAVLINK_MSG_ID_MISSION_ITEM_LEN, MAVLINK_MSG_ID_MISSION_ITEM_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_ITEM, (const char *)packet, MAVLINK_MSG_ID_MISSION_ITEM_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MISSION_ITEM UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_item_reached.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_item_reached.h index f3744fde6..9dfa28043 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_item_reached.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_item_reached.h @@ -146,6 +146,38 @@ static inline void mavlink_msg_mission_item_reached_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_MISSION_ITEM_REACHED_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mission_item_reached_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t seq) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, seq); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_ITEM_REACHED, buf, MAVLINK_MSG_ID_MISSION_ITEM_REACHED_LEN, MAVLINK_MSG_ID_MISSION_ITEM_REACHED_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_ITEM_REACHED, buf, MAVLINK_MSG_ID_MISSION_ITEM_REACHED_LEN); +#endif +#else + mavlink_mission_item_reached_t *packet = (mavlink_mission_item_reached_t *)msgbuf; + packet->seq = seq; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_ITEM_REACHED, (const char *)packet, MAVLINK_MSG_ID_MISSION_ITEM_REACHED_LEN, MAVLINK_MSG_ID_MISSION_ITEM_REACHED_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_ITEM_REACHED, (const char *)packet, MAVLINK_MSG_ID_MISSION_ITEM_REACHED_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MISSION_ITEM_REACHED UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_request.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_request.h index ac84e3554..29b0ef6ef 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_request.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_request.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_mission_request_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_MISSION_REQUEST_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mission_request_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint16_t seq) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, seq); + _mav_put_uint8_t(buf, 2, target_system); + _mav_put_uint8_t(buf, 3, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_REQUEST, buf, MAVLINK_MSG_ID_MISSION_REQUEST_LEN, MAVLINK_MSG_ID_MISSION_REQUEST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_REQUEST, buf, MAVLINK_MSG_ID_MISSION_REQUEST_LEN); +#endif +#else + mavlink_mission_request_t *packet = (mavlink_mission_request_t *)msgbuf; + packet->seq = seq; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_REQUEST, (const char *)packet, MAVLINK_MSG_ID_MISSION_REQUEST_LEN, MAVLINK_MSG_ID_MISSION_REQUEST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_REQUEST, (const char *)packet, MAVLINK_MSG_ID_MISSION_REQUEST_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MISSION_REQUEST UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_request_list.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_request_list.h index d999babdb..a275348ac 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_request_list.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_request_list.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_mission_request_list_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_MISSION_REQUEST_LIST_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mission_request_list_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_REQUEST_LIST, buf, MAVLINK_MSG_ID_MISSION_REQUEST_LIST_LEN, MAVLINK_MSG_ID_MISSION_REQUEST_LIST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_REQUEST_LIST, buf, MAVLINK_MSG_ID_MISSION_REQUEST_LIST_LEN); +#endif +#else + mavlink_mission_request_list_t *packet = (mavlink_mission_request_list_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_REQUEST_LIST, (const char *)packet, MAVLINK_MSG_ID_MISSION_REQUEST_LIST_LEN, MAVLINK_MSG_ID_MISSION_REQUEST_LIST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_REQUEST_LIST, (const char *)packet, MAVLINK_MSG_ID_MISSION_REQUEST_LIST_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MISSION_REQUEST_LIST UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_request_partial_list.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_request_partial_list.h index 35c7e1285..79a88dc08 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_request_partial_list.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_request_partial_list.h @@ -179,6 +179,44 @@ static inline void mavlink_msg_mission_request_partial_list_send(mavlink_channel #endif } +#if MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mission_request_partial_list_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, int16_t start_index, int16_t end_index) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int16_t(buf, 0, start_index); + _mav_put_int16_t(buf, 2, end_index); + _mav_put_uint8_t(buf, 4, target_system); + _mav_put_uint8_t(buf, 5, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST, buf, MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST_LEN, MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST, buf, MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST_LEN); +#endif +#else + mavlink_mission_request_partial_list_t *packet = (mavlink_mission_request_partial_list_t *)msgbuf; + packet->start_index = start_index; + packet->end_index = end_index; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST, (const char *)packet, MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST_LEN, MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST, (const char *)packet, MAVLINK_MSG_ID_MISSION_REQUEST_PARTIAL_LIST_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MISSION_REQUEST_PARTIAL_LIST UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_set_current.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_set_current.h index 63b37cf8c..0c2a3ada4 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_set_current.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_set_current.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_mission_set_current_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_MISSION_SET_CURRENT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mission_set_current_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint16_t seq) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, seq); + _mav_put_uint8_t(buf, 2, target_system); + _mav_put_uint8_t(buf, 3, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_SET_CURRENT, buf, MAVLINK_MSG_ID_MISSION_SET_CURRENT_LEN, MAVLINK_MSG_ID_MISSION_SET_CURRENT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_SET_CURRENT, buf, MAVLINK_MSG_ID_MISSION_SET_CURRENT_LEN); +#endif +#else + mavlink_mission_set_current_t *packet = (mavlink_mission_set_current_t *)msgbuf; + packet->seq = seq; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_SET_CURRENT, (const char *)packet, MAVLINK_MSG_ID_MISSION_SET_CURRENT_LEN, MAVLINK_MSG_ID_MISSION_SET_CURRENT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_SET_CURRENT, (const char *)packet, MAVLINK_MSG_ID_MISSION_SET_CURRENT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MISSION_SET_CURRENT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_write_partial_list.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_write_partial_list.h index 7de38bd7b..17a5a6bdd 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_write_partial_list.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_mission_write_partial_list.h @@ -179,6 +179,44 @@ static inline void mavlink_msg_mission_write_partial_list_send(mavlink_channel_t #endif } +#if MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_mission_write_partial_list_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, int16_t start_index, int16_t end_index) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int16_t(buf, 0, start_index); + _mav_put_int16_t(buf, 2, end_index); + _mav_put_uint8_t(buf, 4, target_system); + _mav_put_uint8_t(buf, 5, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST, buf, MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST_LEN, MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST, buf, MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST_LEN); +#endif +#else + mavlink_mission_write_partial_list_t *packet = (mavlink_mission_write_partial_list_t *)msgbuf; + packet->start_index = start_index; + packet->end_index = end_index; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST, (const char *)packet, MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST_LEN, MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST, (const char *)packet, MAVLINK_MSG_ID_MISSION_WRITE_PARTIAL_LIST_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MISSION_WRITE_PARTIAL_LIST UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_named_value_float.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_named_value_float.h index fbf4f75c9..df82704a4 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_named_value_float.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_named_value_float.h @@ -162,6 +162,40 @@ static inline void mavlink_msg_named_value_float_send(mavlink_channel_t chan, ui #endif } +#if MAVLINK_MSG_ID_NAMED_VALUE_FLOAT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_named_value_float_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, const char *name, float value) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_float(buf, 4, value); + _mav_put_char_array(buf, 8, name, 10); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT, buf, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT_LEN, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT, buf, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT_LEN); +#endif +#else + mavlink_named_value_float_t *packet = (mavlink_named_value_float_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->value = value; + mav_array_memcpy(packet->name, name, sizeof(char)*10); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT, (const char *)packet, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT_LEN, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT, (const char *)packet, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE NAMED_VALUE_FLOAT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_named_value_int.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_named_value_int.h index 052f24793..cfdd73d61 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_named_value_int.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_named_value_int.h @@ -162,6 +162,40 @@ static inline void mavlink_msg_named_value_int_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_NAMED_VALUE_INT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_named_value_int_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, const char *name, int32_t value) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_int32_t(buf, 4, value); + _mav_put_char_array(buf, 8, name, 10); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_NAMED_VALUE_INT, buf, MAVLINK_MSG_ID_NAMED_VALUE_INT_LEN, MAVLINK_MSG_ID_NAMED_VALUE_INT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_NAMED_VALUE_INT, buf, MAVLINK_MSG_ID_NAMED_VALUE_INT_LEN); +#endif +#else + mavlink_named_value_int_t *packet = (mavlink_named_value_int_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->value = value; + mav_array_memcpy(packet->name, name, sizeof(char)*10); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_NAMED_VALUE_INT, (const char *)packet, MAVLINK_MSG_ID_NAMED_VALUE_INT_LEN, MAVLINK_MSG_ID_NAMED_VALUE_INT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_NAMED_VALUE_INT, (const char *)packet, MAVLINK_MSG_ID_NAMED_VALUE_INT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE NAMED_VALUE_INT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_nav_controller_output.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_nav_controller_output.h index e95c144de..b9a748b22 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_nav_controller_output.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_nav_controller_output.h @@ -223,6 +223,52 @@ static inline void mavlink_msg_nav_controller_output_send(mavlink_channel_t chan #endif } +#if MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_nav_controller_output_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float nav_roll, float nav_pitch, int16_t nav_bearing, int16_t target_bearing, uint16_t wp_dist, float alt_error, float aspd_error, float xtrack_error) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, nav_roll); + _mav_put_float(buf, 4, nav_pitch); + _mav_put_float(buf, 8, alt_error); + _mav_put_float(buf, 12, aspd_error); + _mav_put_float(buf, 16, xtrack_error); + _mav_put_int16_t(buf, 20, nav_bearing); + _mav_put_int16_t(buf, 22, target_bearing); + _mav_put_uint16_t(buf, 24, wp_dist); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT, buf, MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT_LEN, MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT, buf, MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT_LEN); +#endif +#else + mavlink_nav_controller_output_t *packet = (mavlink_nav_controller_output_t *)msgbuf; + packet->nav_roll = nav_roll; + packet->nav_pitch = nav_pitch; + packet->alt_error = alt_error; + packet->aspd_error = aspd_error; + packet->xtrack_error = xtrack_error; + packet->nav_bearing = nav_bearing; + packet->target_bearing = target_bearing; + packet->wp_dist = wp_dist; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT, (const char *)packet, MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT_LEN, MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT, (const char *)packet, MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE NAV_CONTROLLER_OUTPUT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_omnidirectional_flow.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_omnidirectional_flow.h index 4debb6e66..4ee9c452f 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_omnidirectional_flow.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_omnidirectional_flow.h @@ -196,6 +196,46 @@ static inline void mavlink_msg_omnidirectional_flow_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_OMNIDIRECTIONAL_FLOW_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_omnidirectional_flow_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, uint8_t sensor_id, const int16_t *left, const int16_t *right, uint8_t quality, float front_distance_m) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_float(buf, 8, front_distance_m); + _mav_put_uint8_t(buf, 52, sensor_id); + _mav_put_uint8_t(buf, 53, quality); + _mav_put_int16_t_array(buf, 12, left, 10); + _mav_put_int16_t_array(buf, 32, right, 10); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OMNIDIRECTIONAL_FLOW, buf, MAVLINK_MSG_ID_OMNIDIRECTIONAL_FLOW_LEN, MAVLINK_MSG_ID_OMNIDIRECTIONAL_FLOW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OMNIDIRECTIONAL_FLOW, buf, MAVLINK_MSG_ID_OMNIDIRECTIONAL_FLOW_LEN); +#endif +#else + mavlink_omnidirectional_flow_t *packet = (mavlink_omnidirectional_flow_t *)msgbuf; + packet->time_usec = time_usec; + packet->front_distance_m = front_distance_m; + packet->sensor_id = sensor_id; + packet->quality = quality; + mav_array_memcpy(packet->left, left, sizeof(int16_t)*10); + mav_array_memcpy(packet->right, right, sizeof(int16_t)*10); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OMNIDIRECTIONAL_FLOW, (const char *)packet, MAVLINK_MSG_ID_OMNIDIRECTIONAL_FLOW_LEN, MAVLINK_MSG_ID_OMNIDIRECTIONAL_FLOW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OMNIDIRECTIONAL_FLOW, (const char *)packet, MAVLINK_MSG_ID_OMNIDIRECTIONAL_FLOW_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE OMNIDIRECTIONAL_FLOW UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_optical_flow.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_optical_flow.h index cf6db9147..6a2efc664 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_optical_flow.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_optical_flow.h @@ -223,6 +223,52 @@ static inline void mavlink_msg_optical_flow_send(mavlink_channel_t chan, uint64_ #endif } +#if MAVLINK_MSG_ID_OPTICAL_FLOW_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_optical_flow_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, uint8_t sensor_id, int16_t flow_x, int16_t flow_y, float flow_comp_m_x, float flow_comp_m_y, uint8_t quality, float ground_distance) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_float(buf, 8, flow_comp_m_x); + _mav_put_float(buf, 12, flow_comp_m_y); + _mav_put_float(buf, 16, ground_distance); + _mav_put_int16_t(buf, 20, flow_x); + _mav_put_int16_t(buf, 22, flow_y); + _mav_put_uint8_t(buf, 24, sensor_id); + _mav_put_uint8_t(buf, 25, quality); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OPTICAL_FLOW, buf, MAVLINK_MSG_ID_OPTICAL_FLOW_LEN, MAVLINK_MSG_ID_OPTICAL_FLOW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OPTICAL_FLOW, buf, MAVLINK_MSG_ID_OPTICAL_FLOW_LEN); +#endif +#else + mavlink_optical_flow_t *packet = (mavlink_optical_flow_t *)msgbuf; + packet->time_usec = time_usec; + packet->flow_comp_m_x = flow_comp_m_x; + packet->flow_comp_m_y = flow_comp_m_y; + packet->ground_distance = ground_distance; + packet->flow_x = flow_x; + packet->flow_y = flow_y; + packet->sensor_id = sensor_id; + packet->quality = quality; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OPTICAL_FLOW, (const char *)packet, MAVLINK_MSG_ID_OPTICAL_FLOW_LEN, MAVLINK_MSG_ID_OPTICAL_FLOW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OPTICAL_FLOW, (const char *)packet, MAVLINK_MSG_ID_OPTICAL_FLOW_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE OPTICAL_FLOW UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_request_list.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_request_list.h index 39e007274..f9466b002 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_request_list.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_request_list.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_param_request_list_send(mavlink_channel_t chan, u #endif } +#if MAVLINK_MSG_ID_PARAM_REQUEST_LIST_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_param_request_list_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_REQUEST_LIST, buf, MAVLINK_MSG_ID_PARAM_REQUEST_LIST_LEN, MAVLINK_MSG_ID_PARAM_REQUEST_LIST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_REQUEST_LIST, buf, MAVLINK_MSG_ID_PARAM_REQUEST_LIST_LEN); +#endif +#else + mavlink_param_request_list_t *packet = (mavlink_param_request_list_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_REQUEST_LIST, (const char *)packet, MAVLINK_MSG_ID_PARAM_REQUEST_LIST_LEN, MAVLINK_MSG_ID_PARAM_REQUEST_LIST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_REQUEST_LIST, (const char *)packet, MAVLINK_MSG_ID_PARAM_REQUEST_LIST_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE PARAM_REQUEST_LIST UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_request_read.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_request_read.h index 5d9113114..730cff066 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_request_read.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_request_read.h @@ -173,6 +173,42 @@ static inline void mavlink_msg_param_request_read_send(mavlink_channel_t chan, u #endif } +#if MAVLINK_MSG_ID_PARAM_REQUEST_READ_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_param_request_read_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, const char *param_id, int16_t param_index) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int16_t(buf, 0, param_index); + _mav_put_uint8_t(buf, 2, target_system); + _mav_put_uint8_t(buf, 3, target_component); + _mav_put_char_array(buf, 4, param_id, 16); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_REQUEST_READ, buf, MAVLINK_MSG_ID_PARAM_REQUEST_READ_LEN, MAVLINK_MSG_ID_PARAM_REQUEST_READ_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_REQUEST_READ, buf, MAVLINK_MSG_ID_PARAM_REQUEST_READ_LEN); +#endif +#else + mavlink_param_request_read_t *packet = (mavlink_param_request_read_t *)msgbuf; + packet->param_index = param_index; + packet->target_system = target_system; + packet->target_component = target_component; + mav_array_memcpy(packet->param_id, param_id, sizeof(char)*16); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_REQUEST_READ, (const char *)packet, MAVLINK_MSG_ID_PARAM_REQUEST_READ_LEN, MAVLINK_MSG_ID_PARAM_REQUEST_READ_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_REQUEST_READ, (const char *)packet, MAVLINK_MSG_ID_PARAM_REQUEST_READ_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE PARAM_REQUEST_READ UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_set.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_set.h index 1bd1f0059..f669af1a2 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_set.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_set.h @@ -184,6 +184,44 @@ static inline void mavlink_msg_param_set_send(mavlink_channel_t chan, uint8_t ta #endif } +#if MAVLINK_MSG_ID_PARAM_SET_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_param_set_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, const char *param_id, float param_value, uint8_t param_type) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, param_value); + _mav_put_uint8_t(buf, 4, target_system); + _mav_put_uint8_t(buf, 5, target_component); + _mav_put_uint8_t(buf, 22, param_type); + _mav_put_char_array(buf, 6, param_id, 16); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_SET, buf, MAVLINK_MSG_ID_PARAM_SET_LEN, MAVLINK_MSG_ID_PARAM_SET_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_SET, buf, MAVLINK_MSG_ID_PARAM_SET_LEN); +#endif +#else + mavlink_param_set_t *packet = (mavlink_param_set_t *)msgbuf; + packet->param_value = param_value; + packet->target_system = target_system; + packet->target_component = target_component; + packet->param_type = param_type; + mav_array_memcpy(packet->param_id, param_id, sizeof(char)*16); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_SET, (const char *)packet, MAVLINK_MSG_ID_PARAM_SET_LEN, MAVLINK_MSG_ID_PARAM_SET_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_SET, (const char *)packet, MAVLINK_MSG_ID_PARAM_SET_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE PARAM_SET UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_value.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_value.h index 17c759811..c27957913 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_value.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_param_value.h @@ -184,6 +184,44 @@ static inline void mavlink_msg_param_value_send(mavlink_channel_t chan, const ch #endif } +#if MAVLINK_MSG_ID_PARAM_VALUE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_param_value_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, const char *param_id, float param_value, uint8_t param_type, uint16_t param_count, uint16_t param_index) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, param_value); + _mav_put_uint16_t(buf, 4, param_count); + _mav_put_uint16_t(buf, 6, param_index); + _mav_put_uint8_t(buf, 24, param_type); + _mav_put_char_array(buf, 8, param_id, 16); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_VALUE, buf, MAVLINK_MSG_ID_PARAM_VALUE_LEN, MAVLINK_MSG_ID_PARAM_VALUE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_VALUE, buf, MAVLINK_MSG_ID_PARAM_VALUE_LEN); +#endif +#else + mavlink_param_value_t *packet = (mavlink_param_value_t *)msgbuf; + packet->param_value = param_value; + packet->param_count = param_count; + packet->param_index = param_index; + packet->param_type = param_type; + mav_array_memcpy(packet->param_id, param_id, sizeof(char)*16); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_VALUE, (const char *)packet, MAVLINK_MSG_ID_PARAM_VALUE_LEN, MAVLINK_MSG_ID_PARAM_VALUE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PARAM_VALUE, (const char *)packet, MAVLINK_MSG_ID_PARAM_VALUE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE PARAM_VALUE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_ping.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_ping.h index 0c68ca176..b1501ba1f 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_ping.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_ping.h @@ -179,6 +179,44 @@ static inline void mavlink_msg_ping_send(mavlink_channel_t chan, uint64_t time_u #endif } +#if MAVLINK_MSG_ID_PING_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_ping_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, uint32_t seq, uint8_t target_system, uint8_t target_component) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_uint32_t(buf, 8, seq); + _mav_put_uint8_t(buf, 12, target_system); + _mav_put_uint8_t(buf, 13, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PING, buf, MAVLINK_MSG_ID_PING_LEN, MAVLINK_MSG_ID_PING_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PING, buf, MAVLINK_MSG_ID_PING_LEN); +#endif +#else + mavlink_ping_t *packet = (mavlink_ping_t *)msgbuf; + packet->time_usec = time_usec; + packet->seq = seq; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PING, (const char *)packet, MAVLINK_MSG_ID_PING_LEN, MAVLINK_MSG_ID_PING_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PING, (const char *)packet, MAVLINK_MSG_ID_PING_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE PING UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_power_status.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_power_status.h new file mode 100644 index 000000000..1a6259aa3 --- /dev/null +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_power_status.h @@ -0,0 +1,257 @@ +// MESSAGE POWER_STATUS PACKING + +#define MAVLINK_MSG_ID_POWER_STATUS 125 + +typedef struct __mavlink_power_status_t +{ + uint16_t Vcc; ///< 5V rail voltage in millivolts + uint16_t Vservo; ///< servo rail voltage in millivolts + uint16_t flags; ///< power supply status flags (see MAV_POWER_STATUS enum) +} mavlink_power_status_t; + +#define MAVLINK_MSG_ID_POWER_STATUS_LEN 6 +#define MAVLINK_MSG_ID_125_LEN 6 + +#define MAVLINK_MSG_ID_POWER_STATUS_CRC 203 +#define MAVLINK_MSG_ID_125_CRC 203 + + + +#define MAVLINK_MESSAGE_INFO_POWER_STATUS { \ + "POWER_STATUS", \ + 3, \ + { { "Vcc", NULL, MAVLINK_TYPE_UINT16_T, 0, 0, offsetof(mavlink_power_status_t, Vcc) }, \ + { "Vservo", NULL, MAVLINK_TYPE_UINT16_T, 0, 2, offsetof(mavlink_power_status_t, Vservo) }, \ + { "flags", NULL, MAVLINK_TYPE_UINT16_T, 0, 4, offsetof(mavlink_power_status_t, flags) }, \ + } \ +} + + +/** + * @brief Pack a power_status message + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param msg The MAVLink message to compress the data into + * + * @param Vcc 5V rail voltage in millivolts + * @param Vservo servo rail voltage in millivolts + * @param flags power supply status flags (see MAV_POWER_STATUS enum) + * @return length of the message in bytes (excluding serial stream start sign) + */ +static inline uint16_t mavlink_msg_power_status_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, + uint16_t Vcc, uint16_t Vservo, uint16_t flags) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_POWER_STATUS_LEN]; + _mav_put_uint16_t(buf, 0, Vcc); + _mav_put_uint16_t(buf, 2, Vservo); + _mav_put_uint16_t(buf, 4, flags); + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_POWER_STATUS_LEN); +#else + mavlink_power_status_t packet; + packet.Vcc = Vcc; + packet.Vservo = Vservo; + packet.flags = flags; + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_POWER_STATUS_LEN); +#endif + + msg->msgid = MAVLINK_MSG_ID_POWER_STATUS; +#if MAVLINK_CRC_EXTRA + return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_POWER_STATUS_LEN, MAVLINK_MSG_ID_POWER_STATUS_CRC); +#else + return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_POWER_STATUS_LEN); +#endif +} + +/** + * @brief Pack a power_status message on a channel + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param chan The MAVLink channel this message will be sent over + * @param msg The MAVLink message to compress the data into + * @param Vcc 5V rail voltage in millivolts + * @param Vservo servo rail voltage in millivolts + * @param flags power supply status flags (see MAV_POWER_STATUS enum) + * @return length of the message in bytes (excluding serial stream start sign) + */ +static inline uint16_t mavlink_msg_power_status_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, + mavlink_message_t* msg, + uint16_t Vcc,uint16_t Vservo,uint16_t flags) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_POWER_STATUS_LEN]; + _mav_put_uint16_t(buf, 0, Vcc); + _mav_put_uint16_t(buf, 2, Vservo); + _mav_put_uint16_t(buf, 4, flags); + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_POWER_STATUS_LEN); +#else + mavlink_power_status_t packet; + packet.Vcc = Vcc; + packet.Vservo = Vservo; + packet.flags = flags; + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_POWER_STATUS_LEN); +#endif + + msg->msgid = MAVLINK_MSG_ID_POWER_STATUS; +#if MAVLINK_CRC_EXTRA + return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_POWER_STATUS_LEN, MAVLINK_MSG_ID_POWER_STATUS_CRC); +#else + return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_POWER_STATUS_LEN); +#endif +} + +/** + * @brief Encode a power_status struct + * + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param msg The MAVLink message to compress the data into + * @param power_status C-struct to read the message contents from + */ +static inline uint16_t mavlink_msg_power_status_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_power_status_t* power_status) +{ + return mavlink_msg_power_status_pack(system_id, component_id, msg, power_status->Vcc, power_status->Vservo, power_status->flags); +} + +/** + * @brief Encode a power_status struct on a channel + * + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param chan The MAVLink channel this message will be sent over + * @param msg The MAVLink message to compress the data into + * @param power_status C-struct to read the message contents from + */ +static inline uint16_t mavlink_msg_power_status_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_power_status_t* power_status) +{ + return mavlink_msg_power_status_pack_chan(system_id, component_id, chan, msg, power_status->Vcc, power_status->Vservo, power_status->flags); +} + +/** + * @brief Send a power_status message + * @param chan MAVLink channel to send the message + * + * @param Vcc 5V rail voltage in millivolts + * @param Vservo servo rail voltage in millivolts + * @param flags power supply status flags (see MAV_POWER_STATUS enum) + */ +#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS + +static inline void mavlink_msg_power_status_send(mavlink_channel_t chan, uint16_t Vcc, uint16_t Vservo, uint16_t flags) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_POWER_STATUS_LEN]; + _mav_put_uint16_t(buf, 0, Vcc); + _mav_put_uint16_t(buf, 2, Vservo); + _mav_put_uint16_t(buf, 4, flags); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POWER_STATUS, buf, MAVLINK_MSG_ID_POWER_STATUS_LEN, MAVLINK_MSG_ID_POWER_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POWER_STATUS, buf, MAVLINK_MSG_ID_POWER_STATUS_LEN); +#endif +#else + mavlink_power_status_t packet; + packet.Vcc = Vcc; + packet.Vservo = Vservo; + packet.flags = flags; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POWER_STATUS, (const char *)&packet, MAVLINK_MSG_ID_POWER_STATUS_LEN, MAVLINK_MSG_ID_POWER_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POWER_STATUS, (const char *)&packet, MAVLINK_MSG_ID_POWER_STATUS_LEN); +#endif +#endif +} + +#if MAVLINK_MSG_ID_POWER_STATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_power_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t Vcc, uint16_t Vservo, uint16_t flags) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, Vcc); + _mav_put_uint16_t(buf, 2, Vservo); + _mav_put_uint16_t(buf, 4, flags); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POWER_STATUS, buf, MAVLINK_MSG_ID_POWER_STATUS_LEN, MAVLINK_MSG_ID_POWER_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POWER_STATUS, buf, MAVLINK_MSG_ID_POWER_STATUS_LEN); +#endif +#else + mavlink_power_status_t *packet = (mavlink_power_status_t *)msgbuf; + packet->Vcc = Vcc; + packet->Vservo = Vservo; + packet->flags = flags; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POWER_STATUS, (const char *)packet, MAVLINK_MSG_ID_POWER_STATUS_LEN, MAVLINK_MSG_ID_POWER_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POWER_STATUS, (const char *)packet, MAVLINK_MSG_ID_POWER_STATUS_LEN); +#endif +#endif +} +#endif + +#endif + +// MESSAGE POWER_STATUS UNPACKING + + +/** + * @brief Get field Vcc from power_status message + * + * @return 5V rail voltage in millivolts + */ +static inline uint16_t mavlink_msg_power_status_get_Vcc(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 0); +} + +/** + * @brief Get field Vservo from power_status message + * + * @return servo rail voltage in millivolts + */ +static inline uint16_t mavlink_msg_power_status_get_Vservo(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 2); +} + +/** + * @brief Get field flags from power_status message + * + * @return power supply status flags (see MAV_POWER_STATUS enum) + */ +static inline uint16_t mavlink_msg_power_status_get_flags(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 4); +} + +/** + * @brief Decode a power_status message into a struct + * + * @param msg The message to decode + * @param power_status C-struct to decode the message contents into + */ +static inline void mavlink_msg_power_status_decode(const mavlink_message_t* msg, mavlink_power_status_t* power_status) +{ +#if MAVLINK_NEED_BYTE_SWAP + power_status->Vcc = mavlink_msg_power_status_get_Vcc(msg); + power_status->Vservo = mavlink_msg_power_status_get_Vservo(msg); + power_status->flags = mavlink_msg_power_status_get_flags(msg); +#else + memcpy(power_status, _MAV_PAYLOAD(msg), MAVLINK_MSG_ID_POWER_STATUS_LEN); +#endif +} diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_radio_status.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_radio_status.h index fceb7d168..5763008fe 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_radio_status.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_radio_status.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_radio_status_send(mavlink_channel_t chan, uint8_t #endif } +#if MAVLINK_MSG_ID_RADIO_STATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_radio_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t rssi, uint8_t remrssi, uint8_t txbuf, uint8_t noise, uint8_t remnoise, uint16_t rxerrors, uint16_t fixed) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, rxerrors); + _mav_put_uint16_t(buf, 2, fixed); + _mav_put_uint8_t(buf, 4, rssi); + _mav_put_uint8_t(buf, 5, remrssi); + _mav_put_uint8_t(buf, 6, txbuf); + _mav_put_uint8_t(buf, 7, noise); + _mav_put_uint8_t(buf, 8, remnoise); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO_STATUS, buf, MAVLINK_MSG_ID_RADIO_STATUS_LEN, MAVLINK_MSG_ID_RADIO_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO_STATUS, buf, MAVLINK_MSG_ID_RADIO_STATUS_LEN); +#endif +#else + mavlink_radio_status_t *packet = (mavlink_radio_status_t *)msgbuf; + packet->rxerrors = rxerrors; + packet->fixed = fixed; + packet->rssi = rssi; + packet->remrssi = remrssi; + packet->txbuf = txbuf; + packet->noise = noise; + packet->remnoise = remnoise; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO_STATUS, (const char *)packet, MAVLINK_MSG_ID_RADIO_STATUS_LEN, MAVLINK_MSG_ID_RADIO_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO_STATUS, (const char *)packet, MAVLINK_MSG_ID_RADIO_STATUS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE RADIO_STATUS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_raw_imu.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_raw_imu.h index 62a9b6eea..a98e8ce72 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_raw_imu.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_raw_imu.h @@ -245,6 +245,56 @@ static inline void mavlink_msg_raw_imu_send(mavlink_channel_t chan, uint64_t tim #endif } +#if MAVLINK_MSG_ID_RAW_IMU_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_raw_imu_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, int16_t xacc, int16_t yacc, int16_t zacc, int16_t xgyro, int16_t ygyro, int16_t zgyro, int16_t xmag, int16_t ymag, int16_t zmag) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_int16_t(buf, 8, xacc); + _mav_put_int16_t(buf, 10, yacc); + _mav_put_int16_t(buf, 12, zacc); + _mav_put_int16_t(buf, 14, xgyro); + _mav_put_int16_t(buf, 16, ygyro); + _mav_put_int16_t(buf, 18, zgyro); + _mav_put_int16_t(buf, 20, xmag); + _mav_put_int16_t(buf, 22, ymag); + _mav_put_int16_t(buf, 24, zmag); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RAW_IMU, buf, MAVLINK_MSG_ID_RAW_IMU_LEN, MAVLINK_MSG_ID_RAW_IMU_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RAW_IMU, buf, MAVLINK_MSG_ID_RAW_IMU_LEN); +#endif +#else + mavlink_raw_imu_t *packet = (mavlink_raw_imu_t *)msgbuf; + packet->time_usec = time_usec; + packet->xacc = xacc; + packet->yacc = yacc; + packet->zacc = zacc; + packet->xgyro = xgyro; + packet->ygyro = ygyro; + packet->zgyro = zgyro; + packet->xmag = xmag; + packet->ymag = ymag; + packet->zmag = zmag; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RAW_IMU, (const char *)packet, MAVLINK_MSG_ID_RAW_IMU_LEN, MAVLINK_MSG_ID_RAW_IMU_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RAW_IMU, (const char *)packet, MAVLINK_MSG_ID_RAW_IMU_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE RAW_IMU UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_raw_pressure.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_raw_pressure.h index 82c5fad4a..6bd37fcae 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_raw_pressure.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_raw_pressure.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_raw_pressure_send(mavlink_channel_t chan, uint64_ #endif } +#if MAVLINK_MSG_ID_RAW_PRESSURE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_raw_pressure_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, int16_t press_abs, int16_t press_diff1, int16_t press_diff2, int16_t temperature) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_usec); + _mav_put_int16_t(buf, 8, press_abs); + _mav_put_int16_t(buf, 10, press_diff1); + _mav_put_int16_t(buf, 12, press_diff2); + _mav_put_int16_t(buf, 14, temperature); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RAW_PRESSURE, buf, MAVLINK_MSG_ID_RAW_PRESSURE_LEN, MAVLINK_MSG_ID_RAW_PRESSURE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RAW_PRESSURE, buf, MAVLINK_MSG_ID_RAW_PRESSURE_LEN); +#endif +#else + mavlink_raw_pressure_t *packet = (mavlink_raw_pressure_t *)msgbuf; + packet->time_usec = time_usec; + packet->press_abs = press_abs; + packet->press_diff1 = press_diff1; + packet->press_diff2 = press_diff2; + packet->temperature = temperature; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RAW_PRESSURE, (const char *)packet, MAVLINK_MSG_ID_RAW_PRESSURE_LEN, MAVLINK_MSG_ID_RAW_PRESSURE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RAW_PRESSURE, (const char *)packet, MAVLINK_MSG_ID_RAW_PRESSURE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE RAW_PRESSURE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels.h new file mode 100644 index 000000000..479af122f --- /dev/null +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels.h @@ -0,0 +1,689 @@ +// MESSAGE RC_CHANNELS PACKING + +#define MAVLINK_MSG_ID_RC_CHANNELS 65 + +typedef struct __mavlink_rc_channels_t +{ + uint32_t time_boot_ms; ///< Timestamp (milliseconds since system boot) + uint16_t chan1_raw; ///< RC channel 1 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan2_raw; ///< RC channel 2 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan3_raw; ///< RC channel 3 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan4_raw; ///< RC channel 4 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan5_raw; ///< RC channel 5 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan6_raw; ///< RC channel 6 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan7_raw; ///< RC channel 7 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan8_raw; ///< RC channel 8 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan9_raw; ///< RC channel 9 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan10_raw; ///< RC channel 10 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan11_raw; ///< RC channel 11 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan12_raw; ///< RC channel 12 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan13_raw; ///< RC channel 13 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan14_raw; ///< RC channel 14 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan15_raw; ///< RC channel 15 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan16_raw; ///< RC channel 16 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan17_raw; ///< RC channel 17 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint16_t chan18_raw; ///< RC channel 18 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + uint8_t chancount; ///< Total number of RC channels being received. This can be larger than 18, indicating that more channels are available but not given in this message. This value should be 0 when no RC channels are available. + uint8_t rssi; ///< Receive signal strength indicator, 0: 0%, 100: 100%, 255: invalid/unknown. +} mavlink_rc_channels_t; + +#define MAVLINK_MSG_ID_RC_CHANNELS_LEN 42 +#define MAVLINK_MSG_ID_65_LEN 42 + +#define MAVLINK_MSG_ID_RC_CHANNELS_CRC 118 +#define MAVLINK_MSG_ID_65_CRC 118 + + + +#define MAVLINK_MESSAGE_INFO_RC_CHANNELS { \ + "RC_CHANNELS", \ + 21, \ + { { "time_boot_ms", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_rc_channels_t, time_boot_ms) }, \ + { "chan1_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 4, offsetof(mavlink_rc_channels_t, chan1_raw) }, \ + { "chan2_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 6, offsetof(mavlink_rc_channels_t, chan2_raw) }, \ + { "chan3_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 8, offsetof(mavlink_rc_channels_t, chan3_raw) }, \ + { "chan4_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 10, offsetof(mavlink_rc_channels_t, chan4_raw) }, \ + { "chan5_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 12, offsetof(mavlink_rc_channels_t, chan5_raw) }, \ + { "chan6_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 14, offsetof(mavlink_rc_channels_t, chan6_raw) }, \ + { "chan7_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 16, offsetof(mavlink_rc_channels_t, chan7_raw) }, \ + { "chan8_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 18, offsetof(mavlink_rc_channels_t, chan8_raw) }, \ + { "chan9_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 20, offsetof(mavlink_rc_channels_t, chan9_raw) }, \ + { "chan10_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 22, offsetof(mavlink_rc_channels_t, chan10_raw) }, \ + { "chan11_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 24, offsetof(mavlink_rc_channels_t, chan11_raw) }, \ + { "chan12_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 26, offsetof(mavlink_rc_channels_t, chan12_raw) }, \ + { "chan13_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 28, offsetof(mavlink_rc_channels_t, chan13_raw) }, \ + { "chan14_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 30, offsetof(mavlink_rc_channels_t, chan14_raw) }, \ + { "chan15_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 32, offsetof(mavlink_rc_channels_t, chan15_raw) }, \ + { "chan16_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 34, offsetof(mavlink_rc_channels_t, chan16_raw) }, \ + { "chan17_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 36, offsetof(mavlink_rc_channels_t, chan17_raw) }, \ + { "chan18_raw", NULL, MAVLINK_TYPE_UINT16_T, 0, 38, offsetof(mavlink_rc_channels_t, chan18_raw) }, \ + { "chancount", NULL, MAVLINK_TYPE_UINT8_T, 0, 40, offsetof(mavlink_rc_channels_t, chancount) }, \ + { "rssi", NULL, MAVLINK_TYPE_UINT8_T, 0, 41, offsetof(mavlink_rc_channels_t, rssi) }, \ + } \ +} + + +/** + * @brief Pack a rc_channels message + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param msg The MAVLink message to compress the data into + * + * @param time_boot_ms Timestamp (milliseconds since system boot) + * @param chancount Total number of RC channels being received. This can be larger than 18, indicating that more channels are available but not given in this message. This value should be 0 when no RC channels are available. + * @param chan1_raw RC channel 1 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan2_raw RC channel 2 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan3_raw RC channel 3 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan4_raw RC channel 4 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan5_raw RC channel 5 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan6_raw RC channel 6 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan7_raw RC channel 7 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan8_raw RC channel 8 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan9_raw RC channel 9 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan10_raw RC channel 10 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan11_raw RC channel 11 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan12_raw RC channel 12 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan13_raw RC channel 13 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan14_raw RC channel 14 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan15_raw RC channel 15 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan16_raw RC channel 16 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan17_raw RC channel 17 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan18_raw RC channel 18 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param rssi Receive signal strength indicator, 0: 0%, 100: 100%, 255: invalid/unknown. + * @return length of the message in bytes (excluding serial stream start sign) + */ +static inline uint16_t mavlink_msg_rc_channels_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, + uint32_t time_boot_ms, uint8_t chancount, uint16_t chan1_raw, uint16_t chan2_raw, uint16_t chan3_raw, uint16_t chan4_raw, uint16_t chan5_raw, uint16_t chan6_raw, uint16_t chan7_raw, uint16_t chan8_raw, uint16_t chan9_raw, uint16_t chan10_raw, uint16_t chan11_raw, uint16_t chan12_raw, uint16_t chan13_raw, uint16_t chan14_raw, uint16_t chan15_raw, uint16_t chan16_raw, uint16_t chan17_raw, uint16_t chan18_raw, uint8_t rssi) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_RC_CHANNELS_LEN]; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_uint16_t(buf, 4, chan1_raw); + _mav_put_uint16_t(buf, 6, chan2_raw); + _mav_put_uint16_t(buf, 8, chan3_raw); + _mav_put_uint16_t(buf, 10, chan4_raw); + _mav_put_uint16_t(buf, 12, chan5_raw); + _mav_put_uint16_t(buf, 14, chan6_raw); + _mav_put_uint16_t(buf, 16, chan7_raw); + _mav_put_uint16_t(buf, 18, chan8_raw); + _mav_put_uint16_t(buf, 20, chan9_raw); + _mav_put_uint16_t(buf, 22, chan10_raw); + _mav_put_uint16_t(buf, 24, chan11_raw); + _mav_put_uint16_t(buf, 26, chan12_raw); + _mav_put_uint16_t(buf, 28, chan13_raw); + _mav_put_uint16_t(buf, 30, chan14_raw); + _mav_put_uint16_t(buf, 32, chan15_raw); + _mav_put_uint16_t(buf, 34, chan16_raw); + _mav_put_uint16_t(buf, 36, chan17_raw); + _mav_put_uint16_t(buf, 38, chan18_raw); + _mav_put_uint8_t(buf, 40, chancount); + _mav_put_uint8_t(buf, 41, rssi); + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_RC_CHANNELS_LEN); +#else + mavlink_rc_channels_t packet; + packet.time_boot_ms = time_boot_ms; + packet.chan1_raw = chan1_raw; + packet.chan2_raw = chan2_raw; + packet.chan3_raw = chan3_raw; + packet.chan4_raw = chan4_raw; + packet.chan5_raw = chan5_raw; + packet.chan6_raw = chan6_raw; + packet.chan7_raw = chan7_raw; + packet.chan8_raw = chan8_raw; + packet.chan9_raw = chan9_raw; + packet.chan10_raw = chan10_raw; + packet.chan11_raw = chan11_raw; + packet.chan12_raw = chan12_raw; + packet.chan13_raw = chan13_raw; + packet.chan14_raw = chan14_raw; + packet.chan15_raw = chan15_raw; + packet.chan16_raw = chan16_raw; + packet.chan17_raw = chan17_raw; + packet.chan18_raw = chan18_raw; + packet.chancount = chancount; + packet.rssi = rssi; + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_RC_CHANNELS_LEN); +#endif + + msg->msgid = MAVLINK_MSG_ID_RC_CHANNELS; +#if MAVLINK_CRC_EXTRA + return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_RC_CHANNELS_LEN, MAVLINK_MSG_ID_RC_CHANNELS_CRC); +#else + return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_RC_CHANNELS_LEN); +#endif +} + +/** + * @brief Pack a rc_channels message on a channel + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param chan The MAVLink channel this message will be sent over + * @param msg The MAVLink message to compress the data into + * @param time_boot_ms Timestamp (milliseconds since system boot) + * @param chancount Total number of RC channels being received. This can be larger than 18, indicating that more channels are available but not given in this message. This value should be 0 when no RC channels are available. + * @param chan1_raw RC channel 1 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan2_raw RC channel 2 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan3_raw RC channel 3 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan4_raw RC channel 4 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan5_raw RC channel 5 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan6_raw RC channel 6 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan7_raw RC channel 7 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan8_raw RC channel 8 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan9_raw RC channel 9 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan10_raw RC channel 10 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan11_raw RC channel 11 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan12_raw RC channel 12 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan13_raw RC channel 13 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan14_raw RC channel 14 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan15_raw RC channel 15 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan16_raw RC channel 16 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan17_raw RC channel 17 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan18_raw RC channel 18 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param rssi Receive signal strength indicator, 0: 0%, 100: 100%, 255: invalid/unknown. + * @return length of the message in bytes (excluding serial stream start sign) + */ +static inline uint16_t mavlink_msg_rc_channels_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, + mavlink_message_t* msg, + uint32_t time_boot_ms,uint8_t chancount,uint16_t chan1_raw,uint16_t chan2_raw,uint16_t chan3_raw,uint16_t chan4_raw,uint16_t chan5_raw,uint16_t chan6_raw,uint16_t chan7_raw,uint16_t chan8_raw,uint16_t chan9_raw,uint16_t chan10_raw,uint16_t chan11_raw,uint16_t chan12_raw,uint16_t chan13_raw,uint16_t chan14_raw,uint16_t chan15_raw,uint16_t chan16_raw,uint16_t chan17_raw,uint16_t chan18_raw,uint8_t rssi) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_RC_CHANNELS_LEN]; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_uint16_t(buf, 4, chan1_raw); + _mav_put_uint16_t(buf, 6, chan2_raw); + _mav_put_uint16_t(buf, 8, chan3_raw); + _mav_put_uint16_t(buf, 10, chan4_raw); + _mav_put_uint16_t(buf, 12, chan5_raw); + _mav_put_uint16_t(buf, 14, chan6_raw); + _mav_put_uint16_t(buf, 16, chan7_raw); + _mav_put_uint16_t(buf, 18, chan8_raw); + _mav_put_uint16_t(buf, 20, chan9_raw); + _mav_put_uint16_t(buf, 22, chan10_raw); + _mav_put_uint16_t(buf, 24, chan11_raw); + _mav_put_uint16_t(buf, 26, chan12_raw); + _mav_put_uint16_t(buf, 28, chan13_raw); + _mav_put_uint16_t(buf, 30, chan14_raw); + _mav_put_uint16_t(buf, 32, chan15_raw); + _mav_put_uint16_t(buf, 34, chan16_raw); + _mav_put_uint16_t(buf, 36, chan17_raw); + _mav_put_uint16_t(buf, 38, chan18_raw); + _mav_put_uint8_t(buf, 40, chancount); + _mav_put_uint8_t(buf, 41, rssi); + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_RC_CHANNELS_LEN); +#else + mavlink_rc_channels_t packet; + packet.time_boot_ms = time_boot_ms; + packet.chan1_raw = chan1_raw; + packet.chan2_raw = chan2_raw; + packet.chan3_raw = chan3_raw; + packet.chan4_raw = chan4_raw; + packet.chan5_raw = chan5_raw; + packet.chan6_raw = chan6_raw; + packet.chan7_raw = chan7_raw; + packet.chan8_raw = chan8_raw; + packet.chan9_raw = chan9_raw; + packet.chan10_raw = chan10_raw; + packet.chan11_raw = chan11_raw; + packet.chan12_raw = chan12_raw; + packet.chan13_raw = chan13_raw; + packet.chan14_raw = chan14_raw; + packet.chan15_raw = chan15_raw; + packet.chan16_raw = chan16_raw; + packet.chan17_raw = chan17_raw; + packet.chan18_raw = chan18_raw; + packet.chancount = chancount; + packet.rssi = rssi; + + memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_RC_CHANNELS_LEN); +#endif + + msg->msgid = MAVLINK_MSG_ID_RC_CHANNELS; +#if MAVLINK_CRC_EXTRA + return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_RC_CHANNELS_LEN, MAVLINK_MSG_ID_RC_CHANNELS_CRC); +#else + return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_RC_CHANNELS_LEN); +#endif +} + +/** + * @brief Encode a rc_channels struct + * + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param msg The MAVLink message to compress the data into + * @param rc_channels C-struct to read the message contents from + */ +static inline uint16_t mavlink_msg_rc_channels_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_rc_channels_t* rc_channels) +{ + return mavlink_msg_rc_channels_pack(system_id, component_id, msg, rc_channels->time_boot_ms, rc_channels->chancount, rc_channels->chan1_raw, rc_channels->chan2_raw, rc_channels->chan3_raw, rc_channels->chan4_raw, rc_channels->chan5_raw, rc_channels->chan6_raw, rc_channels->chan7_raw, rc_channels->chan8_raw, rc_channels->chan9_raw, rc_channels->chan10_raw, rc_channels->chan11_raw, rc_channels->chan12_raw, rc_channels->chan13_raw, rc_channels->chan14_raw, rc_channels->chan15_raw, rc_channels->chan16_raw, rc_channels->chan17_raw, rc_channels->chan18_raw, rc_channels->rssi); +} + +/** + * @brief Encode a rc_channels struct on a channel + * + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param chan The MAVLink channel this message will be sent over + * @param msg The MAVLink message to compress the data into + * @param rc_channels C-struct to read the message contents from + */ +static inline uint16_t mavlink_msg_rc_channels_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_rc_channels_t* rc_channels) +{ + return mavlink_msg_rc_channels_pack_chan(system_id, component_id, chan, msg, rc_channels->time_boot_ms, rc_channels->chancount, rc_channels->chan1_raw, rc_channels->chan2_raw, rc_channels->chan3_raw, rc_channels->chan4_raw, rc_channels->chan5_raw, rc_channels->chan6_raw, rc_channels->chan7_raw, rc_channels->chan8_raw, rc_channels->chan9_raw, rc_channels->chan10_raw, rc_channels->chan11_raw, rc_channels->chan12_raw, rc_channels->chan13_raw, rc_channels->chan14_raw, rc_channels->chan15_raw, rc_channels->chan16_raw, rc_channels->chan17_raw, rc_channels->chan18_raw, rc_channels->rssi); +} + +/** + * @brief Send a rc_channels message + * @param chan MAVLink channel to send the message + * + * @param time_boot_ms Timestamp (milliseconds since system boot) + * @param chancount Total number of RC channels being received. This can be larger than 18, indicating that more channels are available but not given in this message. This value should be 0 when no RC channels are available. + * @param chan1_raw RC channel 1 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan2_raw RC channel 2 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan3_raw RC channel 3 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan4_raw RC channel 4 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan5_raw RC channel 5 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan6_raw RC channel 6 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan7_raw RC channel 7 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan8_raw RC channel 8 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan9_raw RC channel 9 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan10_raw RC channel 10 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan11_raw RC channel 11 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan12_raw RC channel 12 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan13_raw RC channel 13 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan14_raw RC channel 14 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan15_raw RC channel 15 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan16_raw RC channel 16 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan17_raw RC channel 17 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param chan18_raw RC channel 18 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + * @param rssi Receive signal strength indicator, 0: 0%, 100: 100%, 255: invalid/unknown. + */ +#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS + +static inline void mavlink_msg_rc_channels_send(mavlink_channel_t chan, uint32_t time_boot_ms, uint8_t chancount, uint16_t chan1_raw, uint16_t chan2_raw, uint16_t chan3_raw, uint16_t chan4_raw, uint16_t chan5_raw, uint16_t chan6_raw, uint16_t chan7_raw, uint16_t chan8_raw, uint16_t chan9_raw, uint16_t chan10_raw, uint16_t chan11_raw, uint16_t chan12_raw, uint16_t chan13_raw, uint16_t chan14_raw, uint16_t chan15_raw, uint16_t chan16_raw, uint16_t chan17_raw, uint16_t chan18_raw, uint8_t rssi) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_RC_CHANNELS_LEN]; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_uint16_t(buf, 4, chan1_raw); + _mav_put_uint16_t(buf, 6, chan2_raw); + _mav_put_uint16_t(buf, 8, chan3_raw); + _mav_put_uint16_t(buf, 10, chan4_raw); + _mav_put_uint16_t(buf, 12, chan5_raw); + _mav_put_uint16_t(buf, 14, chan6_raw); + _mav_put_uint16_t(buf, 16, chan7_raw); + _mav_put_uint16_t(buf, 18, chan8_raw); + _mav_put_uint16_t(buf, 20, chan9_raw); + _mav_put_uint16_t(buf, 22, chan10_raw); + _mav_put_uint16_t(buf, 24, chan11_raw); + _mav_put_uint16_t(buf, 26, chan12_raw); + _mav_put_uint16_t(buf, 28, chan13_raw); + _mav_put_uint16_t(buf, 30, chan14_raw); + _mav_put_uint16_t(buf, 32, chan15_raw); + _mav_put_uint16_t(buf, 34, chan16_raw); + _mav_put_uint16_t(buf, 36, chan17_raw); + _mav_put_uint16_t(buf, 38, chan18_raw); + _mav_put_uint8_t(buf, 40, chancount); + _mav_put_uint8_t(buf, 41, rssi); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS, buf, MAVLINK_MSG_ID_RC_CHANNELS_LEN, MAVLINK_MSG_ID_RC_CHANNELS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS, buf, MAVLINK_MSG_ID_RC_CHANNELS_LEN); +#endif +#else + mavlink_rc_channels_t packet; + packet.time_boot_ms = time_boot_ms; + packet.chan1_raw = chan1_raw; + packet.chan2_raw = chan2_raw; + packet.chan3_raw = chan3_raw; + packet.chan4_raw = chan4_raw; + packet.chan5_raw = chan5_raw; + packet.chan6_raw = chan6_raw; + packet.chan7_raw = chan7_raw; + packet.chan8_raw = chan8_raw; + packet.chan9_raw = chan9_raw; + packet.chan10_raw = chan10_raw; + packet.chan11_raw = chan11_raw; + packet.chan12_raw = chan12_raw; + packet.chan13_raw = chan13_raw; + packet.chan14_raw = chan14_raw; + packet.chan15_raw = chan15_raw; + packet.chan16_raw = chan16_raw; + packet.chan17_raw = chan17_raw; + packet.chan18_raw = chan18_raw; + packet.chancount = chancount; + packet.rssi = rssi; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS, (const char *)&packet, MAVLINK_MSG_ID_RC_CHANNELS_LEN, MAVLINK_MSG_ID_RC_CHANNELS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS, (const char *)&packet, MAVLINK_MSG_ID_RC_CHANNELS_LEN); +#endif +#endif +} + +#if MAVLINK_MSG_ID_RC_CHANNELS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_rc_channels_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, uint8_t chancount, uint16_t chan1_raw, uint16_t chan2_raw, uint16_t chan3_raw, uint16_t chan4_raw, uint16_t chan5_raw, uint16_t chan6_raw, uint16_t chan7_raw, uint16_t chan8_raw, uint16_t chan9_raw, uint16_t chan10_raw, uint16_t chan11_raw, uint16_t chan12_raw, uint16_t chan13_raw, uint16_t chan14_raw, uint16_t chan15_raw, uint16_t chan16_raw, uint16_t chan17_raw, uint16_t chan18_raw, uint8_t rssi) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_uint16_t(buf, 4, chan1_raw); + _mav_put_uint16_t(buf, 6, chan2_raw); + _mav_put_uint16_t(buf, 8, chan3_raw); + _mav_put_uint16_t(buf, 10, chan4_raw); + _mav_put_uint16_t(buf, 12, chan5_raw); + _mav_put_uint16_t(buf, 14, chan6_raw); + _mav_put_uint16_t(buf, 16, chan7_raw); + _mav_put_uint16_t(buf, 18, chan8_raw); + _mav_put_uint16_t(buf, 20, chan9_raw); + _mav_put_uint16_t(buf, 22, chan10_raw); + _mav_put_uint16_t(buf, 24, chan11_raw); + _mav_put_uint16_t(buf, 26, chan12_raw); + _mav_put_uint16_t(buf, 28, chan13_raw); + _mav_put_uint16_t(buf, 30, chan14_raw); + _mav_put_uint16_t(buf, 32, chan15_raw); + _mav_put_uint16_t(buf, 34, chan16_raw); + _mav_put_uint16_t(buf, 36, chan17_raw); + _mav_put_uint16_t(buf, 38, chan18_raw); + _mav_put_uint8_t(buf, 40, chancount); + _mav_put_uint8_t(buf, 41, rssi); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS, buf, MAVLINK_MSG_ID_RC_CHANNELS_LEN, MAVLINK_MSG_ID_RC_CHANNELS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS, buf, MAVLINK_MSG_ID_RC_CHANNELS_LEN); +#endif +#else + mavlink_rc_channels_t *packet = (mavlink_rc_channels_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->chan1_raw = chan1_raw; + packet->chan2_raw = chan2_raw; + packet->chan3_raw = chan3_raw; + packet->chan4_raw = chan4_raw; + packet->chan5_raw = chan5_raw; + packet->chan6_raw = chan6_raw; + packet->chan7_raw = chan7_raw; + packet->chan8_raw = chan8_raw; + packet->chan9_raw = chan9_raw; + packet->chan10_raw = chan10_raw; + packet->chan11_raw = chan11_raw; + packet->chan12_raw = chan12_raw; + packet->chan13_raw = chan13_raw; + packet->chan14_raw = chan14_raw; + packet->chan15_raw = chan15_raw; + packet->chan16_raw = chan16_raw; + packet->chan17_raw = chan17_raw; + packet->chan18_raw = chan18_raw; + packet->chancount = chancount; + packet->rssi = rssi; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS, (const char *)packet, MAVLINK_MSG_ID_RC_CHANNELS_LEN, MAVLINK_MSG_ID_RC_CHANNELS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS, (const char *)packet, MAVLINK_MSG_ID_RC_CHANNELS_LEN); +#endif +#endif +} +#endif + +#endif + +// MESSAGE RC_CHANNELS UNPACKING + + +/** + * @brief Get field time_boot_ms from rc_channels message + * + * @return Timestamp (milliseconds since system boot) + */ +static inline uint32_t mavlink_msg_rc_channels_get_time_boot_ms(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint32_t(msg, 0); +} + +/** + * @brief Get field chancount from rc_channels message + * + * @return Total number of RC channels being received. This can be larger than 18, indicating that more channels are available but not given in this message. This value should be 0 when no RC channels are available. + */ +static inline uint8_t mavlink_msg_rc_channels_get_chancount(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint8_t(msg, 40); +} + +/** + * @brief Get field chan1_raw from rc_channels message + * + * @return RC channel 1 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan1_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 4); +} + +/** + * @brief Get field chan2_raw from rc_channels message + * + * @return RC channel 2 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan2_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 6); +} + +/** + * @brief Get field chan3_raw from rc_channels message + * + * @return RC channel 3 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan3_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 8); +} + +/** + * @brief Get field chan4_raw from rc_channels message + * + * @return RC channel 4 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan4_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 10); +} + +/** + * @brief Get field chan5_raw from rc_channels message + * + * @return RC channel 5 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan5_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 12); +} + +/** + * @brief Get field chan6_raw from rc_channels message + * + * @return RC channel 6 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan6_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 14); +} + +/** + * @brief Get field chan7_raw from rc_channels message + * + * @return RC channel 7 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan7_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 16); +} + +/** + * @brief Get field chan8_raw from rc_channels message + * + * @return RC channel 8 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan8_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 18); +} + +/** + * @brief Get field chan9_raw from rc_channels message + * + * @return RC channel 9 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan9_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 20); +} + +/** + * @brief Get field chan10_raw from rc_channels message + * + * @return RC channel 10 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan10_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 22); +} + +/** + * @brief Get field chan11_raw from rc_channels message + * + * @return RC channel 11 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan11_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 24); +} + +/** + * @brief Get field chan12_raw from rc_channels message + * + * @return RC channel 12 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan12_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 26); +} + +/** + * @brief Get field chan13_raw from rc_channels message + * + * @return RC channel 13 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan13_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 28); +} + +/** + * @brief Get field chan14_raw from rc_channels message + * + * @return RC channel 14 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan14_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 30); +} + +/** + * @brief Get field chan15_raw from rc_channels message + * + * @return RC channel 15 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan15_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 32); +} + +/** + * @brief Get field chan16_raw from rc_channels message + * + * @return RC channel 16 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan16_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 34); +} + +/** + * @brief Get field chan17_raw from rc_channels message + * + * @return RC channel 17 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan17_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 36); +} + +/** + * @brief Get field chan18_raw from rc_channels message + * + * @return RC channel 18 value, in microseconds. A value of UINT16_MAX implies the channel is unused. + */ +static inline uint16_t mavlink_msg_rc_channels_get_chan18_raw(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 38); +} + +/** + * @brief Get field rssi from rc_channels message + * + * @return Receive signal strength indicator, 0: 0%, 100: 100%, 255: invalid/unknown. + */ +static inline uint8_t mavlink_msg_rc_channels_get_rssi(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint8_t(msg, 41); +} + +/** + * @brief Decode a rc_channels message into a struct + * + * @param msg The message to decode + * @param rc_channels C-struct to decode the message contents into + */ +static inline void mavlink_msg_rc_channels_decode(const mavlink_message_t* msg, mavlink_rc_channels_t* rc_channels) +{ +#if MAVLINK_NEED_BYTE_SWAP + rc_channels->time_boot_ms = mavlink_msg_rc_channels_get_time_boot_ms(msg); + rc_channels->chan1_raw = mavlink_msg_rc_channels_get_chan1_raw(msg); + rc_channels->chan2_raw = mavlink_msg_rc_channels_get_chan2_raw(msg); + rc_channels->chan3_raw = mavlink_msg_rc_channels_get_chan3_raw(msg); + rc_channels->chan4_raw = mavlink_msg_rc_channels_get_chan4_raw(msg); + rc_channels->chan5_raw = mavlink_msg_rc_channels_get_chan5_raw(msg); + rc_channels->chan6_raw = mavlink_msg_rc_channels_get_chan6_raw(msg); + rc_channels->chan7_raw = mavlink_msg_rc_channels_get_chan7_raw(msg); + rc_channels->chan8_raw = mavlink_msg_rc_channels_get_chan8_raw(msg); + rc_channels->chan9_raw = mavlink_msg_rc_channels_get_chan9_raw(msg); + rc_channels->chan10_raw = mavlink_msg_rc_channels_get_chan10_raw(msg); + rc_channels->chan11_raw = mavlink_msg_rc_channels_get_chan11_raw(msg); + rc_channels->chan12_raw = mavlink_msg_rc_channels_get_chan12_raw(msg); + rc_channels->chan13_raw = mavlink_msg_rc_channels_get_chan13_raw(msg); + rc_channels->chan14_raw = mavlink_msg_rc_channels_get_chan14_raw(msg); + rc_channels->chan15_raw = mavlink_msg_rc_channels_get_chan15_raw(msg); + rc_channels->chan16_raw = mavlink_msg_rc_channels_get_chan16_raw(msg); + rc_channels->chan17_raw = mavlink_msg_rc_channels_get_chan17_raw(msg); + rc_channels->chan18_raw = mavlink_msg_rc_channels_get_chan18_raw(msg); + rc_channels->chancount = mavlink_msg_rc_channels_get_chancount(msg); + rc_channels->rssi = mavlink_msg_rc_channels_get_rssi(msg); +#else + memcpy(rc_channels, _MAV_PAYLOAD(msg), MAVLINK_MSG_ID_RC_CHANNELS_LEN); +#endif +} diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels_override.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels_override.h index 0d8a1514b..15d4c6f95 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels_override.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels_override.h @@ -245,6 +245,56 @@ static inline void mavlink_msg_rc_channels_override_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_rc_channels_override_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint16_t chan1_raw, uint16_t chan2_raw, uint16_t chan3_raw, uint16_t chan4_raw, uint16_t chan5_raw, uint16_t chan6_raw, uint16_t chan7_raw, uint16_t chan8_raw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, chan1_raw); + _mav_put_uint16_t(buf, 2, chan2_raw); + _mav_put_uint16_t(buf, 4, chan3_raw); + _mav_put_uint16_t(buf, 6, chan4_raw); + _mav_put_uint16_t(buf, 8, chan5_raw); + _mav_put_uint16_t(buf, 10, chan6_raw); + _mav_put_uint16_t(buf, 12, chan7_raw); + _mav_put_uint16_t(buf, 14, chan8_raw); + _mav_put_uint8_t(buf, 16, target_system); + _mav_put_uint8_t(buf, 17, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE, buf, MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE_LEN, MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE, buf, MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE_LEN); +#endif +#else + mavlink_rc_channels_override_t *packet = (mavlink_rc_channels_override_t *)msgbuf; + packet->chan1_raw = chan1_raw; + packet->chan2_raw = chan2_raw; + packet->chan3_raw = chan3_raw; + packet->chan4_raw = chan4_raw; + packet->chan5_raw = chan5_raw; + packet->chan6_raw = chan6_raw; + packet->chan7_raw = chan7_raw; + packet->chan8_raw = chan8_raw; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE, (const char *)packet, MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE_LEN, MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE, (const char *)packet, MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE RC_CHANNELS_OVERRIDE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels_raw.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels_raw.h index 3c0aed020..d75a5934a 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels_raw.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels_raw.h @@ -256,6 +256,58 @@ static inline void mavlink_msg_rc_channels_raw_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_RC_CHANNELS_RAW_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_rc_channels_raw_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, uint8_t port, uint16_t chan1_raw, uint16_t chan2_raw, uint16_t chan3_raw, uint16_t chan4_raw, uint16_t chan5_raw, uint16_t chan6_raw, uint16_t chan7_raw, uint16_t chan8_raw, uint8_t rssi) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_uint16_t(buf, 4, chan1_raw); + _mav_put_uint16_t(buf, 6, chan2_raw); + _mav_put_uint16_t(buf, 8, chan3_raw); + _mav_put_uint16_t(buf, 10, chan4_raw); + _mav_put_uint16_t(buf, 12, chan5_raw); + _mav_put_uint16_t(buf, 14, chan6_raw); + _mav_put_uint16_t(buf, 16, chan7_raw); + _mav_put_uint16_t(buf, 18, chan8_raw); + _mav_put_uint8_t(buf, 20, port); + _mav_put_uint8_t(buf, 21, rssi); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS_RAW, buf, MAVLINK_MSG_ID_RC_CHANNELS_RAW_LEN, MAVLINK_MSG_ID_RC_CHANNELS_RAW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS_RAW, buf, MAVLINK_MSG_ID_RC_CHANNELS_RAW_LEN); +#endif +#else + mavlink_rc_channels_raw_t *packet = (mavlink_rc_channels_raw_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->chan1_raw = chan1_raw; + packet->chan2_raw = chan2_raw; + packet->chan3_raw = chan3_raw; + packet->chan4_raw = chan4_raw; + packet->chan5_raw = chan5_raw; + packet->chan6_raw = chan6_raw; + packet->chan7_raw = chan7_raw; + packet->chan8_raw = chan8_raw; + packet->port = port; + packet->rssi = rssi; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS_RAW, (const char *)packet, MAVLINK_MSG_ID_RC_CHANNELS_RAW_LEN, MAVLINK_MSG_ID_RC_CHANNELS_RAW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS_RAW, (const char *)packet, MAVLINK_MSG_ID_RC_CHANNELS_RAW_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE RC_CHANNELS_RAW UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels_scaled.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels_scaled.h index 2153ab392..f400f987d 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels_scaled.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_rc_channels_scaled.h @@ -256,6 +256,58 @@ static inline void mavlink_msg_rc_channels_scaled_send(mavlink_channel_t chan, u #endif } +#if MAVLINK_MSG_ID_RC_CHANNELS_SCALED_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_rc_channels_scaled_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, uint8_t port, int16_t chan1_scaled, int16_t chan2_scaled, int16_t chan3_scaled, int16_t chan4_scaled, int16_t chan5_scaled, int16_t chan6_scaled, int16_t chan7_scaled, int16_t chan8_scaled, uint8_t rssi) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_int16_t(buf, 4, chan1_scaled); + _mav_put_int16_t(buf, 6, chan2_scaled); + _mav_put_int16_t(buf, 8, chan3_scaled); + _mav_put_int16_t(buf, 10, chan4_scaled); + _mav_put_int16_t(buf, 12, chan5_scaled); + _mav_put_int16_t(buf, 14, chan6_scaled); + _mav_put_int16_t(buf, 16, chan7_scaled); + _mav_put_int16_t(buf, 18, chan8_scaled); + _mav_put_uint8_t(buf, 20, port); + _mav_put_uint8_t(buf, 21, rssi); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS_SCALED, buf, MAVLINK_MSG_ID_RC_CHANNELS_SCALED_LEN, MAVLINK_MSG_ID_RC_CHANNELS_SCALED_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS_SCALED, buf, MAVLINK_MSG_ID_RC_CHANNELS_SCALED_LEN); +#endif +#else + mavlink_rc_channels_scaled_t *packet = (mavlink_rc_channels_scaled_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->chan1_scaled = chan1_scaled; + packet->chan2_scaled = chan2_scaled; + packet->chan3_scaled = chan3_scaled; + packet->chan4_scaled = chan4_scaled; + packet->chan5_scaled = chan5_scaled; + packet->chan6_scaled = chan6_scaled; + packet->chan7_scaled = chan7_scaled; + packet->chan8_scaled = chan8_scaled; + packet->port = port; + packet->rssi = rssi; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS_SCALED, (const char *)packet, MAVLINK_MSG_ID_RC_CHANNELS_SCALED_LEN, MAVLINK_MSG_ID_RC_CHANNELS_SCALED_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RC_CHANNELS_SCALED, (const char *)packet, MAVLINK_MSG_ID_RC_CHANNELS_SCALED_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE RC_CHANNELS_SCALED UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_request_data_stream.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_request_data_stream.h index c754ad876..2ebcc54da 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_request_data_stream.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_request_data_stream.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_request_data_stream_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_REQUEST_DATA_STREAM_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_request_data_stream_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t req_stream_id, uint16_t req_message_rate, uint8_t start_stop) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, req_message_rate); + _mav_put_uint8_t(buf, 2, target_system); + _mav_put_uint8_t(buf, 3, target_component); + _mav_put_uint8_t(buf, 4, req_stream_id); + _mav_put_uint8_t(buf, 5, start_stop); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_REQUEST_DATA_STREAM, buf, MAVLINK_MSG_ID_REQUEST_DATA_STREAM_LEN, MAVLINK_MSG_ID_REQUEST_DATA_STREAM_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_REQUEST_DATA_STREAM, buf, MAVLINK_MSG_ID_REQUEST_DATA_STREAM_LEN); +#endif +#else + mavlink_request_data_stream_t *packet = (mavlink_request_data_stream_t *)msgbuf; + packet->req_message_rate = req_message_rate; + packet->target_system = target_system; + packet->target_component = target_component; + packet->req_stream_id = req_stream_id; + packet->start_stop = start_stop; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_REQUEST_DATA_STREAM, (const char *)packet, MAVLINK_MSG_ID_REQUEST_DATA_STREAM_LEN, MAVLINK_MSG_ID_REQUEST_DATA_STREAM_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_REQUEST_DATA_STREAM, (const char *)packet, MAVLINK_MSG_ID_REQUEST_DATA_STREAM_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE REQUEST_DATA_STREAM UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_roll_pitch_yaw_rates_thrust_setpoint.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_roll_pitch_yaw_rates_thrust_setpoint.h index ac3ef4fa9..131b756b6 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_roll_pitch_yaw_rates_thrust_setpoint.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_roll_pitch_yaw_rates_thrust_setpoint.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_roll_pitch_yaw_rates_thrust_setpoint_send(mavlink #endif } +#if MAVLINK_MSG_ID_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_roll_pitch_yaw_rates_thrust_setpoint_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, float roll_rate, float pitch_rate, float yaw_rate, float thrust) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_float(buf, 4, roll_rate); + _mav_put_float(buf, 8, pitch_rate); + _mav_put_float(buf, 12, yaw_rate); + _mav_put_float(buf, 16, thrust); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, buf, MAVLINK_MSG_ID_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT_LEN, MAVLINK_MSG_ID_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, buf, MAVLINK_MSG_ID_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT_LEN); +#endif +#else + mavlink_roll_pitch_yaw_rates_thrust_setpoint_t *packet = (mavlink_roll_pitch_yaw_rates_thrust_setpoint_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->roll_rate = roll_rate; + packet->pitch_rate = pitch_rate; + packet->yaw_rate = yaw_rate; + packet->thrust = thrust; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT_LEN, MAVLINK_MSG_ID_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE ROLL_PITCH_YAW_RATES_THRUST_SETPOINT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_roll_pitch_yaw_speed_thrust_setpoint.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_roll_pitch_yaw_speed_thrust_setpoint.h index 626477322..757e6d138 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_roll_pitch_yaw_speed_thrust_setpoint.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_roll_pitch_yaw_speed_thrust_setpoint.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_roll_pitch_yaw_speed_thrust_setpoint_send(mavlink #endif } +#if MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_roll_pitch_yaw_speed_thrust_setpoint_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, float roll_speed, float pitch_speed, float yaw_speed, float thrust) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_float(buf, 4, roll_speed); + _mav_put_float(buf, 8, pitch_speed); + _mav_put_float(buf, 12, yaw_speed); + _mav_put_float(buf, 16, thrust); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, buf, MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT_LEN, MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, buf, MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT_LEN); +#endif +#else + mavlink_roll_pitch_yaw_speed_thrust_setpoint_t *packet = (mavlink_roll_pitch_yaw_speed_thrust_setpoint_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->roll_speed = roll_speed; + packet->pitch_speed = pitch_speed; + packet->yaw_speed = yaw_speed; + packet->thrust = thrust; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT_LEN, MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_roll_pitch_yaw_thrust_setpoint.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_roll_pitch_yaw_thrust_setpoint.h index ffcdc547b..f04eedcb3 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_roll_pitch_yaw_thrust_setpoint.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_roll_pitch_yaw_thrust_setpoint.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_roll_pitch_yaw_thrust_setpoint_send(mavlink_chann #endif } +#if MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_roll_pitch_yaw_thrust_setpoint_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, float roll, float pitch, float yaw, float thrust) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_float(buf, 4, roll); + _mav_put_float(buf, 8, pitch); + _mav_put_float(buf, 12, yaw); + _mav_put_float(buf, 16, thrust); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT, buf, MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT_LEN, MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT, buf, MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT_LEN); +#endif +#else + mavlink_roll_pitch_yaw_thrust_setpoint_t *packet = (mavlink_roll_pitch_yaw_thrust_setpoint_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + packet->thrust = thrust; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT_LEN, MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE ROLL_PITCH_YAW_THRUST_SETPOINT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_safety_allowed_area.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_safety_allowed_area.h index fcd54cbb7..0176dfcc8 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_safety_allowed_area.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_safety_allowed_area.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_safety_allowed_area_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_safety_allowed_area_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t frame, float p1x, float p1y, float p1z, float p2x, float p2y, float p2z) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, p1x); + _mav_put_float(buf, 4, p1y); + _mav_put_float(buf, 8, p1z); + _mav_put_float(buf, 12, p2x); + _mav_put_float(buf, 16, p2y); + _mav_put_float(buf, 20, p2z); + _mav_put_uint8_t(buf, 24, frame); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA, buf, MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA_LEN, MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA, buf, MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA_LEN); +#endif +#else + mavlink_safety_allowed_area_t *packet = (mavlink_safety_allowed_area_t *)msgbuf; + packet->p1x = p1x; + packet->p1y = p1y; + packet->p1z = p1z; + packet->p2x = p2x; + packet->p2y = p2y; + packet->p2z = p2z; + packet->frame = frame; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA, (const char *)packet, MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA_LEN, MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA, (const char *)packet, MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SAFETY_ALLOWED_AREA UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_safety_set_allowed_area.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_safety_set_allowed_area.h index 61f6af155..dafbc260b 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_safety_set_allowed_area.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_safety_set_allowed_area.h @@ -234,6 +234,54 @@ static inline void mavlink_msg_safety_set_allowed_area_send(mavlink_channel_t ch #endif } +#if MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_safety_set_allowed_area_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t frame, float p1x, float p1y, float p1z, float p2x, float p2y, float p2z) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, p1x); + _mav_put_float(buf, 4, p1y); + _mav_put_float(buf, 8, p1z); + _mav_put_float(buf, 12, p2x); + _mav_put_float(buf, 16, p2y); + _mav_put_float(buf, 20, p2z); + _mav_put_uint8_t(buf, 24, target_system); + _mav_put_uint8_t(buf, 25, target_component); + _mav_put_uint8_t(buf, 26, frame); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA, buf, MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA_LEN, MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA, buf, MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA_LEN); +#endif +#else + mavlink_safety_set_allowed_area_t *packet = (mavlink_safety_set_allowed_area_t *)msgbuf; + packet->p1x = p1x; + packet->p1y = p1y; + packet->p1z = p1z; + packet->p2x = p2x; + packet->p2y = p2y; + packet->p2z = p2z; + packet->target_system = target_system; + packet->target_component = target_component; + packet->frame = frame; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA, (const char *)packet, MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA_LEN, MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA, (const char *)packet, MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SAFETY_SET_ALLOWED_AREA UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_scaled_imu.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_scaled_imu.h index 3010d051a..1648a56f8 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_scaled_imu.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_scaled_imu.h @@ -245,6 +245,56 @@ static inline void mavlink_msg_scaled_imu_send(mavlink_channel_t chan, uint32_t #endif } +#if MAVLINK_MSG_ID_SCALED_IMU_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_scaled_imu_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, int16_t xacc, int16_t yacc, int16_t zacc, int16_t xgyro, int16_t ygyro, int16_t zgyro, int16_t xmag, int16_t ymag, int16_t zmag) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_int16_t(buf, 4, xacc); + _mav_put_int16_t(buf, 6, yacc); + _mav_put_int16_t(buf, 8, zacc); + _mav_put_int16_t(buf, 10, xgyro); + _mav_put_int16_t(buf, 12, ygyro); + _mav_put_int16_t(buf, 14, zgyro); + _mav_put_int16_t(buf, 16, xmag); + _mav_put_int16_t(buf, 18, ymag); + _mav_put_int16_t(buf, 20, zmag); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SCALED_IMU, buf, MAVLINK_MSG_ID_SCALED_IMU_LEN, MAVLINK_MSG_ID_SCALED_IMU_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SCALED_IMU, buf, MAVLINK_MSG_ID_SCALED_IMU_LEN); +#endif +#else + mavlink_scaled_imu_t *packet = (mavlink_scaled_imu_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->xacc = xacc; + packet->yacc = yacc; + packet->zacc = zacc; + packet->xgyro = xgyro; + packet->ygyro = ygyro; + packet->zgyro = zgyro; + packet->xmag = xmag; + packet->ymag = ymag; + packet->zmag = zmag; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SCALED_IMU, (const char *)packet, MAVLINK_MSG_ID_SCALED_IMU_LEN, MAVLINK_MSG_ID_SCALED_IMU_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SCALED_IMU, (const char *)packet, MAVLINK_MSG_ID_SCALED_IMU_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SCALED_IMU UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_scaled_imu2.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_scaled_imu2.h index ea4dbbf81..1dea121dd 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_scaled_imu2.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_scaled_imu2.h @@ -245,6 +245,56 @@ static inline void mavlink_msg_scaled_imu2_send(mavlink_channel_t chan, uint32_t #endif } +#if MAVLINK_MSG_ID_SCALED_IMU2_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_scaled_imu2_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, int16_t xacc, int16_t yacc, int16_t zacc, int16_t xgyro, int16_t ygyro, int16_t zgyro, int16_t xmag, int16_t ymag, int16_t zmag) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_int16_t(buf, 4, xacc); + _mav_put_int16_t(buf, 6, yacc); + _mav_put_int16_t(buf, 8, zacc); + _mav_put_int16_t(buf, 10, xgyro); + _mav_put_int16_t(buf, 12, ygyro); + _mav_put_int16_t(buf, 14, zgyro); + _mav_put_int16_t(buf, 16, xmag); + _mav_put_int16_t(buf, 18, ymag); + _mav_put_int16_t(buf, 20, zmag); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SCALED_IMU2, buf, MAVLINK_MSG_ID_SCALED_IMU2_LEN, MAVLINK_MSG_ID_SCALED_IMU2_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SCALED_IMU2, buf, MAVLINK_MSG_ID_SCALED_IMU2_LEN); +#endif +#else + mavlink_scaled_imu2_t *packet = (mavlink_scaled_imu2_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->xacc = xacc; + packet->yacc = yacc; + packet->zacc = zacc; + packet->xgyro = xgyro; + packet->ygyro = ygyro; + packet->zgyro = zgyro; + packet->xmag = xmag; + packet->ymag = ymag; + packet->zmag = zmag; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SCALED_IMU2, (const char *)packet, MAVLINK_MSG_ID_SCALED_IMU2_LEN, MAVLINK_MSG_ID_SCALED_IMU2_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SCALED_IMU2, (const char *)packet, MAVLINK_MSG_ID_SCALED_IMU2_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SCALED_IMU2 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_scaled_pressure.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_scaled_pressure.h index 10324bc94..e0d6d8766 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_scaled_pressure.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_scaled_pressure.h @@ -179,6 +179,44 @@ static inline void mavlink_msg_scaled_pressure_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_SCALED_PRESSURE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_scaled_pressure_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, float press_abs, float press_diff, int16_t temperature) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_float(buf, 4, press_abs); + _mav_put_float(buf, 8, press_diff); + _mav_put_int16_t(buf, 12, temperature); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SCALED_PRESSURE, buf, MAVLINK_MSG_ID_SCALED_PRESSURE_LEN, MAVLINK_MSG_ID_SCALED_PRESSURE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SCALED_PRESSURE, buf, MAVLINK_MSG_ID_SCALED_PRESSURE_LEN); +#endif +#else + mavlink_scaled_pressure_t *packet = (mavlink_scaled_pressure_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->press_abs = press_abs; + packet->press_diff = press_diff; + packet->temperature = temperature; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SCALED_PRESSURE, (const char *)packet, MAVLINK_MSG_ID_SCALED_PRESSURE_LEN, MAVLINK_MSG_ID_SCALED_PRESSURE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SCALED_PRESSURE, (const char *)packet, MAVLINK_MSG_ID_SCALED_PRESSURE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SCALED_PRESSURE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_serial_control.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_serial_control.h new file mode 100644 index 000000000..cbf72bae3 --- /dev/null +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_serial_control.h @@ -0,0 +1,321 @@ +// MESSAGE SERIAL_CONTROL PACKING + +#define MAVLINK_MSG_ID_SERIAL_CONTROL 126 + +typedef struct __mavlink_serial_control_t +{ + uint32_t baudrate; ///< Baudrate of transfer. Zero means no change. + uint16_t timeout; ///< Timeout for reply data in milliseconds + uint8_t device; ///< See SERIAL_CONTROL_DEV enum + uint8_t flags; ///< See SERIAL_CONTROL_FLAG enum + uint8_t count; ///< how many bytes in this transfer + uint8_t data[70]; ///< serial data +} mavlink_serial_control_t; + +#define MAVLINK_MSG_ID_SERIAL_CONTROL_LEN 79 +#define MAVLINK_MSG_ID_126_LEN 79 + +#define MAVLINK_MSG_ID_SERIAL_CONTROL_CRC 220 +#define MAVLINK_MSG_ID_126_CRC 220 + +#define MAVLINK_MSG_SERIAL_CONTROL_FIELD_DATA_LEN 70 + +#define MAVLINK_MESSAGE_INFO_SERIAL_CONTROL { \ + "SERIAL_CONTROL", \ + 6, \ + { { "baudrate", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_serial_control_t, baudrate) }, \ + { "timeout", NULL, MAVLINK_TYPE_UINT16_T, 0, 4, offsetof(mavlink_serial_control_t, timeout) }, \ + { "device", NULL, MAVLINK_TYPE_UINT8_T, 0, 6, offsetof(mavlink_serial_control_t, device) }, \ + { "flags", NULL, MAVLINK_TYPE_UINT8_T, 0, 7, offsetof(mavlink_serial_control_t, flags) }, \ + { "count", NULL, MAVLINK_TYPE_UINT8_T, 0, 8, offsetof(mavlink_serial_control_t, count) }, \ + { "data", NULL, MAVLINK_TYPE_UINT8_T, 70, 9, offsetof(mavlink_serial_control_t, data) }, \ + } \ +} + + +/** + * @brief Pack a serial_control message + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param msg The MAVLink message to compress the data into + * + * @param device See SERIAL_CONTROL_DEV enum + * @param flags See SERIAL_CONTROL_FLAG enum + * @param timeout Timeout for reply data in milliseconds + * @param baudrate Baudrate of transfer. Zero means no change. + * @param count how many bytes in this transfer + * @param data serial data + * @return length of the message in bytes (excluding serial stream start sign) + */ +static inline uint16_t mavlink_msg_serial_control_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, + uint8_t device, uint8_t flags, uint16_t timeout, uint32_t baudrate, uint8_t count, const uint8_t *data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_SERIAL_CONTROL_LEN]; + _mav_put_uint32_t(buf, 0, baudrate); + _mav_put_uint16_t(buf, 4, timeout); + _mav_put_uint8_t(buf, 6, device); + _mav_put_uint8_t(buf, 7, flags); + _mav_put_uint8_t(buf, 8, count); + _mav_put_uint8_t_array(buf, 9, data, 70); + memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN); +#else + mavlink_serial_control_t packet; + packet.baudrate = baudrate; + packet.timeout = timeout; + packet.device = device; + packet.flags = flags; + packet.count = count; + mav_array_memcpy(packet.data, data, sizeof(uint8_t)*70); + memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN); +#endif + + msg->msgid = MAVLINK_MSG_ID_SERIAL_CONTROL; +#if MAVLINK_CRC_EXTRA + return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN, MAVLINK_MSG_ID_SERIAL_CONTROL_CRC); +#else + return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN); +#endif +} + +/** + * @brief Pack a serial_control message on a channel + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param chan The MAVLink channel this message will be sent over + * @param msg The MAVLink message to compress the data into + * @param device See SERIAL_CONTROL_DEV enum + * @param flags See SERIAL_CONTROL_FLAG enum + * @param timeout Timeout for reply data in milliseconds + * @param baudrate Baudrate of transfer. Zero means no change. + * @param count how many bytes in this transfer + * @param data serial data + * @return length of the message in bytes (excluding serial stream start sign) + */ +static inline uint16_t mavlink_msg_serial_control_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, + mavlink_message_t* msg, + uint8_t device,uint8_t flags,uint16_t timeout,uint32_t baudrate,uint8_t count,const uint8_t *data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_SERIAL_CONTROL_LEN]; + _mav_put_uint32_t(buf, 0, baudrate); + _mav_put_uint16_t(buf, 4, timeout); + _mav_put_uint8_t(buf, 6, device); + _mav_put_uint8_t(buf, 7, flags); + _mav_put_uint8_t(buf, 8, count); + _mav_put_uint8_t_array(buf, 9, data, 70); + memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN); +#else + mavlink_serial_control_t packet; + packet.baudrate = baudrate; + packet.timeout = timeout; + packet.device = device; + packet.flags = flags; + packet.count = count; + mav_array_memcpy(packet.data, data, sizeof(uint8_t)*70); + memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN); +#endif + + msg->msgid = MAVLINK_MSG_ID_SERIAL_CONTROL; +#if MAVLINK_CRC_EXTRA + return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN, MAVLINK_MSG_ID_SERIAL_CONTROL_CRC); +#else + return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN); +#endif +} + +/** + * @brief Encode a serial_control struct + * + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param msg The MAVLink message to compress the data into + * @param serial_control C-struct to read the message contents from + */ +static inline uint16_t mavlink_msg_serial_control_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_serial_control_t* serial_control) +{ + return mavlink_msg_serial_control_pack(system_id, component_id, msg, serial_control->device, serial_control->flags, serial_control->timeout, serial_control->baudrate, serial_control->count, serial_control->data); +} + +/** + * @brief Encode a serial_control struct on a channel + * + * @param system_id ID of this system + * @param component_id ID of this component (e.g. 200 for IMU) + * @param chan The MAVLink channel this message will be sent over + * @param msg The MAVLink message to compress the data into + * @param serial_control C-struct to read the message contents from + */ +static inline uint16_t mavlink_msg_serial_control_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_serial_control_t* serial_control) +{ + return mavlink_msg_serial_control_pack_chan(system_id, component_id, chan, msg, serial_control->device, serial_control->flags, serial_control->timeout, serial_control->baudrate, serial_control->count, serial_control->data); +} + +/** + * @brief Send a serial_control message + * @param chan MAVLink channel to send the message + * + * @param device See SERIAL_CONTROL_DEV enum + * @param flags See SERIAL_CONTROL_FLAG enum + * @param timeout Timeout for reply data in milliseconds + * @param baudrate Baudrate of transfer. Zero means no change. + * @param count how many bytes in this transfer + * @param data serial data + */ +#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS + +static inline void mavlink_msg_serial_control_send(mavlink_channel_t chan, uint8_t device, uint8_t flags, uint16_t timeout, uint32_t baudrate, uint8_t count, const uint8_t *data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char buf[MAVLINK_MSG_ID_SERIAL_CONTROL_LEN]; + _mav_put_uint32_t(buf, 0, baudrate); + _mav_put_uint16_t(buf, 4, timeout); + _mav_put_uint8_t(buf, 6, device); + _mav_put_uint8_t(buf, 7, flags); + _mav_put_uint8_t(buf, 8, count); + _mav_put_uint8_t_array(buf, 9, data, 70); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_CONTROL, buf, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN, MAVLINK_MSG_ID_SERIAL_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_CONTROL, buf, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN); +#endif +#else + mavlink_serial_control_t packet; + packet.baudrate = baudrate; + packet.timeout = timeout; + packet.device = device; + packet.flags = flags; + packet.count = count; + mav_array_memcpy(packet.data, data, sizeof(uint8_t)*70); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_CONTROL, (const char *)&packet, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN, MAVLINK_MSG_ID_SERIAL_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_CONTROL, (const char *)&packet, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN); +#endif +#endif +} + +#if MAVLINK_MSG_ID_SERIAL_CONTROL_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_serial_control_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t device, uint8_t flags, uint16_t timeout, uint32_t baudrate, uint8_t count, const uint8_t *data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, baudrate); + _mav_put_uint16_t(buf, 4, timeout); + _mav_put_uint8_t(buf, 6, device); + _mav_put_uint8_t(buf, 7, flags); + _mav_put_uint8_t(buf, 8, count); + _mav_put_uint8_t_array(buf, 9, data, 70); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_CONTROL, buf, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN, MAVLINK_MSG_ID_SERIAL_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_CONTROL, buf, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN); +#endif +#else + mavlink_serial_control_t *packet = (mavlink_serial_control_t *)msgbuf; + packet->baudrate = baudrate; + packet->timeout = timeout; + packet->device = device; + packet->flags = flags; + packet->count = count; + mav_array_memcpy(packet->data, data, sizeof(uint8_t)*70); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_CONTROL, (const char *)packet, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN, MAVLINK_MSG_ID_SERIAL_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_CONTROL, (const char *)packet, MAVLINK_MSG_ID_SERIAL_CONTROL_LEN); +#endif +#endif +} +#endif + +#endif + +// MESSAGE SERIAL_CONTROL UNPACKING + + +/** + * @brief Get field device from serial_control message + * + * @return See SERIAL_CONTROL_DEV enum + */ +static inline uint8_t mavlink_msg_serial_control_get_device(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint8_t(msg, 6); +} + +/** + * @brief Get field flags from serial_control message + * + * @return See SERIAL_CONTROL_FLAG enum + */ +static inline uint8_t mavlink_msg_serial_control_get_flags(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint8_t(msg, 7); +} + +/** + * @brief Get field timeout from serial_control message + * + * @return Timeout for reply data in milliseconds + */ +static inline uint16_t mavlink_msg_serial_control_get_timeout(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint16_t(msg, 4); +} + +/** + * @brief Get field baudrate from serial_control message + * + * @return Baudrate of transfer. Zero means no change. + */ +static inline uint32_t mavlink_msg_serial_control_get_baudrate(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint32_t(msg, 0); +} + +/** + * @brief Get field count from serial_control message + * + * @return how many bytes in this transfer + */ +static inline uint8_t mavlink_msg_serial_control_get_count(const mavlink_message_t* msg) +{ + return _MAV_RETURN_uint8_t(msg, 8); +} + +/** + * @brief Get field data from serial_control message + * + * @return serial data + */ +static inline uint16_t mavlink_msg_serial_control_get_data(const mavlink_message_t* msg, uint8_t *data) +{ + return _MAV_RETURN_uint8_t_array(msg, data, 70, 9); +} + +/** + * @brief Decode a serial_control message into a struct + * + * @param msg The message to decode + * @param serial_control C-struct to decode the message contents into + */ +static inline void mavlink_msg_serial_control_decode(const mavlink_message_t* msg, mavlink_serial_control_t* serial_control) +{ +#if MAVLINK_NEED_BYTE_SWAP + serial_control->baudrate = mavlink_msg_serial_control_get_baudrate(msg); + serial_control->timeout = mavlink_msg_serial_control_get_timeout(msg); + serial_control->device = mavlink_msg_serial_control_get_device(msg); + serial_control->flags = mavlink_msg_serial_control_get_flags(msg); + serial_control->count = mavlink_msg_serial_control_get_count(msg); + mavlink_msg_serial_control_get_data(msg, serial_control->data); +#else + memcpy(serial_control, _MAV_PAYLOAD(msg), MAVLINK_MSG_ID_SERIAL_CONTROL_LEN); +#endif +} diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_servo_output_raw.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_servo_output_raw.h index 6a14e93ed..e8408862f 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_servo_output_raw.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_servo_output_raw.h @@ -245,6 +245,56 @@ static inline void mavlink_msg_servo_output_raw_send(mavlink_channel_t chan, uin #endif } +#if MAVLINK_MSG_ID_SERVO_OUTPUT_RAW_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_servo_output_raw_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_usec, uint8_t port, uint16_t servo1_raw, uint16_t servo2_raw, uint16_t servo3_raw, uint16_t servo4_raw, uint16_t servo5_raw, uint16_t servo6_raw, uint16_t servo7_raw, uint16_t servo8_raw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_usec); + _mav_put_uint16_t(buf, 4, servo1_raw); + _mav_put_uint16_t(buf, 6, servo2_raw); + _mav_put_uint16_t(buf, 8, servo3_raw); + _mav_put_uint16_t(buf, 10, servo4_raw); + _mav_put_uint16_t(buf, 12, servo5_raw); + _mav_put_uint16_t(buf, 14, servo6_raw); + _mav_put_uint16_t(buf, 16, servo7_raw); + _mav_put_uint16_t(buf, 18, servo8_raw); + _mav_put_uint8_t(buf, 20, port); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERVO_OUTPUT_RAW, buf, MAVLINK_MSG_ID_SERVO_OUTPUT_RAW_LEN, MAVLINK_MSG_ID_SERVO_OUTPUT_RAW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERVO_OUTPUT_RAW, buf, MAVLINK_MSG_ID_SERVO_OUTPUT_RAW_LEN); +#endif +#else + mavlink_servo_output_raw_t *packet = (mavlink_servo_output_raw_t *)msgbuf; + packet->time_usec = time_usec; + packet->servo1_raw = servo1_raw; + packet->servo2_raw = servo2_raw; + packet->servo3_raw = servo3_raw; + packet->servo4_raw = servo4_raw; + packet->servo5_raw = servo5_raw; + packet->servo6_raw = servo6_raw; + packet->servo7_raw = servo7_raw; + packet->servo8_raw = servo8_raw; + packet->port = port; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERVO_OUTPUT_RAW, (const char *)packet, MAVLINK_MSG_ID_SERVO_OUTPUT_RAW_LEN, MAVLINK_MSG_ID_SERVO_OUTPUT_RAW_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERVO_OUTPUT_RAW, (const char *)packet, MAVLINK_MSG_ID_SERVO_OUTPUT_RAW_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SERVO_OUTPUT_RAW UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_global_position_setpoint_int.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_global_position_setpoint_int.h index 6f0d7a69d..94a7b432b 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_global_position_setpoint_int.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_global_position_setpoint_int.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_set_global_position_setpoint_int_send(mavlink_cha #endif } +#if MAVLINK_MSG_ID_SET_GLOBAL_POSITION_SETPOINT_INT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_set_global_position_setpoint_int_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t coordinate_frame, int32_t latitude, int32_t longitude, int32_t altitude, int16_t yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, latitude); + _mav_put_int32_t(buf, 4, longitude); + _mav_put_int32_t(buf, 8, altitude); + _mav_put_int16_t(buf, 12, yaw); + _mav_put_uint8_t(buf, 14, coordinate_frame); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_GLOBAL_POSITION_SETPOINT_INT, buf, MAVLINK_MSG_ID_SET_GLOBAL_POSITION_SETPOINT_INT_LEN, MAVLINK_MSG_ID_SET_GLOBAL_POSITION_SETPOINT_INT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_GLOBAL_POSITION_SETPOINT_INT, buf, MAVLINK_MSG_ID_SET_GLOBAL_POSITION_SETPOINT_INT_LEN); +#endif +#else + mavlink_set_global_position_setpoint_int_t *packet = (mavlink_set_global_position_setpoint_int_t *)msgbuf; + packet->latitude = latitude; + packet->longitude = longitude; + packet->altitude = altitude; + packet->yaw = yaw; + packet->coordinate_frame = coordinate_frame; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_GLOBAL_POSITION_SETPOINT_INT, (const char *)packet, MAVLINK_MSG_ID_SET_GLOBAL_POSITION_SETPOINT_INT_LEN, MAVLINK_MSG_ID_SET_GLOBAL_POSITION_SETPOINT_INT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_GLOBAL_POSITION_SETPOINT_INT, (const char *)packet, MAVLINK_MSG_ID_SET_GLOBAL_POSITION_SETPOINT_INT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SET_GLOBAL_POSITION_SETPOINT_INT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_gps_global_origin.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_gps_global_origin.h index c444d8d52..1c018cbee 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_gps_global_origin.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_gps_global_origin.h @@ -179,6 +179,44 @@ static inline void mavlink_msg_set_gps_global_origin_send(mavlink_channel_t chan #endif } +#if MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_set_gps_global_origin_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, int32_t latitude, int32_t longitude, int32_t altitude) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, latitude); + _mav_put_int32_t(buf, 4, longitude); + _mav_put_int32_t(buf, 8, altitude); + _mav_put_uint8_t(buf, 12, target_system); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN, buf, MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN_LEN, MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN, buf, MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN_LEN); +#endif +#else + mavlink_set_gps_global_origin_t *packet = (mavlink_set_gps_global_origin_t *)msgbuf; + packet->latitude = latitude; + packet->longitude = longitude; + packet->altitude = altitude; + packet->target_system = target_system; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN, (const char *)packet, MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN_LEN, MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN, (const char *)packet, MAVLINK_MSG_ID_SET_GPS_GLOBAL_ORIGIN_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SET_GPS_GLOBAL_ORIGIN UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_local_position_setpoint.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_local_position_setpoint.h index 6f2835e03..04dbe6e9a 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_local_position_setpoint.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_local_position_setpoint.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_set_local_position_setpoint_send(mavlink_channel_ #endif } +#if MAVLINK_MSG_ID_SET_LOCAL_POSITION_SETPOINT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_set_local_position_setpoint_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t coordinate_frame, float x, float y, float z, float yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, x); + _mav_put_float(buf, 4, y); + _mav_put_float(buf, 8, z); + _mav_put_float(buf, 12, yaw); + _mav_put_uint8_t(buf, 16, target_system); + _mav_put_uint8_t(buf, 17, target_component); + _mav_put_uint8_t(buf, 18, coordinate_frame); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_LOCAL_POSITION_SETPOINT, buf, MAVLINK_MSG_ID_SET_LOCAL_POSITION_SETPOINT_LEN, MAVLINK_MSG_ID_SET_LOCAL_POSITION_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_LOCAL_POSITION_SETPOINT, buf, MAVLINK_MSG_ID_SET_LOCAL_POSITION_SETPOINT_LEN); +#endif +#else + mavlink_set_local_position_setpoint_t *packet = (mavlink_set_local_position_setpoint_t *)msgbuf; + packet->x = x; + packet->y = y; + packet->z = z; + packet->yaw = yaw; + packet->target_system = target_system; + packet->target_component = target_component; + packet->coordinate_frame = coordinate_frame; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_LOCAL_POSITION_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_SET_LOCAL_POSITION_SETPOINT_LEN, MAVLINK_MSG_ID_SET_LOCAL_POSITION_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_LOCAL_POSITION_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_SET_LOCAL_POSITION_SETPOINT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SET_LOCAL_POSITION_SETPOINT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_mode.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_mode.h index 1aff42cce..4b60a4120 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_mode.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_mode.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_set_mode_send(mavlink_channel_t chan, uint8_t tar #endif } +#if MAVLINK_MSG_ID_SET_MODE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_set_mode_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t base_mode, uint32_t custom_mode) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, custom_mode); + _mav_put_uint8_t(buf, 4, target_system); + _mav_put_uint8_t(buf, 5, base_mode); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_MODE, buf, MAVLINK_MSG_ID_SET_MODE_LEN, MAVLINK_MSG_ID_SET_MODE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_MODE, buf, MAVLINK_MSG_ID_SET_MODE_LEN); +#endif +#else + mavlink_set_mode_t *packet = (mavlink_set_mode_t *)msgbuf; + packet->custom_mode = custom_mode; + packet->target_system = target_system; + packet->base_mode = base_mode; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_MODE, (const char *)packet, MAVLINK_MSG_ID_SET_MODE_LEN, MAVLINK_MSG_ID_SET_MODE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_MODE, (const char *)packet, MAVLINK_MSG_ID_SET_MODE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SET_MODE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_quad_motors_setpoint.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_quad_motors_setpoint.h index 8ceb8888f..8c0e2a014 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_quad_motors_setpoint.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_quad_motors_setpoint.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_set_quad_motors_setpoint_send(mavlink_channel_t c #endif } +#if MAVLINK_MSG_ID_SET_QUAD_MOTORS_SETPOINT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_set_quad_motors_setpoint_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint16_t motor_front_nw, uint16_t motor_right_ne, uint16_t motor_back_se, uint16_t motor_left_sw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, motor_front_nw); + _mav_put_uint16_t(buf, 2, motor_right_ne); + _mav_put_uint16_t(buf, 4, motor_back_se); + _mav_put_uint16_t(buf, 6, motor_left_sw); + _mav_put_uint8_t(buf, 8, target_system); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_QUAD_MOTORS_SETPOINT, buf, MAVLINK_MSG_ID_SET_QUAD_MOTORS_SETPOINT_LEN, MAVLINK_MSG_ID_SET_QUAD_MOTORS_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_QUAD_MOTORS_SETPOINT, buf, MAVLINK_MSG_ID_SET_QUAD_MOTORS_SETPOINT_LEN); +#endif +#else + mavlink_set_quad_motors_setpoint_t *packet = (mavlink_set_quad_motors_setpoint_t *)msgbuf; + packet->motor_front_nw = motor_front_nw; + packet->motor_right_ne = motor_right_ne; + packet->motor_back_se = motor_back_se; + packet->motor_left_sw = motor_left_sw; + packet->target_system = target_system; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_QUAD_MOTORS_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_SET_QUAD_MOTORS_SETPOINT_LEN, MAVLINK_MSG_ID_SET_QUAD_MOTORS_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_QUAD_MOTORS_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_SET_QUAD_MOTORS_SETPOINT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SET_QUAD_MOTORS_SETPOINT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_quad_swarm_led_roll_pitch_yaw_thrust.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_quad_swarm_led_roll_pitch_yaw_thrust.h index 9ef294cc9..c9a084773 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_quad_swarm_led_roll_pitch_yaw_thrust.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_quad_swarm_led_roll_pitch_yaw_thrust.h @@ -234,6 +234,52 @@ static inline void mavlink_msg_set_quad_swarm_led_roll_pitch_yaw_thrust_send(mav #endif } +#if MAVLINK_MSG_ID_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_set_quad_swarm_led_roll_pitch_yaw_thrust_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t group, uint8_t mode, const uint8_t *led_red, const uint8_t *led_blue, const uint8_t *led_green, const int16_t *roll, const int16_t *pitch, const int16_t *yaw, const uint16_t *thrust) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 32, group); + _mav_put_uint8_t(buf, 33, mode); + _mav_put_int16_t_array(buf, 0, roll, 4); + _mav_put_int16_t_array(buf, 8, pitch, 4); + _mav_put_int16_t_array(buf, 16, yaw, 4); + _mav_put_uint16_t_array(buf, 24, thrust, 4); + _mav_put_uint8_t_array(buf, 34, led_red, 4); + _mav_put_uint8_t_array(buf, 38, led_blue, 4); + _mav_put_uint8_t_array(buf, 42, led_green, 4); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, buf, MAVLINK_MSG_ID_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST_LEN, MAVLINK_MSG_ID_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, buf, MAVLINK_MSG_ID_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST_LEN); +#endif +#else + mavlink_set_quad_swarm_led_roll_pitch_yaw_thrust_t *packet = (mavlink_set_quad_swarm_led_roll_pitch_yaw_thrust_t *)msgbuf; + packet->group = group; + packet->mode = mode; + mav_array_memcpy(packet->roll, roll, sizeof(int16_t)*4); + mav_array_memcpy(packet->pitch, pitch, sizeof(int16_t)*4); + mav_array_memcpy(packet->yaw, yaw, sizeof(int16_t)*4); + mav_array_memcpy(packet->thrust, thrust, sizeof(uint16_t)*4); + mav_array_memcpy(packet->led_red, led_red, sizeof(uint8_t)*4); + mav_array_memcpy(packet->led_blue, led_blue, sizeof(uint8_t)*4); + mav_array_memcpy(packet->led_green, led_green, sizeof(uint8_t)*4); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, (const char *)packet, MAVLINK_MSG_ID_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST_LEN, MAVLINK_MSG_ID_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, (const char *)packet, MAVLINK_MSG_ID_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_quad_swarm_roll_pitch_yaw_thrust.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_quad_swarm_roll_pitch_yaw_thrust.h index 7d8d526f8..338bf0e43 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_quad_swarm_roll_pitch_yaw_thrust.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_quad_swarm_roll_pitch_yaw_thrust.h @@ -198,6 +198,46 @@ static inline void mavlink_msg_set_quad_swarm_roll_pitch_yaw_thrust_send(mavlink #endif } +#if MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_set_quad_swarm_roll_pitch_yaw_thrust_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t group, uint8_t mode, const int16_t *roll, const int16_t *pitch, const int16_t *yaw, const uint16_t *thrust) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 32, group); + _mav_put_uint8_t(buf, 33, mode); + _mav_put_int16_t_array(buf, 0, roll, 4); + _mav_put_int16_t_array(buf, 8, pitch, 4); + _mav_put_int16_t_array(buf, 16, yaw, 4); + _mav_put_uint16_t_array(buf, 24, thrust, 4); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, buf, MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST_LEN, MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, buf, MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST_LEN); +#endif +#else + mavlink_set_quad_swarm_roll_pitch_yaw_thrust_t *packet = (mavlink_set_quad_swarm_roll_pitch_yaw_thrust_t *)msgbuf; + packet->group = group; + packet->mode = mode; + mav_array_memcpy(packet->roll, roll, sizeof(int16_t)*4); + mav_array_memcpy(packet->pitch, pitch, sizeof(int16_t)*4); + mav_array_memcpy(packet->yaw, yaw, sizeof(int16_t)*4); + mav_array_memcpy(packet->thrust, thrust, sizeof(uint16_t)*4); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, (const char *)packet, MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST_LEN, MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, (const char *)packet, MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_roll_pitch_yaw_speed_thrust.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_roll_pitch_yaw_speed_thrust.h index 5846ba41f..4d0e5931f 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_roll_pitch_yaw_speed_thrust.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_roll_pitch_yaw_speed_thrust.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_set_roll_pitch_yaw_speed_thrust_send(mavlink_chan #endif } +#if MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_set_roll_pitch_yaw_speed_thrust_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, float roll_speed, float pitch_speed, float yaw_speed, float thrust) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, roll_speed); + _mav_put_float(buf, 4, pitch_speed); + _mav_put_float(buf, 8, yaw_speed); + _mav_put_float(buf, 12, thrust); + _mav_put_uint8_t(buf, 16, target_system); + _mav_put_uint8_t(buf, 17, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST, buf, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST_LEN, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST, buf, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST_LEN); +#endif +#else + mavlink_set_roll_pitch_yaw_speed_thrust_t *packet = (mavlink_set_roll_pitch_yaw_speed_thrust_t *)msgbuf; + packet->roll_speed = roll_speed; + packet->pitch_speed = pitch_speed; + packet->yaw_speed = yaw_speed; + packet->thrust = thrust; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST, (const char *)packet, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST_LEN, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST, (const char *)packet, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SET_ROLL_PITCH_YAW_SPEED_THRUST UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_roll_pitch_yaw_thrust.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_roll_pitch_yaw_thrust.h index 334fd39e3..21e0a43f2 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_roll_pitch_yaw_thrust.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_set_roll_pitch_yaw_thrust.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_set_roll_pitch_yaw_thrust_send(mavlink_channel_t #endif } +#if MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_set_roll_pitch_yaw_thrust_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, float roll, float pitch, float yaw, float thrust) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, roll); + _mav_put_float(buf, 4, pitch); + _mav_put_float(buf, 8, yaw); + _mav_put_float(buf, 12, thrust); + _mav_put_uint8_t(buf, 16, target_system); + _mav_put_uint8_t(buf, 17, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST, buf, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST_LEN, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST, buf, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST_LEN); +#endif +#else + mavlink_set_roll_pitch_yaw_thrust_t *packet = (mavlink_set_roll_pitch_yaw_thrust_t *)msgbuf; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + packet->thrust = thrust; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST, (const char *)packet, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST_LEN, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST, (const char *)packet, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SET_ROLL_PITCH_YAW_THRUST UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_setpoint_6dof.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_setpoint_6dof.h index 93ce345b6..90b63427b 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_setpoint_6dof.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_setpoint_6dof.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_setpoint_6dof_send(mavlink_channel_t chan, uint8_ #endif } +#if MAVLINK_MSG_ID_SETPOINT_6DOF_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_setpoint_6dof_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, float trans_x, float trans_y, float trans_z, float rot_x, float rot_y, float rot_z) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, trans_x); + _mav_put_float(buf, 4, trans_y); + _mav_put_float(buf, 8, trans_z); + _mav_put_float(buf, 12, rot_x); + _mav_put_float(buf, 16, rot_y); + _mav_put_float(buf, 20, rot_z); + _mav_put_uint8_t(buf, 24, target_system); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SETPOINT_6DOF, buf, MAVLINK_MSG_ID_SETPOINT_6DOF_LEN, MAVLINK_MSG_ID_SETPOINT_6DOF_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SETPOINT_6DOF, buf, MAVLINK_MSG_ID_SETPOINT_6DOF_LEN); +#endif +#else + mavlink_setpoint_6dof_t *packet = (mavlink_setpoint_6dof_t *)msgbuf; + packet->trans_x = trans_x; + packet->trans_y = trans_y; + packet->trans_z = trans_z; + packet->rot_x = rot_x; + packet->rot_y = rot_y; + packet->rot_z = rot_z; + packet->target_system = target_system; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SETPOINT_6DOF, (const char *)packet, MAVLINK_MSG_ID_SETPOINT_6DOF_LEN, MAVLINK_MSG_ID_SETPOINT_6DOF_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SETPOINT_6DOF, (const char *)packet, MAVLINK_MSG_ID_SETPOINT_6DOF_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SETPOINT_6DOF UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_setpoint_8dof.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_setpoint_8dof.h index de80e4645..308a211cd 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_setpoint_8dof.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_setpoint_8dof.h @@ -234,6 +234,54 @@ static inline void mavlink_msg_setpoint_8dof_send(mavlink_channel_t chan, uint8_ #endif } +#if MAVLINK_MSG_ID_SETPOINT_8DOF_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_setpoint_8dof_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, float val1, float val2, float val3, float val4, float val5, float val6, float val7, float val8) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, val1); + _mav_put_float(buf, 4, val2); + _mav_put_float(buf, 8, val3); + _mav_put_float(buf, 12, val4); + _mav_put_float(buf, 16, val5); + _mav_put_float(buf, 20, val6); + _mav_put_float(buf, 24, val7); + _mav_put_float(buf, 28, val8); + _mav_put_uint8_t(buf, 32, target_system); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SETPOINT_8DOF, buf, MAVLINK_MSG_ID_SETPOINT_8DOF_LEN, MAVLINK_MSG_ID_SETPOINT_8DOF_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SETPOINT_8DOF, buf, MAVLINK_MSG_ID_SETPOINT_8DOF_LEN); +#endif +#else + mavlink_setpoint_8dof_t *packet = (mavlink_setpoint_8dof_t *)msgbuf; + packet->val1 = val1; + packet->val2 = val2; + packet->val3 = val3; + packet->val4 = val4; + packet->val5 = val5; + packet->val6 = val6; + packet->val7 = val7; + packet->val8 = val8; + packet->target_system = target_system; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SETPOINT_8DOF, (const char *)packet, MAVLINK_MSG_ID_SETPOINT_8DOF_LEN, MAVLINK_MSG_ID_SETPOINT_8DOF_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SETPOINT_8DOF, (const char *)packet, MAVLINK_MSG_ID_SETPOINT_8DOF_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SETPOINT_8DOF UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_sim_state.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_sim_state.h index ebd657cf3..db3a92642 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_sim_state.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_sim_state.h @@ -366,6 +366,78 @@ static inline void mavlink_msg_sim_state_send(mavlink_channel_t chan, float q1, #endif } +#if MAVLINK_MSG_ID_SIM_STATE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_sim_state_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float q1, float q2, float q3, float q4, float roll, float pitch, float yaw, float xacc, float yacc, float zacc, float xgyro, float ygyro, float zgyro, float lat, float lon, float alt, float std_dev_horz, float std_dev_vert, float vn, float ve, float vd) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, q1); + _mav_put_float(buf, 4, q2); + _mav_put_float(buf, 8, q3); + _mav_put_float(buf, 12, q4); + _mav_put_float(buf, 16, roll); + _mav_put_float(buf, 20, pitch); + _mav_put_float(buf, 24, yaw); + _mav_put_float(buf, 28, xacc); + _mav_put_float(buf, 32, yacc); + _mav_put_float(buf, 36, zacc); + _mav_put_float(buf, 40, xgyro); + _mav_put_float(buf, 44, ygyro); + _mav_put_float(buf, 48, zgyro); + _mav_put_float(buf, 52, lat); + _mav_put_float(buf, 56, lon); + _mav_put_float(buf, 60, alt); + _mav_put_float(buf, 64, std_dev_horz); + _mav_put_float(buf, 68, std_dev_vert); + _mav_put_float(buf, 72, vn); + _mav_put_float(buf, 76, ve); + _mav_put_float(buf, 80, vd); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SIM_STATE, buf, MAVLINK_MSG_ID_SIM_STATE_LEN, MAVLINK_MSG_ID_SIM_STATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SIM_STATE, buf, MAVLINK_MSG_ID_SIM_STATE_LEN); +#endif +#else + mavlink_sim_state_t *packet = (mavlink_sim_state_t *)msgbuf; + packet->q1 = q1; + packet->q2 = q2; + packet->q3 = q3; + packet->q4 = q4; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + packet->xacc = xacc; + packet->yacc = yacc; + packet->zacc = zacc; + packet->xgyro = xgyro; + packet->ygyro = ygyro; + packet->zgyro = zgyro; + packet->lat = lat; + packet->lon = lon; + packet->alt = alt; + packet->std_dev_horz = std_dev_horz; + packet->std_dev_vert = std_dev_vert; + packet->vn = vn; + packet->ve = ve; + packet->vd = vd; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SIM_STATE, (const char *)packet, MAVLINK_MSG_ID_SIM_STATE_LEN, MAVLINK_MSG_ID_SIM_STATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SIM_STATE, (const char *)packet, MAVLINK_MSG_ID_SIM_STATE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SIM_STATE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_state_correction.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_state_correction.h index 2db627b96..be2629dd8 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_state_correction.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_state_correction.h @@ -234,6 +234,54 @@ static inline void mavlink_msg_state_correction_send(mavlink_channel_t chan, flo #endif } +#if MAVLINK_MSG_ID_STATE_CORRECTION_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_state_correction_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float xErr, float yErr, float zErr, float rollErr, float pitchErr, float yawErr, float vxErr, float vyErr, float vzErr) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, xErr); + _mav_put_float(buf, 4, yErr); + _mav_put_float(buf, 8, zErr); + _mav_put_float(buf, 12, rollErr); + _mav_put_float(buf, 16, pitchErr); + _mav_put_float(buf, 20, yawErr); + _mav_put_float(buf, 24, vxErr); + _mav_put_float(buf, 28, vyErr); + _mav_put_float(buf, 32, vzErr); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_STATE_CORRECTION, buf, MAVLINK_MSG_ID_STATE_CORRECTION_LEN, MAVLINK_MSG_ID_STATE_CORRECTION_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_STATE_CORRECTION, buf, MAVLINK_MSG_ID_STATE_CORRECTION_LEN); +#endif +#else + mavlink_state_correction_t *packet = (mavlink_state_correction_t *)msgbuf; + packet->xErr = xErr; + packet->yErr = yErr; + packet->zErr = zErr; + packet->rollErr = rollErr; + packet->pitchErr = pitchErr; + packet->yawErr = yawErr; + packet->vxErr = vxErr; + packet->vyErr = vyErr; + packet->vzErr = vzErr; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_STATE_CORRECTION, (const char *)packet, MAVLINK_MSG_ID_STATE_CORRECTION_LEN, MAVLINK_MSG_ID_STATE_CORRECTION_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_STATE_CORRECTION, (const char *)packet, MAVLINK_MSG_ID_STATE_CORRECTION_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE STATE_CORRECTION UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_statustext.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_statustext.h index 536ca0634..c8c2547b3 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_statustext.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_statustext.h @@ -151,6 +151,38 @@ static inline void mavlink_msg_statustext_send(mavlink_channel_t chan, uint8_t s #endif } +#if MAVLINK_MSG_ID_STATUSTEXT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_statustext_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t severity, const char *text) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, severity); + _mav_put_char_array(buf, 1, text, 50); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_STATUSTEXT, buf, MAVLINK_MSG_ID_STATUSTEXT_LEN, MAVLINK_MSG_ID_STATUSTEXT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_STATUSTEXT, buf, MAVLINK_MSG_ID_STATUSTEXT_LEN); +#endif +#else + mavlink_statustext_t *packet = (mavlink_statustext_t *)msgbuf; + packet->severity = severity; + mav_array_memcpy(packet->text, text, sizeof(char)*50); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_STATUSTEXT, (const char *)packet, MAVLINK_MSG_ID_STATUSTEXT_LEN, MAVLINK_MSG_ID_STATUSTEXT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_STATUSTEXT, (const char *)packet, MAVLINK_MSG_ID_STATUSTEXT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE STATUSTEXT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_sys_status.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_sys_status.h index 101b36678..1b1730d5f 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_sys_status.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_sys_status.h @@ -278,6 +278,62 @@ static inline void mavlink_msg_sys_status_send(mavlink_channel_t chan, uint32_t #endif } +#if MAVLINK_MSG_ID_SYS_STATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_sys_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t onboard_control_sensors_present, uint32_t onboard_control_sensors_enabled, uint32_t onboard_control_sensors_health, uint16_t load, uint16_t voltage_battery, int16_t current_battery, int8_t battery_remaining, uint16_t drop_rate_comm, uint16_t errors_comm, uint16_t errors_count1, uint16_t errors_count2, uint16_t errors_count3, uint16_t errors_count4) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, onboard_control_sensors_present); + _mav_put_uint32_t(buf, 4, onboard_control_sensors_enabled); + _mav_put_uint32_t(buf, 8, onboard_control_sensors_health); + _mav_put_uint16_t(buf, 12, load); + _mav_put_uint16_t(buf, 14, voltage_battery); + _mav_put_int16_t(buf, 16, current_battery); + _mav_put_uint16_t(buf, 18, drop_rate_comm); + _mav_put_uint16_t(buf, 20, errors_comm); + _mav_put_uint16_t(buf, 22, errors_count1); + _mav_put_uint16_t(buf, 24, errors_count2); + _mav_put_uint16_t(buf, 26, errors_count3); + _mav_put_uint16_t(buf, 28, errors_count4); + _mav_put_int8_t(buf, 30, battery_remaining); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SYS_STATUS, buf, MAVLINK_MSG_ID_SYS_STATUS_LEN, MAVLINK_MSG_ID_SYS_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SYS_STATUS, buf, MAVLINK_MSG_ID_SYS_STATUS_LEN); +#endif +#else + mavlink_sys_status_t *packet = (mavlink_sys_status_t *)msgbuf; + packet->onboard_control_sensors_present = onboard_control_sensors_present; + packet->onboard_control_sensors_enabled = onboard_control_sensors_enabled; + packet->onboard_control_sensors_health = onboard_control_sensors_health; + packet->load = load; + packet->voltage_battery = voltage_battery; + packet->current_battery = current_battery; + packet->drop_rate_comm = drop_rate_comm; + packet->errors_comm = errors_comm; + packet->errors_count1 = errors_count1; + packet->errors_count2 = errors_count2; + packet->errors_count3 = errors_count3; + packet->errors_count4 = errors_count4; + packet->battery_remaining = battery_remaining; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SYS_STATUS, (const char *)packet, MAVLINK_MSG_ID_SYS_STATUS_LEN, MAVLINK_MSG_ID_SYS_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SYS_STATUS, (const char *)packet, MAVLINK_MSG_ID_SYS_STATUS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SYS_STATUS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_system_time.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_system_time.h index 1807567ae..988c669c3 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_system_time.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_system_time.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_system_time_send(mavlink_channel_t chan, uint64_t #endif } +#if MAVLINK_MSG_ID_SYSTEM_TIME_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_system_time_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_unix_usec, uint32_t time_boot_ms) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, time_unix_usec); + _mav_put_uint32_t(buf, 8, time_boot_ms); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SYSTEM_TIME, buf, MAVLINK_MSG_ID_SYSTEM_TIME_LEN, MAVLINK_MSG_ID_SYSTEM_TIME_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SYSTEM_TIME, buf, MAVLINK_MSG_ID_SYSTEM_TIME_LEN); +#endif +#else + mavlink_system_time_t *packet = (mavlink_system_time_t *)msgbuf; + packet->time_unix_usec = time_unix_usec; + packet->time_boot_ms = time_boot_ms; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SYSTEM_TIME, (const char *)packet, MAVLINK_MSG_ID_SYSTEM_TIME_LEN, MAVLINK_MSG_ID_SYSTEM_TIME_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SYSTEM_TIME, (const char *)packet, MAVLINK_MSG_ID_SYSTEM_TIME_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SYSTEM_TIME UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_vfr_hud.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_vfr_hud.h index 5b1093a3d..b130ee50b 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_vfr_hud.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_vfr_hud.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_vfr_hud_send(mavlink_channel_t chan, float airspe #endif } +#if MAVLINK_MSG_ID_VFR_HUD_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_vfr_hud_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float airspeed, float groundspeed, int16_t heading, uint16_t throttle, float alt, float climb) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, airspeed); + _mav_put_float(buf, 4, groundspeed); + _mav_put_float(buf, 8, alt); + _mav_put_float(buf, 12, climb); + _mav_put_int16_t(buf, 16, heading); + _mav_put_uint16_t(buf, 18, throttle); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VFR_HUD, buf, MAVLINK_MSG_ID_VFR_HUD_LEN, MAVLINK_MSG_ID_VFR_HUD_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VFR_HUD, buf, MAVLINK_MSG_ID_VFR_HUD_LEN); +#endif +#else + mavlink_vfr_hud_t *packet = (mavlink_vfr_hud_t *)msgbuf; + packet->airspeed = airspeed; + packet->groundspeed = groundspeed; + packet->alt = alt; + packet->climb = climb; + packet->heading = heading; + packet->throttle = throttle; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VFR_HUD, (const char *)packet, MAVLINK_MSG_ID_VFR_HUD_LEN, MAVLINK_MSG_ID_VFR_HUD_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VFR_HUD, (const char *)packet, MAVLINK_MSG_ID_VFR_HUD_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE VFR_HUD UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_vicon_position_estimate.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_vicon_position_estimate.h index a254202e4..b3fa7bc1c 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_vicon_position_estimate.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_vicon_position_estimate.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_vicon_position_estimate_send(mavlink_channel_t ch #endif } +#if MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_vicon_position_estimate_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t usec, float x, float y, float z, float roll, float pitch, float yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, usec); + _mav_put_float(buf, 8, x); + _mav_put_float(buf, 12, y); + _mav_put_float(buf, 16, z); + _mav_put_float(buf, 20, roll); + _mav_put_float(buf, 24, pitch); + _mav_put_float(buf, 28, yaw); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE, buf, MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE_LEN, MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE, buf, MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE_LEN); +#endif +#else + mavlink_vicon_position_estimate_t *packet = (mavlink_vicon_position_estimate_t *)msgbuf; + packet->usec = usec; + packet->x = x; + packet->y = y; + packet->z = z; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE, (const char *)packet, MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE_LEN, MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE, (const char *)packet, MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE VICON_POSITION_ESTIMATE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_vision_position_estimate.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_vision_position_estimate.h index f7a741b09..8f82fb682 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_vision_position_estimate.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_vision_position_estimate.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_vision_position_estimate_send(mavlink_channel_t c #endif } +#if MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_vision_position_estimate_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t usec, float x, float y, float z, float roll, float pitch, float yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, usec); + _mav_put_float(buf, 8, x); + _mav_put_float(buf, 12, y); + _mav_put_float(buf, 16, z); + _mav_put_float(buf, 20, roll); + _mav_put_float(buf, 24, pitch); + _mav_put_float(buf, 28, yaw); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE, buf, MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE_LEN, MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE, buf, MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE_LEN); +#endif +#else + mavlink_vision_position_estimate_t *packet = (mavlink_vision_position_estimate_t *)msgbuf; + packet->usec = usec; + packet->x = x; + packet->y = y; + packet->z = z; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE, (const char *)packet, MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE_LEN, MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE, (const char *)packet, MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE VISION_POSITION_ESTIMATE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_vision_speed_estimate.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_vision_speed_estimate.h index 660225128..7528014c7 100644 --- a/mavlink/include/mavlink/v1.0/common/mavlink_msg_vision_speed_estimate.h +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_vision_speed_estimate.h @@ -179,6 +179,44 @@ static inline void mavlink_msg_vision_speed_estimate_send(mavlink_channel_t chan #endif } +#if MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_vision_speed_estimate_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t usec, float x, float y, float z) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, usec); + _mav_put_float(buf, 8, x); + _mav_put_float(buf, 12, y); + _mav_put_float(buf, 16, z); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE, buf, MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE_LEN, MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE, buf, MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE_LEN); +#endif +#else + mavlink_vision_speed_estimate_t *packet = (mavlink_vision_speed_estimate_t *)msgbuf; + packet->usec = usec; + packet->x = x; + packet->y = y; + packet->z = z; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE, (const char *)packet, MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE_LEN, MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE, (const char *)packet, MAVLINK_MSG_ID_VISION_SPEED_ESTIMATE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE VISION_SPEED_ESTIMATE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/common/testsuite.h b/mavlink/include/mavlink/v1.0/common/testsuite.h index c5aa9ddf3..de23fcb2a 100644 --- a/mavlink/include/mavlink/v1.0/common/testsuite.h +++ b/mavlink/include/mavlink/v1.0/common/testsuite.h @@ -2805,6 +2805,89 @@ static void mavlink_test_state_correction(uint8_t system_id, uint8_t component_i MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); } +static void mavlink_test_rc_channels(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg) +{ + mavlink_message_t msg; + uint8_t buffer[MAVLINK_MAX_PACKET_LEN]; + uint16_t i; + mavlink_rc_channels_t packet_in = { + 963497464, + }17443, + }17547, + }17651, + }17755, + }17859, + }17963, + }18067, + }18171, + }18275, + }18379, + }18483, + }18587, + }18691, + }18795, + }18899, + }19003, + }19107, + }19211, + }125, + }192, + }; + mavlink_rc_channels_t packet1, packet2; + memset(&packet1, 0, sizeof(packet1)); + packet1.time_boot_ms = packet_in.time_boot_ms; + packet1.chan1_raw = packet_in.chan1_raw; + packet1.chan2_raw = packet_in.chan2_raw; + packet1.chan3_raw = packet_in.chan3_raw; + packet1.chan4_raw = packet_in.chan4_raw; + packet1.chan5_raw = packet_in.chan5_raw; + packet1.chan6_raw = packet_in.chan6_raw; + packet1.chan7_raw = packet_in.chan7_raw; + packet1.chan8_raw = packet_in.chan8_raw; + packet1.chan9_raw = packet_in.chan9_raw; + packet1.chan10_raw = packet_in.chan10_raw; + packet1.chan11_raw = packet_in.chan11_raw; + packet1.chan12_raw = packet_in.chan12_raw; + packet1.chan13_raw = packet_in.chan13_raw; + packet1.chan14_raw = packet_in.chan14_raw; + packet1.chan15_raw = packet_in.chan15_raw; + packet1.chan16_raw = packet_in.chan16_raw; + packet1.chan17_raw = packet_in.chan17_raw; + packet1.chan18_raw = packet_in.chan18_raw; + packet1.chancount = packet_in.chancount; + packet1.rssi = packet_in.rssi; + + + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_rc_channels_encode(system_id, component_id, &msg, &packet1); + mavlink_msg_rc_channels_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_rc_channels_pack(system_id, component_id, &msg , packet1.time_boot_ms , packet1.chancount , packet1.chan1_raw , packet1.chan2_raw , packet1.chan3_raw , packet1.chan4_raw , packet1.chan5_raw , packet1.chan6_raw , packet1.chan7_raw , packet1.chan8_raw , packet1.chan9_raw , packet1.chan10_raw , packet1.chan11_raw , packet1.chan12_raw , packet1.chan13_raw , packet1.chan14_raw , packet1.chan15_raw , packet1.chan16_raw , packet1.chan17_raw , packet1.chan18_raw , packet1.rssi ); + mavlink_msg_rc_channels_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_rc_channels_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.time_boot_ms , packet1.chancount , packet1.chan1_raw , packet1.chan2_raw , packet1.chan3_raw , packet1.chan4_raw , packet1.chan5_raw , packet1.chan6_raw , packet1.chan7_raw , packet1.chan8_raw , packet1.chan9_raw , packet1.chan10_raw , packet1.chan11_raw , packet1.chan12_raw , packet1.chan13_raw , packet1.chan14_raw , packet1.chan15_raw , packet1.chan16_raw , packet1.chan17_raw , packet1.chan18_raw , packet1.rssi ); + mavlink_msg_rc_channels_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_to_send_buffer(buffer, &msg); + for (i=0; i<mavlink_msg_get_send_buffer_length(&msg); i++) { + comm_send_ch(MAVLINK_COMM_0, buffer[i]); + } + mavlink_msg_rc_channels_decode(last_msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_rc_channels_send(MAVLINK_COMM_1 , packet1.time_boot_ms , packet1.chancount , packet1.chan1_raw , packet1.chan2_raw , packet1.chan3_raw , packet1.chan4_raw , packet1.chan5_raw , packet1.chan6_raw , packet1.chan7_raw , packet1.chan8_raw , packet1.chan9_raw , packet1.chan10_raw , packet1.chan11_raw , packet1.chan12_raw , packet1.chan13_raw , packet1.chan14_raw , packet1.chan15_raw , packet1.chan16_raw , packet1.chan17_raw , packet1.chan18_raw , packet1.rssi ); + mavlink_msg_rc_channels_decode(last_msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); +} + static void mavlink_test_request_data_stream(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg) { mavlink_message_t msg; @@ -4953,6 +5036,106 @@ static void mavlink_test_gps2_raw(uint8_t system_id, uint8_t component_id, mavli MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); } +static void mavlink_test_power_status(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg) +{ + mavlink_message_t msg; + uint8_t buffer[MAVLINK_MAX_PACKET_LEN]; + uint16_t i; + mavlink_power_status_t packet_in = { + 17235, + }17339, + }17443, + }; + mavlink_power_status_t packet1, packet2; + memset(&packet1, 0, sizeof(packet1)); + packet1.Vcc = packet_in.Vcc; + packet1.Vservo = packet_in.Vservo; + packet1.flags = packet_in.flags; + + + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_power_status_encode(system_id, component_id, &msg, &packet1); + mavlink_msg_power_status_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_power_status_pack(system_id, component_id, &msg , packet1.Vcc , packet1.Vservo , packet1.flags ); + mavlink_msg_power_status_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_power_status_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.Vcc , packet1.Vservo , packet1.flags ); + mavlink_msg_power_status_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_to_send_buffer(buffer, &msg); + for (i=0; i<mavlink_msg_get_send_buffer_length(&msg); i++) { + comm_send_ch(MAVLINK_COMM_0, buffer[i]); + } + mavlink_msg_power_status_decode(last_msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_power_status_send(MAVLINK_COMM_1 , packet1.Vcc , packet1.Vservo , packet1.flags ); + mavlink_msg_power_status_decode(last_msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); +} + +static void mavlink_test_serial_control(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg) +{ + mavlink_message_t msg; + uint8_t buffer[MAVLINK_MAX_PACKET_LEN]; + uint16_t i; + mavlink_serial_control_t packet_in = { + 963497464, + }17443, + }151, + }218, + }29, + }{ 96, 97, 98, 99, 100, 101, 102, 103, 104, 105, 106, 107, 108, 109, 110, 111, 112, 113, 114, 115, 116, 117, 118, 119, 120, 121, 122, 123, 124, 125, 126, 127, 128, 129, 130, 131, 132, 133, 134, 135, 136, 137, 138, 139, 140, 141, 142, 143, 144, 145, 146, 147, 148, 149, 150, 151, 152, 153, 154, 155, 156, 157, 158, 159, 160, 161, 162, 163, 164, 165 }, + }; + mavlink_serial_control_t packet1, packet2; + memset(&packet1, 0, sizeof(packet1)); + packet1.baudrate = packet_in.baudrate; + packet1.timeout = packet_in.timeout; + packet1.device = packet_in.device; + packet1.flags = packet_in.flags; + packet1.count = packet_in.count; + + mav_array_memcpy(packet1.data, packet_in.data, sizeof(uint8_t)*70); + + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_serial_control_encode(system_id, component_id, &msg, &packet1); + mavlink_msg_serial_control_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_serial_control_pack(system_id, component_id, &msg , packet1.device , packet1.flags , packet1.timeout , packet1.baudrate , packet1.count , packet1.data ); + mavlink_msg_serial_control_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_serial_control_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.device , packet1.flags , packet1.timeout , packet1.baudrate , packet1.count , packet1.data ); + mavlink_msg_serial_control_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_to_send_buffer(buffer, &msg); + for (i=0; i<mavlink_msg_get_send_buffer_length(&msg); i++) { + comm_send_ch(MAVLINK_COMM_0, buffer[i]); + } + mavlink_msg_serial_control_decode(last_msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_serial_control_send(MAVLINK_COMM_1 , packet1.device , packet1.flags , packet1.timeout , packet1.baudrate , packet1.count , packet1.data ); + mavlink_msg_serial_control_decode(last_msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); +} + static void mavlink_test_data_transmission_handshake(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg) { mavlink_message_t msg; @@ -5053,6 +5236,63 @@ static void mavlink_test_encapsulated_data(uint8_t system_id, uint8_t component_ MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); } +static void mavlink_test_distance_sensor(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg) +{ + mavlink_message_t msg; + uint8_t buffer[MAVLINK_MAX_PACKET_LEN]; + uint16_t i; + mavlink_distance_sensor_t packet_in = { + 963497464, + }17443, + }17547, + }17651, + }163, + }230, + }41, + }108, + }; + mavlink_distance_sensor_t packet1, packet2; + memset(&packet1, 0, sizeof(packet1)); + packet1.time_boot_ms = packet_in.time_boot_ms; + packet1.min_distance = packet_in.min_distance; + packet1.max_distance = packet_in.max_distance; + packet1.current_distance = packet_in.current_distance; + packet1.type = packet_in.type; + packet1.id = packet_in.id; + packet1.orientation = packet_in.orientation; + packet1.covariance = packet_in.covariance; + + + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_distance_sensor_encode(system_id, component_id, &msg, &packet1); + mavlink_msg_distance_sensor_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_distance_sensor_pack(system_id, component_id, &msg , packet1.time_boot_ms , packet1.type , packet1.id , packet1.orientation , packet1.min_distance , packet1.max_distance , packet1.current_distance , packet1.covariance ); + mavlink_msg_distance_sensor_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_distance_sensor_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.time_boot_ms , packet1.type , packet1.id , packet1.orientation , packet1.min_distance , packet1.max_distance , packet1.current_distance , packet1.covariance ); + mavlink_msg_distance_sensor_decode(&msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_to_send_buffer(buffer, &msg); + for (i=0; i<mavlink_msg_get_send_buffer_length(&msg); i++) { + comm_send_ch(MAVLINK_COMM_0, buffer[i]); + } + mavlink_msg_distance_sensor_decode(last_msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); + + memset(&packet2, 0, sizeof(packet2)); + mavlink_msg_distance_sensor_send(MAVLINK_COMM_1 , packet1.time_boot_ms , packet1.type , packet1.id , packet1.orientation , packet1.min_distance , packet1.max_distance , packet1.current_distance , packet1.covariance ); + mavlink_msg_distance_sensor_decode(last_msg, &packet2); + MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0); +} + static void mavlink_test_battery_status(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg) { mavlink_message_t msg; @@ -5571,6 +5811,7 @@ static void mavlink_test_common(uint8_t system_id, uint8_t component_id, mavlink mavlink_test_nav_controller_output(system_id, component_id, last_msg); mavlink_test_set_quad_swarm_led_roll_pitch_yaw_thrust(system_id, component_id, last_msg); mavlink_test_state_correction(system_id, component_id, last_msg); + mavlink_test_rc_channels(system_id, component_id, last_msg); mavlink_test_request_data_stream(system_id, component_id, last_msg); mavlink_test_data_stream(system_id, component_id, last_msg); mavlink_test_manual_control(system_id, component_id, last_msg); @@ -5609,8 +5850,11 @@ static void mavlink_test_common(uint8_t system_id, uint8_t component_id, mavlink mavlink_test_log_request_end(system_id, component_id, last_msg); mavlink_test_gps_inject_data(system_id, component_id, last_msg); mavlink_test_gps2_raw(system_id, component_id, last_msg); + mavlink_test_power_status(system_id, component_id, last_msg); + mavlink_test_serial_control(system_id, component_id, last_msg); mavlink_test_data_transmission_handshake(system_id, component_id, last_msg); mavlink_test_encapsulated_data(system_id, component_id, last_msg); + mavlink_test_distance_sensor(system_id, component_id, last_msg); mavlink_test_battery_status(system_id, component_id, last_msg); mavlink_test_setpoint_8dof(system_id, component_id, last_msg); mavlink_test_setpoint_6dof(system_id, component_id, last_msg); diff --git a/mavlink/include/mavlink/v1.0/common/version.h b/mavlink/include/mavlink/v1.0/common/version.h index 2f3736f45..8ad378355 100644 --- a/mavlink/include/mavlink/v1.0/common/version.h +++ b/mavlink/include/mavlink/v1.0/common/version.h @@ -5,7 +5,7 @@ #ifndef MAVLINK_VERSION_H #define MAVLINK_VERSION_H -#define MAVLINK_BUILD_DATE "Tue Feb 4 15:28:29 2014" +#define MAVLINK_BUILD_DATE "Sun Apr 13 09:39:04 2014" #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0" #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255 diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/matrixpilot.h b/mavlink/include/mavlink/v1.0/matrixpilot/matrixpilot.h index 2f15d31c4..cc7545cfe 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/matrixpilot.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/matrixpilot.h @@ -12,15 +12,15 @@ extern "C" { // MESSAGE LENGTHS AND CRCS #ifndef MAVLINK_MESSAGE_LENGTHS -#define MAVLINK_MESSAGE_LENGTHS {9, 31, 12, 0, 14, 28, 3, 32, 0, 0, 0, 6, 0, 0, 0, 0, 0, 0, 0, 0, 20, 2, 25, 23, 30, 101, 22, 26, 16, 14, 28, 32, 28, 28, 22, 22, 21, 6, 6, 37, 4, 4, 2, 2, 4, 2, 2, 3, 13, 12, 19, 17, 15, 15, 27, 25, 18, 18, 20, 20, 9, 34, 26, 46, 36, 0, 6, 4, 0, 11, 18, 0, 0, 0, 20, 0, 33, 3, 0, 0, 20, 22, 0, 0, 0, 0, 0, 0, 0, 28, 56, 42, 33, 0, 0, 0, 0, 0, 0, 0, 26, 32, 32, 20, 32, 62, 54, 64, 84, 9, 254, 249, 9, 36, 26, 64, 22, 6, 14, 12, 97, 2, 2, 113, 35, 0, 0, 0, 0, 0, 13, 255, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 24, 33, 25, 2, 6, 58, 6, 0, 53, 7, 3, 4, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 63, 70, 10, 24, 20, 24, 28, 14, 17, 60, 110, 28, 16, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 30, 18, 18, 51, 9, 0} +#define MAVLINK_MESSAGE_LENGTHS {9, 31, 12, 0, 14, 28, 3, 32, 0, 0, 0, 6, 0, 0, 0, 0, 0, 0, 0, 0, 20, 2, 25, 23, 30, 101, 22, 26, 16, 14, 28, 32, 28, 28, 22, 22, 21, 6, 6, 37, 4, 4, 2, 2, 4, 2, 2, 3, 13, 12, 19, 17, 15, 15, 27, 25, 18, 18, 20, 20, 9, 34, 26, 46, 36, 42, 6, 4, 0, 11, 18, 0, 0, 0, 20, 0, 33, 3, 0, 0, 20, 22, 0, 0, 0, 0, 0, 0, 0, 28, 56, 42, 33, 0, 0, 0, 0, 0, 0, 0, 26, 32, 32, 20, 32, 62, 54, 64, 84, 9, 254, 249, 9, 36, 26, 64, 22, 6, 14, 12, 97, 2, 2, 113, 35, 6, 79, 0, 0, 0, 13, 255, 14, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 24, 33, 25, 2, 6, 58, 6, 0, 53, 7, 3, 4, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 63, 70, 10, 24, 20, 24, 28, 14, 17, 60, 110, 28, 16, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 30, 18, 18, 51, 9, 0} #endif #ifndef MAVLINK_MESSAGE_CRCS -#define MAVLINK_MESSAGE_CRCS {50, 124, 137, 0, 237, 217, 104, 119, 0, 0, 0, 89, 0, 0, 0, 0, 0, 0, 0, 0, 214, 159, 220, 168, 24, 23, 170, 144, 67, 115, 39, 246, 185, 104, 237, 244, 222, 212, 9, 254, 230, 28, 28, 132, 221, 232, 11, 153, 41, 39, 214, 223, 141, 33, 15, 3, 100, 24, 239, 238, 30, 240, 183, 130, 130, 0, 148, 21, 0, 243, 124, 0, 0, 0, 20, 0, 152, 143, 0, 0, 127, 106, 0, 0, 0, 0, 0, 0, 0, 231, 183, 63, 54, 0, 0, 0, 0, 0, 0, 0, 175, 102, 158, 208, 56, 93, 211, 108, 32, 185, 235, 93, 124, 124, 119, 4, 76, 128, 56, 116, 134, 237, 203, 250, 87, 0, 0, 0, 0, 0, 29, 223, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 177, 241, 15, 181, 26, 101, 109, 0, 12, 218, 133, 208, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 150, 169, 191, 121, 54, 171, 142, 249, 123, 7, 222, 55, 154, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 204, 49, 170, 44, 83, 46, 0} +#define MAVLINK_MESSAGE_CRCS {50, 124, 137, 0, 237, 217, 104, 119, 0, 0, 0, 89, 0, 0, 0, 0, 0, 0, 0, 0, 214, 159, 220, 168, 24, 23, 170, 144, 67, 115, 39, 246, 185, 104, 237, 244, 222, 212, 9, 254, 230, 28, 28, 132, 221, 232, 11, 153, 41, 39, 214, 223, 141, 33, 15, 3, 100, 24, 239, 238, 30, 240, 183, 130, 130, 118, 148, 21, 0, 243, 124, 0, 0, 0, 20, 0, 152, 143, 0, 0, 127, 106, 0, 0, 0, 0, 0, 0, 0, 231, 183, 63, 54, 0, 0, 0, 0, 0, 0, 0, 175, 102, 158, 208, 56, 93, 211, 108, 32, 185, 235, 93, 124, 124, 119, 4, 76, 128, 56, 116, 134, 237, 203, 250, 87, 203, 220, 0, 0, 0, 29, 223, 85, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 177, 241, 15, 181, 26, 101, 109, 0, 12, 218, 133, 208, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 150, 169, 191, 121, 54, 171, 142, 249, 123, 7, 222, 55, 154, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 204, 49, 170, 44, 83, 46, 0} #endif #ifndef MAVLINK_MESSAGE_INFO -#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_MODE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_ATTITUDE_QUATERNION, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_WRITE_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_ITEM, MAVLINK_MESSAGE_INFO_MISSION_REQUEST, MAVLINK_MESSAGE_INFO_MISSION_SET_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_LIST, MAVLINK_MESSAGE_INFO_MISSION_COUNT, MAVLINK_MESSAGE_INFO_MISSION_CLEAR_ALL, MAVLINK_MESSAGE_INFO_MISSION_ITEM_REACHED, MAVLINK_MESSAGE_INFO_MISSION_ACK, MAVLINK_MESSAGE_INFO_SET_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_SET_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SET_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_MOTORS_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_DATA_STREAM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_VFR_HUD, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_COMMAND_LONG, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_MANUAL_SETPOINT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_HIL_RC_INPUTS_RAW, 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MAVLINK_MESSAGE_INFO_SCALED_IMU2, MAVLINK_MESSAGE_INFO_LOG_REQUEST_LIST, MAVLINK_MESSAGE_INFO_LOG_ENTRY, MAVLINK_MESSAGE_INFO_LOG_REQUEST_DATA, MAVLINK_MESSAGE_INFO_LOG_DATA, MAVLINK_MESSAGE_INFO_LOG_ERASE, MAVLINK_MESSAGE_INFO_LOG_REQUEST_END, MAVLINK_MESSAGE_INFO_GPS_INJECT_DATA, MAVLINK_MESSAGE_INFO_GPS2_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_DATA_TRANSMISSION_HANDSHAKE, MAVLINK_MESSAGE_INFO_ENCAPSULATED_DATA, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, 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{"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F2_A, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F2_B, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F4, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F5, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F6, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F7, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F8, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F13, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F14, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F15, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F16, MAVLINK_MESSAGE_INFO_ALTITUDES, 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{"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MEMORY_VECT, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}} +#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_MODE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_ATTITUDE_QUATERNION, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_WRITE_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_ITEM, MAVLINK_MESSAGE_INFO_MISSION_REQUEST, MAVLINK_MESSAGE_INFO_MISSION_SET_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_LIST, MAVLINK_MESSAGE_INFO_MISSION_COUNT, MAVLINK_MESSAGE_INFO_MISSION_CLEAR_ALL, MAVLINK_MESSAGE_INFO_MISSION_ITEM_REACHED, MAVLINK_MESSAGE_INFO_MISSION_ACK, MAVLINK_MESSAGE_INFO_SET_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_SET_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SET_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_MOTORS_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, MAVLINK_MESSAGE_INFO_RC_CHANNELS, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_DATA_STREAM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_VFR_HUD, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_COMMAND_LONG, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_MANUAL_SETPOINT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_HIL_RC_INPUTS_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_GLOBAL_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_SPEED_ESTIMATE, MAVLINK_MESSAGE_INFO_VICON_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_HIGHRES_IMU, MAVLINK_MESSAGE_INFO_OMNIDIRECTIONAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_SENSOR, MAVLINK_MESSAGE_INFO_SIM_STATE, MAVLINK_MESSAGE_INFO_RADIO_STATUS, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_START, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_DIR_LIST, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_RES, MAVLINK_MESSAGE_INFO_HIL_GPS, MAVLINK_MESSAGE_INFO_HIL_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION, MAVLINK_MESSAGE_INFO_SCALED_IMU2, MAVLINK_MESSAGE_INFO_LOG_REQUEST_LIST, MAVLINK_MESSAGE_INFO_LOG_ENTRY, MAVLINK_MESSAGE_INFO_LOG_REQUEST_DATA, MAVLINK_MESSAGE_INFO_LOG_DATA, MAVLINK_MESSAGE_INFO_LOG_ERASE, MAVLINK_MESSAGE_INFO_LOG_REQUEST_END, MAVLINK_MESSAGE_INFO_GPS_INJECT_DATA, MAVLINK_MESSAGE_INFO_GPS2_RAW, MAVLINK_MESSAGE_INFO_POWER_STATUS, MAVLINK_MESSAGE_INFO_SERIAL_CONTROL, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_DATA_TRANSMISSION_HANDSHAKE, MAVLINK_MESSAGE_INFO_ENCAPSULATED_DATA, MAVLINK_MESSAGE_INFO_DISTANCE_SENSOR, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_BATTERY_STATUS, MAVLINK_MESSAGE_INFO_SETPOINT_8DOF, MAVLINK_MESSAGE_INFO_SETPOINT_6DOF, MAVLINK_MESSAGE_INFO_FLEXIFUNCTION_SET, MAVLINK_MESSAGE_INFO_FLEXIFUNCTION_READ_REQ, MAVLINK_MESSAGE_INFO_FLEXIFUNCTION_BUFFER_FUNCTION, MAVLINK_MESSAGE_INFO_FLEXIFUNCTION_BUFFER_FUNCTION_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_FLEXIFUNCTION_DIRECTORY, MAVLINK_MESSAGE_INFO_FLEXIFUNCTION_DIRECTORY_ACK, MAVLINK_MESSAGE_INFO_FLEXIFUNCTION_COMMAND, MAVLINK_MESSAGE_INFO_FLEXIFUNCTION_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F2_A, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F2_B, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F4, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F5, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F6, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F7, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F8, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F13, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F14, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F15, MAVLINK_MESSAGE_INFO_SERIAL_UDB_EXTRA_F16, MAVLINK_MESSAGE_INFO_ALTITUDES, MAVLINK_MESSAGE_INFO_AIRSPEEDS, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MEMORY_VECT, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}} #endif #include "../protocol.h" @@ -61,6 +61,7 @@ enum MAV_CMD MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer| Latitude| Longitude| Altitude| */ MAV_CMD_NAV_ROI=80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */ MAV_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */ + MAV_CMD_NAV_SPLINE_WAYPOINT=82, /* Navigate to MISSION using a spline path. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Empty| Empty| Empty| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */ MAV_CMD_NAV_LAST=95, /* NOP - This command is only used to mark the upper limit of the NAV/ACTION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ MAV_CMD_CONDITION_DELAY=112, /* Delay mission state machine. |Delay in seconds (decimal)| Empty| Empty| Empty| Empty| Empty| Empty| */ MAV_CMD_CONDITION_CHANGE_ALT=113, /* Ascend/descend at rate. Delay mission state machine until desired altitude reached. |Descent / Ascend rate (m/s)| Empty| Empty| Empty| Empty| Empty| Finish Altitude| */ @@ -78,8 +79,16 @@ enum MAV_CMD MAV_CMD_DO_REPEAT_SERVO=184, /* Cycle a between its nominal setting and a desired PWM for a desired number of cycles with a desired period. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Cycle count| Cycle time (seconds)| Empty| Empty| Empty| */ MAV_CMD_DO_CONTROL_VIDEO=200, /* Control onboard camera system. |Camera ID (-1 for all)| Transmission: 0: disabled, 1: enabled compressed, 2: enabled raw| Transmission mode: 0: video stream, >0: single images every n seconds (decimal)| Recording: 0: disabled, 1: enabled compressed, 2: enabled raw| Empty| Empty| Empty| */ MAV_CMD_DO_SET_ROI=201, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */ + MAV_CMD_DO_DIGICAM_CONFIGURE=202, /* Mission command to configure an on-board camera controller system. |Modes: P, TV, AV, M, Etc| Shutter speed: Divisor number for one second| Aperture: F stop number| ISO number e.g. 80, 100, 200, Etc| Exposure type enumerator| Command Identity| Main engine cut-off time before camera trigger in seconds/10 (0 means no cut-off)| */ + MAV_CMD_DO_DIGICAM_CONTROL=203, /* Mission command to control an on-board camera controller system. |Session control e.g. show/hide lens| Zoom's absolute position| Zooming step value to offset zoom from the current position| Focus Locking, Unlocking or Re-locking| Shooting Command| Command Identity| Empty| */ + MAV_CMD_DO_MOUNT_CONFIGURE=204, /* Mission command to configure a camera or antenna mount |Mount operation mode (see MAV_MOUNT_MODE enum)| stabilize roll? (1 = yes, 0 = no)| stabilize pitch? (1 = yes, 0 = no)| stabilize yaw? (1 = yes, 0 = no)| Empty| Empty| Empty| */ + MAV_CMD_DO_MOUNT_CONTROL=205, /* Mission command to control a camera or antenna mount |pitch or lat in degrees, depending on mount mode.| roll or lon in degrees depending on mount mode| yaw or alt (in meters) depending on mount mode| reserved| reserved| reserved| MAV_MOUNT_MODE enum value| */ + MAV_CMD_DO_SET_CAM_TRIGG_DIST=206, /* Mission command to set CAM_TRIGG_DIST for this flight |Camera trigger distance (meters)| Empty| Empty| Empty| Empty| Empty| Empty| */ + MAV_CMD_DO_FENCE_ENABLE=207, /* Mission command to enable the geofence |enable? (0=disable, 1=enable)| Empty| Empty| Empty| Empty| Empty| Empty| */ + MAV_CMD_DO_PARACHUTE=208, /* Mission command to trigger a parachute |action (0=disable, 1=enable, 2=release, for some systems see PARACHUTE_ACTION enum, not in general message set.)| Empty| Empty| Empty| Empty| Empty| Empty| */ + MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1| q2 - quaternion param #2| q3 - quaternion param #3| q4 - quaternion param #4| Empty| Empty| Empty| */ MAV_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_PREFLIGHT_CALIBRATION=241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Empty| Empty| */ + MAV_CMD_PREFLIGHT_CALIBRATION=241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Compass/Motor interference calibration: 0: no, 1: yes| Empty| */ MAV_CMD_PREFLIGHT_SET_SENSOR_OFFSETS=242, /* Set sensor offsets. This command will be only accepted if in pre-flight mode. |Sensor to adjust the offsets for: 0: gyros, 1: accelerometer, 2: magnetometer, 3: barometer, 4: optical flow| X axis offset (or generic dimension 1), in the sensor's raw units| Y axis offset (or generic dimension 2), in the sensor's raw units| Z axis offset (or generic dimension 3), in the sensor's raw units| Generic dimension 4, in the sensor's raw units| Generic dimension 5, in the sensor's raw units| Generic dimension 6, in the sensor's raw units| */ MAV_CMD_PREFLIGHT_STORAGE=245, /* Request storage of different parameter values and logs. This command will be only accepted if in pre-flight mode. |Parameter storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Mission storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Reserved| Reserved| Empty| Empty| Empty| */ MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN=246, /* Request the reboot or shutdown of system components. |0: Do nothing for autopilot, 1: Reboot autopilot, 2: Shutdown autopilot.| 0: Do nothing for onboard computer, 1: Reboot onboard computer, 2: Shutdown onboard computer.| Reserved| Reserved| Empty| Empty| Empty| */ diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_airspeeds.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_airspeeds.h index bc47a547a..c834a3df0 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_airspeeds.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_airspeeds.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_airspeeds_send(mavlink_channel_t chan, uint32_t t #endif } +#if MAVLINK_MSG_ID_AIRSPEEDS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_airspeeds_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, int16_t airspeed_imu, int16_t airspeed_pitot, int16_t airspeed_hot_wire, int16_t airspeed_ultrasonic, int16_t aoa, int16_t aoy) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_int16_t(buf, 4, airspeed_imu); + _mav_put_int16_t(buf, 6, airspeed_pitot); + _mav_put_int16_t(buf, 8, airspeed_hot_wire); + _mav_put_int16_t(buf, 10, airspeed_ultrasonic); + _mav_put_int16_t(buf, 12, aoa); + _mav_put_int16_t(buf, 14, aoy); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEEDS, buf, MAVLINK_MSG_ID_AIRSPEEDS_LEN, MAVLINK_MSG_ID_AIRSPEEDS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEEDS, buf, MAVLINK_MSG_ID_AIRSPEEDS_LEN); +#endif +#else + mavlink_airspeeds_t *packet = (mavlink_airspeeds_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->airspeed_imu = airspeed_imu; + packet->airspeed_pitot = airspeed_pitot; + packet->airspeed_hot_wire = airspeed_hot_wire; + packet->airspeed_ultrasonic = airspeed_ultrasonic; + packet->aoa = aoa; + packet->aoy = aoy; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEEDS, (const char *)packet, MAVLINK_MSG_ID_AIRSPEEDS_LEN, MAVLINK_MSG_ID_AIRSPEEDS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AIRSPEEDS, (const char *)packet, MAVLINK_MSG_ID_AIRSPEEDS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE AIRSPEEDS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_altitudes.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_altitudes.h index e64787cc7..b009068ff 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_altitudes.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_altitudes.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_altitudes_send(mavlink_channel_t chan, uint32_t t #endif } +#if MAVLINK_MSG_ID_ALTITUDES_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_altitudes_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_boot_ms, int32_t alt_gps, int32_t alt_imu, int32_t alt_barometric, int32_t alt_optical_flow, int32_t alt_range_finder, int32_t alt_extra) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, time_boot_ms); + _mav_put_int32_t(buf, 4, alt_gps); + _mav_put_int32_t(buf, 8, alt_imu); + _mav_put_int32_t(buf, 12, alt_barometric); + _mav_put_int32_t(buf, 16, alt_optical_flow); + _mav_put_int32_t(buf, 20, alt_range_finder); + _mav_put_int32_t(buf, 24, alt_extra); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ALTITUDES, buf, MAVLINK_MSG_ID_ALTITUDES_LEN, MAVLINK_MSG_ID_ALTITUDES_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ALTITUDES, buf, MAVLINK_MSG_ID_ALTITUDES_LEN); +#endif +#else + mavlink_altitudes_t *packet = (mavlink_altitudes_t *)msgbuf; + packet->time_boot_ms = time_boot_ms; + packet->alt_gps = alt_gps; + packet->alt_imu = alt_imu; + packet->alt_barometric = alt_barometric; + packet->alt_optical_flow = alt_optical_flow; + packet->alt_range_finder = alt_range_finder; + packet->alt_extra = alt_extra; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ALTITUDES, (const char *)packet, MAVLINK_MSG_ID_ALTITUDES_LEN, MAVLINK_MSG_ID_ALTITUDES_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ALTITUDES, (const char *)packet, MAVLINK_MSG_ID_ALTITUDES_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE ALTITUDES UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_buffer_function.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_buffer_function.h index 581bd35dc..e7b803a14 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_buffer_function.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_buffer_function.h @@ -206,6 +206,48 @@ static inline void mavlink_msg_flexifunction_buffer_function_send(mavlink_channe #endif } +#if MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_flexifunction_buffer_function_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint16_t func_index, uint16_t func_count, uint16_t data_address, uint16_t data_size, const int8_t *data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, func_index); + _mav_put_uint16_t(buf, 2, func_count); + _mav_put_uint16_t(buf, 4, data_address); + _mav_put_uint16_t(buf, 6, data_size); + _mav_put_uint8_t(buf, 8, target_system); + _mav_put_uint8_t(buf, 9, target_component); + _mav_put_int8_t_array(buf, 10, data, 48); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_LEN); +#endif +#else + mavlink_flexifunction_buffer_function_t *packet = (mavlink_flexifunction_buffer_function_t *)msgbuf; + packet->func_index = func_index; + packet->func_count = func_count; + packet->data_address = data_address; + packet->data_size = data_size; + packet->target_system = target_system; + packet->target_component = target_component; + mav_array_memcpy(packet->data, data, sizeof(int8_t)*48); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FLEXIFUNCTION_BUFFER_FUNCTION UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_buffer_function_ack.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_buffer_function_ack.h index 790afd52b..06631b40e 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_buffer_function_ack.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_buffer_function_ack.h @@ -179,6 +179,44 @@ static inline void mavlink_msg_flexifunction_buffer_function_ack_send(mavlink_ch #endif } +#if MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_ACK_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_flexifunction_buffer_function_ack_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint16_t func_index, uint16_t result) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, func_index); + _mav_put_uint16_t(buf, 2, result); + _mav_put_uint8_t(buf, 4, target_system); + _mav_put_uint8_t(buf, 5, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_ACK, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_ACK_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_ACK, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_ACK_LEN); +#endif +#else + mavlink_flexifunction_buffer_function_ack_t *packet = (mavlink_flexifunction_buffer_function_ack_t *)msgbuf; + packet->func_index = func_index; + packet->result = result; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_ACK, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_ACK_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_ACK, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_BUFFER_FUNCTION_ACK_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FLEXIFUNCTION_BUFFER_FUNCTION_ACK UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_command.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_command.h index ce722c8a4..ac8366eef 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_command.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_command.h @@ -168,6 +168,42 @@ static inline void mavlink_msg_flexifunction_command_send(mavlink_channel_t chan #endif } +#if MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_flexifunction_command_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t command_type) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + _mav_put_uint8_t(buf, 2, command_type); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_LEN); +#endif +#else + mavlink_flexifunction_command_t *packet = (mavlink_flexifunction_command_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + packet->command_type = command_type; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FLEXIFUNCTION_COMMAND UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_command_ack.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_command_ack.h index 070dc4bf8..c88e2dc39 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_command_ack.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_command_ack.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_flexifunction_command_ack_send(mavlink_channel_t #endif } +#if MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_ACK_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_flexifunction_command_ack_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t command_type, uint16_t result) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, command_type); + _mav_put_uint16_t(buf, 2, result); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_ACK, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_ACK_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_ACK, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_ACK_LEN); +#endif +#else + mavlink_flexifunction_command_ack_t *packet = (mavlink_flexifunction_command_ack_t *)msgbuf; + packet->command_type = command_type; + packet->result = result; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_ACK, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_ACK_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_ACK, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_COMMAND_ACK_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FLEXIFUNCTION_COMMAND_ACK UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_directory.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_directory.h index ef262a6b1..619f810c5 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_directory.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_directory.h @@ -195,6 +195,46 @@ static inline void mavlink_msg_flexifunction_directory_send(mavlink_channel_t ch #endif } +#if MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_flexifunction_directory_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t directory_type, uint8_t start_index, uint8_t count, const int8_t *directory_data) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + _mav_put_uint8_t(buf, 2, directory_type); + _mav_put_uint8_t(buf, 3, start_index); + _mav_put_uint8_t(buf, 4, count); + _mav_put_int8_t_array(buf, 5, directory_data, 48); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_LEN); +#endif +#else + mavlink_flexifunction_directory_t *packet = (mavlink_flexifunction_directory_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + packet->directory_type = directory_type; + packet->start_index = start_index; + packet->count = count; + mav_array_memcpy(packet->directory_data, directory_data, sizeof(int8_t)*48); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FLEXIFUNCTION_DIRECTORY UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_directory_ack.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_directory_ack.h index d3a386ce5..0287183d8 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_directory_ack.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_directory_ack.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_flexifunction_directory_ack_send(mavlink_channel_ #endif } +#if MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_ACK_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_flexifunction_directory_ack_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, uint8_t directory_type, uint8_t start_index, uint8_t count, uint16_t result) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, result); + _mav_put_uint8_t(buf, 2, target_system); + _mav_put_uint8_t(buf, 3, target_component); + _mav_put_uint8_t(buf, 4, directory_type); + _mav_put_uint8_t(buf, 5, start_index); + _mav_put_uint8_t(buf, 6, count); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_ACK, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_ACK_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_ACK, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_ACK_LEN); +#endif +#else + mavlink_flexifunction_directory_ack_t *packet = (mavlink_flexifunction_directory_ack_t *)msgbuf; + packet->result = result; + packet->target_system = target_system; + packet->target_component = target_component; + packet->directory_type = directory_type; + packet->start_index = start_index; + packet->count = count; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_ACK, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_ACK_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_ACK, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_DIRECTORY_ACK_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FLEXIFUNCTION_DIRECTORY_ACK UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_read_req.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_read_req.h index e50f77b08..570782e79 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_read_req.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_read_req.h @@ -179,6 +179,44 @@ static inline void mavlink_msg_flexifunction_read_req_send(mavlink_channel_t cha #endif } +#if MAVLINK_MSG_ID_FLEXIFUNCTION_READ_REQ_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_flexifunction_read_req_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, int16_t read_req_type, int16_t data_index) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int16_t(buf, 0, read_req_type); + _mav_put_int16_t(buf, 2, data_index); + _mav_put_uint8_t(buf, 4, target_system); + _mav_put_uint8_t(buf, 5, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_READ_REQ, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_READ_REQ_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_READ_REQ_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_READ_REQ, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_READ_REQ_LEN); +#endif +#else + mavlink_flexifunction_read_req_t *packet = (mavlink_flexifunction_read_req_t *)msgbuf; + packet->read_req_type = read_req_type; + packet->data_index = data_index; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_READ_REQ, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_READ_REQ_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_READ_REQ_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_READ_REQ, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_READ_REQ_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FLEXIFUNCTION_READ_REQ UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_set.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_set.h index 41afb3811..c10000640 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_set.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_flexifunction_set.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_flexifunction_set_send(mavlink_channel_t chan, ui #endif } +#if MAVLINK_MSG_ID_FLEXIFUNCTION_SET_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_flexifunction_set_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, target_system); + _mav_put_uint8_t(buf, 1, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_SET, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_SET_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_SET_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_SET, buf, MAVLINK_MSG_ID_FLEXIFUNCTION_SET_LEN); +#endif +#else + mavlink_flexifunction_set_t *packet = (mavlink_flexifunction_set_t *)msgbuf; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_SET, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_SET_LEN, MAVLINK_MSG_ID_FLEXIFUNCTION_SET_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FLEXIFUNCTION_SET, (const char *)packet, MAVLINK_MSG_ID_FLEXIFUNCTION_SET_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FLEXIFUNCTION_SET UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f13.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f13.h index d21ab4816..bbb753a06 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f13.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f13.h @@ -179,6 +179,44 @@ static inline void mavlink_msg_serial_udb_extra_f13_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F13_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_serial_udb_extra_f13_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, int16_t sue_week_no, int32_t sue_lat_origin, int32_t sue_lon_origin, int32_t sue_alt_origin) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, sue_lat_origin); + _mav_put_int32_t(buf, 4, sue_lon_origin); + _mav_put_int32_t(buf, 8, sue_alt_origin); + _mav_put_int16_t(buf, 12, sue_week_no); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F13, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F13_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F13_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F13, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F13_LEN); +#endif +#else + mavlink_serial_udb_extra_f13_t *packet = (mavlink_serial_udb_extra_f13_t *)msgbuf; + packet->sue_lat_origin = sue_lat_origin; + packet->sue_lon_origin = sue_lon_origin; + packet->sue_alt_origin = sue_alt_origin; + packet->sue_week_no = sue_week_no; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F13, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F13_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F13_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F13, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F13_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SERIAL_UDB_EXTRA_F13 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f14.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f14.h index 6ac12f28a..112564d00 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f14.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f14.h @@ -256,6 +256,58 @@ static inline void mavlink_msg_serial_udb_extra_f14_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F14_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_serial_udb_extra_f14_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t sue_WIND_ESTIMATION, uint8_t sue_GPS_TYPE, uint8_t sue_DR, uint8_t sue_BOARD_TYPE, uint8_t sue_AIRFRAME, int16_t sue_RCON, int16_t sue_TRAP_FLAGS, uint32_t sue_TRAP_SOURCE, int16_t sue_osc_fail_count, uint8_t sue_CLOCK_CONFIG, uint8_t sue_FLIGHT_PLAN_TYPE) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, sue_TRAP_SOURCE); + _mav_put_int16_t(buf, 4, sue_RCON); + _mav_put_int16_t(buf, 6, sue_TRAP_FLAGS); + _mav_put_int16_t(buf, 8, sue_osc_fail_count); + _mav_put_uint8_t(buf, 10, sue_WIND_ESTIMATION); + _mav_put_uint8_t(buf, 11, sue_GPS_TYPE); + _mav_put_uint8_t(buf, 12, sue_DR); + _mav_put_uint8_t(buf, 13, sue_BOARD_TYPE); + _mav_put_uint8_t(buf, 14, sue_AIRFRAME); + _mav_put_uint8_t(buf, 15, sue_CLOCK_CONFIG); + _mav_put_uint8_t(buf, 16, sue_FLIGHT_PLAN_TYPE); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F14, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F14_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F14_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F14, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F14_LEN); +#endif +#else + mavlink_serial_udb_extra_f14_t *packet = (mavlink_serial_udb_extra_f14_t *)msgbuf; + packet->sue_TRAP_SOURCE = sue_TRAP_SOURCE; + packet->sue_RCON = sue_RCON; + packet->sue_TRAP_FLAGS = sue_TRAP_FLAGS; + packet->sue_osc_fail_count = sue_osc_fail_count; + packet->sue_WIND_ESTIMATION = sue_WIND_ESTIMATION; + packet->sue_GPS_TYPE = sue_GPS_TYPE; + packet->sue_DR = sue_DR; + packet->sue_BOARD_TYPE = sue_BOARD_TYPE; + packet->sue_AIRFRAME = sue_AIRFRAME; + packet->sue_CLOCK_CONFIG = sue_CLOCK_CONFIG; + packet->sue_FLIGHT_PLAN_TYPE = sue_FLIGHT_PLAN_TYPE; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F14, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F14_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F14_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F14, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F14_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SERIAL_UDB_EXTRA_F14 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f15.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f15.h index 10c3f4ca4..77666407d 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f15.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f15.h @@ -158,6 +158,40 @@ static inline void mavlink_msg_serial_udb_extra_f15_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F15_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_serial_udb_extra_f15_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, const uint8_t *sue_ID_VEHICLE_MODEL_NAME, const uint8_t *sue_ID_VEHICLE_REGISTRATION) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + + _mav_put_uint8_t_array(buf, 0, sue_ID_VEHICLE_MODEL_NAME, 40); + _mav_put_uint8_t_array(buf, 40, sue_ID_VEHICLE_REGISTRATION, 20); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F15, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F15_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F15_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F15, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F15_LEN); +#endif +#else + mavlink_serial_udb_extra_f15_t *packet = (mavlink_serial_udb_extra_f15_t *)msgbuf; + + mav_array_memcpy(packet->sue_ID_VEHICLE_MODEL_NAME, sue_ID_VEHICLE_MODEL_NAME, sizeof(uint8_t)*40); + mav_array_memcpy(packet->sue_ID_VEHICLE_REGISTRATION, sue_ID_VEHICLE_REGISTRATION, sizeof(uint8_t)*20); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F15, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F15_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F15_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F15, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F15_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SERIAL_UDB_EXTRA_F15 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f16.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f16.h index 659e6b7c5..ca9f0556f 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f16.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f16.h @@ -158,6 +158,40 @@ static inline void mavlink_msg_serial_udb_extra_f16_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F16_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_serial_udb_extra_f16_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, const uint8_t *sue_ID_LEAD_PILOT, const uint8_t *sue_ID_DIY_DRONES_URL) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + + _mav_put_uint8_t_array(buf, 0, sue_ID_LEAD_PILOT, 40); + _mav_put_uint8_t_array(buf, 40, sue_ID_DIY_DRONES_URL, 70); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F16, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F16_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F16_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F16, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F16_LEN); +#endif +#else + mavlink_serial_udb_extra_f16_t *packet = (mavlink_serial_udb_extra_f16_t *)msgbuf; + + mav_array_memcpy(packet->sue_ID_LEAD_PILOT, sue_ID_LEAD_PILOT, sizeof(uint8_t)*40); + mav_array_memcpy(packet->sue_ID_DIY_DRONES_URL, sue_ID_DIY_DRONES_URL, sizeof(uint8_t)*70); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F16, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F16_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F16_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F16, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F16_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SERIAL_UDB_EXTRA_F16 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f2_a.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f2_a.h index 15ba68a34..41b9f09c0 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f2_a.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f2_a.h @@ -443,6 +443,92 @@ static inline void mavlink_msg_serial_udb_extra_f2_a_send(mavlink_channel_t chan #endif } +#if MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_A_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_serial_udb_extra_f2_a_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t sue_time, uint8_t sue_status, int32_t sue_latitude, int32_t sue_longitude, int32_t sue_altitude, uint16_t sue_waypoint_index, int16_t sue_rmat0, int16_t sue_rmat1, int16_t sue_rmat2, int16_t sue_rmat3, int16_t sue_rmat4, int16_t sue_rmat5, int16_t sue_rmat6, int16_t sue_rmat7, int16_t sue_rmat8, uint16_t sue_cog, int16_t sue_sog, uint16_t sue_cpu_load, int16_t sue_voltage_milis, uint16_t sue_air_speed_3DIMU, int16_t sue_estimated_wind_0, int16_t sue_estimated_wind_1, int16_t sue_estimated_wind_2, int16_t sue_magFieldEarth0, int16_t sue_magFieldEarth1, int16_t sue_magFieldEarth2, int16_t sue_svs, int16_t sue_hdop) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, sue_time); + _mav_put_int32_t(buf, 4, sue_latitude); + _mav_put_int32_t(buf, 8, sue_longitude); + _mav_put_int32_t(buf, 12, sue_altitude); + _mav_put_uint16_t(buf, 16, sue_waypoint_index); + _mav_put_int16_t(buf, 18, sue_rmat0); + _mav_put_int16_t(buf, 20, sue_rmat1); + _mav_put_int16_t(buf, 22, sue_rmat2); + _mav_put_int16_t(buf, 24, sue_rmat3); + _mav_put_int16_t(buf, 26, sue_rmat4); + _mav_put_int16_t(buf, 28, sue_rmat5); + _mav_put_int16_t(buf, 30, sue_rmat6); + _mav_put_int16_t(buf, 32, sue_rmat7); + _mav_put_int16_t(buf, 34, sue_rmat8); + _mav_put_uint16_t(buf, 36, sue_cog); + _mav_put_int16_t(buf, 38, sue_sog); + _mav_put_uint16_t(buf, 40, sue_cpu_load); + _mav_put_int16_t(buf, 42, sue_voltage_milis); + _mav_put_uint16_t(buf, 44, sue_air_speed_3DIMU); + _mav_put_int16_t(buf, 46, sue_estimated_wind_0); + _mav_put_int16_t(buf, 48, sue_estimated_wind_1); + _mav_put_int16_t(buf, 50, sue_estimated_wind_2); + _mav_put_int16_t(buf, 52, sue_magFieldEarth0); + _mav_put_int16_t(buf, 54, sue_magFieldEarth1); + _mav_put_int16_t(buf, 56, sue_magFieldEarth2); + _mav_put_int16_t(buf, 58, sue_svs); + _mav_put_int16_t(buf, 60, sue_hdop); + _mav_put_uint8_t(buf, 62, sue_status); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_A, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_A_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_A_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_A, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_A_LEN); +#endif +#else + mavlink_serial_udb_extra_f2_a_t *packet = (mavlink_serial_udb_extra_f2_a_t *)msgbuf; + packet->sue_time = sue_time; + packet->sue_latitude = sue_latitude; + packet->sue_longitude = sue_longitude; + packet->sue_altitude = sue_altitude; + packet->sue_waypoint_index = sue_waypoint_index; + packet->sue_rmat0 = sue_rmat0; + packet->sue_rmat1 = sue_rmat1; + packet->sue_rmat2 = sue_rmat2; + packet->sue_rmat3 = sue_rmat3; + packet->sue_rmat4 = sue_rmat4; + packet->sue_rmat5 = sue_rmat5; + packet->sue_rmat6 = sue_rmat6; + packet->sue_rmat7 = sue_rmat7; + packet->sue_rmat8 = sue_rmat8; + packet->sue_cog = sue_cog; + packet->sue_sog = sue_sog; + packet->sue_cpu_load = sue_cpu_load; + packet->sue_voltage_milis = sue_voltage_milis; + packet->sue_air_speed_3DIMU = sue_air_speed_3DIMU; + packet->sue_estimated_wind_0 = sue_estimated_wind_0; + packet->sue_estimated_wind_1 = sue_estimated_wind_1; + packet->sue_estimated_wind_2 = sue_estimated_wind_2; + packet->sue_magFieldEarth0 = sue_magFieldEarth0; + packet->sue_magFieldEarth1 = sue_magFieldEarth1; + packet->sue_magFieldEarth2 = sue_magFieldEarth2; + packet->sue_svs = sue_svs; + packet->sue_hdop = sue_hdop; + packet->sue_status = sue_status; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_A, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_A_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_A_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_A, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_A_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SERIAL_UDB_EXTRA_F2_A UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f2_b.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f2_b.h index 7cb8c87da..3e1757f74 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f2_b.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f2_b.h @@ -498,6 +498,102 @@ static inline void mavlink_msg_serial_udb_extra_f2_b_send(mavlink_channel_t chan #endif } +#if MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_B_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_serial_udb_extra_f2_b_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t sue_time, int16_t sue_pwm_input_1, int16_t sue_pwm_input_2, int16_t sue_pwm_input_3, int16_t sue_pwm_input_4, int16_t sue_pwm_input_5, int16_t sue_pwm_input_6, int16_t sue_pwm_input_7, int16_t sue_pwm_input_8, int16_t sue_pwm_input_9, int16_t sue_pwm_input_10, int16_t sue_pwm_output_1, int16_t sue_pwm_output_2, int16_t sue_pwm_output_3, int16_t sue_pwm_output_4, int16_t sue_pwm_output_5, int16_t sue_pwm_output_6, int16_t sue_pwm_output_7, int16_t sue_pwm_output_8, int16_t sue_pwm_output_9, int16_t sue_pwm_output_10, int16_t sue_imu_location_x, int16_t sue_imu_location_y, int16_t sue_imu_location_z, uint32_t sue_flags, int16_t sue_osc_fails, int16_t sue_imu_velocity_x, int16_t sue_imu_velocity_y, int16_t sue_imu_velocity_z, int16_t sue_waypoint_goal_x, int16_t sue_waypoint_goal_y, int16_t sue_waypoint_goal_z, int16_t sue_memory_stack_free) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint32_t(buf, 0, sue_time); + _mav_put_uint32_t(buf, 4, sue_flags); + _mav_put_int16_t(buf, 8, sue_pwm_input_1); + _mav_put_int16_t(buf, 10, sue_pwm_input_2); + _mav_put_int16_t(buf, 12, sue_pwm_input_3); + _mav_put_int16_t(buf, 14, sue_pwm_input_4); + _mav_put_int16_t(buf, 16, sue_pwm_input_5); + _mav_put_int16_t(buf, 18, sue_pwm_input_6); + _mav_put_int16_t(buf, 20, sue_pwm_input_7); + _mav_put_int16_t(buf, 22, sue_pwm_input_8); + _mav_put_int16_t(buf, 24, sue_pwm_input_9); + _mav_put_int16_t(buf, 26, sue_pwm_input_10); + _mav_put_int16_t(buf, 28, sue_pwm_output_1); + _mav_put_int16_t(buf, 30, sue_pwm_output_2); + _mav_put_int16_t(buf, 32, sue_pwm_output_3); + _mav_put_int16_t(buf, 34, sue_pwm_output_4); + _mav_put_int16_t(buf, 36, sue_pwm_output_5); + _mav_put_int16_t(buf, 38, sue_pwm_output_6); + _mav_put_int16_t(buf, 40, sue_pwm_output_7); + _mav_put_int16_t(buf, 42, sue_pwm_output_8); + _mav_put_int16_t(buf, 44, sue_pwm_output_9); + _mav_put_int16_t(buf, 46, sue_pwm_output_10); + _mav_put_int16_t(buf, 48, sue_imu_location_x); + _mav_put_int16_t(buf, 50, sue_imu_location_y); + _mav_put_int16_t(buf, 52, sue_imu_location_z); + _mav_put_int16_t(buf, 54, sue_osc_fails); + _mav_put_int16_t(buf, 56, sue_imu_velocity_x); + _mav_put_int16_t(buf, 58, sue_imu_velocity_y); + _mav_put_int16_t(buf, 60, sue_imu_velocity_z); + _mav_put_int16_t(buf, 62, sue_waypoint_goal_x); + _mav_put_int16_t(buf, 64, sue_waypoint_goal_y); + _mav_put_int16_t(buf, 66, sue_waypoint_goal_z); + _mav_put_int16_t(buf, 68, sue_memory_stack_free); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_B, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_B_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_B_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_B, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_B_LEN); +#endif +#else + mavlink_serial_udb_extra_f2_b_t *packet = (mavlink_serial_udb_extra_f2_b_t *)msgbuf; + packet->sue_time = sue_time; + packet->sue_flags = sue_flags; + packet->sue_pwm_input_1 = sue_pwm_input_1; + packet->sue_pwm_input_2 = sue_pwm_input_2; + packet->sue_pwm_input_3 = sue_pwm_input_3; + packet->sue_pwm_input_4 = sue_pwm_input_4; + packet->sue_pwm_input_5 = sue_pwm_input_5; + packet->sue_pwm_input_6 = sue_pwm_input_6; + packet->sue_pwm_input_7 = sue_pwm_input_7; + packet->sue_pwm_input_8 = sue_pwm_input_8; + packet->sue_pwm_input_9 = sue_pwm_input_9; + packet->sue_pwm_input_10 = sue_pwm_input_10; + packet->sue_pwm_output_1 = sue_pwm_output_1; + packet->sue_pwm_output_2 = sue_pwm_output_2; + packet->sue_pwm_output_3 = sue_pwm_output_3; + packet->sue_pwm_output_4 = sue_pwm_output_4; + packet->sue_pwm_output_5 = sue_pwm_output_5; + packet->sue_pwm_output_6 = sue_pwm_output_6; + packet->sue_pwm_output_7 = sue_pwm_output_7; + packet->sue_pwm_output_8 = sue_pwm_output_8; + packet->sue_pwm_output_9 = sue_pwm_output_9; + packet->sue_pwm_output_10 = sue_pwm_output_10; + packet->sue_imu_location_x = sue_imu_location_x; + packet->sue_imu_location_y = sue_imu_location_y; + packet->sue_imu_location_z = sue_imu_location_z; + packet->sue_osc_fails = sue_osc_fails; + packet->sue_imu_velocity_x = sue_imu_velocity_x; + packet->sue_imu_velocity_y = sue_imu_velocity_y; + packet->sue_imu_velocity_z = sue_imu_velocity_z; + packet->sue_waypoint_goal_x = sue_waypoint_goal_x; + packet->sue_waypoint_goal_y = sue_waypoint_goal_y; + packet->sue_waypoint_goal_z = sue_waypoint_goal_z; + packet->sue_memory_stack_free = sue_memory_stack_free; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_B, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_B_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_B_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_B, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F2_B_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SERIAL_UDB_EXTRA_F2_B UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f4.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f4.h index 77c616cc2..edd1e924c 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f4.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f4.h @@ -245,6 +245,56 @@ static inline void mavlink_msg_serial_udb_extra_f4_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F4_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_serial_udb_extra_f4_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t sue_ROLL_STABILIZATION_AILERONS, uint8_t sue_ROLL_STABILIZATION_RUDDER, uint8_t sue_PITCH_STABILIZATION, uint8_t sue_YAW_STABILIZATION_RUDDER, uint8_t sue_YAW_STABILIZATION_AILERON, uint8_t sue_AILERON_NAVIGATION, uint8_t sue_RUDDER_NAVIGATION, uint8_t sue_ALTITUDEHOLD_STABILIZED, uint8_t sue_ALTITUDEHOLD_WAYPOINT, uint8_t sue_RACING_MODE) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, sue_ROLL_STABILIZATION_AILERONS); + _mav_put_uint8_t(buf, 1, sue_ROLL_STABILIZATION_RUDDER); + _mav_put_uint8_t(buf, 2, sue_PITCH_STABILIZATION); + _mav_put_uint8_t(buf, 3, sue_YAW_STABILIZATION_RUDDER); + _mav_put_uint8_t(buf, 4, sue_YAW_STABILIZATION_AILERON); + _mav_put_uint8_t(buf, 5, sue_AILERON_NAVIGATION); + _mav_put_uint8_t(buf, 6, sue_RUDDER_NAVIGATION); + _mav_put_uint8_t(buf, 7, sue_ALTITUDEHOLD_STABILIZED); + _mav_put_uint8_t(buf, 8, sue_ALTITUDEHOLD_WAYPOINT); + _mav_put_uint8_t(buf, 9, sue_RACING_MODE); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F4, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F4_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F4_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F4, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F4_LEN); +#endif +#else + mavlink_serial_udb_extra_f4_t *packet = (mavlink_serial_udb_extra_f4_t *)msgbuf; + packet->sue_ROLL_STABILIZATION_AILERONS = sue_ROLL_STABILIZATION_AILERONS; + packet->sue_ROLL_STABILIZATION_RUDDER = sue_ROLL_STABILIZATION_RUDDER; + packet->sue_PITCH_STABILIZATION = sue_PITCH_STABILIZATION; + packet->sue_YAW_STABILIZATION_RUDDER = sue_YAW_STABILIZATION_RUDDER; + packet->sue_YAW_STABILIZATION_AILERON = sue_YAW_STABILIZATION_AILERON; + packet->sue_AILERON_NAVIGATION = sue_AILERON_NAVIGATION; + packet->sue_RUDDER_NAVIGATION = sue_RUDDER_NAVIGATION; + packet->sue_ALTITUDEHOLD_STABILIZED = sue_ALTITUDEHOLD_STABILIZED; + packet->sue_ALTITUDEHOLD_WAYPOINT = sue_ALTITUDEHOLD_WAYPOINT; + packet->sue_RACING_MODE = sue_RACING_MODE; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F4, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F4_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F4_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F4, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F4_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SERIAL_UDB_EXTRA_F4 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f5.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f5.h index e115a9b44..a821f65bb 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f5.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f5.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_serial_udb_extra_f5_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F5_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_serial_udb_extra_f5_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float sue_YAWKP_AILERON, float sue_YAWKD_AILERON, float sue_ROLLKP, float sue_ROLLKD, float sue_YAW_STABILIZATION_AILERON, float sue_AILERON_BOOST) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, sue_YAWKP_AILERON); + _mav_put_float(buf, 4, sue_YAWKD_AILERON); + _mav_put_float(buf, 8, sue_ROLLKP); + _mav_put_float(buf, 12, sue_ROLLKD); + _mav_put_float(buf, 16, sue_YAW_STABILIZATION_AILERON); + _mav_put_float(buf, 20, sue_AILERON_BOOST); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F5, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F5_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F5_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F5, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F5_LEN); +#endif +#else + mavlink_serial_udb_extra_f5_t *packet = (mavlink_serial_udb_extra_f5_t *)msgbuf; + packet->sue_YAWKP_AILERON = sue_YAWKP_AILERON; + packet->sue_YAWKD_AILERON = sue_YAWKD_AILERON; + packet->sue_ROLLKP = sue_ROLLKP; + packet->sue_ROLLKD = sue_ROLLKD; + packet->sue_YAW_STABILIZATION_AILERON = sue_YAW_STABILIZATION_AILERON; + packet->sue_AILERON_BOOST = sue_AILERON_BOOST; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F5, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F5_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F5_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F5, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F5_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SERIAL_UDB_EXTRA_F5 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f6.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f6.h index 656103d09..0eb24c986 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f6.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f6.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_serial_udb_extra_f6_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F6_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_serial_udb_extra_f6_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float sue_PITCHGAIN, float sue_PITCHKD, float sue_RUDDER_ELEV_MIX, float sue_ROLL_ELEV_MIX, float sue_ELEVATOR_BOOST) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, sue_PITCHGAIN); + _mav_put_float(buf, 4, sue_PITCHKD); + _mav_put_float(buf, 8, sue_RUDDER_ELEV_MIX); + _mav_put_float(buf, 12, sue_ROLL_ELEV_MIX); + _mav_put_float(buf, 16, sue_ELEVATOR_BOOST); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F6, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F6_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F6_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F6, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F6_LEN); +#endif +#else + mavlink_serial_udb_extra_f6_t *packet = (mavlink_serial_udb_extra_f6_t *)msgbuf; + packet->sue_PITCHGAIN = sue_PITCHGAIN; + packet->sue_PITCHKD = sue_PITCHKD; + packet->sue_RUDDER_ELEV_MIX = sue_RUDDER_ELEV_MIX; + packet->sue_ROLL_ELEV_MIX = sue_ROLL_ELEV_MIX; + packet->sue_ELEVATOR_BOOST = sue_ELEVATOR_BOOST; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F6, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F6_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F6_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F6, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F6_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SERIAL_UDB_EXTRA_F6 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f7.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f7.h index 51c98e6b7..58de7d01c 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f7.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f7.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_serial_udb_extra_f7_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F7_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_serial_udb_extra_f7_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float sue_YAWKP_RUDDER, float sue_YAWKD_RUDDER, float sue_ROLLKP_RUDDER, float sue_ROLLKD_RUDDER, float sue_RUDDER_BOOST, float sue_RTL_PITCH_DOWN) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, sue_YAWKP_RUDDER); + _mav_put_float(buf, 4, sue_YAWKD_RUDDER); + _mav_put_float(buf, 8, sue_ROLLKP_RUDDER); + _mav_put_float(buf, 12, sue_ROLLKD_RUDDER); + _mav_put_float(buf, 16, sue_RUDDER_BOOST); + _mav_put_float(buf, 20, sue_RTL_PITCH_DOWN); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F7, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F7_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F7_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F7, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F7_LEN); +#endif +#else + mavlink_serial_udb_extra_f7_t *packet = (mavlink_serial_udb_extra_f7_t *)msgbuf; + packet->sue_YAWKP_RUDDER = sue_YAWKP_RUDDER; + packet->sue_YAWKD_RUDDER = sue_YAWKD_RUDDER; + packet->sue_ROLLKP_RUDDER = sue_ROLLKP_RUDDER; + packet->sue_ROLLKD_RUDDER = sue_ROLLKD_RUDDER; + packet->sue_RUDDER_BOOST = sue_RUDDER_BOOST; + packet->sue_RTL_PITCH_DOWN = sue_RTL_PITCH_DOWN; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F7, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F7_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F7_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F7, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F7_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SERIAL_UDB_EXTRA_F7 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f8.h b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f8.h index 8557a95e2..5cab81655 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f8.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/mavlink_msg_serial_udb_extra_f8.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_serial_udb_extra_f8_send(mavlink_channel_t chan, #endif } +#if MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F8_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_serial_udb_extra_f8_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float sue_HEIGHT_TARGET_MAX, float sue_HEIGHT_TARGET_MIN, float sue_ALT_HOLD_THROTTLE_MIN, float sue_ALT_HOLD_THROTTLE_MAX, float sue_ALT_HOLD_PITCH_MIN, float sue_ALT_HOLD_PITCH_MAX, float sue_ALT_HOLD_PITCH_HIGH) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, sue_HEIGHT_TARGET_MAX); + _mav_put_float(buf, 4, sue_HEIGHT_TARGET_MIN); + _mav_put_float(buf, 8, sue_ALT_HOLD_THROTTLE_MIN); + _mav_put_float(buf, 12, sue_ALT_HOLD_THROTTLE_MAX); + _mav_put_float(buf, 16, sue_ALT_HOLD_PITCH_MIN); + _mav_put_float(buf, 20, sue_ALT_HOLD_PITCH_MAX); + _mav_put_float(buf, 24, sue_ALT_HOLD_PITCH_HIGH); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F8, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F8_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F8_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F8, buf, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F8_LEN); +#endif +#else + mavlink_serial_udb_extra_f8_t *packet = (mavlink_serial_udb_extra_f8_t *)msgbuf; + packet->sue_HEIGHT_TARGET_MAX = sue_HEIGHT_TARGET_MAX; + packet->sue_HEIGHT_TARGET_MIN = sue_HEIGHT_TARGET_MIN; + packet->sue_ALT_HOLD_THROTTLE_MIN = sue_ALT_HOLD_THROTTLE_MIN; + packet->sue_ALT_HOLD_THROTTLE_MAX = sue_ALT_HOLD_THROTTLE_MAX; + packet->sue_ALT_HOLD_PITCH_MIN = sue_ALT_HOLD_PITCH_MIN; + packet->sue_ALT_HOLD_PITCH_MAX = sue_ALT_HOLD_PITCH_MAX; + packet->sue_ALT_HOLD_PITCH_HIGH = sue_ALT_HOLD_PITCH_HIGH; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F8, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F8_LEN, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F8_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F8, (const char *)packet, MAVLINK_MSG_ID_SERIAL_UDB_EXTRA_F8_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SERIAL_UDB_EXTRA_F8 UNPACKING diff --git a/mavlink/include/mavlink/v1.0/matrixpilot/version.h b/mavlink/include/mavlink/v1.0/matrixpilot/version.h index a8be16c42..50cbda6c7 100644 --- a/mavlink/include/mavlink/v1.0/matrixpilot/version.h +++ b/mavlink/include/mavlink/v1.0/matrixpilot/version.h @@ -5,7 +5,7 @@ #ifndef MAVLINK_VERSION_H #define MAVLINK_VERSION_H -#define MAVLINK_BUILD_DATE "Tue Feb 4 15:28:04 2014" +#define MAVLINK_BUILD_DATE "Sun Apr 13 09:38:32 2014" #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0" #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255 diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_attitude_control.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_attitude_control.h index ef5354d5e..f1cac9f2c 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_attitude_control.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_attitude_control.h @@ -234,6 +234,54 @@ static inline void mavlink_msg_attitude_control_send(mavlink_channel_t chan, uin #endif } +#if MAVLINK_MSG_ID_ATTITUDE_CONTROL_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_attitude_control_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target, float roll, float pitch, float yaw, float thrust, uint8_t roll_manual, uint8_t pitch_manual, uint8_t yaw_manual, uint8_t thrust_manual) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, roll); + _mav_put_float(buf, 4, pitch); + _mav_put_float(buf, 8, yaw); + _mav_put_float(buf, 12, thrust); + _mav_put_uint8_t(buf, 16, target); + _mav_put_uint8_t(buf, 17, roll_manual); + _mav_put_uint8_t(buf, 18, pitch_manual); + _mav_put_uint8_t(buf, 19, yaw_manual); + _mav_put_uint8_t(buf, 20, thrust_manual); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ATTITUDE_CONTROL, buf, MAVLINK_MSG_ID_ATTITUDE_CONTROL_LEN, MAVLINK_MSG_ID_ATTITUDE_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ATTITUDE_CONTROL, buf, MAVLINK_MSG_ID_ATTITUDE_CONTROL_LEN); +#endif +#else + mavlink_attitude_control_t *packet = (mavlink_attitude_control_t *)msgbuf; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + packet->thrust = thrust; + packet->target = target; + packet->roll_manual = roll_manual; + packet->pitch_manual = pitch_manual; + packet->yaw_manual = yaw_manual; + packet->thrust_manual = thrust_manual; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ATTITUDE_CONTROL, (const char *)packet, MAVLINK_MSG_ID_ATTITUDE_CONTROL_LEN, MAVLINK_MSG_ID_ATTITUDE_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ATTITUDE_CONTROL, (const char *)packet, MAVLINK_MSG_ID_ATTITUDE_CONTROL_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE ATTITUDE_CONTROL UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_brief_feature.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_brief_feature.h index d41093792..7bc27982a 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_brief_feature.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_brief_feature.h @@ -217,6 +217,50 @@ static inline void mavlink_msg_brief_feature_send(mavlink_channel_t chan, float #endif } +#if MAVLINK_MSG_ID_BRIEF_FEATURE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_brief_feature_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float x, float y, float z, uint8_t orientation_assignment, uint16_t size, uint16_t orientation, const uint8_t *descriptor, float response) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, x); + _mav_put_float(buf, 4, y); + _mav_put_float(buf, 8, z); + _mav_put_float(buf, 12, response); + _mav_put_uint16_t(buf, 16, size); + _mav_put_uint16_t(buf, 18, orientation); + _mav_put_uint8_t(buf, 20, orientation_assignment); + _mav_put_uint8_t_array(buf, 21, descriptor, 32); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_BRIEF_FEATURE, buf, MAVLINK_MSG_ID_BRIEF_FEATURE_LEN, MAVLINK_MSG_ID_BRIEF_FEATURE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_BRIEF_FEATURE, buf, MAVLINK_MSG_ID_BRIEF_FEATURE_LEN); +#endif +#else + mavlink_brief_feature_t *packet = (mavlink_brief_feature_t *)msgbuf; + packet->x = x; + packet->y = y; + packet->z = z; + packet->response = response; + packet->size = size; + packet->orientation = orientation; + packet->orientation_assignment = orientation_assignment; + mav_array_memcpy(packet->descriptor, descriptor, sizeof(uint8_t)*32); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_BRIEF_FEATURE, (const char *)packet, MAVLINK_MSG_ID_BRIEF_FEATURE_LEN, MAVLINK_MSG_ID_BRIEF_FEATURE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_BRIEF_FEATURE, (const char *)packet, MAVLINK_MSG_ID_BRIEF_FEATURE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE BRIEF_FEATURE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_image_available.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_image_available.h index ae4db825d..37270d49c 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_image_available.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_image_available.h @@ -388,6 +388,82 @@ static inline void mavlink_msg_image_available_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_IMAGE_AVAILABLE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_image_available_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t cam_id, uint8_t cam_no, uint64_t timestamp, uint64_t valid_until, uint32_t img_seq, uint32_t img_buf_index, uint16_t width, uint16_t height, uint16_t depth, uint8_t channels, uint32_t key, uint32_t exposure, float gain, float roll, float pitch, float yaw, float local_z, float lat, float lon, float alt, float ground_x, float ground_y, float ground_z) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, cam_id); + _mav_put_uint64_t(buf, 8, timestamp); + _mav_put_uint64_t(buf, 16, valid_until); + _mav_put_uint32_t(buf, 24, img_seq); + _mav_put_uint32_t(buf, 28, img_buf_index); + _mav_put_uint32_t(buf, 32, key); + _mav_put_uint32_t(buf, 36, exposure); + _mav_put_float(buf, 40, gain); + _mav_put_float(buf, 44, roll); + _mav_put_float(buf, 48, pitch); + _mav_put_float(buf, 52, yaw); + _mav_put_float(buf, 56, local_z); + _mav_put_float(buf, 60, lat); + _mav_put_float(buf, 64, lon); + _mav_put_float(buf, 68, alt); + _mav_put_float(buf, 72, ground_x); + _mav_put_float(buf, 76, ground_y); + _mav_put_float(buf, 80, ground_z); + _mav_put_uint16_t(buf, 84, width); + _mav_put_uint16_t(buf, 86, height); + _mav_put_uint16_t(buf, 88, depth); + _mav_put_uint8_t(buf, 90, cam_no); + _mav_put_uint8_t(buf, 91, channels); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_IMAGE_AVAILABLE, buf, MAVLINK_MSG_ID_IMAGE_AVAILABLE_LEN, MAVLINK_MSG_ID_IMAGE_AVAILABLE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_IMAGE_AVAILABLE, buf, MAVLINK_MSG_ID_IMAGE_AVAILABLE_LEN); +#endif +#else + mavlink_image_available_t *packet = (mavlink_image_available_t *)msgbuf; + packet->cam_id = cam_id; + packet->timestamp = timestamp; + packet->valid_until = valid_until; + packet->img_seq = img_seq; + packet->img_buf_index = img_buf_index; + packet->key = key; + packet->exposure = exposure; + packet->gain = gain; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + packet->local_z = local_z; + packet->lat = lat; + packet->lon = lon; + packet->alt = alt; + packet->ground_x = ground_x; + packet->ground_y = ground_y; + packet->ground_z = ground_z; + packet->width = width; + packet->height = height; + packet->depth = depth; + packet->cam_no = cam_no; + packet->channels = channels; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_IMAGE_AVAILABLE, (const char *)packet, MAVLINK_MSG_ID_IMAGE_AVAILABLE_LEN, MAVLINK_MSG_ID_IMAGE_AVAILABLE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_IMAGE_AVAILABLE, (const char *)packet, MAVLINK_MSG_ID_IMAGE_AVAILABLE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE IMAGE_AVAILABLE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_image_trigger_control.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_image_trigger_control.h index 664574be9..85f8eff55 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_image_trigger_control.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_image_trigger_control.h @@ -146,6 +146,38 @@ static inline void mavlink_msg_image_trigger_control_send(mavlink_channel_t chan #endif } +#if MAVLINK_MSG_ID_IMAGE_TRIGGER_CONTROL_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_image_trigger_control_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t enable) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, enable); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_IMAGE_TRIGGER_CONTROL, buf, MAVLINK_MSG_ID_IMAGE_TRIGGER_CONTROL_LEN, MAVLINK_MSG_ID_IMAGE_TRIGGER_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_IMAGE_TRIGGER_CONTROL, buf, MAVLINK_MSG_ID_IMAGE_TRIGGER_CONTROL_LEN); +#endif +#else + mavlink_image_trigger_control_t *packet = (mavlink_image_trigger_control_t *)msgbuf; + packet->enable = enable; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_IMAGE_TRIGGER_CONTROL, (const char *)packet, MAVLINK_MSG_ID_IMAGE_TRIGGER_CONTROL_LEN, MAVLINK_MSG_ID_IMAGE_TRIGGER_CONTROL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_IMAGE_TRIGGER_CONTROL, (const char *)packet, MAVLINK_MSG_ID_IMAGE_TRIGGER_CONTROL_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE IMAGE_TRIGGER_CONTROL UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_image_triggered.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_image_triggered.h index f3a2243af..b438c74ea 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_image_triggered.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_image_triggered.h @@ -267,6 +267,60 @@ static inline void mavlink_msg_image_triggered_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_IMAGE_TRIGGERED_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_image_triggered_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, uint32_t seq, float roll, float pitch, float yaw, float local_z, float lat, float lon, float alt, float ground_x, float ground_y, float ground_z) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint64_t(buf, 0, timestamp); + _mav_put_uint32_t(buf, 8, seq); + _mav_put_float(buf, 12, roll); + _mav_put_float(buf, 16, pitch); + _mav_put_float(buf, 20, yaw); + _mav_put_float(buf, 24, local_z); + _mav_put_float(buf, 28, lat); + _mav_put_float(buf, 32, lon); + _mav_put_float(buf, 36, alt); + _mav_put_float(buf, 40, ground_x); + _mav_put_float(buf, 44, ground_y); + _mav_put_float(buf, 48, ground_z); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_IMAGE_TRIGGERED, buf, MAVLINK_MSG_ID_IMAGE_TRIGGERED_LEN, MAVLINK_MSG_ID_IMAGE_TRIGGERED_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_IMAGE_TRIGGERED, buf, MAVLINK_MSG_ID_IMAGE_TRIGGERED_LEN); +#endif +#else + mavlink_image_triggered_t *packet = (mavlink_image_triggered_t *)msgbuf; + packet->timestamp = timestamp; + packet->seq = seq; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + packet->local_z = local_z; + packet->lat = lat; + packet->lon = lon; + packet->alt = alt; + packet->ground_x = ground_x; + packet->ground_y = ground_y; + packet->ground_z = ground_z; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_IMAGE_TRIGGERED, (const char *)packet, MAVLINK_MSG_ID_IMAGE_TRIGGERED_LEN, MAVLINK_MSG_ID_IMAGE_TRIGGERED_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_IMAGE_TRIGGERED, (const char *)packet, MAVLINK_MSG_ID_IMAGE_TRIGGERED_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE IMAGE_TRIGGERED UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_marker.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_marker.h index 6bdcceaf9..05452637e 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_marker.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_marker.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_marker_send(mavlink_channel_t chan, uint16_t id, #endif } +#if MAVLINK_MSG_ID_MARKER_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_marker_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t id, float x, float y, float z, float roll, float pitch, float yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, x); + _mav_put_float(buf, 4, y); + _mav_put_float(buf, 8, z); + _mav_put_float(buf, 12, roll); + _mav_put_float(buf, 16, pitch); + _mav_put_float(buf, 20, yaw); + _mav_put_uint16_t(buf, 24, id); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MARKER, buf, MAVLINK_MSG_ID_MARKER_LEN, MAVLINK_MSG_ID_MARKER_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MARKER, buf, MAVLINK_MSG_ID_MARKER_LEN); +#endif +#else + mavlink_marker_t *packet = (mavlink_marker_t *)msgbuf; + packet->x = x; + packet->y = y; + packet->z = z; + packet->roll = roll; + packet->pitch = pitch; + packet->yaw = yaw; + packet->id = id; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MARKER, (const char *)packet, MAVLINK_MSG_ID_MARKER_LEN, MAVLINK_MSG_ID_MARKER_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MARKER, (const char *)packet, MAVLINK_MSG_ID_MARKER_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE MARKER UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_pattern_detected.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_pattern_detected.h index aa7b827a3..bde400da9 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_pattern_detected.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_pattern_detected.h @@ -173,6 +173,42 @@ static inline void mavlink_msg_pattern_detected_send(mavlink_channel_t chan, uin #endif } +#if MAVLINK_MSG_ID_PATTERN_DETECTED_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_pattern_detected_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t type, float confidence, const char *file, uint8_t detected) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, confidence); + _mav_put_uint8_t(buf, 4, type); + _mav_put_uint8_t(buf, 105, detected); + _mav_put_char_array(buf, 5, file, 100); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PATTERN_DETECTED, buf, MAVLINK_MSG_ID_PATTERN_DETECTED_LEN, MAVLINK_MSG_ID_PATTERN_DETECTED_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PATTERN_DETECTED, buf, MAVLINK_MSG_ID_PATTERN_DETECTED_LEN); +#endif +#else + mavlink_pattern_detected_t *packet = (mavlink_pattern_detected_t *)msgbuf; + packet->confidence = confidence; + packet->type = type; + packet->detected = detected; + mav_array_memcpy(packet->file, file, sizeof(char)*100); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PATTERN_DETECTED, (const char *)packet, MAVLINK_MSG_ID_PATTERN_DETECTED_LEN, MAVLINK_MSG_ID_PATTERN_DETECTED_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PATTERN_DETECTED, (const char *)packet, MAVLINK_MSG_ID_PATTERN_DETECTED_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE PATTERN_DETECTED UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_point_of_interest.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_point_of_interest.h index 913a52897..86e934519 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_point_of_interest.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_point_of_interest.h @@ -217,6 +217,50 @@ static inline void mavlink_msg_point_of_interest_send(mavlink_channel_t chan, ui #endif } +#if MAVLINK_MSG_ID_POINT_OF_INTEREST_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_point_of_interest_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t type, uint8_t color, uint8_t coordinate_system, uint16_t timeout, float x, float y, float z, const char *name) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, x); + _mav_put_float(buf, 4, y); + _mav_put_float(buf, 8, z); + _mav_put_uint16_t(buf, 12, timeout); + _mav_put_uint8_t(buf, 14, type); + _mav_put_uint8_t(buf, 15, color); + _mav_put_uint8_t(buf, 16, coordinate_system); + _mav_put_char_array(buf, 17, name, 26); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POINT_OF_INTEREST, buf, MAVLINK_MSG_ID_POINT_OF_INTEREST_LEN, MAVLINK_MSG_ID_POINT_OF_INTEREST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POINT_OF_INTEREST, buf, MAVLINK_MSG_ID_POINT_OF_INTEREST_LEN); +#endif +#else + mavlink_point_of_interest_t *packet = (mavlink_point_of_interest_t *)msgbuf; + packet->x = x; + packet->y = y; + packet->z = z; + packet->timeout = timeout; + packet->type = type; + packet->color = color; + packet->coordinate_system = coordinate_system; + mav_array_memcpy(packet->name, name, sizeof(char)*26); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POINT_OF_INTEREST, (const char *)packet, MAVLINK_MSG_ID_POINT_OF_INTEREST_LEN, MAVLINK_MSG_ID_POINT_OF_INTEREST_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POINT_OF_INTEREST, (const char *)packet, MAVLINK_MSG_ID_POINT_OF_INTEREST_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE POINT_OF_INTEREST UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_point_of_interest_connection.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_point_of_interest_connection.h index e24436431..e5c04a851 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_point_of_interest_connection.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_point_of_interest_connection.h @@ -250,6 +250,56 @@ static inline void mavlink_msg_point_of_interest_connection_send(mavlink_channel #endif } +#if MAVLINK_MSG_ID_POINT_OF_INTEREST_CONNECTION_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_point_of_interest_connection_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t type, uint8_t color, uint8_t coordinate_system, uint16_t timeout, float xp1, float yp1, float zp1, float xp2, float yp2, float zp2, const char *name) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, xp1); + _mav_put_float(buf, 4, yp1); + _mav_put_float(buf, 8, zp1); + _mav_put_float(buf, 12, xp2); + _mav_put_float(buf, 16, yp2); + _mav_put_float(buf, 20, zp2); + _mav_put_uint16_t(buf, 24, timeout); + _mav_put_uint8_t(buf, 26, type); + _mav_put_uint8_t(buf, 27, color); + _mav_put_uint8_t(buf, 28, coordinate_system); + _mav_put_char_array(buf, 29, name, 26); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POINT_OF_INTEREST_CONNECTION, buf, MAVLINK_MSG_ID_POINT_OF_INTEREST_CONNECTION_LEN, MAVLINK_MSG_ID_POINT_OF_INTEREST_CONNECTION_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POINT_OF_INTEREST_CONNECTION, buf, MAVLINK_MSG_ID_POINT_OF_INTEREST_CONNECTION_LEN); +#endif +#else + mavlink_point_of_interest_connection_t *packet = (mavlink_point_of_interest_connection_t *)msgbuf; + packet->xp1 = xp1; + packet->yp1 = yp1; + packet->zp1 = zp1; + packet->xp2 = xp2; + packet->yp2 = yp2; + packet->zp2 = zp2; + packet->timeout = timeout; + packet->type = type; + packet->color = color; + packet->coordinate_system = coordinate_system; + mav_array_memcpy(packet->name, name, sizeof(char)*26); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POINT_OF_INTEREST_CONNECTION, (const char *)packet, MAVLINK_MSG_ID_POINT_OF_INTEREST_CONNECTION_LEN, MAVLINK_MSG_ID_POINT_OF_INTEREST_CONNECTION_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POINT_OF_INTEREST_CONNECTION, (const char *)packet, MAVLINK_MSG_ID_POINT_OF_INTEREST_CONNECTION_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE POINT_OF_INTEREST_CONNECTION UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_position_control_setpoint.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_position_control_setpoint.h index 6f4ca510a..480004cef 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_position_control_setpoint.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_position_control_setpoint.h @@ -190,6 +190,46 @@ static inline void mavlink_msg_position_control_setpoint_send(mavlink_channel_t #endif } +#if MAVLINK_MSG_ID_POSITION_CONTROL_SETPOINT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_position_control_setpoint_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t id, float x, float y, float z, float yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, x); + _mav_put_float(buf, 4, y); + _mav_put_float(buf, 8, z); + _mav_put_float(buf, 12, yaw); + _mav_put_uint16_t(buf, 16, id); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POSITION_CONTROL_SETPOINT, buf, MAVLINK_MSG_ID_POSITION_CONTROL_SETPOINT_LEN, MAVLINK_MSG_ID_POSITION_CONTROL_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POSITION_CONTROL_SETPOINT, buf, MAVLINK_MSG_ID_POSITION_CONTROL_SETPOINT_LEN); +#endif +#else + mavlink_position_control_setpoint_t *packet = (mavlink_position_control_setpoint_t *)msgbuf; + packet->x = x; + packet->y = y; + packet->z = z; + packet->yaw = yaw; + packet->id = id; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POSITION_CONTROL_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_POSITION_CONTROL_SETPOINT_LEN, MAVLINK_MSG_ID_POSITION_CONTROL_SETPOINT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_POSITION_CONTROL_SETPOINT, (const char *)packet, MAVLINK_MSG_ID_POSITION_CONTROL_SETPOINT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE POSITION_CONTROL_SETPOINT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_raw_aux.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_raw_aux.h index 08cedbb4b..41a512648 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_raw_aux.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_raw_aux.h @@ -212,6 +212,50 @@ static inline void mavlink_msg_raw_aux_send(mavlink_channel_t chan, uint16_t adc #endif } +#if MAVLINK_MSG_ID_RAW_AUX_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_raw_aux_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t adc1, uint16_t adc2, uint16_t adc3, uint16_t adc4, uint16_t vbat, int16_t temp, int32_t baro) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, baro); + _mav_put_uint16_t(buf, 4, adc1); + _mav_put_uint16_t(buf, 6, adc2); + _mav_put_uint16_t(buf, 8, adc3); + _mav_put_uint16_t(buf, 10, adc4); + _mav_put_uint16_t(buf, 12, vbat); + _mav_put_int16_t(buf, 14, temp); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RAW_AUX, buf, MAVLINK_MSG_ID_RAW_AUX_LEN, MAVLINK_MSG_ID_RAW_AUX_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RAW_AUX, buf, MAVLINK_MSG_ID_RAW_AUX_LEN); +#endif +#else + mavlink_raw_aux_t *packet = (mavlink_raw_aux_t *)msgbuf; + packet->baro = baro; + packet->adc1 = adc1; + packet->adc2 = adc2; + packet->adc3 = adc3; + packet->adc4 = adc4; + packet->vbat = vbat; + packet->temp = temp; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RAW_AUX, (const char *)packet, MAVLINK_MSG_ID_RAW_AUX_LEN, MAVLINK_MSG_ID_RAW_AUX_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RAW_AUX, (const char *)packet, MAVLINK_MSG_ID_RAW_AUX_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE RAW_AUX UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_set_cam_shutter.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_set_cam_shutter.h index b26d748c2..8fe14dd54 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_set_cam_shutter.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_set_cam_shutter.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_set_cam_shutter_send(mavlink_channel_t chan, uint #endif } +#if MAVLINK_MSG_ID_SET_CAM_SHUTTER_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_set_cam_shutter_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t cam_no, uint8_t cam_mode, uint8_t trigger_pin, uint16_t interval, uint16_t exposure, float gain) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, gain); + _mav_put_uint16_t(buf, 4, interval); + _mav_put_uint16_t(buf, 6, exposure); + _mav_put_uint8_t(buf, 8, cam_no); + _mav_put_uint8_t(buf, 9, cam_mode); + _mav_put_uint8_t(buf, 10, trigger_pin); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_CAM_SHUTTER, buf, MAVLINK_MSG_ID_SET_CAM_SHUTTER_LEN, MAVLINK_MSG_ID_SET_CAM_SHUTTER_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_CAM_SHUTTER, buf, MAVLINK_MSG_ID_SET_CAM_SHUTTER_LEN); +#endif +#else + mavlink_set_cam_shutter_t *packet = (mavlink_set_cam_shutter_t *)msgbuf; + packet->gain = gain; + packet->interval = interval; + packet->exposure = exposure; + packet->cam_no = cam_no; + packet->cam_mode = cam_mode; + packet->trigger_pin = trigger_pin; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_CAM_SHUTTER, (const char *)packet, MAVLINK_MSG_ID_SET_CAM_SHUTTER_LEN, MAVLINK_MSG_ID_SET_CAM_SHUTTER_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_CAM_SHUTTER, (const char *)packet, MAVLINK_MSG_ID_SET_CAM_SHUTTER_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SET_CAM_SHUTTER UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_set_position_control_offset.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_set_position_control_offset.h index f1f9e698f..c4e4fc19a 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_set_position_control_offset.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_set_position_control_offset.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_set_position_control_offset_send(mavlink_channel_ #endif } +#if MAVLINK_MSG_ID_SET_POSITION_CONTROL_OFFSET_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_set_position_control_offset_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system, uint8_t target_component, float x, float y, float z, float yaw) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, x); + _mav_put_float(buf, 4, y); + _mav_put_float(buf, 8, z); + _mav_put_float(buf, 12, yaw); + _mav_put_uint8_t(buf, 16, target_system); + _mav_put_uint8_t(buf, 17, target_component); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_POSITION_CONTROL_OFFSET, buf, MAVLINK_MSG_ID_SET_POSITION_CONTROL_OFFSET_LEN, MAVLINK_MSG_ID_SET_POSITION_CONTROL_OFFSET_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_POSITION_CONTROL_OFFSET, buf, MAVLINK_MSG_ID_SET_POSITION_CONTROL_OFFSET_LEN); +#endif +#else + mavlink_set_position_control_offset_t *packet = (mavlink_set_position_control_offset_t *)msgbuf; + packet->x = x; + packet->y = y; + packet->z = z; + packet->yaw = yaw; + packet->target_system = target_system; + packet->target_component = target_component; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_POSITION_CONTROL_OFFSET, (const char *)packet, MAVLINK_MSG_ID_SET_POSITION_CONTROL_OFFSET_LEN, MAVLINK_MSG_ID_SET_POSITION_CONTROL_OFFSET_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SET_POSITION_CONTROL_OFFSET, (const char *)packet, MAVLINK_MSG_ID_SET_POSITION_CONTROL_OFFSET_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SET_POSITION_CONTROL_OFFSET UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_command.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_command.h index 9458087da..d71a2ed2e 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_command.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_command.h @@ -179,6 +179,44 @@ static inline void mavlink_msg_watchdog_command_send(mavlink_channel_t chan, uin #endif } +#if MAVLINK_MSG_ID_WATCHDOG_COMMAND_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_watchdog_command_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target_system_id, uint16_t watchdog_id, uint16_t process_id, uint8_t command_id) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, watchdog_id); + _mav_put_uint16_t(buf, 2, process_id); + _mav_put_uint8_t(buf, 4, target_system_id); + _mav_put_uint8_t(buf, 5, command_id); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_COMMAND, buf, MAVLINK_MSG_ID_WATCHDOG_COMMAND_LEN, MAVLINK_MSG_ID_WATCHDOG_COMMAND_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_COMMAND, buf, MAVLINK_MSG_ID_WATCHDOG_COMMAND_LEN); +#endif +#else + mavlink_watchdog_command_t *packet = (mavlink_watchdog_command_t *)msgbuf; + packet->watchdog_id = watchdog_id; + packet->process_id = process_id; + packet->target_system_id = target_system_id; + packet->command_id = command_id; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_COMMAND, (const char *)packet, MAVLINK_MSG_ID_WATCHDOG_COMMAND_LEN, MAVLINK_MSG_ID_WATCHDOG_COMMAND_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_COMMAND, (const char *)packet, MAVLINK_MSG_ID_WATCHDOG_COMMAND_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE WATCHDOG_COMMAND UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_heartbeat.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_heartbeat.h index 3f4295ee5..a8e49b642 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_heartbeat.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_heartbeat.h @@ -157,6 +157,40 @@ static inline void mavlink_msg_watchdog_heartbeat_send(mavlink_channel_t chan, u #endif } +#if MAVLINK_MSG_ID_WATCHDOG_HEARTBEAT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_watchdog_heartbeat_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t watchdog_id, uint16_t process_count) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint16_t(buf, 0, watchdog_id); + _mav_put_uint16_t(buf, 2, process_count); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_HEARTBEAT, buf, MAVLINK_MSG_ID_WATCHDOG_HEARTBEAT_LEN, MAVLINK_MSG_ID_WATCHDOG_HEARTBEAT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_HEARTBEAT, buf, MAVLINK_MSG_ID_WATCHDOG_HEARTBEAT_LEN); +#endif +#else + mavlink_watchdog_heartbeat_t *packet = (mavlink_watchdog_heartbeat_t *)msgbuf; + packet->watchdog_id = watchdog_id; + packet->process_count = process_count; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_HEARTBEAT, (const char *)packet, MAVLINK_MSG_ID_WATCHDOG_HEARTBEAT_LEN, MAVLINK_MSG_ID_WATCHDOG_HEARTBEAT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_HEARTBEAT, (const char *)packet, MAVLINK_MSG_ID_WATCHDOG_HEARTBEAT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE WATCHDOG_HEARTBEAT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_process_info.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_process_info.h index 55853cdde..a5e0cc67e 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_process_info.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_process_info.h @@ -185,6 +185,44 @@ static inline void mavlink_msg_watchdog_process_info_send(mavlink_channel_t chan #endif } +#if MAVLINK_MSG_ID_WATCHDOG_PROCESS_INFO_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_watchdog_process_info_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t watchdog_id, uint16_t process_id, const char *name, const char *arguments, int32_t timeout) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, timeout); + _mav_put_uint16_t(buf, 4, watchdog_id); + _mav_put_uint16_t(buf, 6, process_id); + _mav_put_char_array(buf, 8, name, 100); + _mav_put_char_array(buf, 108, arguments, 147); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_PROCESS_INFO, buf, MAVLINK_MSG_ID_WATCHDOG_PROCESS_INFO_LEN, MAVLINK_MSG_ID_WATCHDOG_PROCESS_INFO_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_PROCESS_INFO, buf, MAVLINK_MSG_ID_WATCHDOG_PROCESS_INFO_LEN); +#endif +#else + mavlink_watchdog_process_info_t *packet = (mavlink_watchdog_process_info_t *)msgbuf; + packet->timeout = timeout; + packet->watchdog_id = watchdog_id; + packet->process_id = process_id; + mav_array_memcpy(packet->name, name, sizeof(char)*100); + mav_array_memcpy(packet->arguments, arguments, sizeof(char)*147); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_PROCESS_INFO, (const char *)packet, MAVLINK_MSG_ID_WATCHDOG_PROCESS_INFO_LEN, MAVLINK_MSG_ID_WATCHDOG_PROCESS_INFO_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_PROCESS_INFO, (const char *)packet, MAVLINK_MSG_ID_WATCHDOG_PROCESS_INFO_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE WATCHDOG_PROCESS_INFO UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_process_status.h b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_process_status.h index a0410d803..15c9598e4 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_process_status.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/mavlink_msg_watchdog_process_status.h @@ -201,6 +201,48 @@ static inline void mavlink_msg_watchdog_process_status_send(mavlink_channel_t ch #endif } +#if MAVLINK_MSG_ID_WATCHDOG_PROCESS_STATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_watchdog_process_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint16_t watchdog_id, uint16_t process_id, uint8_t state, uint8_t muted, int32_t pid, uint16_t crashes) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, pid); + _mav_put_uint16_t(buf, 4, watchdog_id); + _mav_put_uint16_t(buf, 6, process_id); + _mav_put_uint16_t(buf, 8, crashes); + _mav_put_uint8_t(buf, 10, state); + _mav_put_uint8_t(buf, 11, muted); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_PROCESS_STATUS, buf, MAVLINK_MSG_ID_WATCHDOG_PROCESS_STATUS_LEN, MAVLINK_MSG_ID_WATCHDOG_PROCESS_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_PROCESS_STATUS, buf, MAVLINK_MSG_ID_WATCHDOG_PROCESS_STATUS_LEN); +#endif +#else + mavlink_watchdog_process_status_t *packet = (mavlink_watchdog_process_status_t *)msgbuf; + packet->pid = pid; + packet->watchdog_id = watchdog_id; + packet->process_id = process_id; + packet->crashes = crashes; + packet->state = state; + packet->muted = muted; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_PROCESS_STATUS, (const char *)packet, MAVLINK_MSG_ID_WATCHDOG_PROCESS_STATUS_LEN, MAVLINK_MSG_ID_WATCHDOG_PROCESS_STATUS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_WATCHDOG_PROCESS_STATUS, (const char *)packet, MAVLINK_MSG_ID_WATCHDOG_PROCESS_STATUS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE WATCHDOG_PROCESS_STATUS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/pixhawk/pixhawk.h b/mavlink/include/mavlink/v1.0/pixhawk/pixhawk.h index 428619eed..a624a2579 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/pixhawk.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/pixhawk.h @@ -12,15 +12,15 @@ extern "C" { // MESSAGE LENGTHS AND CRCS #ifndef MAVLINK_MESSAGE_LENGTHS -#define MAVLINK_MESSAGE_LENGTHS {9, 31, 12, 0, 14, 28, 3, 32, 0, 0, 0, 6, 0, 0, 0, 0, 0, 0, 0, 0, 20, 2, 25, 23, 30, 101, 22, 26, 16, 14, 28, 32, 28, 28, 22, 22, 21, 6, 6, 37, 4, 4, 2, 2, 4, 2, 2, 3, 13, 12, 19, 17, 15, 15, 27, 25, 18, 18, 20, 20, 9, 34, 26, 46, 36, 0, 6, 4, 0, 11, 18, 0, 0, 0, 20, 0, 33, 3, 0, 0, 20, 22, 0, 0, 0, 0, 0, 0, 0, 28, 56, 42, 33, 0, 0, 0, 0, 0, 0, 0, 26, 32, 32, 20, 32, 62, 54, 64, 84, 9, 254, 249, 9, 36, 26, 64, 22, 6, 14, 12, 97, 2, 2, 113, 35, 0, 0, 0, 0, 0, 13, 255, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 24, 33, 25, 0, 11, 52, 1, 92, 0, 0, 0, 0, 0, 18, 0, 0, 0, 0, 0, 0, 0, 0, 0, 18, 26, 16, 0, 0, 0, 0, 0, 0, 0, 4, 255, 12, 6, 0, 0, 0, 0, 0, 0, 106, 43, 55, 0, 0, 53, 0, 0, 0, 0, 21, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 30, 18, 18, 51, 9, 0} +#define MAVLINK_MESSAGE_LENGTHS {9, 31, 12, 0, 14, 28, 3, 32, 0, 0, 0, 6, 0, 0, 0, 0, 0, 0, 0, 0, 20, 2, 25, 23, 30, 101, 22, 26, 16, 14, 28, 32, 28, 28, 22, 22, 21, 6, 6, 37, 4, 4, 2, 2, 4, 2, 2, 3, 13, 12, 19, 17, 15, 15, 27, 25, 18, 18, 20, 20, 9, 34, 26, 46, 36, 42, 6, 4, 0, 11, 18, 0, 0, 0, 20, 0, 33, 3, 0, 0, 20, 22, 0, 0, 0, 0, 0, 0, 0, 28, 56, 42, 33, 0, 0, 0, 0, 0, 0, 0, 26, 32, 32, 20, 32, 62, 54, 64, 84, 9, 254, 249, 9, 36, 26, 64, 22, 6, 14, 12, 97, 2, 2, 113, 35, 6, 79, 0, 0, 0, 13, 255, 14, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 24, 33, 25, 0, 11, 52, 1, 92, 0, 0, 0, 0, 0, 18, 0, 0, 0, 0, 0, 0, 0, 0, 0, 18, 26, 16, 0, 0, 0, 0, 0, 0, 0, 4, 255, 12, 6, 0, 0, 0, 0, 0, 0, 106, 43, 55, 0, 0, 53, 0, 0, 0, 0, 21, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 30, 18, 18, 51, 9, 0} #endif #ifndef MAVLINK_MESSAGE_CRCS -#define MAVLINK_MESSAGE_CRCS {50, 124, 137, 0, 237, 217, 104, 119, 0, 0, 0, 89, 0, 0, 0, 0, 0, 0, 0, 0, 214, 159, 220, 168, 24, 23, 170, 144, 67, 115, 39, 246, 185, 104, 237, 244, 222, 212, 9, 254, 230, 28, 28, 132, 221, 232, 11, 153, 41, 39, 214, 223, 141, 33, 15, 3, 100, 24, 239, 238, 30, 240, 183, 130, 130, 0, 148, 21, 0, 243, 124, 0, 0, 0, 20, 0, 152, 143, 0, 0, 127, 106, 0, 0, 0, 0, 0, 0, 0, 231, 183, 63, 54, 0, 0, 0, 0, 0, 0, 0, 175, 102, 158, 208, 56, 93, 211, 108, 32, 185, 235, 93, 124, 124, 119, 4, 76, 128, 56, 116, 134, 237, 203, 250, 87, 0, 0, 0, 0, 0, 29, 223, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 177, 241, 15, 0, 108, 86, 95, 224, 0, 0, 0, 0, 0, 22, 0, 0, 0, 0, 0, 0, 0, 0, 0, 28, 249, 182, 0, 0, 0, 0, 0, 0, 0, 153, 16, 29, 162, 0, 0, 0, 0, 0, 0, 90, 95, 36, 0, 0, 88, 0, 0, 0, 0, 254, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 204, 49, 170, 44, 83, 46, 0} +#define MAVLINK_MESSAGE_CRCS {50, 124, 137, 0, 237, 217, 104, 119, 0, 0, 0, 89, 0, 0, 0, 0, 0, 0, 0, 0, 214, 159, 220, 168, 24, 23, 170, 144, 67, 115, 39, 246, 185, 104, 237, 244, 222, 212, 9, 254, 230, 28, 28, 132, 221, 232, 11, 153, 41, 39, 214, 223, 141, 33, 15, 3, 100, 24, 239, 238, 30, 240, 183, 130, 130, 118, 148, 21, 0, 243, 124, 0, 0, 0, 20, 0, 152, 143, 0, 0, 127, 106, 0, 0, 0, 0, 0, 0, 0, 231, 183, 63, 54, 0, 0, 0, 0, 0, 0, 0, 175, 102, 158, 208, 56, 93, 211, 108, 32, 185, 235, 93, 124, 124, 119, 4, 76, 128, 56, 116, 134, 237, 203, 250, 87, 203, 220, 0, 0, 0, 29, 223, 85, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 177, 241, 15, 0, 108, 86, 95, 224, 0, 0, 0, 0, 0, 22, 0, 0, 0, 0, 0, 0, 0, 0, 0, 28, 249, 182, 0, 0, 0, 0, 0, 0, 0, 153, 16, 29, 162, 0, 0, 0, 0, 0, 0, 90, 95, 36, 0, 0, 88, 0, 0, 0, 0, 254, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 204, 49, 170, 44, 83, 46, 0} #endif #ifndef MAVLINK_MESSAGE_INFO -#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_MODE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_ATTITUDE_QUATERNION, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_WRITE_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_ITEM, MAVLINK_MESSAGE_INFO_MISSION_REQUEST, MAVLINK_MESSAGE_INFO_MISSION_SET_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_LIST, MAVLINK_MESSAGE_INFO_MISSION_COUNT, MAVLINK_MESSAGE_INFO_MISSION_CLEAR_ALL, MAVLINK_MESSAGE_INFO_MISSION_ITEM_REACHED, MAVLINK_MESSAGE_INFO_MISSION_ACK, MAVLINK_MESSAGE_INFO_SET_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_SET_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SET_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_MOTORS_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_DATA_STREAM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_VFR_HUD, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_COMMAND_LONG, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_MANUAL_SETPOINT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_HIL_RC_INPUTS_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_GLOBAL_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_SPEED_ESTIMATE, MAVLINK_MESSAGE_INFO_VICON_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_HIGHRES_IMU, MAVLINK_MESSAGE_INFO_OMNIDIRECTIONAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_SENSOR, MAVLINK_MESSAGE_INFO_SIM_STATE, MAVLINK_MESSAGE_INFO_RADIO_STATUS, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_START, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_DIR_LIST, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_RES, MAVLINK_MESSAGE_INFO_HIL_GPS, MAVLINK_MESSAGE_INFO_HIL_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION, MAVLINK_MESSAGE_INFO_SCALED_IMU2, MAVLINK_MESSAGE_INFO_LOG_REQUEST_LIST, MAVLINK_MESSAGE_INFO_LOG_ENTRY, MAVLINK_MESSAGE_INFO_LOG_REQUEST_DATA, MAVLINK_MESSAGE_INFO_LOG_DATA, MAVLINK_MESSAGE_INFO_LOG_ERASE, MAVLINK_MESSAGE_INFO_LOG_REQUEST_END, MAVLINK_MESSAGE_INFO_GPS_INJECT_DATA, MAVLINK_MESSAGE_INFO_GPS2_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_DATA_TRANSMISSION_HANDSHAKE, MAVLINK_MESSAGE_INFO_ENCAPSULATED_DATA, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_BATTERY_STATUS, MAVLINK_MESSAGE_INFO_SETPOINT_8DOF, MAVLINK_MESSAGE_INFO_SETPOINT_6DOF, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_CAM_SHUTTER, MAVLINK_MESSAGE_INFO_IMAGE_TRIGGERED, MAVLINK_MESSAGE_INFO_IMAGE_TRIGGER_CONTROL, MAVLINK_MESSAGE_INFO_IMAGE_AVAILABLE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_POSITION_CONTROL_OFFSET, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_POSITION_CONTROL_SETPOINT, MAVLINK_MESSAGE_INFO_MARKER, MAVLINK_MESSAGE_INFO_RAW_AUX, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_WATCHDOG_HEARTBEAT, MAVLINK_MESSAGE_INFO_WATCHDOG_PROCESS_INFO, MAVLINK_MESSAGE_INFO_WATCHDOG_PROCESS_STATUS, MAVLINK_MESSAGE_INFO_WATCHDOG_COMMAND, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PATTERN_DETECTED, MAVLINK_MESSAGE_INFO_POINT_OF_INTEREST, MAVLINK_MESSAGE_INFO_POINT_OF_INTEREST_CONNECTION, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_BRIEF_FEATURE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ATTITUDE_CONTROL, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MEMORY_VECT, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}} +#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_MODE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_ATTITUDE_QUATERNION, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_WRITE_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_ITEM, MAVLINK_MESSAGE_INFO_MISSION_REQUEST, MAVLINK_MESSAGE_INFO_MISSION_SET_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_LIST, MAVLINK_MESSAGE_INFO_MISSION_COUNT, MAVLINK_MESSAGE_INFO_MISSION_CLEAR_ALL, MAVLINK_MESSAGE_INFO_MISSION_ITEM_REACHED, MAVLINK_MESSAGE_INFO_MISSION_ACK, MAVLINK_MESSAGE_INFO_SET_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_SET_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SET_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_MOTORS_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, MAVLINK_MESSAGE_INFO_RC_CHANNELS, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_DATA_STREAM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_VFR_HUD, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_COMMAND_LONG, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_MANUAL_SETPOINT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_HIL_RC_INPUTS_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_GLOBAL_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_SPEED_ESTIMATE, MAVLINK_MESSAGE_INFO_VICON_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_HIGHRES_IMU, MAVLINK_MESSAGE_INFO_OMNIDIRECTIONAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_SENSOR, MAVLINK_MESSAGE_INFO_SIM_STATE, MAVLINK_MESSAGE_INFO_RADIO_STATUS, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_START, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_DIR_LIST, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_RES, MAVLINK_MESSAGE_INFO_HIL_GPS, MAVLINK_MESSAGE_INFO_HIL_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION, MAVLINK_MESSAGE_INFO_SCALED_IMU2, MAVLINK_MESSAGE_INFO_LOG_REQUEST_LIST, MAVLINK_MESSAGE_INFO_LOG_ENTRY, MAVLINK_MESSAGE_INFO_LOG_REQUEST_DATA, MAVLINK_MESSAGE_INFO_LOG_DATA, MAVLINK_MESSAGE_INFO_LOG_ERASE, MAVLINK_MESSAGE_INFO_LOG_REQUEST_END, MAVLINK_MESSAGE_INFO_GPS_INJECT_DATA, MAVLINK_MESSAGE_INFO_GPS2_RAW, MAVLINK_MESSAGE_INFO_POWER_STATUS, MAVLINK_MESSAGE_INFO_SERIAL_CONTROL, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_DATA_TRANSMISSION_HANDSHAKE, MAVLINK_MESSAGE_INFO_ENCAPSULATED_DATA, MAVLINK_MESSAGE_INFO_DISTANCE_SENSOR, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_BATTERY_STATUS, MAVLINK_MESSAGE_INFO_SETPOINT_8DOF, MAVLINK_MESSAGE_INFO_SETPOINT_6DOF, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_CAM_SHUTTER, MAVLINK_MESSAGE_INFO_IMAGE_TRIGGERED, MAVLINK_MESSAGE_INFO_IMAGE_TRIGGER_CONTROL, MAVLINK_MESSAGE_INFO_IMAGE_AVAILABLE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_POSITION_CONTROL_OFFSET, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_POSITION_CONTROL_SETPOINT, MAVLINK_MESSAGE_INFO_MARKER, MAVLINK_MESSAGE_INFO_RAW_AUX, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_WATCHDOG_HEARTBEAT, MAVLINK_MESSAGE_INFO_WATCHDOG_PROCESS_INFO, MAVLINK_MESSAGE_INFO_WATCHDOG_PROCESS_STATUS, MAVLINK_MESSAGE_INFO_WATCHDOG_COMMAND, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PATTERN_DETECTED, MAVLINK_MESSAGE_INFO_POINT_OF_INTEREST, MAVLINK_MESSAGE_INFO_POINT_OF_INTEREST_CONNECTION, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_BRIEF_FEATURE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ATTITUDE_CONTROL, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MEMORY_VECT, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}} #endif #include "../protocol.h" @@ -56,6 +56,7 @@ enum MAV_CMD MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer| Latitude| Longitude| Altitude| */ MAV_CMD_NAV_ROI=80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */ MAV_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */ + MAV_CMD_NAV_SPLINE_WAYPOINT=82, /* Navigate to MISSION using a spline path. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Empty| Empty| Empty| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */ MAV_CMD_NAV_LAST=95, /* NOP - This command is only used to mark the upper limit of the NAV/ACTION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ MAV_CMD_CONDITION_DELAY=112, /* Delay mission state machine. |Delay in seconds (decimal)| Empty| Empty| Empty| Empty| Empty| Empty| */ MAV_CMD_CONDITION_CHANGE_ALT=113, /* Ascend/descend at rate. Delay mission state machine until desired altitude reached. |Descent / Ascend rate (m/s)| Empty| Empty| Empty| Empty| Empty| Finish Altitude| */ @@ -73,8 +74,16 @@ enum MAV_CMD MAV_CMD_DO_REPEAT_SERVO=184, /* Cycle a between its nominal setting and a desired PWM for a desired number of cycles with a desired period. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Cycle count| Cycle time (seconds)| Empty| Empty| Empty| */ MAV_CMD_DO_CONTROL_VIDEO=200, /* Control onboard camera system. |Camera ID (-1 for all)| Transmission: 0: disabled, 1: enabled compressed, 2: enabled raw| Transmission mode: 0: video stream, >0: single images every n seconds (decimal)| Recording: 0: disabled, 1: enabled compressed, 2: enabled raw| Empty| Empty| Empty| */ MAV_CMD_DO_SET_ROI=201, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */ + MAV_CMD_DO_DIGICAM_CONFIGURE=202, /* Mission command to configure an on-board camera controller system. |Modes: P, TV, AV, M, Etc| Shutter speed: Divisor number for one second| Aperture: F stop number| ISO number e.g. 80, 100, 200, Etc| Exposure type enumerator| Command Identity| Main engine cut-off time before camera trigger in seconds/10 (0 means no cut-off)| */ + MAV_CMD_DO_DIGICAM_CONTROL=203, /* Mission command to control an on-board camera controller system. |Session control e.g. show/hide lens| Zoom's absolute position| Zooming step value to offset zoom from the current position| Focus Locking, Unlocking or Re-locking| Shooting Command| Command Identity| Empty| */ + MAV_CMD_DO_MOUNT_CONFIGURE=204, /* Mission command to configure a camera or antenna mount |Mount operation mode (see MAV_MOUNT_MODE enum)| stabilize roll? (1 = yes, 0 = no)| stabilize pitch? (1 = yes, 0 = no)| stabilize yaw? (1 = yes, 0 = no)| Empty| Empty| Empty| */ + MAV_CMD_DO_MOUNT_CONTROL=205, /* Mission command to control a camera or antenna mount |pitch or lat in degrees, depending on mount mode.| roll or lon in degrees depending on mount mode| yaw or alt (in meters) depending on mount mode| reserved| reserved| reserved| MAV_MOUNT_MODE enum value| */ + MAV_CMD_DO_SET_CAM_TRIGG_DIST=206, /* Mission command to set CAM_TRIGG_DIST for this flight |Camera trigger distance (meters)| Empty| Empty| Empty| Empty| Empty| Empty| */ + MAV_CMD_DO_FENCE_ENABLE=207, /* Mission command to enable the geofence |enable? (0=disable, 1=enable)| Empty| Empty| Empty| Empty| Empty| Empty| */ + MAV_CMD_DO_PARACHUTE=208, /* Mission command to trigger a parachute |action (0=disable, 1=enable, 2=release, for some systems see PARACHUTE_ACTION enum, not in general message set.)| Empty| Empty| Empty| Empty| Empty| Empty| */ + MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1| q2 - quaternion param #2| q3 - quaternion param #3| q4 - quaternion param #4| Empty| Empty| Empty| */ MAV_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ - MAV_CMD_PREFLIGHT_CALIBRATION=241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Empty| Empty| */ + MAV_CMD_PREFLIGHT_CALIBRATION=241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Compass/Motor interference calibration: 0: no, 1: yes| Empty| */ MAV_CMD_PREFLIGHT_SET_SENSOR_OFFSETS=242, /* Set sensor offsets. This command will be only accepted if in pre-flight mode. |Sensor to adjust the offsets for: 0: gyros, 1: accelerometer, 2: magnetometer, 3: barometer, 4: optical flow| X axis offset (or generic dimension 1), in the sensor's raw units| Y axis offset (or generic dimension 2), in the sensor's raw units| Z axis offset (or generic dimension 3), in the sensor's raw units| Generic dimension 4, in the sensor's raw units| Generic dimension 5, in the sensor's raw units| Generic dimension 6, in the sensor's raw units| */ MAV_CMD_PREFLIGHT_STORAGE=245, /* Request storage of different parameter values and logs. This command will be only accepted if in pre-flight mode. |Parameter storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Mission storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Reserved| Reserved| Empty| Empty| Empty| */ MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN=246, /* Request the reboot or shutdown of system components. |0: Do nothing for autopilot, 1: Reboot autopilot, 2: Shutdown autopilot.| 0: Do nothing for onboard computer, 1: Reboot onboard computer, 2: Shutdown onboard computer.| Reserved| Reserved| Empty| Empty| Empty| */ diff --git a/mavlink/include/mavlink/v1.0/pixhawk/version.h b/mavlink/include/mavlink/v1.0/pixhawk/version.h index aa79f6ffb..6610a894c 100644 --- a/mavlink/include/mavlink/v1.0/pixhawk/version.h +++ b/mavlink/include/mavlink/v1.0/pixhawk/version.h @@ -5,7 +5,7 @@ #ifndef MAVLINK_VERSION_H #define MAVLINK_VERSION_H -#define MAVLINK_BUILD_DATE "Tue Feb 4 15:28:16 2014" +#define MAVLINK_BUILD_DATE "Sun Apr 13 09:38:46 2014" #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0" #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255 diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_cmd_airspeed_ack.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_cmd_airspeed_ack.h index 73e9d75db..a87ce87d3 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_cmd_airspeed_ack.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_cmd_airspeed_ack.h @@ -173,6 +173,40 @@ static inline void mavlink_msg_cmd_airspeed_ack_send(mavlink_channel_t chan, flo #endif } +#if MAVLINK_MSG_ID_CMD_AIRSPEED_ACK_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_cmd_airspeed_ack_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float spCmd, uint8_t ack) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, spCmd); + _mav_put_uint8_t(buf, 4, ack); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CMD_AIRSPEED_ACK, buf, MAVLINK_MSG_ID_CMD_AIRSPEED_ACK_LEN, MAVLINK_MSG_ID_CMD_AIRSPEED_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CMD_AIRSPEED_ACK, buf, MAVLINK_MSG_ID_CMD_AIRSPEED_ACK_LEN); +#endif +#else + mavlink_cmd_airspeed_ack_t *packet = (mavlink_cmd_airspeed_ack_t *)msgbuf; + packet->spCmd = spCmd; + packet->ack = ack; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CMD_AIRSPEED_ACK, (const char *)packet, MAVLINK_MSG_ID_CMD_AIRSPEED_ACK_LEN, MAVLINK_MSG_ID_CMD_AIRSPEED_ACK_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CMD_AIRSPEED_ACK, (const char *)packet, MAVLINK_MSG_ID_CMD_AIRSPEED_ACK_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE CMD_AIRSPEED_ACK UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_cmd_airspeed_chng.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_cmd_airspeed_chng.h index b6b567f99..71d61e1e0 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_cmd_airspeed_chng.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_cmd_airspeed_chng.h @@ -173,6 +173,40 @@ static inline void mavlink_msg_cmd_airspeed_chng_send(mavlink_channel_t chan, ui #endif } +#if MAVLINK_MSG_ID_CMD_AIRSPEED_CHNG_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_cmd_airspeed_chng_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t target, float spCmd) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, spCmd); + _mav_put_uint8_t(buf, 4, target); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CMD_AIRSPEED_CHNG, buf, MAVLINK_MSG_ID_CMD_AIRSPEED_CHNG_LEN, MAVLINK_MSG_ID_CMD_AIRSPEED_CHNG_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CMD_AIRSPEED_CHNG, buf, MAVLINK_MSG_ID_CMD_AIRSPEED_CHNG_LEN); +#endif +#else + mavlink_cmd_airspeed_chng_t *packet = (mavlink_cmd_airspeed_chng_t *)msgbuf; + packet->spCmd = spCmd; + packet->target = target; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CMD_AIRSPEED_CHNG, (const char *)packet, MAVLINK_MSG_ID_CMD_AIRSPEED_CHNG_LEN, MAVLINK_MSG_ID_CMD_AIRSPEED_CHNG_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CMD_AIRSPEED_CHNG, (const char *)packet, MAVLINK_MSG_ID_CMD_AIRSPEED_CHNG_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE CMD_AIRSPEED_CHNG UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_filt_rot_vel.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_filt_rot_vel.h index 642f7aab9..40a3db25a 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_filt_rot_vel.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_filt_rot_vel.h @@ -154,6 +154,38 @@ static inline void mavlink_msg_filt_rot_vel_send(mavlink_channel_t chan, const f #endif } +#if MAVLINK_MSG_ID_FILT_ROT_VEL_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_filt_rot_vel_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, const float *rotVel) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + + _mav_put_float_array(buf, 0, rotVel, 3); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILT_ROT_VEL, buf, MAVLINK_MSG_ID_FILT_ROT_VEL_LEN, MAVLINK_MSG_ID_FILT_ROT_VEL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILT_ROT_VEL, buf, MAVLINK_MSG_ID_FILT_ROT_VEL_LEN); +#endif +#else + mavlink_filt_rot_vel_t *packet = (mavlink_filt_rot_vel_t *)msgbuf; + + mav_array_memcpy(packet->rotVel, rotVel, sizeof(float)*3); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILT_ROT_VEL, (const char *)packet, MAVLINK_MSG_ID_FILT_ROT_VEL_LEN, MAVLINK_MSG_ID_FILT_ROT_VEL_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_FILT_ROT_VEL, (const char *)packet, MAVLINK_MSG_ID_FILT_ROT_VEL_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE FILT_ROT_VEL UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_llc_out.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_llc_out.h index 0f8369881..bceed1013 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_llc_out.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_llc_out.h @@ -174,6 +174,40 @@ static inline void mavlink_msg_llc_out_send(mavlink_channel_t chan, const int16_ #endif } +#if MAVLINK_MSG_ID_LLC_OUT_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_llc_out_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, const int16_t *servoOut, const int16_t *MotorOut) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + + _mav_put_int16_t_array(buf, 0, servoOut, 4); + _mav_put_int16_t_array(buf, 8, MotorOut, 2); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LLC_OUT, buf, MAVLINK_MSG_ID_LLC_OUT_LEN, MAVLINK_MSG_ID_LLC_OUT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LLC_OUT, buf, MAVLINK_MSG_ID_LLC_OUT_LEN); +#endif +#else + mavlink_llc_out_t *packet = (mavlink_llc_out_t *)msgbuf; + + mav_array_memcpy(packet->servoOut, servoOut, sizeof(int16_t)*4); + mav_array_memcpy(packet->MotorOut, MotorOut, sizeof(int16_t)*2); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LLC_OUT, (const char *)packet, MAVLINK_MSG_ID_LLC_OUT_LEN, MAVLINK_MSG_ID_LLC_OUT_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_LLC_OUT, (const char *)packet, MAVLINK_MSG_ID_LLC_OUT_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE LLC_OUT UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_air_temp.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_air_temp.h index 5d9382326..f5a43e4fa 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_air_temp.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_air_temp.h @@ -154,6 +154,38 @@ static inline void mavlink_msg_obs_air_temp_send(mavlink_channel_t chan, float a #endif } +#if MAVLINK_MSG_ID_OBS_AIR_TEMP_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_obs_air_temp_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float airT) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, airT); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_AIR_TEMP, buf, MAVLINK_MSG_ID_OBS_AIR_TEMP_LEN, MAVLINK_MSG_ID_OBS_AIR_TEMP_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_AIR_TEMP, buf, MAVLINK_MSG_ID_OBS_AIR_TEMP_LEN); +#endif +#else + mavlink_obs_air_temp_t *packet = (mavlink_obs_air_temp_t *)msgbuf; + packet->airT = airT; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_AIR_TEMP, (const char *)packet, MAVLINK_MSG_ID_OBS_AIR_TEMP_LEN, MAVLINK_MSG_ID_OBS_AIR_TEMP_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_AIR_TEMP, (const char *)packet, MAVLINK_MSG_ID_OBS_AIR_TEMP_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE OBS_AIR_TEMP UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_air_velocity.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_air_velocity.h index 35d813ca1..67d5ab2a2 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_air_velocity.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_air_velocity.h @@ -192,6 +192,42 @@ static inline void mavlink_msg_obs_air_velocity_send(mavlink_channel_t chan, flo #endif } +#if MAVLINK_MSG_ID_OBS_AIR_VELOCITY_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_obs_air_velocity_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float magnitude, float aoa, float slip) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, magnitude); + _mav_put_float(buf, 4, aoa); + _mav_put_float(buf, 8, slip); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_AIR_VELOCITY, buf, MAVLINK_MSG_ID_OBS_AIR_VELOCITY_LEN, MAVLINK_MSG_ID_OBS_AIR_VELOCITY_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_AIR_VELOCITY, buf, MAVLINK_MSG_ID_OBS_AIR_VELOCITY_LEN); +#endif +#else + mavlink_obs_air_velocity_t *packet = (mavlink_obs_air_velocity_t *)msgbuf; + packet->magnitude = magnitude; + packet->aoa = aoa; + packet->slip = slip; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_AIR_VELOCITY, (const char *)packet, MAVLINK_MSG_ID_OBS_AIR_VELOCITY_LEN, MAVLINK_MSG_ID_OBS_AIR_VELOCITY_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_AIR_VELOCITY, (const char *)packet, MAVLINK_MSG_ID_OBS_AIR_VELOCITY_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE OBS_AIR_VELOCITY UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_attitude.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_attitude.h index 9c80cd66e..e1178e25f 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_attitude.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_attitude.h @@ -154,6 +154,38 @@ static inline void mavlink_msg_obs_attitude_send(mavlink_channel_t chan, const d #endif } +#if MAVLINK_MSG_ID_OBS_ATTITUDE_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_obs_attitude_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, const double *quat) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + + _mav_put_double_array(buf, 0, quat, 4); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_ATTITUDE, buf, MAVLINK_MSG_ID_OBS_ATTITUDE_LEN, MAVLINK_MSG_ID_OBS_ATTITUDE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_ATTITUDE, buf, MAVLINK_MSG_ID_OBS_ATTITUDE_LEN); +#endif +#else + mavlink_obs_attitude_t *packet = (mavlink_obs_attitude_t *)msgbuf; + + mav_array_memcpy(packet->quat, quat, sizeof(double)*4); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_ATTITUDE, (const char *)packet, MAVLINK_MSG_ID_OBS_ATTITUDE_LEN, MAVLINK_MSG_ID_OBS_ATTITUDE_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_ATTITUDE, (const char *)packet, MAVLINK_MSG_ID_OBS_ATTITUDE_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE OBS_ATTITUDE UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_bias.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_bias.h index 24dd43b57..b164687ff 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_bias.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_bias.h @@ -174,6 +174,40 @@ static inline void mavlink_msg_obs_bias_send(mavlink_channel_t chan, const float #endif } +#if MAVLINK_MSG_ID_OBS_BIAS_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_obs_bias_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, const float *accBias, const float *gyroBias) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + + _mav_put_float_array(buf, 0, accBias, 3); + _mav_put_float_array(buf, 12, gyroBias, 3); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_BIAS, buf, MAVLINK_MSG_ID_OBS_BIAS_LEN, MAVLINK_MSG_ID_OBS_BIAS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_BIAS, buf, MAVLINK_MSG_ID_OBS_BIAS_LEN); +#endif +#else + mavlink_obs_bias_t *packet = (mavlink_obs_bias_t *)msgbuf; + + mav_array_memcpy(packet->accBias, accBias, sizeof(float)*3); + mav_array_memcpy(packet->gyroBias, gyroBias, sizeof(float)*3); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_BIAS, (const char *)packet, MAVLINK_MSG_ID_OBS_BIAS_LEN, MAVLINK_MSG_ID_OBS_BIAS_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_BIAS, (const char *)packet, MAVLINK_MSG_ID_OBS_BIAS_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE OBS_BIAS UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_position.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_position.h index cfc2fe7e1..f0ecef0e7 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_position.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_position.h @@ -192,6 +192,42 @@ static inline void mavlink_msg_obs_position_send(mavlink_channel_t chan, int32_t #endif } +#if MAVLINK_MSG_ID_OBS_POSITION_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_obs_position_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, int32_t lon, int32_t lat, int32_t alt) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_int32_t(buf, 0, lon); + _mav_put_int32_t(buf, 4, lat); + _mav_put_int32_t(buf, 8, alt); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_POSITION, buf, MAVLINK_MSG_ID_OBS_POSITION_LEN, MAVLINK_MSG_ID_OBS_POSITION_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_POSITION, buf, MAVLINK_MSG_ID_OBS_POSITION_LEN); +#endif +#else + mavlink_obs_position_t *packet = (mavlink_obs_position_t *)msgbuf; + packet->lon = lon; + packet->lat = lat; + packet->alt = alt; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_POSITION, (const char *)packet, MAVLINK_MSG_ID_OBS_POSITION_LEN, MAVLINK_MSG_ID_OBS_POSITION_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_POSITION, (const char *)packet, MAVLINK_MSG_ID_OBS_POSITION_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE OBS_POSITION UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_qff.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_qff.h index 24e272bf7..31617c883 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_qff.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_qff.h @@ -154,6 +154,38 @@ static inline void mavlink_msg_obs_qff_send(mavlink_channel_t chan, float qff) #endif } +#if MAVLINK_MSG_ID_OBS_QFF_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_obs_qff_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float qff) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, qff); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_QFF, buf, MAVLINK_MSG_ID_OBS_QFF_LEN, MAVLINK_MSG_ID_OBS_QFF_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_QFF, buf, MAVLINK_MSG_ID_OBS_QFF_LEN); +#endif +#else + mavlink_obs_qff_t *packet = (mavlink_obs_qff_t *)msgbuf; + packet->qff = qff; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_QFF, (const char *)packet, MAVLINK_MSG_ID_OBS_QFF_LEN, MAVLINK_MSG_ID_OBS_QFF_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_QFF, (const char *)packet, MAVLINK_MSG_ID_OBS_QFF_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE OBS_QFF UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_velocity.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_velocity.h index 6e3776632..ec815d692 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_velocity.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_velocity.h @@ -154,6 +154,38 @@ static inline void mavlink_msg_obs_velocity_send(mavlink_channel_t chan, const f #endif } +#if MAVLINK_MSG_ID_OBS_VELOCITY_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_obs_velocity_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, const float *vel) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + + _mav_put_float_array(buf, 0, vel, 3); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_VELOCITY, buf, MAVLINK_MSG_ID_OBS_VELOCITY_LEN, MAVLINK_MSG_ID_OBS_VELOCITY_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_VELOCITY, buf, MAVLINK_MSG_ID_OBS_VELOCITY_LEN); +#endif +#else + mavlink_obs_velocity_t *packet = (mavlink_obs_velocity_t *)msgbuf; + + mav_array_memcpy(packet->vel, vel, sizeof(float)*3); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_VELOCITY, (const char *)packet, MAVLINK_MSG_ID_OBS_VELOCITY_LEN, MAVLINK_MSG_ID_OBS_VELOCITY_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_VELOCITY, (const char *)packet, MAVLINK_MSG_ID_OBS_VELOCITY_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE OBS_VELOCITY UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_wind.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_wind.h index 55f7cb2ae..c40391d44 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_wind.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_obs_wind.h @@ -154,6 +154,38 @@ static inline void mavlink_msg_obs_wind_send(mavlink_channel_t chan, const float #endif } +#if MAVLINK_MSG_ID_OBS_WIND_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_obs_wind_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, const float *wind) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + + _mav_put_float_array(buf, 0, wind, 3); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_WIND, buf, MAVLINK_MSG_ID_OBS_WIND_LEN, MAVLINK_MSG_ID_OBS_WIND_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_WIND, buf, MAVLINK_MSG_ID_OBS_WIND_LEN); +#endif +#else + mavlink_obs_wind_t *packet = (mavlink_obs_wind_t *)msgbuf; + + mav_array_memcpy(packet->wind, wind, sizeof(float)*3); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_WIND, (const char *)packet, MAVLINK_MSG_ID_OBS_WIND_LEN, MAVLINK_MSG_ID_OBS_WIND_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_OBS_WIND, (const char *)packet, MAVLINK_MSG_ID_OBS_WIND_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE OBS_WIND UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_pm_elec.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_pm_elec.h index e0963ece7..70524f464 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_pm_elec.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_pm_elec.h @@ -186,6 +186,40 @@ static inline void mavlink_msg_pm_elec_send(mavlink_channel_t chan, float PwCons #endif } +#if MAVLINK_MSG_ID_PM_ELEC_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_pm_elec_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, float PwCons, float BatStat, const float *PwGen) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_float(buf, 0, PwCons); + _mav_put_float(buf, 4, BatStat); + _mav_put_float_array(buf, 8, PwGen, 3); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PM_ELEC, buf, MAVLINK_MSG_ID_PM_ELEC_LEN, MAVLINK_MSG_ID_PM_ELEC_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PM_ELEC, buf, MAVLINK_MSG_ID_PM_ELEC_LEN); +#endif +#else + mavlink_pm_elec_t *packet = (mavlink_pm_elec_t *)msgbuf; + packet->PwCons = PwCons; + packet->BatStat = BatStat; + mav_array_memcpy(packet->PwGen, PwGen, sizeof(float)*3); +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PM_ELEC, (const char *)packet, MAVLINK_MSG_ID_PM_ELEC_LEN, MAVLINK_MSG_ID_PM_ELEC_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PM_ELEC, (const char *)packet, MAVLINK_MSG_ID_PM_ELEC_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE PM_ELEC UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_sys_stat.h b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_sys_stat.h index 94f3e58bb..72f8a8193 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_sys_stat.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/mavlink_msg_sys_stat.h @@ -211,6 +211,44 @@ static inline void mavlink_msg_sys_stat_send(mavlink_channel_t chan, uint8_t gps #endif } +#if MAVLINK_MSG_ID_SYS_Stat_LEN <= MAVLINK_MAX_PAYLOAD_LEN +/* + This varient of _send() can be used to save stack space by re-using + memory from the receive buffer. The caller provides a + mavlink_message_t which is the size of a full mavlink message. This + is usually the receive buffer for the channel, and allows a reply to an + incoming message with minimum stack space usage. + */ +static inline void mavlink_msg_sys_stat_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t gps, uint8_t act, uint8_t mod, uint8_t commRssi) +{ +#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS + char *buf = (char *)msgbuf; + _mav_put_uint8_t(buf, 0, gps); + _mav_put_uint8_t(buf, 1, act); + _mav_put_uint8_t(buf, 2, mod); + _mav_put_uint8_t(buf, 3, commRssi); + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SYS_Stat, buf, MAVLINK_MSG_ID_SYS_Stat_LEN, MAVLINK_MSG_ID_SYS_Stat_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SYS_Stat, buf, MAVLINK_MSG_ID_SYS_Stat_LEN); +#endif +#else + mavlink_sys_stat_t *packet = (mavlink_sys_stat_t *)msgbuf; + packet->gps = gps; + packet->act = act; + packet->mod = mod; + packet->commRssi = commRssi; + +#if MAVLINK_CRC_EXTRA + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SYS_Stat, (const char *)packet, MAVLINK_MSG_ID_SYS_Stat_LEN, MAVLINK_MSG_ID_SYS_Stat_CRC); +#else + _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_SYS_Stat, (const char *)packet, MAVLINK_MSG_ID_SYS_Stat_LEN); +#endif +#endif +} +#endif + #endif // MESSAGE SYS_Stat UNPACKING diff --git a/mavlink/include/mavlink/v1.0/sensesoar/sensesoar.h b/mavlink/include/mavlink/v1.0/sensesoar/sensesoar.h index 26666b0cc..2eab86354 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/sensesoar.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/sensesoar.h @@ -12,15 +12,15 @@ extern "C" { // MESSAGE LENGTHS AND CRCS #ifndef MAVLINK_MESSAGE_LENGTHS -#define MAVLINK_MESSAGE_LENGTHS {9, 31, 12, 0, 14, 28, 3, 32, 0, 0, 0, 6, 0, 0, 0, 0, 0, 0, 0, 0, 20, 2, 25, 23, 30, 101, 22, 26, 16, 14, 28, 32, 28, 28, 22, 22, 21, 6, 6, 37, 4, 4, 2, 2, 4, 2, 2, 3, 13, 12, 19, 17, 15, 15, 27, 25, 18, 18, 20, 20, 9, 34, 26, 46, 36, 0, 6, 4, 0, 11, 18, 0, 0, 0, 20, 0, 33, 3, 0, 0, 20, 22, 0, 0, 0, 0, 0, 0, 0, 28, 56, 42, 33, 0, 0, 0, 0, 0, 0, 0, 26, 32, 32, 20, 32, 62, 54, 64, 84, 9, 254, 249, 9, 36, 26, 64, 22, 6, 14, 12, 97, 2, 2, 113, 35, 0, 0, 0, 0, 0, 13, 255, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 24, 33, 25, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 12, 0, 12, 0, 32, 0, 12, 0, 12, 0, 24, 0, 4, 4, 12, 0, 12, 0, 20, 0, 4, 0, 5, 0, 5, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 30, 18, 18, 51, 9, 0} +#define MAVLINK_MESSAGE_LENGTHS {9, 31, 12, 0, 14, 28, 3, 32, 0, 0, 0, 6, 0, 0, 0, 0, 0, 0, 0, 0, 20, 2, 25, 23, 30, 101, 22, 26, 16, 14, 28, 32, 28, 28, 22, 22, 21, 6, 6, 37, 4, 4, 2, 2, 4, 2, 2, 3, 13, 12, 19, 17, 15, 15, 27, 25, 18, 18, 20, 20, 9, 34, 26, 46, 36, 42, 6, 4, 0, 11, 18, 0, 0, 0, 20, 0, 33, 3, 0, 0, 20, 22, 0, 0, 0, 0, 0, 0, 0, 28, 56, 42, 33, 0, 0, 0, 0, 0, 0, 0, 26, 32, 32, 20, 32, 62, 54, 64, 84, 9, 254, 249, 9, 36, 26, 64, 22, 6, 14, 12, 97, 2, 2, 113, 35, 6, 79, 0, 0, 0, 13, 255, 14, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 24, 33, 25, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 12, 0, 12, 0, 32, 0, 12, 0, 12, 0, 24, 0, 4, 4, 12, 0, 12, 0, 20, 0, 4, 0, 5, 0, 5, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 30, 18, 18, 51, 9, 0} #endif #ifndef MAVLINK_MESSAGE_CRCS -#define MAVLINK_MESSAGE_CRCS {50, 124, 137, 0, 237, 217, 104, 119, 0, 0, 0, 89, 0, 0, 0, 0, 0, 0, 0, 0, 214, 159, 220, 168, 24, 23, 170, 144, 67, 115, 39, 246, 185, 104, 237, 244, 222, 212, 9, 254, 230, 28, 28, 132, 221, 232, 11, 153, 41, 39, 214, 223, 141, 33, 15, 3, 100, 24, 239, 238, 30, 240, 183, 130, 130, 0, 148, 21, 0, 243, 124, 0, 0, 0, 20, 0, 152, 143, 0, 0, 127, 106, 0, 0, 0, 0, 0, 0, 0, 231, 183, 63, 54, 0, 0, 0, 0, 0, 0, 0, 175, 102, 158, 208, 56, 93, 211, 108, 32, 185, 235, 93, 124, 124, 119, 4, 76, 128, 56, 116, 134, 237, 203, 250, 87, 0, 0, 0, 0, 0, 29, 223, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 177, 241, 15, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 15, 0, 108, 0, 146, 0, 16, 0, 32, 0, 159, 0, 24, 248, 79, 0, 5, 0, 170, 0, 157, 0, 209, 0, 243, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 204, 49, 170, 44, 83, 46, 0} +#define MAVLINK_MESSAGE_CRCS {50, 124, 137, 0, 237, 217, 104, 119, 0, 0, 0, 89, 0, 0, 0, 0, 0, 0, 0, 0, 214, 159, 220, 168, 24, 23, 170, 144, 67, 115, 39, 246, 185, 104, 237, 244, 222, 212, 9, 254, 230, 28, 28, 132, 221, 232, 11, 153, 41, 39, 214, 223, 141, 33, 15, 3, 100, 24, 239, 238, 30, 240, 183, 130, 130, 118, 148, 21, 0, 243, 124, 0, 0, 0, 20, 0, 152, 143, 0, 0, 127, 106, 0, 0, 0, 0, 0, 0, 0, 231, 183, 63, 54, 0, 0, 0, 0, 0, 0, 0, 175, 102, 158, 208, 56, 93, 211, 108, 32, 185, 235, 93, 124, 124, 119, 4, 76, 128, 56, 116, 134, 237, 203, 250, 87, 203, 220, 0, 0, 0, 29, 223, 85, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 177, 241, 15, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 15, 0, 108, 0, 146, 0, 16, 0, 32, 0, 159, 0, 24, 248, 79, 0, 5, 0, 170, 0, 157, 0, 209, 0, 243, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 204, 49, 170, 44, 83, 46, 0} #endif #ifndef MAVLINK_MESSAGE_INFO -#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_MODE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_ATTITUDE_QUATERNION, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_WRITE_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_ITEM, MAVLINK_MESSAGE_INFO_MISSION_REQUEST, MAVLINK_MESSAGE_INFO_MISSION_SET_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_LIST, MAVLINK_MESSAGE_INFO_MISSION_COUNT, MAVLINK_MESSAGE_INFO_MISSION_CLEAR_ALL, MAVLINK_MESSAGE_INFO_MISSION_ITEM_REACHED, MAVLINK_MESSAGE_INFO_MISSION_ACK, MAVLINK_MESSAGE_INFO_SET_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_SET_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SET_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_MOTORS_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_DATA_STREAM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_VFR_HUD, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_COMMAND_LONG, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_MANUAL_SETPOINT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_HIL_RC_INPUTS_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_GLOBAL_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_SPEED_ESTIMATE, MAVLINK_MESSAGE_INFO_VICON_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_HIGHRES_IMU, MAVLINK_MESSAGE_INFO_OMNIDIRECTIONAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_SENSOR, MAVLINK_MESSAGE_INFO_SIM_STATE, MAVLINK_MESSAGE_INFO_RADIO_STATUS, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_START, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_DIR_LIST, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_RES, MAVLINK_MESSAGE_INFO_HIL_GPS, MAVLINK_MESSAGE_INFO_HIL_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION, MAVLINK_MESSAGE_INFO_SCALED_IMU2, MAVLINK_MESSAGE_INFO_LOG_REQUEST_LIST, MAVLINK_MESSAGE_INFO_LOG_ENTRY, MAVLINK_MESSAGE_INFO_LOG_REQUEST_DATA, MAVLINK_MESSAGE_INFO_LOG_DATA, MAVLINK_MESSAGE_INFO_LOG_ERASE, MAVLINK_MESSAGE_INFO_LOG_REQUEST_END, MAVLINK_MESSAGE_INFO_GPS_INJECT_DATA, MAVLINK_MESSAGE_INFO_GPS2_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_DATA_TRANSMISSION_HANDSHAKE, MAVLINK_MESSAGE_INFO_ENCAPSULATED_DATA, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_BATTERY_STATUS, MAVLINK_MESSAGE_INFO_SETPOINT_8DOF, MAVLINK_MESSAGE_INFO_SETPOINT_6DOF, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_POSITION, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_VELOCITY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_ATTITUDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_WIND, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_AIR_VELOCITY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_BIAS, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_QFF, MAVLINK_MESSAGE_INFO_OBS_AIR_TEMP, MAVLINK_MESSAGE_INFO_FILT_ROT_VEL, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LLC_OUT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PM_ELEC, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SYS_Stat, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_CMD_AIRSPEED_CHNG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_CMD_AIRSPEED_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MEMORY_VECT, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}} +#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_MODE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_ATTITUDE_QUATERNION, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_WRITE_PARTIAL_LIST, MAVLINK_MESSAGE_INFO_MISSION_ITEM, MAVLINK_MESSAGE_INFO_MISSION_REQUEST, MAVLINK_MESSAGE_INFO_MISSION_SET_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_CURRENT, MAVLINK_MESSAGE_INFO_MISSION_REQUEST_LIST, MAVLINK_MESSAGE_INFO_MISSION_COUNT, MAVLINK_MESSAGE_INFO_MISSION_CLEAR_ALL, MAVLINK_MESSAGE_INFO_MISSION_ITEM_REACHED, MAVLINK_MESSAGE_INFO_MISSION_ACK, MAVLINK_MESSAGE_INFO_SET_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_SET_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SET_GLOBAL_POSITION_SETPOINT_INT, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_MOTORS_SETPOINT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_SET_QUAD_SWARM_LED_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, MAVLINK_MESSAGE_INFO_RC_CHANNELS, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_DATA_STREAM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_VFR_HUD, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_COMMAND_LONG, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_RATES_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_MANUAL_SETPOINT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_NED_SYSTEM_GLOBAL_OFFSET, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_HIL_RC_INPUTS_RAW, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_GLOBAL_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_VISION_SPEED_ESTIMATE, MAVLINK_MESSAGE_INFO_VICON_POSITION_ESTIMATE, MAVLINK_MESSAGE_INFO_HIGHRES_IMU, MAVLINK_MESSAGE_INFO_OMNIDIRECTIONAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_SENSOR, MAVLINK_MESSAGE_INFO_SIM_STATE, MAVLINK_MESSAGE_INFO_RADIO_STATUS, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_START, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_DIR_LIST, MAVLINK_MESSAGE_INFO_FILE_TRANSFER_RES, MAVLINK_MESSAGE_INFO_HIL_GPS, MAVLINK_MESSAGE_INFO_HIL_OPTICAL_FLOW, MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION, MAVLINK_MESSAGE_INFO_SCALED_IMU2, MAVLINK_MESSAGE_INFO_LOG_REQUEST_LIST, MAVLINK_MESSAGE_INFO_LOG_ENTRY, MAVLINK_MESSAGE_INFO_LOG_REQUEST_DATA, MAVLINK_MESSAGE_INFO_LOG_DATA, MAVLINK_MESSAGE_INFO_LOG_ERASE, MAVLINK_MESSAGE_INFO_LOG_REQUEST_END, MAVLINK_MESSAGE_INFO_GPS_INJECT_DATA, MAVLINK_MESSAGE_INFO_GPS2_RAW, MAVLINK_MESSAGE_INFO_POWER_STATUS, MAVLINK_MESSAGE_INFO_SERIAL_CONTROL, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_DATA_TRANSMISSION_HANDSHAKE, MAVLINK_MESSAGE_INFO_ENCAPSULATED_DATA, MAVLINK_MESSAGE_INFO_DISTANCE_SENSOR, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_BATTERY_STATUS, MAVLINK_MESSAGE_INFO_SETPOINT_8DOF, MAVLINK_MESSAGE_INFO_SETPOINT_6DOF, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_POSITION, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_VELOCITY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_ATTITUDE, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_WIND, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_AIR_VELOCITY, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_BIAS, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_OBS_QFF, MAVLINK_MESSAGE_INFO_OBS_AIR_TEMP, MAVLINK_MESSAGE_INFO_FILT_ROT_VEL, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_LLC_OUT, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PM_ELEC, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SYS_Stat, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_CMD_AIRSPEED_CHNG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_CMD_AIRSPEED_ACK, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_MEMORY_VECT, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}} #endif #include "../protocol.h" diff --git a/mavlink/include/mavlink/v1.0/sensesoar/version.h b/mavlink/include/mavlink/v1.0/sensesoar/version.h index cdd683949..78d562803 100644 --- a/mavlink/include/mavlink/v1.0/sensesoar/version.h +++ b/mavlink/include/mavlink/v1.0/sensesoar/version.h @@ -5,7 +5,7 @@ #ifndef MAVLINK_VERSION_H #define MAVLINK_VERSION_H -#define MAVLINK_BUILD_DATE "Tue Feb 4 15:28:27 2014" +#define MAVLINK_BUILD_DATE "Sun Apr 13 09:39:00 2014" #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0" #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255 diff --git a/nuttx-configs/aerocore/include/board.h b/nuttx-configs/aerocore/include/board.h new file mode 100644 index 000000000..8705c1bc2 --- /dev/null +++ b/nuttx-configs/aerocore/include/board.h @@ -0,0 +1,263 @@ +/************************************************************************************ + * configs/aerocore/include/board.h + * include/arch/board/board.h + * + * Copyright (C) 2009 Gregory Nutt. All rights reserved. + * Author: Gregory Nutt <gnutt@nuttx.org> + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name NuttX nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ************************************************************************************/ + +#ifndef __ARCH_BOARD_BOARD_H +#define __ARCH_BOARD_BOARD_H + +/************************************************************************************ + * Included Files + ************************************************************************************/ + +#include <nuttx/config.h> +#ifndef __ASSEMBLY__ +# include <stdint.h> +#endif + +#include <stm32.h> + +/************************************************************************************ + * Definitions + ************************************************************************************/ + +/* Clocking *************************************************************************/ +/* The AeroCore uses a 24MHz crystal connected to the HSE. + * + * This is the "standard" configuration as set up by arch/arm/src/stm32f40xx_rcc.c: + * System Clock source : PLL (HSE) + * SYSCLK(Hz) : 168000000 Determined by PLL configuration + * HCLK(Hz) : 168000000 (STM32_RCC_CFGR_HPRE) + * AHB Prescaler : 1 (STM32_RCC_CFGR_HPRE) + * APB1 Prescaler : 4 (STM32_RCC_CFGR_PPRE1) + * APB2 Prescaler : 2 (STM32_RCC_CFGR_PPRE2) + * HSE Frequency(Hz) : 24000000 (STM32_BOARD_XTAL) + * PLLM : 24 (STM32_PLLCFG_PLLM) + * PLLN : 336 (STM32_PLLCFG_PLLN) + * PLLP : 2 (STM32_PLLCFG_PLLP) + * PLLQ : 7 (STM32_PLLCFG_PPQ) + * Main regulator output voltage : Scale1 mode Needed for high speed SYSCLK + * Flash Latency(WS) : 5 + * Prefetch Buffer : OFF + * Instruction cache : ON + * Data cache : ON + * Require 48MHz for USB OTG FS, : Enabled + * SDIO and RNG clock + */ + +/* HSI - 16 MHz RC factory-trimmed + * LSI - 32 KHz RC + * HSE - On-board crystal frequency is 24MHz + * LSE - not installed + */ + +#define STM32_BOARD_XTAL 24000000ul + +#define STM32_HSI_FREQUENCY 16000000ul +#define STM32_LSI_FREQUENCY 32000 +#define STM32_HSE_FREQUENCY STM32_BOARD_XTAL + +/* Main PLL Configuration. + * + * PLL source is HSE + * PLL_VCO = (STM32_HSE_FREQUENCY / PLLM) * PLLN + * = (24,000,000 / 24) * 336 + * = 336,000,000 + * SYSCLK = PLL_VCO / PLLP + * = 336,000,000 / 2 = 168,000,000 + * USB OTG FS, SDIO and RNG Clock + * = PLL_VCO / PLLQ + * = 48,000,000 + */ + +#define STM32_PLLCFG_PLLM RCC_PLLCFG_PLLM(24) +#define STM32_PLLCFG_PLLN RCC_PLLCFG_PLLN(336) +#define STM32_PLLCFG_PLLP RCC_PLLCFG_PLLP_2 +#define STM32_PLLCFG_PLLQ RCC_PLLCFG_PLLQ(7) + +#define STM32_SYSCLK_FREQUENCY 168000000ul + +/* AHB clock (HCLK) is SYSCLK (168MHz) */ + +#define STM32_RCC_CFGR_HPRE RCC_CFGR_HPRE_SYSCLK /* HCLK = SYSCLK / 1 */ +#define STM32_HCLK_FREQUENCY STM32_SYSCLK_FREQUENCY +#define STM32_BOARD_HCLK STM32_HCLK_FREQUENCY /* same as above, to satisfy compiler */ + +/* APB1 clock (PCLK1) is HCLK/4 (42MHz) */ + +#define STM32_RCC_CFGR_PPRE1 RCC_CFGR_PPRE1_HCLKd4 /* PCLK1 = HCLK / 4 */ +#define STM32_PCLK1_FREQUENCY (STM32_HCLK_FREQUENCY/4) + +/* Timers driven from APB1 will be twice PCLK1 */ + +#define STM32_APB1_TIM2_CLKIN (2*STM32_PCLK1_FREQUENCY) +#define STM32_APB1_TIM3_CLKIN (2*STM32_PCLK1_FREQUENCY) +#define STM32_APB1_TIM4_CLKIN (2*STM32_PCLK1_FREQUENCY) +#define STM32_APB1_TIM5_CLKIN (2*STM32_PCLK1_FREQUENCY) +#define STM32_APB1_TIM6_CLKIN (2*STM32_PCLK1_FREQUENCY) +#define STM32_APB1_TIM7_CLKIN (2*STM32_PCLK1_FREQUENCY) +#define STM32_APB1_TIM12_CLKIN (2*STM32_PCLK1_FREQUENCY) +#define STM32_APB1_TIM13_CLKIN (2*STM32_PCLK1_FREQUENCY) +#define STM32_APB1_TIM14_CLKIN (2*STM32_PCLK1_FREQUENCY) + +/* APB2 clock (PCLK2) is HCLK/2 (84MHz) */ + +#define STM32_RCC_CFGR_PPRE2 RCC_CFGR_PPRE2_HCLKd2 /* PCLK2 = HCLK / 2 */ +#define STM32_PCLK2_FREQUENCY (STM32_HCLK_FREQUENCY/2) + +/* Timers driven from APB2 will be twice PCLK2 */ + +#define STM32_APB2_TIM1_CLKIN (2*STM32_PCLK2_FREQUENCY) +#define STM32_APB2_TIM8_CLKIN (2*STM32_PCLK2_FREQUENCY) +#define STM32_APB2_TIM9_CLKIN (2*STM32_PCLK2_FREQUENCY) +#define STM32_APB2_TIM10_CLKIN (2*STM32_PCLK2_FREQUENCY) +#define STM32_APB2_TIM11_CLKIN (2*STM32_PCLK2_FREQUENCY) + +/* Timer Frequencies, if APBx is set to 1, frequency is same to APBx + * otherwise frequency is 2xAPBx. + * Note: TIM1,8 are on APB2, others on APB1 + */ + +#define STM32_TIM18_FREQUENCY (2*STM32_PCLK2_FREQUENCY) +#define STM32_TIM27_FREQUENCY (2*STM32_PCLK1_FREQUENCY) + +/* Alternate function pin selections ************************************************/ + +/* + * UARTs. + */ +/* USART1 on PB[6,7]: GPS */ +#define GPIO_USART1_RX GPIO_USART1_RX_2 +#define GPIO_USART1_TX GPIO_USART1_TX_2 + +/* USART2 on PD[5,6]: J5 Breakout */ +#define GPIO_USART2_RX GPIO_USART2_RX_2 +#define GPIO_USART2_TX GPIO_USART2_TX_2 +#define GPIO_USART2_CTS 0 // unused +#define GPIO_USART2_RTS 0 // unused + +/* USART3 on PD[8,9]: to DuoVero UART2 */ +#define GPIO_USART3_RX GPIO_USART3_RX_3 +#define GPIO_USART3_TX GPIO_USART3_TX_3 +#define GPIO_USART3_CTS 0 // unused +#define GPIO_USART3_RTS 0 // unused + +/* UART7 on PE[78]: J7 Breakout */ +#define GPIO_UART7_RX GPIO_UART7_RX_1 +#define GPIO_UART7_TX GPIO_UART7_TX_1 + +/* + * UART8 on PE[0-1]: System Console on Port C of USB (J7) + * No alternate pin config +*/ + +/* USART[1,6] require a RX DMA configuration */ +#define DMAMAP_USART1_RX DMAMAP_USART1_RX_2 +#define DMAMAP_USART6_RX DMAMAP_USART6_RX_2 + +/* + * I2C + * + * The optional _GPIO configurations allow the I2C driver to manually + * reset the bus to clear stuck slaves. They match the pin configuration, + * but are normally-high GPIOs. + */ + +/* PB[10-11]: I2C2 is broken out on J9 header */ +#define GPIO_I2C2_SCL GPIO_I2C2_SCL_1 +#define GPIO_I2C2_SDA GPIO_I2C2_SDA_1 +#define GPIO_I2C2_SCL_GPIO (GPIO_OUTPUT|GPIO_OPENDRAIN|GPIO_SPEED_50MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN10) +#define GPIO_I2C2_SDA_GPIO (GPIO_OUTPUT|GPIO_OPENDRAIN|GPIO_SPEED_50MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN11) + +/* + * SPI + */ +/* PA[4-7] SPI1 broken out on J12 */ +#define GPIO_SPI1_NSS (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTA|GPIO_PIN4) /* should be GPIO_SPI1_NSS_2 but use as a GPIO */ +#define GPIO_SPI1_SCK (GPIO_SPI1_SCK_1|GPIO_SPEED_50MHz) +#define GPIO_SPI1_MISO (GPIO_SPI1_MISO_1|GPIO_SPEED_50MHz) +#define GPIO_SPI1_MOSI (GPIO_SPI1_MOSI_1|GPIO_SPEED_50MHz) + +/* PB[12-15]: SPI2 connected to DuoVero SPI1 */ +#define GPIO_SPI2_NSS (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN9) /* should be GPIO_SPI2_NSS_2 but use as a GPIO */ +#define GPIO_SPI2_SCK (GPIO_SPI2_SCK_2|GPIO_SPEED_50MHz) +#define GPIO_SPI2_MISO (GPIO_SPI2_MISO_1|GPIO_SPEED_50MHz) +#define GPIO_SPI2_MOSI (GPIO_SPI2_MOSI_1|GPIO_SPEED_50MHz) + +/* PC[10-12]: SPI3 connected to onboard sensors */ +#define GPIO_SPI3_SCK (GPIO_SPI3_SCK_2|GPIO_SPEED_50MHz) +#define GPIO_SPI3_MISO (GPIO_SPI3_MISO_2|GPIO_SPEED_50MHz) +#define GPIO_SPI3_MOSI (GPIO_SPI3_MOSI_2|GPIO_SPEED_50MHz) + +/* PE[11-14]: SPI4 connected to FRAM */ +#define GPIO_SPI4_NSS (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTE|GPIO_PIN11) /* should be GPIO_SPI4_NSS_2 but use as a GPIO */ +#define GPIO_SPI4_SCK (GPIO_SPI4_SCK_2|GPIO_SPEED_50MHz) +#define GPIO_SPI4_MISO (GPIO_SPI4_MISO_2|GPIO_SPEED_50MHz) +#define GPIO_SPI4_MOSI (GPIO_SPI4_MOSI_2|GPIO_SPEED_50MHz) + +/************************************************************************************ + * Public Data + ************************************************************************************/ +#ifndef __ASSEMBLY__ + +#undef EXTERN +#if defined(__cplusplus) +#define EXTERN extern "C" +extern "C" { +#else +#define EXTERN extern +#endif + +/************************************************************************************ + * Public Function Prototypes + ************************************************************************************/ +/************************************************************************************ + * Name: stm32_boardinitialize + * + * Description: + * All STM32 architectures must provide the following entry point. This entry point + * is called early in the intitialization -- after all memory has been configured + * and mapped but before any devices have been initialized. + * + ************************************************************************************/ + +EXTERN void stm32_boardinitialize(void); + +#undef EXTERN +#if defined(__cplusplus) +} +#endif + +#endif /* __ASSEMBLY__ */ +#endif /* __ARCH_BOARD_BOARD_H */ diff --git a/src/modules/fixedwing_att_control/fixedwing_att_control_rate.h b/nuttx-configs/aerocore/include/nsh_romfsimg.h index 500e3e197..15e4e7a8d 100644 --- a/src/modules/fixedwing_att_control/fixedwing_att_control_rate.h +++ b/nuttx-configs/aerocore/include/nsh_romfsimg.h @@ -1,8 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: @author Thomas Gubler <thomasgubler@student.ethz.ch> - * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -33,16 +31,12 @@ * ****************************************************************************/ -/* @file Fixed Wing Attitude Rate Control */ - -#ifndef FIXEDWING_ATT_CONTROL_RATE_H_ -#define FIXEDWING_ATT_CONTROL_RATE_H_ - -#include <uORB/topics/vehicle_rates_setpoint.h> -#include <uORB/topics/actuator_controls.h> - -int fixedwing_att_control_rates(const struct vehicle_rates_setpoint_s *rate_sp, - const float rates[], - struct actuator_controls_s *actuators); +/** + * nsh_romfsetc.h + * + * This file is a stub for 'make export' purposes; the actual ROMFS + * must be supplied by the library client. + */ -#endif /* FIXEDWING_ATT_CONTROL_RATE_H_ */ +extern unsigned char romfs_img[]; +extern unsigned int romfs_img_len; diff --git a/nuttx-configs/aerocore/nsh/Make.defs b/nuttx-configs/aerocore/nsh/Make.defs new file mode 100644 index 000000000..c7a1b71bb --- /dev/null +++ b/nuttx-configs/aerocore/nsh/Make.defs @@ -0,0 +1,179 @@ +############################################################################ +# configs/aerocore/nsh/Make.defs +# +# Copyright (C) 2011 Gregory Nutt. All rights reserved. +# Author: Gregory Nutt <gnutt@nuttx.org> +# +# Redistribution and use in source and binary forms, with or without +# modification, are permitted provided that the following conditions +# are met: +# +# 1. Redistributions of source code must retain the above copyright +# notice, this list of conditions and the following disclaimer. +# 2. Redistributions in binary form must reproduce the above copyright +# notice, this list of conditions and the following disclaimer in +# the documentation and/or other materials provided with the +# distribution. +# 3. Neither the name NuttX nor the names of its contributors may be +# used to endorse or promote products derived from this software +# without specific prior written permission. +# +# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS +# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT +# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS +# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE +# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, +# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, +# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS +# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED +# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT +# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN +# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE +# POSSIBILITY OF SUCH DAMAGE. +# +############################################################################ + +include ${TOPDIR}/.config +include ${TOPDIR}/tools/Config.mk + +# +# We only support building with the ARM bare-metal toolchain from +# https://launchpad.net/gcc-arm-embedded on Windows, Linux or Mac OS. +# +CONFIG_ARMV7M_TOOLCHAIN := GNU_EABI + +include ${TOPDIR}/arch/arm/src/armv7-m/Toolchain.defs + +CC = $(CROSSDEV)gcc +CXX = $(CROSSDEV)g++ +CPP = $(CROSSDEV)gcc -E +LD = $(CROSSDEV)ld +AR = $(CROSSDEV)ar rcs +NM = $(CROSSDEV)nm +OBJCOPY = $(CROSSDEV)objcopy +OBJDUMP = $(CROSSDEV)objdump + +MAXOPTIMIZATION = -O3 +ARCHCPUFLAGS = -mcpu=cortex-m4 \ + -mthumb \ + -march=armv7e-m \ + -mfpu=fpv4-sp-d16 \ + -mfloat-abi=hard + + +# enable precise stack overflow tracking +INSTRUMENTATIONDEFINES = -finstrument-functions \ + -ffixed-r10 + +# pull in *just* libm from the toolchain ... this is grody +LIBM = "${shell $(CC) $(ARCHCPUFLAGS) -print-file-name=libm.a}" +EXTRA_LIBS += $(LIBM) + +# use our linker script +LDSCRIPT = ld.script + +ifeq ($(WINTOOL),y) + # Windows-native toolchains + DIRLINK = $(TOPDIR)/tools/copydir.sh + DIRUNLINK = $(TOPDIR)/tools/unlink.sh + MKDEP = $(TOPDIR)/tools/mknulldeps.sh + ARCHINCLUDES = -I. -isystem "${shell cygpath -w $(TOPDIR)/include}" + ARCHXXINCLUDES = -I. -isystem "${shell cygpath -w $(TOPDIR)/include}" -isystem "${shell cygpath -w $(TOPDIR)/include/cxx}" + ARCHSCRIPT = -T "${shell cygpath -w $(TOPDIR)/configs/$(CONFIG_ARCH_BOARD)/scripts/$(LDSCRIPT)}" +else + ifeq ($(PX4_WINTOOL),y) + # Windows-native toolchains (MSYS) + DIRLINK = $(TOPDIR)/tools/copydir.sh + DIRUNLINK = $(TOPDIR)/tools/unlink.sh + MKDEP = $(TOPDIR)/tools/mknulldeps.sh + ARCHINCLUDES = -I. -isystem $(TOPDIR)/include + ARCHXXINCLUDES = -I. -isystem $(TOPDIR)/include -isystem $(TOPDIR)/include/cxx + ARCHSCRIPT = -T$(TOPDIR)/configs/$(CONFIG_ARCH_BOARD)/scripts/$(LDSCRIPT) + else + # Linux/Cygwin-native toolchain + MKDEP = $(TOPDIR)/tools/mkdeps.sh + ARCHINCLUDES = -I. -isystem $(TOPDIR)/include + ARCHXXINCLUDES = -I. -isystem $(TOPDIR)/include -isystem $(TOPDIR)/include/cxx + ARCHSCRIPT = -T$(TOPDIR)/configs/$(CONFIG_ARCH_BOARD)/scripts/$(LDSCRIPT) + endif +endif + +# tool versions +ARCHCCVERSION = ${shell $(CC) -v 2>&1 | sed -n '/^gcc version/p' | sed -e 's/^gcc version \([0-9\.]\)/\1/g' -e 's/[-\ ].*//g' -e '1q'} +ARCHCCMAJOR = ${shell echo $(ARCHCCVERSION) | cut -d'.' -f1} + +# optimisation flags +ARCHOPTIMIZATION = $(MAXOPTIMIZATION) \ + -fno-strict-aliasing \ + -fno-strength-reduce \ + -fomit-frame-pointer \ + -funsafe-math-optimizations \ + -fno-builtin-printf \ + -ffunction-sections \ + -fdata-sections + +ifeq ("${CONFIG_DEBUG_SYMBOLS}","y") +ARCHOPTIMIZATION += -g +endif + +ARCHCFLAGS = -std=gnu99 +ARCHCXXFLAGS = -fno-exceptions -fno-rtti -std=gnu++0x +ARCHWARNINGS = -Wall \ + -Wextra \ + -Wdouble-promotion \ + -Wshadow \ + -Wfloat-equal \ + -Wframe-larger-than=1024 \ + -Wpointer-arith \ + -Wlogical-op \ + -Wmissing-declarations \ + -Wpacked \ + -Wno-unused-parameter +# -Wcast-qual - generates spurious noreturn attribute warnings, try again later +# -Wconversion - would be nice, but too many "risky-but-safe" conversions in the code +# -Wcast-align - would help catch bad casts in some cases, but generates too many false positives + +ARCHCWARNINGS = $(ARCHWARNINGS) \ + -Wbad-function-cast \ + -Wstrict-prototypes \ + -Wold-style-declaration \ + -Wmissing-parameter-type \ + -Wmissing-prototypes \ + -Wnested-externs \ + -Wunsuffixed-float-constants +ARCHWARNINGSXX = $(ARCHWARNINGS) \ + -Wno-psabi +ARCHDEFINES = +ARCHPICFLAGS = -fpic -msingle-pic-base -mpic-register=r10 + +# this seems to be the only way to add linker flags +EXTRA_LIBS += --warn-common \ + --gc-sections + +CFLAGS = $(ARCHCFLAGS) $(ARCHCWARNINGS) $(ARCHOPTIMIZATION) $(ARCHCPUFLAGS) $(ARCHINCLUDES) $(INSTRUMENTATIONDEFINES) $(ARCHDEFINES) $(EXTRADEFINES) -pipe -fno-common +CPICFLAGS = $(ARCHPICFLAGS) $(CFLAGS) +CXXFLAGS = $(ARCHCXXFLAGS) $(ARCHWARNINGSXX) $(ARCHOPTIMIZATION) $(ARCHCPUFLAGS) $(ARCHXXINCLUDES) $(INSTRUMENTATIONDEFINES) $(ARCHDEFINES) $(EXTRADEFINES) -pipe +CXXPICFLAGS = $(ARCHPICFLAGS) $(CXXFLAGS) +CPPFLAGS = $(ARCHINCLUDES) $(INSTRUMENTATIONDEFINES) $(ARCHDEFINES) $(EXTRADEFINES) +AFLAGS = $(CFLAGS) -D__ASSEMBLY__ + +NXFLATLDFLAGS1 = -r -d -warn-common +NXFLATLDFLAGS2 = $(NXFLATLDFLAGS1) -T$(TOPDIR)/binfmt/libnxflat/gnu-nxflat.ld -no-check-sections +LDNXFLATFLAGS = -e main -s 2048 + +OBJEXT = .o +LIBEXT = .a +EXEEXT = + + +# produce partially-linked $1 from files in $2 +define PRELINK + @echo "PRELINK: $1" + $(Q) $(LD) -Ur -o $1 $2 && $(OBJCOPY) --localize-hidden $1 +endef + +HOSTCC = gcc +HOSTINCLUDES = -I. +HOSTCFLAGS = -Wall -Wstrict-prototypes -Wshadow -g -pipe +HOSTLDFLAGS = + diff --git a/src/modules/fixedwing_pos_control/module.mk b/nuttx-configs/aerocore/nsh/appconfig index b976377e9..2850dac06 100644 --- a/src/modules/fixedwing_pos_control/module.mk +++ b/nuttx-configs/aerocore/nsh/appconfig @@ -1,6 +1,8 @@ ############################################################################ +# configs/aerocore/nsh/appconfig # -# Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved. +# Copyright (C) 2011 Gregory Nutt. All rights reserved. +# Author: Gregory Nutt <gnutt@nuttx.org> # # Redistribution and use in source and binary forms, with or without # modification, are permitted provided that the following conditions @@ -12,7 +14,7 @@ # notice, this list of conditions and the following disclaimer in # the documentation and/or other materials provided with the # distribution. -# 3. Neither the name PX4 nor the names of its contributors may be +# 3. Neither the name NuttX nor the names of its contributors may be # used to endorse or promote products derived from this software # without specific prior written permission. # @@ -31,10 +33,10 @@ # ############################################################################ -# -# Fixedwing PositionControl application -# +# Path to example in apps/examples containing the user_start entry point -MODULE_COMMAND = fixedwing_pos_control +CONFIGURED_APPS += examples/nsh -SRCS = fixedwing_pos_control_main.c +# The NSH application library +CONFIGURED_APPS += nshlib +CONFIGURED_APPS += system/readline diff --git a/nuttx-configs/aerocore/nsh/defconfig b/nuttx-configs/aerocore/nsh/defconfig new file mode 100644 index 000000000..8d0bae7b9 --- /dev/null +++ b/nuttx-configs/aerocore/nsh/defconfig @@ -0,0 +1,950 @@ +# +# Automatically generated file; DO NOT EDIT. +# Nuttx/ Configuration +# +CONFIG_NUTTX_NEWCONFIG=y + +# +# Build Setup +# +# CONFIG_EXPERIMENTAL is not set +CONFIG_HOST_LINUX=y +# CONFIG_HOST_OSX is not set +# CONFIG_HOST_WINDOWS is not set +# CONFIG_HOST_OTHER is not set + +# +# Build Configuration +# +CONFIG_APPS_DIR="../apps" +# CONFIG_BUILD_2PASS is not set + +# +# Binary Output Formats +# +# CONFIG_RRLOAD_BINARY is not set +# CONFIG_INTELHEX_BINARY is not set +# CONFIG_MOTOROLA_SREC is not set +CONFIG_RAW_BINARY=y + +# +# Customize Header Files +# +# CONFIG_ARCH_STDBOOL_H is not set +CONFIG_ARCH_MATH_H=y +# CONFIG_ARCH_FLOAT_H is not set +# CONFIG_ARCH_STDARG_H is not set + +# +# Debug Options +# +# CONFIG_DEBUG is not set +# CONFIG_DEBUG_SYMBOLS is not set + +# +# System Type +# +# CONFIG_ARCH_8051 is not set +CONFIG_ARCH_ARM=y +# CONFIG_ARCH_AVR is not set +# CONFIG_ARCH_HC is not set +# CONFIG_ARCH_MIPS is not set +# CONFIG_ARCH_RGMP is not set +# CONFIG_ARCH_SH is not set +# CONFIG_ARCH_SIM is not set +# CONFIG_ARCH_X86 is not set +# CONFIG_ARCH_Z16 is not set +# CONFIG_ARCH_Z80 is not set +CONFIG_ARCH="arm" + +# +# ARM Options +# +# CONFIG_ARCH_CHIP_C5471 is not set +# CONFIG_ARCH_CHIP_CALYPSO is not set +# CONFIG_ARCH_CHIP_DM320 is not set +# CONFIG_ARCH_CHIP_IMX is not set +# CONFIG_ARCH_CHIP_KINETIS is not set +# CONFIG_ARCH_CHIP_KL is not set +# CONFIG_ARCH_CHIP_LM is not set +# CONFIG_ARCH_CHIP_LPC17XX is not set +# CONFIG_ARCH_CHIP_LPC214X is not set +# CONFIG_ARCH_CHIP_LPC2378 is not set +# CONFIG_ARCH_CHIP_LPC31XX is not set +# CONFIG_ARCH_CHIP_LPC43XX is not set +# CONFIG_ARCH_CHIP_NUC1XX is not set +# CONFIG_ARCH_CHIP_SAM34 is not set +CONFIG_ARCH_CHIP_STM32=y +# CONFIG_ARCH_CHIP_STR71X is not set +CONFIG_ARCH_CORTEXM4=y +CONFIG_ARCH_FAMILY="armv7-m" +CONFIG_ARCH_CHIP="stm32" +CONFIG_ARMV7M_USEBASEPRI=y +CONFIG_ARCH_HAVE_CMNVECTOR=y +CONFIG_ARMV7M_CMNVECTOR=y +CONFIG_ARCH_HAVE_FPU=y +CONFIG_ARCH_FPU=y +CONFIG_ARCH_HAVE_MPU=y +# CONFIG_ARMV7M_MPU is not set + +# +# ARMV7M Configuration Options +# +# CONFIG_ARMV7M_TOOLCHAIN_BUILDROOT is not set +# CONFIG_ARMV7M_TOOLCHAIN_CODEREDL is not set +# CONFIG_ARMV7M_TOOLCHAIN_CODESOURCERYL is not set +CONFIG_ARMV7M_TOOLCHAIN_GNU_EABI=y +CONFIG_ARMV7M_STACKCHECK=y +CONFIG_SERIAL_TERMIOS=y + +# +# STM32 Configuration Options +# +# CONFIG_ARCH_CHIP_STM32L151C6 is not set +# CONFIG_ARCH_CHIP_STM32L151C8 is not set +# CONFIG_ARCH_CHIP_STM32L151CB is not set +# CONFIG_ARCH_CHIP_STM32L151R6 is not set +# CONFIG_ARCH_CHIP_STM32L151R8 is not set +# CONFIG_ARCH_CHIP_STM32L151RB is not set +# CONFIG_ARCH_CHIP_STM32L151V6 is not set +# CONFIG_ARCH_CHIP_STM32L151V8 is not set +# CONFIG_ARCH_CHIP_STM32L151VB is not set +# CONFIG_ARCH_CHIP_STM32L152C6 is not set +# CONFIG_ARCH_CHIP_STM32L152C8 is not set +# CONFIG_ARCH_CHIP_STM32L152CB is not set +# CONFIG_ARCH_CHIP_STM32L152R6 is not set +# CONFIG_ARCH_CHIP_STM32L152R8 is not set +# CONFIG_ARCH_CHIP_STM32L152RB is not set +# CONFIG_ARCH_CHIP_STM32L152V6 is not set +# CONFIG_ARCH_CHIP_STM32L152V8 is not set +# CONFIG_ARCH_CHIP_STM32L152VB is not set +# CONFIG_ARCH_CHIP_STM32F100C8 is not set +# CONFIG_ARCH_CHIP_STM32F100CB is not set +# CONFIG_ARCH_CHIP_STM32F100R8 is not set +# CONFIG_ARCH_CHIP_STM32F100RB is not set +# CONFIG_ARCH_CHIP_STM32F100RC is not set +# CONFIG_ARCH_CHIP_STM32F100RD is not set +# CONFIG_ARCH_CHIP_STM32F100RE is not set +# CONFIG_ARCH_CHIP_STM32F100V8 is not set +# CONFIG_ARCH_CHIP_STM32F100VB is not set +# CONFIG_ARCH_CHIP_STM32F100VC is not set +# CONFIG_ARCH_CHIP_STM32F100VD is not set +# CONFIG_ARCH_CHIP_STM32F100VE is not set +# CONFIG_ARCH_CHIP_STM32F103C4 is not set +# CONFIG_ARCH_CHIP_STM32F103C8 is not set +# CONFIG_ARCH_CHIP_STM32F103RET6 is not set +# CONFIG_ARCH_CHIP_STM32F103VCT6 is not set +# CONFIG_ARCH_CHIP_STM32F103VET6 is not set +# CONFIG_ARCH_CHIP_STM32F103ZET6 is not set +# CONFIG_ARCH_CHIP_STM32F105VBT7 is not set +# CONFIG_ARCH_CHIP_STM32F107VC is not set +# CONFIG_ARCH_CHIP_STM32F207IG is not set +# CONFIG_ARCH_CHIP_STM32F302CB is not set +# CONFIG_ARCH_CHIP_STM32F302CC is not set +# CONFIG_ARCH_CHIP_STM32F302RB is not set +# CONFIG_ARCH_CHIP_STM32F302RC is not set +# CONFIG_ARCH_CHIP_STM32F302VB is not set +# CONFIG_ARCH_CHIP_STM32F302VC is not set +# CONFIG_ARCH_CHIP_STM32F303CB is not set +# CONFIG_ARCH_CHIP_STM32F303CC is not set +# CONFIG_ARCH_CHIP_STM32F303RB is not set +# CONFIG_ARCH_CHIP_STM32F303RC is not set +# CONFIG_ARCH_CHIP_STM32F303VB is not set +# CONFIG_ARCH_CHIP_STM32F303VC is not set +# CONFIG_ARCH_CHIP_STM32F405RG is not set +# CONFIG_ARCH_CHIP_STM32F405VG is not set +# CONFIG_ARCH_CHIP_STM32F405ZG is not set +# CONFIG_ARCH_CHIP_STM32F407VE is not set +# CONFIG_ARCH_CHIP_STM32F407VG is not set +# CONFIG_ARCH_CHIP_STM32F407ZE is not set +# CONFIG_ARCH_CHIP_STM32F407ZG is not set +# CONFIG_ARCH_CHIP_STM32F407IE is not set +# CONFIG_ARCH_CHIP_STM32F407IG is not set +CONFIG_ARCH_CHIP_STM32F427V=y +# CONFIG_ARCH_CHIP_STM32F427Z is not set +# CONFIG_ARCH_CHIP_STM32F427I is not set +# CONFIG_STM32_STM32L15XX is not set +# CONFIG_STM32_ENERGYLITE is not set +# CONFIG_STM32_STM32F10XX is not set +# CONFIG_STM32_VALUELINE is not set +# CONFIG_STM32_CONNECTIVITYLINE is not set +# CONFIG_STM32_PERFORMANCELINE is not set +# CONFIG_STM32_HIGHDENSITY is not set +# CONFIG_STM32_MEDIUMDENSITY is not set +# CONFIG_STM32_LOWDENSITY is not set +# CONFIG_STM32_STM32F20XX is not set +# CONFIG_STM32_STM32F30XX is not set +CONFIG_STM32_STM32F40XX=y +CONFIG_STM32_STM32F427=y +# CONFIG_STM32_DFU is not set + +# +# STM32 Peripheral Support +# +CONFIG_STM32_ADC1=y +# CONFIG_STM32_ADC2 is not set +# CONFIG_STM32_ADC3 is not set +CONFIG_STM32_BKPSRAM=y +# CONFIG_STM32_CAN1 is not set +# CONFIG_STM32_CAN2 is not set +CONFIG_STM32_CCMDATARAM=y +# CONFIG_STM32_CRC is not set +# CONFIG_STM32_CRYP is not set +CONFIG_STM32_DMA1=y +CONFIG_STM32_DMA2=y +# CONFIG_STM32_DAC1 is not set +# CONFIG_STM32_DAC2 is not set +# CONFIG_STM32_DCMI is not set +# CONFIG_STM32_ETHMAC is not set +# CONFIG_STM32_FSMC is not set +# CONFIG_STM32_HASH is not set +# CONFIG_STM32_I2C1 is not set +CONFIG_STM32_I2C2=y +# CONFIG_STM32_I2C3 is not set +# CONFIG_STM32_OTGFS is not set +# CONFIG_STM32_OTGHS is not set +CONFIG_STM32_PWR=y +# CONFIG_STM32_RNG is not set +# CONFIG_STM32_SDIO is not set +CONFIG_STM32_SPI1=y +CONFIG_STM32_SPI2=y +CONFIG_STM32_SPI3=y +CONFIG_STM32_SPI4=y +# CONFIG_STM32_SPI5 is not set +# CONFIG_STM32_SPI6 is not set +CONFIG_STM32_SYSCFG=y +CONFIG_STM32_TIM1=y +# CONFIG_STM32_TIM2 is not set +CONFIG_STM32_TIM3=y +CONFIG_STM32_TIM4=y +CONFIG_STM32_TIM5=y +# CONFIG_STM32_TIM6 is not set +# CONFIG_STM32_TIM7 is not set +# CONFIG_STM32_TIM8 is not set +CONFIG_STM32_TIM9=y +# CONFIG_STM32_TIM10 is not set +# CONFIG_STM32_TIM11 is not set +# CONFIG_STM32_TIM12 is not set +# CONFIG_STM32_TIM13 is not set +# CONFIG_STM32_TIM14 is not set +CONFIG_STM32_USART1=y +CONFIG_STM32_USART2=y +CONFIG_STM32_USART3=y +# CONFIG_STM32_UART4 is not set +# CONFIG_STM32_UART5 is not set +# CONFIG_STM32_USART6 is not set +CONFIG_STM32_UART7=y +CONFIG_STM32_UART8=y +# CONFIG_STM32_IWDG is not set +CONFIG_STM32_WWDG=y +CONFIG_STM32_ADC=y +CONFIG_STM32_SPI=y +CONFIG_STM32_I2C=y + +# +# Alternate Pin Mapping +# +CONFIG_STM32_FLASH_PREFETCH=y +# CONFIG_STM32_JTAG_DISABLE is not set +# CONFIG_STM32_JTAG_FULL_ENABLE is not set +# CONFIG_STM32_JTAG_NOJNTRST_ENABLE is not set +CONFIG_STM32_JTAG_SW_ENABLE=y +CONFIG_STM32_DISABLE_IDLE_SLEEP_DURING_DEBUG=y +# CONFIG_STM32_FORCEPOWER is not set +# CONFIG_ARCH_BOARD_STM32_CUSTOM_CLOCKCONFIG is not set +# CONFIG_STM32_CCMEXCLUDE is not set +CONFIG_STM32_DMACAPABLE=y +# CONFIG_STM32_TIM1_PWM is not set +# CONFIG_STM32_TIM3_PWM is not set +# CONFIG_STM32_TIM4_PWM is not set +# CONFIG_STM32_TIM5_PWM is not set +# CONFIG_STM32_TIM9_PWM is not set +# CONFIG_STM32_TIM1_ADC is not set +# CONFIG_STM32_TIM3_ADC is not set +# CONFIG_STM32_TIM4_ADC is not set +# CONFIG_STM32_TIM5_ADC is not set +CONFIG_STM32_USART=y + +# +# U[S]ART Configuration +# +# CONFIG_USART1_RS485 is not set +CONFIG_USART1_RXDMA=y +# CONFIG_USART2_RS485 is not set +CONFIG_USART2_RXDMA=y +# CONFIG_USART3_RS485 is not set +CONFIG_USART3_RXDMA=y +# CONFIG_UART7_RS485 is not set +CONFIG_UART7_RXDMA=y +# CONFIG_UART8_RS485 is not set +CONFIG_UART8_RXDMA=y +CONFIG_SERIAL_DISABLE_REORDERING=y +CONFIG_STM32_USART_SINGLEWIRE=y + +# +# SPI Configuration +# +# CONFIG_STM32_SPI_INTERRUPTS is not set +# CONFIG_STM32_SPI_DMA is not set + +# +# I2C Configuration +# +# CONFIG_STM32_I2C_DYNTIMEO is not set +CONFIG_STM32_I2CTIMEOSEC=0 +CONFIG_STM32_I2CTIMEOMS=10 +CONFIG_STM32_I2CTIMEOTICKS=500 +# CONFIG_STM32_I2C_DUTY16_9 is not set + +# +# USB Host Configuration +# + +# +# USB Device Configuration +# + +# +# External Memory Configuration +# + +# +# Architecture Options +# +# CONFIG_ARCH_NOINTC is not set +# CONFIG_ARCH_VECNOTIRQ is not set +CONFIG_ARCH_DMA=y +CONFIG_ARCH_IRQPRIO=y +# CONFIG_CUSTOM_STACK is not set +# CONFIG_ADDRENV is not set +CONFIG_ARCH_HAVE_VFORK=y +CONFIG_ARCH_STACKDUMP=y +# CONFIG_ENDIAN_BIG is not set +# CONFIG_ARCH_HAVE_RAMFUNCS is not set +CONFIG_ARCH_HAVE_RAMVECTORS=y +# CONFIG_ARCH_RAMVECTORS is not set + +# +# Board Settings +# +CONFIG_BOARD_LOOPSPERMSEC=16717 +# CONFIG_ARCH_CALIBRATION is not set +CONFIG_DRAM_START=0x20000000 +CONFIG_DRAM_SIZE=262144 +CONFIG_ARCH_HAVE_INTERRUPTSTACK=y +CONFIG_ARCH_INTERRUPTSTACK=4096 + +# +# Boot options +# +# CONFIG_BOOT_RUNFROMEXTSRAM is not set +CONFIG_BOOT_RUNFROMFLASH=y +# CONFIG_BOOT_RUNFROMISRAM is not set +# CONFIG_BOOT_RUNFROMSDRAM is not set +# CONFIG_BOOT_COPYTORAM is not set + +# +# Board Selection +# +CONFIG_ARCH_BOARD_CUSTOM=y +CONFIG_ARCH_BOARD="" + +# +# Common Board Options +# +CONFIG_NSH_MMCSDMINOR=0 + +# +# Board-Specific Options +# + +# +# RTOS Features +# +# CONFIG_BOARD_INITIALIZE is not set +CONFIG_MSEC_PER_TICK=1 +CONFIG_RR_INTERVAL=0 +CONFIG_SCHED_INSTRUMENTATION=y +CONFIG_TASK_NAME_SIZE=24 +# CONFIG_SCHED_HAVE_PARENT is not set +# CONFIG_JULIAN_TIME is not set +CONFIG_START_YEAR=1970 +CONFIG_START_MONTH=1 +CONFIG_START_DAY=1 +CONFIG_DEV_CONSOLE=y +# CONFIG_MUTEX_TYPES is not set +CONFIG_PRIORITY_INHERITANCE=y +CONFIG_SEM_PREALLOCHOLDERS=0 +CONFIG_SEM_NNESTPRIO=8 +# CONFIG_FDCLONE_DISABLE is not set +CONFIG_FDCLONE_STDIO=y +CONFIG_SDCLONE_DISABLE=y +CONFIG_SCHED_WAITPID=y +# CONFIG_SCHED_STARTHOOK is not set +CONFIG_SCHED_ATEXIT=y +CONFIG_SCHED_ATEXIT_MAX=1 +# CONFIG_SCHED_ONEXIT is not set +CONFIG_USER_ENTRYPOINT="nsh_main" +# CONFIG_DISABLE_OS_API is not set + +# +# Signal Numbers +# +CONFIG_SIG_SIGUSR1=1 +CONFIG_SIG_SIGUSR2=2 +CONFIG_SIG_SIGALARM=3 +CONFIG_SIG_SIGCONDTIMEDOUT=16 +CONFIG_SIG_SIGWORK=4 + +# +# Sizes of configurable things (0 disables) +# +CONFIG_MAX_TASKS=32 +CONFIG_MAX_TASK_ARGS=10 +CONFIG_NPTHREAD_KEYS=4 +CONFIG_NFILE_DESCRIPTORS=36 +CONFIG_NFILE_STREAMS=8 +CONFIG_NAME_MAX=32 +CONFIG_PREALLOC_MQ_MSGS=4 +CONFIG_MQ_MAXMSGSIZE=32 +CONFIG_MAX_WDOGPARMS=2 +CONFIG_PREALLOC_WDOGS=50 +CONFIG_PREALLOC_TIMERS=50 + +# +# Stack and heap information +# +CONFIG_IDLETHREAD_STACKSIZE=6000 +CONFIG_USERMAIN_STACKSIZE=4096 +CONFIG_PTHREAD_STACK_MIN=512 +CONFIG_PTHREAD_STACK_DEFAULT=2048 + +# +# Device Drivers +# +# CONFIG_DISABLE_POLL is not set +CONFIG_DEV_NULL=y +# CONFIG_DEV_ZERO is not set +# CONFIG_LOOP is not set +# CONFIG_RAMDISK is not set +# CONFIG_CAN is not set +# CONFIG_PWM is not set +CONFIG_I2C=y +# CONFIG_I2C_SLAVE is not set +CONFIG_I2C_TRANSFER=y +# CONFIG_I2C_WRITEREAD is not set +# CONFIG_I2C_POLLED is not set +# CONFIG_I2C_TRACE is not set +CONFIG_ARCH_HAVE_I2CRESET=y +CONFIG_I2C_RESET=y +CONFIG_SPI=y +# CONFIG_SPI_OWNBUS is not set +CONFIG_SPI_EXCHANGE=y +# CONFIG_SPI_CMDDATA is not set +# CONFIG_RTC is not set +CONFIG_WATCHDOG=y +# CONFIG_ANALOG is not set +# CONFIG_AUDIO_DEVICES is not set +# CONFIG_BCH is not set +# CONFIG_INPUT is not set +# CONFIG_LCD is not set +# CONFIG_MMCSD is not set +CONFIG_MTD=y + +# +# MTD Configuration +# +CONFIG_MTD_PARTITION=y +CONFIG_MTD_BYTE_WRITE=y + +# +# MTD Device Drivers +# +# CONFIG_RAMMTD is not set +# CONFIG_MTD_AT24XX is not set +# CONFIG_MTD_AT45DB is not set +# CONFIG_MTD_M25P is not set +# CONFIG_MTD_SMART is not set +CONFIG_MTD_RAMTRON=y +CONFIG_RAMTRON_FUJITSU=y +# CONFIG_MTD_SST25 is not set +# CONFIG_MTD_SST39FV is not set +# CONFIG_MTD_W25 is not set +CONFIG_PIPES=y +# CONFIG_PM is not set +# CONFIG_POWER is not set +# CONFIG_SENSORS is not set +CONFIG_SERIAL=y +# CONFIG_DEV_LOWCONSOLE is not set +# CONFIG_16550_UART is not set +CONFIG_ARCH_HAVE_UART7=y +CONFIG_ARCH_HAVE_UART8=y +CONFIG_ARCH_HAVE_USART1=y +CONFIG_ARCH_HAVE_USART2=y +CONFIG_ARCH_HAVE_USART3=y +CONFIG_MCU_SERIAL=y +CONFIG_STANDARD_SERIAL=y +CONFIG_SERIAL_NPOLLWAITERS=2 +# CONFIG_USART1_SERIAL_CONSOLE is not set +# CONFIG_USART2_SERIAL_CONSOLE is not set +# CONFIG_USART3_SERIAL_CONSOLE is not set +# CONFIG_UART7_SERIAL_CONSOLE is not set +CONFIG_UART8_SERIAL_CONSOLE=y +# CONFIG_NO_SERIAL_CONSOLE is not set + +# +# USART1 Configuration +# +CONFIG_USART1_RXBUFSIZE=512 +CONFIG_USART1_TXBUFSIZE=512 +CONFIG_USART1_BAUD=115200 +CONFIG_USART1_BITS=8 +CONFIG_USART1_PARITY=0 +CONFIG_USART1_2STOP=0 +# CONFIG_USART1_IFLOWCONTROL is not set +# CONFIG_USART1_OFLOWCONTROL is not set + +# +# USART2 Configuration +# +CONFIG_USART2_RXBUFSIZE=512 +CONFIG_USART2_TXBUFSIZE=512 +CONFIG_USART2_BAUD=115200 +CONFIG_USART2_BITS=8 +CONFIG_USART2_PARITY=0 +CONFIG_USART2_2STOP=0 +# CONFIG_USART2_IFLOWCONTROL is not set +# CONFIG_USART2_OFLOWCONTROL is not set + +# +# USART3 Configuration +# +CONFIG_USART3_RXBUFSIZE=512 +CONFIG_USART3_TXBUFSIZE=512 +CONFIG_USART3_BAUD=115200 +CONFIG_USART3_BITS=8 +CONFIG_USART3_PARITY=0 +CONFIG_USART3_2STOP=0 +# CONFIG_USART3_IFLOWCONTROL is not set +# CONFIG_USART3_OFLOWCONTROL is not set + +# +# UART7 Configuration +# +CONFIG_UART7_RXBUFSIZE=512 +CONFIG_UART7_TXBUFSIZE=512 +CONFIG_UART7_BAUD=115200 +CONFIG_UART7_BITS=8 +CONFIG_UART7_PARITY=0 +CONFIG_UART7_2STOP=0 +# CONFIG_UART7_IFLOWCONTROL is not set +# CONFIG_UART7_OFLOWCONTROL is not set + +# +# UART8 Configuration +# +CONFIG_UART8_RXBUFSIZE=512 +CONFIG_UART8_TXBUFSIZE=512 +CONFIG_UART8_BAUD=115200 +CONFIG_UART8_BITS=8 +CONFIG_UART8_PARITY=0 +CONFIG_UART8_2STOP=0 +# CONFIG_UART8_IFLOWCONTROL is not set +# CONFIG_UART8_OFLOWCONTROL is not set +# CONFIG_SERIAL_IFLOWCONTROL is not set +# CONFIG_SERIAL_OFLOWCONTROL is not set +# CONFIG_USBDEV is not set +# CONFIG_USBHOST is not set +# CONFIG_WIRELESS is not set + +# +# System Logging Device Options +# + +# +# System Logging +# +# CONFIG_RAMLOG is not set + +# +# Networking Support +# +# CONFIG_NET is not set + +# +# File Systems +# + +# +# File system configuration +# +# CONFIG_DISABLE_MOUNTPOINT is not set +# CONFIG_FS_RAMMAP is not set +CONFIG_FS_FAT=y +CONFIG_FAT_LCNAMES=y +CONFIG_FAT_LFN=y +CONFIG_FAT_MAXFNAME=32 +CONFIG_FS_FATTIME=y +CONFIG_FAT_DMAMEMORY=y +CONFIG_FS_NXFFS=y +CONFIG_NXFFS_PREALLOCATED=y +CONFIG_NXFFS_ERASEDSTATE=0xff +CONFIG_NXFFS_PACKTHRESHOLD=32 +CONFIG_NXFFS_MAXNAMLEN=32 +CONFIG_NXFFS_TAILTHRESHOLD=2048 +CONFIG_FS_ROMFS=y +# CONFIG_FS_SMARTFS is not set +CONFIG_FS_BINFS=y + +# +# System Logging +# +# CONFIG_SYSLOG_ENABLE is not set +# CONFIG_SYSLOG is not set + +# +# Graphics Support +# +# CONFIG_NX is not set + +# +# Memory Management +# +# CONFIG_MM_MULTIHEAP is not set +# CONFIG_MM_SMALL is not set +CONFIG_MM_REGIONS=2 +CONFIG_GRAN=y +# CONFIG_GRAN_SINGLE is not set +# CONFIG_GRAN_INTR is not set + +# +# Audio Support +# +# CONFIG_AUDIO is not set + +# +# Binary Formats +# +# CONFIG_BINFMT_DISABLE is not set +# CONFIG_BINFMT_EXEPATH is not set +# CONFIG_NXFLAT is not set +# CONFIG_ELF is not set +CONFIG_BUILTIN=y +# CONFIG_PIC is not set +# CONFIG_SYMTAB_ORDEREDBYNAME is not set + +# +# Library Routines +# + +# +# Standard C Library Options +# +CONFIG_STDIO_BUFFER_SIZE=32 +CONFIG_STDIO_LINEBUFFER=y +CONFIG_NUNGET_CHARS=2 +CONFIG_LIB_HOMEDIR="/" +# CONFIG_NOPRINTF_FIELDWIDTH is not set +CONFIG_LIBC_FLOATINGPOINT=y +CONFIG_LIB_RAND_ORDER=1 +# CONFIG_EOL_IS_CR is not set +# CONFIG_EOL_IS_LF is not set +# CONFIG_EOL_IS_BOTH_CRLF is not set +CONFIG_EOL_IS_EITHER_CRLF=y +# CONFIG_LIBC_EXECFUNCS is not set +CONFIG_POSIX_SPAWN_PROXY_STACKSIZE=1024 +CONFIG_TASK_SPAWN_DEFAULT_STACKSIZE=2048 +CONFIG_LIBC_STRERROR=y +# CONFIG_LIBC_STRERROR_SHORT is not set +# CONFIG_LIBC_PERROR_STDOUT is not set +CONFIG_ARCH_LOWPUTC=y +CONFIG_LIB_SENDFILE_BUFSIZE=512 +# CONFIG_ARCH_ROMGETC is not set +CONFIG_ARCH_OPTIMIZED_FUNCTIONS=y +CONFIG_ARCH_MEMCPY=y +# CONFIG_ARCH_MEMCMP is not set +# CONFIG_ARCH_MEMMOVE is not set +# CONFIG_ARCH_MEMSET is not set +# CONFIG_MEMSET_OPTSPEED is not set +# CONFIG_ARCH_STRCHR is not set +# CONFIG_ARCH_STRCMP is not set +# CONFIG_ARCH_STRCPY is not set +# CONFIG_ARCH_STRNCPY is not set +# CONFIG_ARCH_STRLEN is not set +# CONFIG_ARCH_STRNLEN is not set +# CONFIG_ARCH_BZERO is not set + +# +# Non-standard Library Support +# +CONFIG_SCHED_WORKQUEUE=y +CONFIG_SCHED_HPWORK=y +CONFIG_SCHED_WORKPRIORITY=192 +CONFIG_SCHED_WORKPERIOD=5000 +CONFIG_SCHED_WORKSTACKSIZE=2000 +CONFIG_SCHED_LPWORK=y +CONFIG_SCHED_LPWORKPRIORITY=50 +CONFIG_SCHED_LPWORKPERIOD=50000 +CONFIG_SCHED_LPWORKSTACKSIZE=2000 +# CONFIG_LIB_KBDCODEC is not set +# CONFIG_LIB_SLCDCODEC is not set + +# +# Basic CXX Support +# +CONFIG_C99_BOOL8=y +CONFIG_HAVE_CXX=y +CONFIG_HAVE_CXXINITIALIZE=y +# CONFIG_CXX_NEWLONG is not set + +# +# uClibc++ Standard C++ Library +# +# CONFIG_UCLIBCXX is not set + +# +# Application Configuration +# + +# +# Built-In Applications +# +CONFIG_BUILTIN_PROXY_STACKSIZE=1024 + +# +# Examples +# +# CONFIG_EXAMPLES_BUTTONS is not set +# CONFIG_EXAMPLES_CAN is not set +# CONFIG_EXAMPLES_COMPOSITE is not set +# CONFIG_EXAMPLES_CXXTEST is not set +# CONFIG_EXAMPLES_DHCPD is not set +# CONFIG_EXAMPLES_ELF is not set +# CONFIG_EXAMPLES_FTPC is not set +# CONFIG_EXAMPLES_FTPD is not set +CONFIG_EXAMPLES_HELLO=y +# CONFIG_EXAMPLES_HELLOXX is not set +# CONFIG_EXAMPLES_JSON is not set +# CONFIG_EXAMPLES_HIDKBD is not set +# CONFIG_EXAMPLES_KEYPADTEST is not set +# CONFIG_EXAMPLES_IGMP is not set +# CONFIG_EXAMPLES_LCDRW is not set +# CONFIG_EXAMPLES_MM is not set +# CONFIG_EXAMPLES_MODBUS is not set +CONFIG_EXAMPLES_MOUNT=y +# CONFIG_EXAMPLES_MTDPART is not set +# CONFIG_EXAMPLES_NRF24L01TERM is not set +CONFIG_EXAMPLES_NSH=y +# CONFIG_EXAMPLES_NULL is not set +# CONFIG_EXAMPLES_NX is not set +# CONFIG_EXAMPLES_NXCONSOLE is not set +# CONFIG_EXAMPLES_NXFFS is not set +# CONFIG_EXAMPLES_NXFLAT is not set +# CONFIG_EXAMPLES_NXHELLO is not set +# CONFIG_EXAMPLES_NXIMAGE is not set +# CONFIG_EXAMPLES_NXLINES is not set +# CONFIG_EXAMPLES_NXTEXT is not set +# CONFIG_EXAMPLES_OSTEST is not set +# CONFIG_EXAMPLES_PASHELLO is not set +# CONFIG_EXAMPLES_PIPE is not set +# CONFIG_EXAMPLES_POSIXSPAWN is not set +# CONFIG_EXAMPLES_QENCODER is not set +# CONFIG_EXAMPLES_RGMP is not set +# CONFIG_EXAMPLES_ROMFS is not set +# CONFIG_EXAMPLES_SENDMAIL is not set +# CONFIG_EXAMPLES_SERLOOP is not set +# CONFIG_EXAMPLES_SLCD is not set +# CONFIG_EXAMPLES_SMART_TEST is not set +# CONFIG_EXAMPLES_SMART is not set +# CONFIG_EXAMPLES_TCPECHO is not set +# CONFIG_EXAMPLES_TELNETD is not set +# CONFIG_EXAMPLES_THTTPD is not set +# CONFIG_EXAMPLES_TIFF is not set +# CONFIG_EXAMPLES_TOUCHSCREEN is not set +# CONFIG_EXAMPLES_UDP is not set +# CONFIG_EXAMPLES_UIP is not set +# CONFIG_EXAMPLES_USBSERIAL is not set +# CONFIG_EXAMPLES_USBMSC is not set +# CONFIG_EXAMPLES_USBTERM is not set +# CONFIG_EXAMPLES_WATCHDOG is not set + +# +# Graphics Support +# +# CONFIG_TIFF is not set + +# +# Interpreters +# +# CONFIG_INTERPRETERS_FICL is not set +# CONFIG_INTERPRETERS_PCODE is not set + +# +# Network Utilities +# + +# +# Networking Utilities +# +# CONFIG_NETUTILS_CODECS is not set +# CONFIG_NETUTILS_DHCPC is not set +# CONFIG_NETUTILS_DHCPD is not set +# CONFIG_NETUTILS_FTPC is not set +# CONFIG_NETUTILS_FTPD is not set +# CONFIG_NETUTILS_JSON is not set +# CONFIG_NETUTILS_RESOLV is not set +# CONFIG_NETUTILS_SMTP is not set +# CONFIG_NETUTILS_TELNETD is not set +# CONFIG_NETUTILS_TFTPC is not set +# CONFIG_NETUTILS_THTTPD is not set +# CONFIG_NETUTILS_UIPLIB is not set +# CONFIG_NETUTILS_WEBCLIENT is not set + +# +# FreeModBus +# +# CONFIG_MODBUS is not set + +# +# NSH Library +# +CONFIG_NSH_LIBRARY=y +CONFIG_NSH_BUILTIN_APPS=y + +# +# Disable Individual commands +# +# CONFIG_NSH_DISABLE_CAT is not set +# CONFIG_NSH_DISABLE_CD is not set +# CONFIG_NSH_DISABLE_CP is not set +# CONFIG_NSH_DISABLE_DD is not set +# CONFIG_NSH_DISABLE_ECHO is not set +# CONFIG_NSH_DISABLE_EXEC is not set +# CONFIG_NSH_DISABLE_EXIT is not set +# CONFIG_NSH_DISABLE_FREE is not set +# CONFIG_NSH_DISABLE_GET is not set +# CONFIG_NSH_DISABLE_HELP is not set +# CONFIG_NSH_DISABLE_HEXDUMP is not set +# CONFIG_NSH_DISABLE_IFCONFIG is not set +# CONFIG_NSH_DISABLE_KILL is not set +# CONFIG_NSH_DISABLE_LOSETUP is not set +# CONFIG_NSH_DISABLE_LS is not set +# CONFIG_NSH_DISABLE_MB is not set +# CONFIG_NSH_DISABLE_MKDIR is not set +# CONFIG_NSH_DISABLE_MKFATFS is not set +# CONFIG_NSH_DISABLE_MKFIFO is not set +# CONFIG_NSH_DISABLE_MKRD is not set +# CONFIG_NSH_DISABLE_MH is not set +# CONFIG_NSH_DISABLE_MOUNT is not set +# CONFIG_NSH_DISABLE_MW is not set +# CONFIG_NSH_DISABLE_NSFMOUNT is not set +# CONFIG_NSH_DISABLE_PS is not set +# CONFIG_NSH_DISABLE_PING is not set +# CONFIG_NSH_DISABLE_PUT is not set +# CONFIG_NSH_DISABLE_PWD is not set +# CONFIG_NSH_DISABLE_RM is not set +# CONFIG_NSH_DISABLE_RMDIR is not set +# CONFIG_NSH_DISABLE_SET is not set +# CONFIG_NSH_DISABLE_SH is not set +# CONFIG_NSH_DISABLE_SLEEP is not set +# CONFIG_NSH_DISABLE_TEST is not set +# CONFIG_NSH_DISABLE_UMOUNT is not set +# CONFIG_NSH_DISABLE_UNSET is not set +# CONFIG_NSH_DISABLE_USLEEP is not set +# CONFIG_NSH_DISABLE_WGET is not set +# CONFIG_NSH_DISABLE_XD is not set + +# +# Configure Command Options +# +# CONFIG_NSH_CMDOPT_DF_H is not set +CONFIG_NSH_CODECS_BUFSIZE=128 +CONFIG_NSH_FILEIOSIZE=512 +CONFIG_NSH_STRERROR=y +CONFIG_NSH_LINELEN=128 +CONFIG_NSH_MAXARGUMENTS=12 +CONFIG_NSH_NESTDEPTH=8 +# CONFIG_NSH_DISABLESCRIPT is not set +# CONFIG_NSH_DISABLEBG is not set +CONFIG_NSH_ROMFSETC=y +# CONFIG_NSH_ROMFSRC is not set +CONFIG_NSH_ROMFSMOUNTPT="/etc" +CONFIG_NSH_INITSCRIPT="init.d/rcS" +CONFIG_NSH_ROMFSDEVNO=0 +CONFIG_NSH_ROMFSSECTSIZE=128 +CONFIG_NSH_ARCHROMFS=y +CONFIG_NSH_FATDEVNO=1 +CONFIG_NSH_FATSECTSIZE=512 +CONFIG_NSH_FATNSECTORS=1024 +CONFIG_NSH_FATMOUNTPT="/tmp" +CONFIG_NSH_CONSOLE=y + +# +# USB Trace Support +# +# CONFIG_NSH_CONDEV is not set +CONFIG_NSH_ARCHINIT=y + +# +# NxWidgets/NxWM +# + +# +# System NSH Add-Ons +# + +# +# Custom Free Memory Command +# +# CONFIG_SYSTEM_FREE is not set + +# +# I2C tool +# +CONFIG_SYSTEM_I2CTOOL=y +CONFIG_I2CTOOL_MINBUS=0 +CONFIG_I2CTOOL_MAXBUS=3 +CONFIG_I2CTOOL_MINADDR=0x03 +CONFIG_I2CTOOL_MAXADDR=0x77 +CONFIG_I2CTOOL_MAXREGADDR=0xff +CONFIG_I2CTOOL_DEFFREQ=4000000 + +# +# FLASH Program Installation +# +# CONFIG_SYSTEM_INSTALL is not set + +# +# FLASH Erase-all Command +# +# CONFIG_SYSTEM_FLASH_ERASEALL is not set + +# +# readline() +# +CONFIG_SYSTEM_READLINE=y +CONFIG_READLINE_ECHO=y + +# +# Power Off +# +# CONFIG_SYSTEM_POWEROFF is not set + +# +# RAMTRON +# +# CONFIG_SYSTEM_RAMTRON is not set + +# +# SD Card +# +# CONFIG_SYSTEM_SDCARD is not set + +# +# Sysinfo +# +CONFIG_SYSTEM_SYSINFO=y + +# +# USB Monitor +# diff --git a/src/modules/position_estimator/module.mk b/nuttx-configs/aerocore/nsh/setenv.sh index f64095d9d..2327f38a1 100644..100755 --- a/src/modules/position_estimator/module.mk +++ b/nuttx-configs/aerocore/nsh/setenv.sh @@ -1,6 +1,8 @@ -############################################################################ +#!/bin/bash +# configs/aerocore/nsh/setenv.sh # -# Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved. +# Copyright (C) 2011 Gregory Nutt. All rights reserved. +# Author: Gregory Nutt <gnutt@nuttx.org> # # Redistribution and use in source and binary forms, with or without # modification, are permitted provided that the following conditions @@ -12,7 +14,7 @@ # notice, this list of conditions and the following disclaimer in # the documentation and/or other materials provided with the # distribution. -# 3. Neither the name PX4 nor the names of its contributors may be +# 3. Neither the name NuttX nor the names of its contributors may be # used to endorse or promote products derived from this software # without specific prior written permission. # @@ -29,16 +31,37 @@ # ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE # POSSIBILITY OF SUCH DAMAGE. # -############################################################################ -# -# Makefile to build the position estimator -# +if [ "$_" = "$0" ] ; then + echo "You must source this script, not run it!" 1>&2 + exit 1 +fi + +WD=`pwd` +if [ ! -x "setenv.sh" ]; then + echo "This script must be executed from the top-level NuttX build directory" + exit 1 +fi + +if [ -z "${PATH_ORIG}" ]; then + export PATH_ORIG="${PATH}" +fi + +# This the Cygwin path to the location where I installed the RIDE +# toolchain under windows. You will also have to edit this if you install +# the RIDE toolchain in any other location +#export TOOLCHAIN_BIN="/cygdrive/c/Program Files (x86)/Raisonance/Ride/arm-gcc/bin" + +# This the Cygwin path to the location where I installed the CodeSourcery +# toolchain under windows. You will also have to edit this if you install +# the CodeSourcery toolchain in any other location +export TOOLCHAIN_BIN="/cygdrive/c/Program Files (x86)/CodeSourcery/Sourcery G++ Lite/bin" -MODULE_COMMAND = position_estimator +# This the Cygwin path to the location where I build the buildroot +# toolchain. +#export TOOLCHAIN_BIN="${WD}/../misc/buildroot/build_arm_nofpu/staging_dir/bin" -# XXX this should be converted to a deamon, its a pretty bad example app -MODULE_PRIORITY = SCHED_PRIORITY_DEFAULT -MODULE_STACKSIZE = 4096 +# Add the path to the toolchain to the PATH varialble +export PATH="${TOOLCHAIN_BIN}:/sbin:/usr/sbin:${PATH_ORIG}" -SRCS = position_estimator_main.c +echo "PATH : ${PATH}" diff --git a/nuttx-configs/aerocore/scripts/ld.script b/nuttx-configs/aerocore/scripts/ld.script new file mode 100644 index 000000000..968d3127f --- /dev/null +++ b/nuttx-configs/aerocore/scripts/ld.script @@ -0,0 +1,150 @@ +/**************************************************************************** + * configs/aerocore/common/ld.script + * + * Copyright (C) 2011 Gregory Nutt. All rights reserved. + * Author: Gregory Nutt <gnutt@nuttx.org> + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name NuttX nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/* The STM32F427 has 2048Kb of FLASH beginning at address 0x0800:0000 and + * 256Kb of SRAM. SRAM is split up into three blocks: + * + * 1) 112Kb of SRAM beginning at address 0x2000:0000 + * 2) 16Kb of SRAM beginning at address 0x2001:c000 + * 3) 64Kb of SRAM beginning at address 0x2002:0000 + * 4) 64Kb of TCM SRAM beginning at address 0x1000:0000 + * + * When booting from FLASH, FLASH memory is aliased to address 0x0000:0000 + * where the code expects to begin execution by jumping to the entry point in + * the 0x0800:0000 address range. + * + * The first 0x4000 of flash is reserved for the bootloader. + */ + +MEMORY +{ + flash (rx) : ORIGIN = 0x08004000, LENGTH = 2032K + sram (rwx) : ORIGIN = 0x20000000, LENGTH = 192K + ccsram (rwx) : ORIGIN = 0x10000000, LENGTH = 64K +} + +OUTPUT_ARCH(arm) + +ENTRY(__start) /* treat __start as the anchor for dead code stripping */ +EXTERN(_vectors) /* force the vectors to be included in the output */ + +/* + * Ensure that abort() is present in the final object. The exception handling + * code pulled in by libgcc.a requires it (and that code cannot be easily avoided). + */ +EXTERN(abort) + +SECTIONS +{ + .text : { + _stext = ABSOLUTE(.); + *(.vectors) + *(.text .text.*) + *(.fixup) + *(.gnu.warning) + *(.rodata .rodata.*) + *(.gnu.linkonce.t.*) + *(.got) + *(.gcc_except_table) + *(.gnu.linkonce.r.*) + _etext = ABSOLUTE(.); + + /* + * This is a hack to make the newlib libm __errno() call + * use the NuttX get_errno_ptr() function. + */ + __errno = get_errno_ptr; + } > flash + + /* + * Init functions (static constructors and the like) + */ + .init_section : { + _sinit = ABSOLUTE(.); + KEEP(*(.init_array .init_array.*)) + _einit = ABSOLUTE(.); + } > flash + + /* + * Construction data for parameters. + */ + __param ALIGN(4): { + __param_start = ABSOLUTE(.); + KEEP(*(__param*)) + __param_end = ABSOLUTE(.); + } > flash + + .ARM.extab : { + *(.ARM.extab*) + } > flash + + __exidx_start = ABSOLUTE(.); + .ARM.exidx : { + *(.ARM.exidx*) + } > flash + __exidx_end = ABSOLUTE(.); + + _eronly = ABSOLUTE(.); + + .data : { + _sdata = ABSOLUTE(.); + *(.data .data.*) + *(.gnu.linkonce.d.*) + CONSTRUCTORS + _edata = ABSOLUTE(.); + } > sram AT > flash + + .bss : { + _sbss = ABSOLUTE(.); + *(.bss .bss.*) + *(.gnu.linkonce.b.*) + *(COMMON) + _ebss = ABSOLUTE(.); + } > sram + + /* Stabs debugging sections. */ + .stab 0 : { *(.stab) } + .stabstr 0 : { *(.stabstr) } + .stab.excl 0 : { *(.stab.excl) } + .stab.exclstr 0 : { *(.stab.exclstr) } + .stab.index 0 : { *(.stab.index) } + .stab.indexstr 0 : { *(.stab.indexstr) } + .comment 0 : { *(.comment) } + .debug_abbrev 0 : { *(.debug_abbrev) } + .debug_info 0 : { *(.debug_info) } + .debug_line 0 : { *(.debug_line) } + .debug_pubnames 0 : { *(.debug_pubnames) } + .debug_aranges 0 : { *(.debug_aranges) } +} diff --git a/Tools/px4params/px_process_params.py b/nuttx-configs/aerocore/src/Makefile index 7799f6348..859ba4ab2 100755..100644 --- a/Tools/px4params/px_process_params.py +++ b/nuttx-configs/aerocore/src/Makefile @@ -1,7 +1,8 @@ -#!/usr/bin/env python ############################################################################ +# configs/aerocore/src/Makefile # -# Copyright (C) 2013 PX4 Development Team. All rights reserved. +# Copyright (C) 2011 Gregory Nutt. All rights reserved. +# Author: Gregory Nutt <gnutt@nuttx.org> # # Redistribution and use in source and binary forms, with or without # modification, are permitted provided that the following conditions @@ -13,7 +14,7 @@ # notice, this list of conditions and the following disclaimer in # the documentation and/or other materials provided with the # distribution. -# 3. Neither the name PX4 nor the names of its contributors may be +# 3. Neither the name NuttX nor the names of its contributors may be # used to endorse or promote products derived from this software # without specific prior written permission. # @@ -32,36 +33,52 @@ # ############################################################################ -# -# PX4 paramers processor (main executable file) -# -# It scans src/ subdirectory of the project, collects all parameters -# definitions, and outputs list of parameters in XML and DokuWiki formats. -# +-include $(TOPDIR)/Make.defs + +CFLAGS += -I$(TOPDIR)/sched + +ASRCS = +AOBJS = $(ASRCS:.S=$(OBJEXT)) + +CSRCS = empty.c +COBJS = $(CSRCS:.c=$(OBJEXT)) + +SRCS = $(ASRCS) $(CSRCS) +OBJS = $(AOBJS) $(COBJS) + +ARCH_SRCDIR = $(TOPDIR)/arch/$(CONFIG_ARCH)/src +ifeq ($(WINTOOL),y) + CFLAGS += -I "${shell cygpath -w $(ARCH_SRCDIR)/chip}" \ + -I "${shell cygpath -w $(ARCH_SRCDIR)/common}" \ + -I "${shell cygpath -w $(ARCH_SRCDIR)/armv7-m}" +else + CFLAGS += -I$(ARCH_SRCDIR)/chip -I$(ARCH_SRCDIR)/common -I$(ARCH_SRCDIR)/armv7-m +endif + +all: libboard$(LIBEXT) + +$(AOBJS): %$(OBJEXT): %.S + $(call ASSEMBLE, $<, $@) + +$(COBJS) $(LINKOBJS): %$(OBJEXT): %.c + $(call COMPILE, $<, $@) + +libboard$(LIBEXT): $(OBJS) + $(call ARCHIVE, $@, $(OBJS)) -import scanner -import srcparser -import output_xml -import output_dokuwiki_tables -import output_dokuwiki_listings +.depend: Makefile $(SRCS) + $(Q) $(MKDEP) $(CC) -- $(CFLAGS) -- $(SRCS) >Make.dep + $(Q) touch $@ -# Initialize parser -prs = srcparser.Parser() +depend: .depend -# Scan directories, and parse the files -sc = scanner.Scanner() -sc.ScanDir("../../src", prs) -groups = prs.GetParamGroups() +clean: + $(call DELFILE, libboard$(LIBEXT)) + $(call CLEAN) -# Output into XML -out = output_xml.XMLOutput(groups) -out.Save("parameters.xml") +distclean: clean + $(call DELFILE, Make.dep) + $(call DELFILE, .depend) -# Output to DokuWiki listings -#out = output_dokuwiki_listings.DokuWikiListingsOutput(groups) -#out.Save("parameters.wiki") +-include Make.dep -# Output to DokuWiki tables -out = output_dokuwiki_tables.DokuWikiTablesOutput(groups) -out.Save("parameters.wiki") -out.SaveRpc("parameters.wikirpc.xml") diff --git a/nuttx-configs/aerocore/src/empty.c b/nuttx-configs/aerocore/src/empty.c new file mode 100644 index 000000000..ace900866 --- /dev/null +++ b/nuttx-configs/aerocore/src/empty.c @@ -0,0 +1,4 @@ +/* + * There are no source files here, but libboard.a can't be empty, so + * we have this empty source file to keep it company. + */ diff --git a/nuttx-configs/px4fmu-v1/nsh/defconfig b/nuttx-configs/px4fmu-v1/nsh/defconfig index 00bf83bd5..bc0c12067 100644 --- a/nuttx-configs/px4fmu-v1/nsh/defconfig +++ b/nuttx-configs/px4fmu-v1/nsh/defconfig @@ -405,7 +405,7 @@ CONFIG_SIG_SIGWORK=4 CONFIG_MAX_TASKS=32 CONFIG_MAX_TASK_ARGS=10 CONFIG_NPTHREAD_KEYS=4 -CONFIG_NFILE_DESCRIPTORS=36 +CONFIG_NFILE_DESCRIPTORS=38 CONFIG_NFILE_STREAMS=8 CONFIG_NAME_MAX=32 CONFIG_PREALLOC_MQ_MSGS=4 @@ -418,7 +418,7 @@ CONFIG_PREALLOC_TIMERS=50 # Stack and heap information # CONFIG_IDLETHREAD_STACKSIZE=4096 -CONFIG_USERMAIN_STACKSIZE=4096 +CONFIG_USERMAIN_STACKSIZE=3500 CONFIG_PTHREAD_STACK_MIN=512 CONFIG_PTHREAD_STACK_DEFAULT=2048 @@ -504,8 +504,8 @@ CONFIG_MTD_BYTE_WRITE=y # # USART1 Configuration # -CONFIG_USART1_RXBUFSIZE=512 -CONFIG_USART1_TXBUFSIZE=512 +CONFIG_USART1_RXBUFSIZE=256 +CONFIG_USART1_TXBUFSIZE=128 CONFIG_USART1_BAUD=57600 CONFIG_USART1_BITS=8 CONFIG_USART1_PARITY=0 @@ -528,8 +528,8 @@ CONFIG_USART2_OFLOWCONTROL=y # # UART5 Configuration # -CONFIG_UART5_RXBUFSIZE=512 -CONFIG_UART5_TXBUFSIZE=512 +CONFIG_UART5_RXBUFSIZE=256 +CONFIG_UART5_TXBUFSIZE=128 CONFIG_UART5_BAUD=57600 CONFIG_UART5_BITS=8 CONFIG_UART5_PARITY=0 @@ -540,8 +540,8 @@ CONFIG_UART5_2STOP=0 # # USART6 Configuration # -CONFIG_USART6_RXBUFSIZE=512 -CONFIG_USART6_TXBUFSIZE=512 +CONFIG_USART6_RXBUFSIZE=128 +CONFIG_USART6_TXBUFSIZE=64 CONFIG_USART6_BAUD=57600 CONFIG_USART6_BITS=8 CONFIG_USART6_PARITY=0 diff --git a/nuttx-configs/px4fmu-v2/nsh/defconfig b/nuttx-configs/px4fmu-v2/nsh/defconfig index 9c75e6c59..a982040c6 100644 --- a/nuttx-configs/px4fmu-v2/nsh/defconfig +++ b/nuttx-configs/px4fmu-v2/nsh/defconfig @@ -439,7 +439,7 @@ CONFIG_SIG_SIGWORK=4 CONFIG_MAX_TASKS=32 CONFIG_MAX_TASK_ARGS=10 CONFIG_NPTHREAD_KEYS=4 -CONFIG_NFILE_DESCRIPTORS=36 +CONFIG_NFILE_DESCRIPTORS=38 CONFIG_NFILE_STREAMS=8 CONFIG_NAME_MAX=32 CONFIG_PREALLOC_MQ_MSGS=4 diff --git a/nuttx-configs/px4io-v2/include/board.h b/nuttx-configs/px4io-v2/include/board.h index 4b9c90638..17e77918b 100755 --- a/nuttx-configs/px4io-v2/include/board.h +++ b/nuttx-configs/px4io-v2/include/board.h @@ -103,8 +103,6 @@ #define GPIO_USART2_RTS 0xffffffff #undef GPIO_USART2_CK #define GPIO_USART2_CK 0xffffffff -#undef GPIO_USART3_TX -#define GPIO_USART3_TX 0xffffffff #undef GPIO_USART3_CK #define GPIO_USART3_CK 0xffffffff #undef GPIO_USART3_CTS diff --git a/nuttx-configs/px4io-v2/nsh/defconfig b/nuttx-configs/px4io-v2/nsh/defconfig index 4111e70eb..e6563e587 100755 --- a/nuttx-configs/px4io-v2/nsh/defconfig +++ b/nuttx-configs/px4io-v2/nsh/defconfig @@ -104,9 +104,9 @@ CONFIG_ARMV7M_CMNVECTOR=y # CONFIG_STM32_JTAG_SW_ENABLE - Set JTAG-DP disabled and SW-DP enabled # CONFIG_STM32_DFU=n -CONFIG_STM32_JTAG_FULL_ENABLE=y +CONFIG_STM32_JTAG_FULL_ENABLE=n CONFIG_STM32_JTAG_NOJNTRST_ENABLE=n -CONFIG_STM32_JTAG_SW_ENABLE=n +CONFIG_STM32_JTAG_SW_ENABLE=y # # Individual subsystems can be enabled: diff --git a/src/drivers/airspeed/airspeed.cpp b/src/drivers/airspeed/airspeed.cpp index 524151c90..41942aacd 100644 --- a/src/drivers/airspeed/airspeed.cpp +++ b/src/drivers/airspeed/airspeed.cpp @@ -82,10 +82,12 @@ Airspeed::Airspeed(int bus, int address, unsigned conversion_interval, const cha _buffer_overflows(perf_alloc(PC_COUNT, "airspeed_buffer_overflows")), _max_differential_pressure_pa(0), _sensor_ok(false), + _last_published_sensor_ok(true), /* initialize differently to force publication */ _measure_ticks(0), _collect_phase(false), _diff_pres_offset(0.0f), _airspeed_pub(-1), + _subsys_pub(-1), _class_instance(-1), _conversion_interval(conversion_interval), _sample_perf(perf_alloc(PC_ELAPSED, "airspeed_read")), @@ -149,8 +151,7 @@ Airspeed::init() } ret = OK; - /* sensor is ok, but we don't really know if it is within range */ - _sensor_ok = true; + out: return ret; } @@ -344,22 +345,6 @@ Airspeed::start() /* schedule a cycle to start things */ work_queue(HPWORK, &_work, (worker_t)&Airspeed::cycle_trampoline, this, 1); - - /* notify about state change */ - struct subsystem_info_s info = { - true, - true, - true, - SUBSYSTEM_TYPE_DIFFPRESSURE - }; - static orb_advert_t pub = -1; - - if (pub > 0) { - orb_publish(ORB_ID(subsystem_info), pub, &info); - - } else { - pub = orb_advertise(ORB_ID(subsystem_info), &info); - } } void @@ -369,11 +354,34 @@ Airspeed::stop() } void +Airspeed::update_status() +{ + if (_sensor_ok != _last_published_sensor_ok) { + /* notify about state change */ + struct subsystem_info_s info = { + true, + true, + _sensor_ok, + SUBSYSTEM_TYPE_DIFFPRESSURE + }; + + if (_subsys_pub > 0) { + orb_publish(ORB_ID(subsystem_info), _subsys_pub, &info); + } else { + _subsys_pub = orb_advertise(ORB_ID(subsystem_info), &info); + } + + _last_published_sensor_ok = _sensor_ok; + } +} + +void Airspeed::cycle_trampoline(void *arg) { Airspeed *dev = (Airspeed *)arg; dev->cycle(); + dev->update_status(); } void diff --git a/src/drivers/airspeed/airspeed.h b/src/drivers/airspeed/airspeed.h index 186602eda..0b8e949c9 100644 --- a/src/drivers/airspeed/airspeed.h +++ b/src/drivers/airspeed/airspeed.h @@ -118,14 +118,21 @@ protected: virtual int measure() = 0; virtual int collect() = 0; + /** + * Update the subsystem status + */ + void update_status(); + work_s _work; float _max_differential_pressure_pa; bool _sensor_ok; + bool _last_published_sensor_ok; int _measure_ticks; bool _collect_phase; float _diff_pres_offset; orb_advert_t _airspeed_pub; + orb_advert_t _subsys_pub; int _class_instance; diff --git a/src/drivers/blinkm/blinkm.cpp b/src/drivers/blinkm/blinkm.cpp index 2361f4dd1..5c502f682 100644 --- a/src/drivers/blinkm/blinkm.cpp +++ b/src/drivers/blinkm/blinkm.cpp @@ -48,11 +48,14 @@ * The recognized number off cells, will be blinked 5 times in purple color. * 2 Cells = 2 blinks * ... - * 5 Cells = 5 blinks + * 6 Cells = 6 blinks * Now the Application will show the actual selected Flightmode, GPS-Fix and Battery Warnings and Alerts. * - * System disarmed: - * The BlinkM should lit solid red. + * System disarmed and safe: + * The BlinkM should light solid cyan. + * + * System safety off but not armed: + * The BlinkM should light flashing orange * * System armed: * One message is made of 4 Blinks and a pause in the same length as the 4 blinks. @@ -67,10 +70,10 @@ * (X = on, _=off) * * The first 3 blinks indicates the status of the GPS-Signal (red): - * 0-4 satellites = X-X-X-X-_-_-_-_-_-_- - * 5 satellites = X-X-_-X-_-_-_-_-_-_- - * 6 satellites = X-_-_-X-_-_-_-_-_-_- - * >=7 satellites = _-_-_-X-_-_-_-_-_-_- + * 0-4 satellites = X-X-X-X-X-_-_-_-_-_- + * 5 satellites = X-X-_-X-X-_-_-_-_-_- + * 6 satellites = X-_-_-X-X-_-_-_-_-_- + * >=7 satellites = _-_-_-X-X-_-_-_-_-_- * If no GPS is found the first 3 blinks are white * * The fourth Blink indicates the Flightmode: @@ -119,6 +122,7 @@ #include <uORB/topics/vehicle_control_mode.h> #include <uORB/topics/actuator_armed.h> #include <uORB/topics/vehicle_gps_position.h> +#include <uORB/topics/safety.h> static const float MAX_CELL_VOLTAGE = 4.3f; static const int LED_ONTIME = 120; @@ -166,10 +170,12 @@ private: enum ledColors { LED_OFF, LED_RED, + LED_ORANGE, LED_YELLOW, LED_PURPLE, LED_GREEN, LED_BLUE, + LED_CYAN, LED_WHITE, LED_AMBER }; @@ -188,6 +194,26 @@ private: bool systemstate_run; + int vehicle_status_sub_fd; + int vehicle_control_mode_sub_fd; + int vehicle_gps_position_sub_fd; + int actuator_armed_sub_fd; + int safety_sub_fd; + + int num_of_cells; + int detected_cells_runcount; + + int t_led_color[8]; + int t_led_blink; + int led_thread_runcount; + int led_interval; + + bool topic_initialized; + bool detected_cells_blinked; + bool led_thread_ready; + + int num_of_used_sats; + void setLEDColor(int ledcolor); static void led_trampoline(void *arg); void led(); @@ -259,7 +285,22 @@ BlinkM::BlinkM(int bus, int blinkm) : led_color_7(LED_OFF), led_color_8(LED_OFF), led_blink(LED_NOBLINK), - systemstate_run(false) + systemstate_run(false), + vehicle_status_sub_fd(-1), + vehicle_control_mode_sub_fd(-1), + vehicle_gps_position_sub_fd(-1), + actuator_armed_sub_fd(-1), + safety_sub_fd(-1), + num_of_cells(0), + detected_cells_runcount(0), + t_led_color({0}), + t_led_blink(0), + led_thread_runcount(0), + led_interval(1000), + topic_initialized(false), + detected_cells_blinked(false), + led_thread_ready(true), + num_of_used_sats(0) { memset(&_work, 0, sizeof(_work)); } @@ -376,42 +417,22 @@ void BlinkM::led() { - static int vehicle_status_sub_fd; - static int vehicle_control_mode_sub_fd; - static int vehicle_gps_position_sub_fd; - static int actuator_armed_sub_fd; - - static int num_of_cells = 0; - static int detected_cells_runcount = 0; - - static int t_led_color[8] = { 0, 0, 0, 0, 0, 0, 0, 0}; - static int t_led_blink = 0; - static int led_thread_runcount=0; - static int led_interval = 1000; - - static int no_data_vehicle_status = 0; - static int no_data_vehicle_control_mode = 0; - static int no_data_actuator_armed = 0; - static int no_data_vehicle_gps_position = 0; - - static bool topic_initialized = false; - static bool detected_cells_blinked = false; - static bool led_thread_ready = true; - - int num_of_used_sats = 0; - if(!topic_initialized) { vehicle_status_sub_fd = orb_subscribe(ORB_ID(vehicle_status)); - orb_set_interval(vehicle_status_sub_fd, 1000); + orb_set_interval(vehicle_status_sub_fd, 250); vehicle_control_mode_sub_fd = orb_subscribe(ORB_ID(vehicle_control_mode)); - orb_set_interval(vehicle_control_mode_sub_fd, 1000); + orb_set_interval(vehicle_control_mode_sub_fd, 250); actuator_armed_sub_fd = orb_subscribe(ORB_ID(actuator_armed)); - orb_set_interval(actuator_armed_sub_fd, 1000); + orb_set_interval(actuator_armed_sub_fd, 250); vehicle_gps_position_sub_fd = orb_subscribe(ORB_ID(vehicle_gps_position)); - orb_set_interval(vehicle_gps_position_sub_fd, 1000); + orb_set_interval(vehicle_gps_position_sub_fd, 250); + + /* Subscribe to safety topic */ + safety_sub_fd = orb_subscribe(ORB_ID(safety)); + orb_set_interval(safety_sub_fd, 250); topic_initialized = true; } @@ -433,7 +454,9 @@ BlinkM::led() if(num_of_cells > 4) { t_led_color[4] = LED_PURPLE; } - t_led_color[5] = LED_OFF; + if(num_of_cells > 5) { + t_led_color[5] = LED_PURPLE; + } t_led_color[6] = LED_OFF; t_led_color[7] = LED_OFF; t_led_blink = LED_BLINK; @@ -467,17 +490,25 @@ BlinkM::led() struct vehicle_control_mode_s vehicle_control_mode; struct actuator_armed_s actuator_armed; struct vehicle_gps_position_s vehicle_gps_position_raw; + struct safety_s safety; memset(&vehicle_status_raw, 0, sizeof(vehicle_status_raw)); memset(&vehicle_gps_position_raw, 0, sizeof(vehicle_gps_position_raw)); + memset(&safety, 0, sizeof(safety)); bool new_data_vehicle_status; bool new_data_vehicle_control_mode; bool new_data_actuator_armed; bool new_data_vehicle_gps_position; + bool new_data_safety; orb_check(vehicle_status_sub_fd, &new_data_vehicle_status); + int no_data_vehicle_status = 0; + int no_data_vehicle_control_mode = 0; + int no_data_actuator_armed = 0; + int no_data_vehicle_gps_position = 0; + if (new_data_vehicle_status) { orb_copy(ORB_ID(vehicle_status), vehicle_status_sub_fd, &vehicle_status_raw); no_data_vehicle_status = 0; @@ -520,7 +551,12 @@ BlinkM::led() no_data_vehicle_gps_position = 3; } + /* update safety topic */ + orb_check(safety_sub_fd, &new_data_safety); + if (new_data_safety) { + orb_copy(ORB_ID(safety), safety_sub_fd, &safety); + } /* get number of used satellites in navigation */ num_of_used_sats = 0; @@ -541,19 +577,7 @@ BlinkM::led() printf("<blinkm> cells found:%d\n", num_of_cells); } else { - if(vehicle_status_raw.battery_warning == VEHICLE_BATTERY_WARNING_LOW) { - /* LED Pattern for battery low warning */ - led_color_1 = LED_YELLOW; - led_color_2 = LED_YELLOW; - led_color_3 = LED_YELLOW; - led_color_4 = LED_YELLOW; - led_color_5 = LED_YELLOW; - led_color_6 = LED_YELLOW; - led_color_7 = LED_YELLOW; - led_color_8 = LED_YELLOW; - led_blink = LED_BLINK; - - } else if(vehicle_status_raw.battery_warning == VEHICLE_BATTERY_WARNING_CRITICAL) { + if(vehicle_status_raw.battery_warning == VEHICLE_BATTERY_WARNING_CRITICAL) { /* LED Pattern for battery critical alerting */ led_color_1 = LED_RED; led_color_2 = LED_RED; @@ -565,21 +589,56 @@ BlinkM::led() led_color_8 = LED_RED; led_blink = LED_BLINK; + } else if(vehicle_status_raw.rc_signal_lost) { + /* LED Pattern for FAILSAFE */ + led_color_1 = LED_BLUE; + led_color_2 = LED_BLUE; + led_color_3 = LED_BLUE; + led_color_4 = LED_BLUE; + led_color_5 = LED_BLUE; + led_color_6 = LED_BLUE; + led_color_7 = LED_BLUE; + led_color_8 = LED_BLUE; + led_blink = LED_BLINK; + + } else if(vehicle_status_raw.battery_warning == VEHICLE_BATTERY_WARNING_LOW) { + /* LED Pattern for battery low warning */ + led_color_1 = LED_YELLOW; + led_color_2 = LED_YELLOW; + led_color_3 = LED_YELLOW; + led_color_4 = LED_YELLOW; + led_color_5 = LED_YELLOW; + led_color_6 = LED_YELLOW; + led_color_7 = LED_YELLOW; + led_color_8 = LED_YELLOW; + led_blink = LED_BLINK; + } else { /* no battery warnings here */ if(actuator_armed.armed == false) { /* system not armed */ - led_color_1 = LED_RED; - led_color_2 = LED_RED; - led_color_3 = LED_RED; - led_color_4 = LED_RED; - led_color_5 = LED_RED; - led_color_6 = LED_RED; - led_color_7 = LED_RED; - led_color_8 = LED_RED; - led_blink = LED_NOBLINK; - + if(safety.safety_off){ + led_color_1 = LED_ORANGE; + led_color_2 = LED_ORANGE; + led_color_3 = LED_ORANGE; + led_color_4 = LED_ORANGE; + led_color_5 = LED_ORANGE; + led_color_6 = LED_ORANGE; + led_color_7 = LED_ORANGE; + led_color_8 = LED_ORANGE; + led_blink = LED_BLINK; + }else{ + led_color_1 = LED_CYAN; + led_color_2 = LED_CYAN; + led_color_3 = LED_CYAN; + led_color_4 = LED_CYAN; + led_color_5 = LED_CYAN; + led_color_6 = LED_CYAN; + led_color_7 = LED_CYAN; + led_color_8 = LED_CYAN; + led_blink = LED_NOBLINK; + } } else { /* armed system - initial led pattern */ led_color_1 = LED_RED; @@ -593,23 +652,22 @@ BlinkM::led() led_blink = LED_BLINK; if(new_data_vehicle_control_mode || no_data_vehicle_control_mode < 3) { - - //XXX please check - if (vehicle_control_mode.flag_control_position_enabled) + /* indicate main control state */ + if (vehicle_status_raw.main_state == MAIN_STATE_POSCTL) led_color_4 = LED_GREEN; - else if (vehicle_control_mode.flag_control_velocity_enabled) + else if (vehicle_status_raw.main_state == MAIN_STATE_AUTO) led_color_4 = LED_BLUE; - else if (vehicle_control_mode.flag_control_attitude_enabled) + else if (vehicle_status_raw.main_state == MAIN_STATE_ALTCTL) led_color_4 = LED_YELLOW; - else if (vehicle_control_mode.flag_control_manual_enabled) - led_color_4 = LED_AMBER; + else if (vehicle_status_raw.main_state == MAIN_STATE_MANUAL) + led_color_4 = LED_WHITE; else led_color_4 = LED_OFF; - + led_color_5 = led_color_4; } if(new_data_vehicle_gps_position || no_data_vehicle_gps_position < 3) { - /* handling used sat�s */ + /* handling used satus */ if(num_of_used_sats >= 7) { led_color_1 = LED_OFF; led_color_2 = LED_OFF; @@ -690,8 +748,11 @@ void BlinkM::setLEDColor(int ledcolor) { case LED_RED: // red set_rgb(255,0,0); break; + case LED_ORANGE: // orange + set_rgb(255,150,0); + break; case LED_YELLOW: // yellow - set_rgb(255,70,0); + set_rgb(200,200,0); break; case LED_PURPLE: // purple set_rgb(255,0,255); @@ -702,11 +763,14 @@ void BlinkM::setLEDColor(int ledcolor) { case LED_BLUE: // blue set_rgb(0,0,255); break; + case LED_CYAN: // cyan + set_rgb(0,128,128); + break; case LED_WHITE: // white set_rgb(255,255,255); break; case LED_AMBER: // amber - set_rgb(255,20,0); + set_rgb(255,65,0); break; } } diff --git a/src/drivers/boards/aerocore/aerocore_init.c b/src/drivers/boards/aerocore/aerocore_init.c new file mode 100644 index 000000000..4e3ba2d7e --- /dev/null +++ b/src/drivers/boards/aerocore/aerocore_init.c @@ -0,0 +1,282 @@ +/**************************************************************************** + * + * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file aerocore_init.c + * + * AeroCore-specific early startup code. This file implements the + * nsh_archinitialize() function that is called early by nsh during startup. + * + * Code here is run before the rcS script is invoked; it should start required + * subsystems and perform board-specific initialisation. + */ + +/**************************************************************************** + * Included Files + ****************************************************************************/ + +#include <nuttx/config.h> + +#include <stdbool.h> +#include <stdio.h> +#include <debug.h> +#include <errno.h> + +#include <nuttx/arch.h> +#include <nuttx/spi.h> +#include <nuttx/i2c.h> +#include <nuttx/mmcsd.h> +#include <nuttx/analog/adc.h> +#include <nuttx/gran.h> + +#include <stm32.h> +#include "board_config.h" +#include <stm32_uart.h> + +#include <arch/board/board.h> + +#include <drivers/drv_hrt.h> +#include <drivers/drv_led.h> + +#include <systemlib/cpuload.h> +#include <systemlib/perf_counter.h> + +/**************************************************************************** + * Pre-Processor Definitions + ****************************************************************************/ + +/* Configuration ************************************************************/ + +/* Debug ********************************************************************/ + +#ifdef CONFIG_CPP_HAVE_VARARGS +# ifdef CONFIG_DEBUG +# define message(...) lowsyslog(__VA_ARGS__) +# else +# define message(...) printf(__VA_ARGS__) +# endif +#else +# ifdef CONFIG_DEBUG +# define message lowsyslog +# else +# define message printf +# endif +#endif + +/**************************************************************************** + * Protected Functions + ****************************************************************************/ + +#if defined(CONFIG_FAT_DMAMEMORY) +# if !defined(CONFIG_GRAN) || !defined(CONFIG_FAT_DMAMEMORY) +# error microSD DMA support requires CONFIG_GRAN +# endif + +static GRAN_HANDLE dma_allocator; + +/* + * The DMA heap size constrains the total number of things that can be + * ready to do DMA at a time. + * + * For example, FAT DMA depends on one sector-sized buffer per filesystem plus + * one sector-sized buffer per file. + * + * We use a fundamental alignment / granule size of 64B; this is sufficient + * to guarantee alignment for the largest STM32 DMA burst (16 beats x 32bits). + */ +static uint8_t g_dma_heap[8192] __attribute__((aligned(64))); +static perf_counter_t g_dma_perf; + +static void +dma_alloc_init(void) +{ + dma_allocator = gran_initialize(g_dma_heap, + sizeof(g_dma_heap), + 7, /* 128B granule - must be > alignment (XXX bug?) */ + 6); /* 64B alignment */ + if (dma_allocator == NULL) { + message("[boot] DMA allocator setup FAILED"); + } else { + g_dma_perf = perf_alloc(PC_COUNT, "DMA allocations"); + } +} + +/**************************************************************************** + * Public Functions + ****************************************************************************/ + +/* + * DMA-aware allocator stubs for the FAT filesystem. + */ + +__EXPORT void *fat_dma_alloc(size_t size); +__EXPORT void fat_dma_free(FAR void *memory, size_t size); + +void * +fat_dma_alloc(size_t size) +{ + perf_count(g_dma_perf); + return gran_alloc(dma_allocator, size); +} + +void +fat_dma_free(FAR void *memory, size_t size) +{ + gran_free(dma_allocator, memory, size); +} + +#else + +# define dma_alloc_init() + +#endif + +/************************************************************************************ + * Name: stm32_boardinitialize + * + * Description: + * All STM32 architectures must provide the following entry point. This entry point + * is called early in the intitialization -- after all memory has been configured + * and mapped but before any devices have been initialized. + * + ************************************************************************************/ + +__EXPORT void +stm32_boardinitialize(void) +{ + /* configure SPI interfaces */ + stm32_spiinitialize(); + + /* configure LEDs */ + up_ledinit(); +} + +/**************************************************************************** + * Name: nsh_archinitialize + * + * Description: + * Perform architecture specific initialization + * + ****************************************************************************/ + +static struct spi_dev_s *spi3; +static struct spi_dev_s *spi4; + +#include <math.h> + +#ifdef __cplusplus +__EXPORT int matherr(struct __exception *e) +{ + return 1; +} +#else +__EXPORT int matherr(struct exception *e) +{ + return 1; +} +#endif + +__EXPORT int nsh_archinitialize(void) +{ + + /* configure ADC pins */ + stm32_configgpio(GPIO_ADC1_IN10); /* used by VBUS valid */ + stm32_configgpio(GPIO_ADC1_IN11); /* J1 breakout */ + stm32_configgpio(GPIO_ADC1_IN12); /* J1 breakout */ + stm32_configgpio(GPIO_ADC1_IN13); /* J1 breakout */ + + /* configure the high-resolution time/callout interface */ + hrt_init(); + + /* configure the DMA allocator */ + dma_alloc_init(); + + /* configure CPU load estimation */ +#ifdef CONFIG_SCHED_INSTRUMENTATION + cpuload_initialize_once(); +#endif + + /* set up the serial DMA polling */ + static struct hrt_call serial_dma_call; + struct timespec ts; + + /* + * Poll at 1ms intervals for received bytes that have not triggered + * a DMA event. + */ + ts.tv_sec = 0; + ts.tv_nsec = 1000000; + + hrt_call_every(&serial_dma_call, + ts_to_abstime(&ts), + ts_to_abstime(&ts), + (hrt_callout)stm32_serial_dma_poll, + NULL); + + /* initial LED state */ + drv_led_start(); + led_off(LED_AMBER); + + /* Configure Sensors on SPI bus #3 */ + spi3 = up_spiinitialize(3); + if (!spi3) { + message("[boot] FAILED to initialize SPI port 3\n"); + up_ledon(LED_AMBER); + return -ENODEV; + } + /* Default: 1MHz, 8 bits, Mode 3 */ + SPI_SETFREQUENCY(spi3, 10000000); + SPI_SETBITS(spi3, 8); + SPI_SETMODE(spi3, SPIDEV_MODE3); + SPI_SELECT(spi3, PX4_SPIDEV_GYRO, false); + SPI_SELECT(spi3, PX4_SPIDEV_ACCEL_MAG, false); + SPI_SELECT(spi3, PX4_SPIDEV_BARO, false); + up_udelay(20); + message("[boot] Initialized SPI port 3 (SENSORS)\n"); + + /* Configure FRAM on SPI bus #4 */ + spi4 = up_spiinitialize(4); + if (!spi4) { + message("[boot] FAILED to initialize SPI port 4\n"); + up_ledon(LED_AMBER); + return -ENODEV; + } + /* Default: ~10MHz, 8 bits, Mode 3 */ + SPI_SETFREQUENCY(spi4, 10 * 1000 * 1000); + SPI_SETBITS(spi4, 8); + SPI_SETMODE(spi4, SPIDEV_MODE0); + SPI_SELECT(spi4, SPIDEV_FLASH, false); + message("[boot] Initialized SPI port 4 (FRAM)\n"); + + return OK; +} diff --git a/src/modules/sdlog/sdlog_ringbuffer.c b/src/drivers/boards/aerocore/aerocore_led.c index d7c8a4759..e40d1730c 100644 --- a/src/modules/sdlog/sdlog_ringbuffer.c +++ b/src/drivers/boards/aerocore/aerocore_led.c @@ -1,7 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. - * Author: Lorenz Meier <lm@inf.ethz.ch> + * Copyright (c) 2013 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -33,59 +32,90 @@ ****************************************************************************/ /** - * @file sdlog_log.c - * MAVLink text logging. + * @file aerocore_led.c * - * @author Lorenz Meier <lm@inf.ethz.ch> + * AeroCore LED backend. */ -#include <string.h> -#include <stdlib.h> +#include <nuttx/config.h> -#include "sdlog_ringbuffer.h" +#include <stdbool.h> -void sdlog_logbuffer_init(struct sdlog_logbuffer *lb, int size) -{ - lb->size = size; - lb->start = 0; - lb->count = 0; - lb->elems = (struct sdlog_sysvector *)calloc(lb->size, sizeof(struct sdlog_sysvector)); -} +#include "stm32.h" +#include "board_config.h" + +#include <arch/board/board.h> -int sdlog_logbuffer_is_full(struct sdlog_logbuffer *lb) +/* + * Ideally we'd be able to get these from up_internal.h, + * but since we want to be able to disable the NuttX use + * of leds for system indication at will and there is no + * separate switch, we need to build independent of the + * CONFIG_ARCH_LEDS configuration switch. + */ +__BEGIN_DECLS +extern void led_init(); +extern void led_on(int led); +extern void led_off(int led); +extern void led_toggle(int led); +__END_DECLS + +__EXPORT void led_init() { - return lb->count == (int)lb->size; + stm32_configgpio(GPIO_LED0); + stm32_configgpio(GPIO_LED1); } -int sdlog_logbuffer_is_empty(struct sdlog_logbuffer *lb) +__EXPORT void led_on(int led) { - return lb->count == 0; -} + switch (led) { + case 0: + stm32_gpiowrite(GPIO_LED0, true); + break; + case 1: + stm32_gpiowrite(GPIO_LED1, true); + break; -// XXX make these functions thread-safe -void sdlog_logbuffer_write(struct sdlog_logbuffer *lb, const struct sdlog_sysvector *elem) + default: + warnx("LED ID not recognized\n"); + } +} + +__EXPORT void led_off(int led) { - int end = (lb->start + lb->count) % lb->size; - memcpy(&(lb->elems[end]), elem, sizeof(struct sdlog_sysvector)); + switch (led) { + case 0: + stm32_gpiowrite(GPIO_LED0, false); + break; - if (sdlog_logbuffer_is_full(lb)) { - lb->start = (lb->start + 1) % lb->size; /* full, overwrite */ + case 1: + stm32_gpiowrite(GPIO_LED1, false); + break; - } else { - ++lb->count; + default: + warnx("LED ID not recognized\n"); } } -int sdlog_logbuffer_read(struct sdlog_logbuffer *lb, struct sdlog_sysvector *elem) +__EXPORT void led_toggle(int led) { - if (!sdlog_logbuffer_is_empty(lb)) { - memcpy(elem, &(lb->elems[lb->start]), sizeof(struct sdlog_sysvector)); - lb->start = (lb->start + 1) % lb->size; - --lb->count; - return 0; - - } else { - return 1; + switch (led) { + case 0: + if (stm32_gpioread(GPIO_LED0)) + stm32_gpiowrite(GPIO_LED0, false); + else + stm32_gpiowrite(GPIO_LED0, true); + break; + + case 1: + if (stm32_gpioread(GPIO_LED1)) + stm32_gpiowrite(GPIO_LED1, false); + else + stm32_gpiowrite(GPIO_LED1, true); + break; + + default: + warnx("LED ID not recognized\n"); } } diff --git a/src/modules/fixedwing_att_control/fixedwing_att_control_att.h b/src/drivers/boards/aerocore/aerocore_pwm_servo.c index 600e35b89..251eaff7b 100644 --- a/src/modules/fixedwing_att_control/fixedwing_att_control_att.h +++ b/src/drivers/boards/aerocore/aerocore_pwm_servo.c @@ -1,8 +1,6 @@ /**************************************************************************** * * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: @author Thomas Gubler <thomasgubler@student.ethz.ch> - * * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -33,19 +31,87 @@ * ****************************************************************************/ -/* @file Fixed Wing Attitude Control */ +/* + * @file aerocore_pwm_servo.c + * + * Configuration data for the stm32 pwm_servo driver. + * + * Note that these arrays must always be fully-sized. + */ + +#include <stdint.h> + +#include <stm32.h> +#include <stm32_gpio.h> +#include <stm32_tim.h> -#ifndef FIXEDWING_ATT_CONTROL_ATT_H_ -#define FIXEDWING_ATT_CONTROL_ATT_H_ +#include <drivers/stm32/drv_pwm_servo.h> +#include <drivers/drv_pwm_output.h> -#include <uORB/topics/vehicle_rates_setpoint.h> -#include <uORB/topics/vehicle_attitude_setpoint.h> -#include <uORB/topics/vehicle_attitude.h> -#include <uORB/topics/vehicle_global_position.h> +#include "board_config.h" -int fixedwing_att_control_attitude(const struct vehicle_attitude_setpoint_s *att_sp, - const struct vehicle_attitude_s *att, - const float speed_body[], - struct vehicle_rates_setpoint_s *rates_sp); +__EXPORT const struct pwm_servo_timer pwm_timers[PWM_SERVO_MAX_TIMERS] = { + { + .base = STM32_TIM1_BASE, + .clock_register = STM32_RCC_APB2ENR, + .clock_bit = RCC_APB2ENR_TIM1EN, + .clock_freq = STM32_APB2_TIM1_CLKIN + }, + { + .base = STM32_TIM3_BASE, + .clock_register = STM32_RCC_APB1ENR, + .clock_bit = RCC_APB1ENR_TIM3EN, + .clock_freq = STM32_APB1_TIM3_CLKIN + } +}; -#endif /* FIXEDWING_ATT_CONTROL_ATT_H_ */ +__EXPORT const struct pwm_servo_channel pwm_channels[PWM_SERVO_MAX_CHANNELS] = { + { + .gpio = GPIO_TIM1_CH1OUT, + .timer_index = 0, + .timer_channel = 1, + .default_value = 1500, + }, + { + .gpio = GPIO_TIM1_CH2OUT, + .timer_index = 0, + .timer_channel = 2, + .default_value = 1500, + }, + { + .gpio = GPIO_TIM1_CH3OUT, + .timer_index = 0, + .timer_channel = 3, + .default_value = 1500, + }, + { + .gpio = GPIO_TIM1_CH4OUT, + .timer_index = 0, + .timer_channel = 4, + .default_value = 1500, + }, + { + .gpio = GPIO_TIM3_CH1OUT, + .timer_index = 1, + .timer_channel = 1, + .default_value = 1500, + }, + { + .gpio = GPIO_TIM3_CH2OUT, + .timer_index = 1, + .timer_channel = 2, + .default_value = 1500, + }, + { + .gpio = GPIO_TIM3_CH3OUT, + .timer_index = 1, + .timer_channel = 3, + .default_value = 1500, + }, + { + .gpio = GPIO_TIM3_CH4OUT, + .timer_index = 1, + .timer_channel = 4, + .default_value = 1500, + } +}; diff --git a/src/drivers/boards/aerocore/aerocore_spi.c b/src/drivers/boards/aerocore/aerocore_spi.c new file mode 100644 index 000000000..e329bd9d1 --- /dev/null +++ b/src/drivers/boards/aerocore/aerocore_spi.c @@ -0,0 +1,183 @@ +/**************************************************************************** + * + * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file aerocore_spi.c + * + * Board-specific SPI functions. + */ + +/************************************************************************************ + * Included Files + ************************************************************************************/ + +#include <nuttx/config.h> + +#include <stdint.h> +#include <stdbool.h> +#include <debug.h> + +#include <nuttx/spi.h> +#include <arch/board/board.h> + +#include <up_arch.h> +#include <chip.h> +#include <stm32.h> +#include "board_config.h" + +/************************************************************************************ + * Public Functions + ************************************************************************************/ + +/************************************************************************************ + * Name: stm32_spiinitialize + * + * Description: + * Called to configure SPI chip select GPIO pins for the PX4FMU board. + * + ************************************************************************************/ + +__EXPORT void weak_function stm32_spiinitialize(void) +{ +#ifdef CONFIG_STM32_SPI1 + stm32_configgpio(GPIO_SPI1_NSS); + stm32_gpiowrite(GPIO_SPI1_NSS, 1); +#endif + +#ifdef CONFIG_STM32_SPI2 + stm32_configgpio(GPIO_SPI2_NSS); + stm32_gpiowrite(GPIO_SPI2_NSS, 1); +#endif + +#ifdef CONFIG_STM32_SPI3 + stm32_configgpio(GPIO_SPI_CS_GYRO); + stm32_configgpio(GPIO_SPI_CS_ACCEL_MAG); + stm32_configgpio(GPIO_SPI_CS_BARO); + + /* De-activate all peripherals, + * required for some peripheral + * state machines + */ + stm32_gpiowrite(GPIO_SPI_CS_GYRO, 1); + stm32_gpiowrite(GPIO_SPI_CS_ACCEL_MAG, 1); + stm32_gpiowrite(GPIO_SPI_CS_BARO, 1); + + stm32_configgpio(GPIO_EXTI_GYRO_DRDY); + stm32_configgpio(GPIO_EXTI_MAG_DRDY); + stm32_configgpio(GPIO_EXTI_ACCEL_DRDY); +#endif + +#ifdef CONFIG_STM32_SPI4 + stm32_configgpio(GPIO_SPI4_NSS); + stm32_gpiowrite(GPIO_SPI4_NSS, 1); +#endif +} + +#ifdef CONFIG_STM32_SPI1 +__EXPORT void stm32_spi1select(FAR struct spi_dev_s *dev, enum spi_dev_e devid, bool selected) +{ + /* there is only one device broken-out so select it */ + stm32_gpiowrite(GPIO_SPI1_NSS, !selected); +} + +__EXPORT uint8_t stm32_spi1status(FAR struct spi_dev_s *dev, enum spi_dev_e devid) +{ + return SPI_STATUS_PRESENT; +} +#endif + +#ifdef CONFIG_STM32_SPI2 +__EXPORT void stm32_spi2select(FAR struct spi_dev_s *dev, enum spi_dev_e devid, bool selected) +{ + /* there is only one device broken-out so select it */ + stm32_gpiowrite(GPIO_SPI2_NSS, !selected); +} + +__EXPORT uint8_t stm32_spi2status(FAR struct spi_dev_s *dev, enum spi_dev_e devid) +{ + return SPI_STATUS_PRESENT; +} +#endif + +#ifdef CONFIG_STM32_SPI3 +__EXPORT void stm32_spi3select(FAR struct spi_dev_s *dev, enum spi_dev_e devid, bool selected) +{ + /* SPI select is active low, so write !selected to select the device */ + + switch (devid) { + case PX4_SPIDEV_GYRO: + /* Making sure the other peripherals are not selected */ + stm32_gpiowrite(GPIO_SPI_CS_GYRO, !selected); + stm32_gpiowrite(GPIO_SPI_CS_ACCEL_MAG, 1); + stm32_gpiowrite(GPIO_SPI_CS_BARO, 1); + break; + + case PX4_SPIDEV_ACCEL_MAG: + /* Making sure the other peripherals are not selected */ + stm32_gpiowrite(GPIO_SPI_CS_GYRO, 1); + stm32_gpiowrite(GPIO_SPI_CS_ACCEL_MAG, !selected); + stm32_gpiowrite(GPIO_SPI_CS_BARO, 1); + break; + + case PX4_SPIDEV_BARO: + /* Making sure the other peripherals are not selected */ + stm32_gpiowrite(GPIO_SPI_CS_GYRO, 1); + stm32_gpiowrite(GPIO_SPI_CS_ACCEL_MAG, 1); + stm32_gpiowrite(GPIO_SPI_CS_BARO, !selected); + break; + + default: + break; + } +} + +__EXPORT uint8_t stm32_spi3status(FAR struct spi_dev_s *dev, enum spi_dev_e devid) +{ + return SPI_STATUS_PRESENT; +} +#endif + + +#ifdef CONFIG_STM32_SPI4 +__EXPORT void stm32_spi4select(FAR struct spi_dev_s *dev, enum spi_dev_e devid, bool selected) +{ + /* there can only be one device on this bus, so always select it */ + stm32_gpiowrite(GPIO_SPI4_NSS, !selected); +} + +__EXPORT uint8_t stm32_spi4status(FAR struct spi_dev_s *dev, enum spi_dev_e devid) +{ + /* FRAM is always present */ + return SPI_STATUS_PRESENT; +} +#endif diff --git a/src/drivers/boards/aerocore/board_config.h b/src/drivers/boards/aerocore/board_config.h new file mode 100644 index 000000000..70142a314 --- /dev/null +++ b/src/drivers/boards/aerocore/board_config.h @@ -0,0 +1,176 @@ +/**************************************************************************** + * + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file board_config.h + * + * AeroCore internal definitions + */ + +#pragma once + +/**************************************************************************************************** + * Included Files + ****************************************************************************************************/ + +#include <nuttx/config.h> +#include <nuttx/compiler.h> +#include <stdint.h> + +__BEGIN_DECLS + +/* these headers are not C++ safe */ +#include <stm32.h> +#include <arch/board/board.h> + +#define UDID_START 0x1FFF7A10 + +/**************************************************************************************************** + * Definitions + ****************************************************************************************************/ + +/* LEDs */ +#define GPIO_LED0 (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTE|GPIO_PIN9) +#define GPIO_LED1 (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTE|GPIO_PIN10) + +/* Gyro */ +#define GPIO_EXTI_GYRO_DRDY (GPIO_INPUT|GPIO_FLOAT|GPIO_EXTI|GPIO_PORTD|GPIO_PIN0) +#define SENSOR_BOARD_ROTATION_DEFAULT 3 /* SENSOR_BOARD_ROTATION_270_DEG */ + +/* Accel & Mag */ +#define GPIO_EXTI_MAG_DRDY (GPIO_INPUT|GPIO_FLOAT|GPIO_EXTI|GPIO_PORTD|GPIO_PIN1) +#define GPIO_EXTI_ACCEL_DRDY (GPIO_INPUT|GPIO_FLOAT|GPIO_EXTI|GPIO_PORTD|GPIO_PIN2) + +/* GPS */ +#define GPIO_GPS_NRESET (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_OUTPUT_SET|GPIO_PORTC|GPIO_PIN5) +#define GPIO_GPS_TIMEPULSE (GPIO_INPUT|GPIO_FLOAT|GPIO_PORTC|GPIO_PIN4) +#define GPS_DEFAULT_UART_PORT "/dev/ttyS0" + +/* SPI3--Sensors */ +#define PX4_SPI_BUS_SENSORS 3 +#define GPIO_SPI_CS_ACCEL_MAG (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTE|GPIO_PIN2) +#define GPIO_SPI_CS_GYRO (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTE|GPIO_PIN3) +#define GPIO_SPI_CS_BARO (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTE|GPIO_PIN4) + +/* Nominal chip selects for devices on SPI bus #3 */ +#define PX4_SPIDEV_ACCEL_MAG 0 +#define PX4_SPIDEV_GYRO 1 +#define PX4_SPIDEV_BARO 2 + +/* User GPIOs broken out on J11 */ +#define GPIO_GPIO0_INPUT (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTB|GPIO_PIN0) +#define GPIO_GPIO1_INPUT (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTB|GPIO_PIN1) +#define GPIO_GPIO3_INPUT (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTA|GPIO_PIN1) +#define GPIO_GPIO4_INPUT (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTA|GPIO_PIN2) +#define GPIO_GPIO5_INPUT (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTA|GPIO_PIN3) +#define GPIO_GPIO6_INPUT (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTD|GPIO_PIN12) +#define GPIO_GPIO7_INPUT (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTD|GPIO_PIN13) +#define GPIO_GPIO8_INPUT (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTD|GPIO_PIN14) +#define GPIO_GPIO9_INPUT (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTD|GPIO_PIN15) +#define GPIO_GPIO10_INPUT (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTB|GPIO_PIN5) +#define GPIO_GPIO11_INPUT (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTB|GPIO_PIN8) + +#define GPIO_GPIO0_OUTPUT (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN0) +#define GPIO_GPIO1_OUTPUT (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN1) +#define GPIO_GPIO3_OUTPUT (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTA|GPIO_PIN1) +#define GPIO_GPIO4_OUTPUT (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTA|GPIO_PIN2) +#define GPIO_GPIO5_OUTPUT (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTA|GPIO_PIN3) +#define GPIO_GPIO6_OUTPUT (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTD|GPIO_PIN12) +#define GPIO_GPIO7_OUTPUT (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTD|GPIO_PIN13) +#define GPIO_GPIO8_OUTPUT (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTD|GPIO_PIN14) +#define GPIO_GPIO9_OUTPUT (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTD|GPIO_PIN15) +#define GPIO_GPIO10_OUTPUT (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN5) +#define GPIO_GPIO11_OUTPUT (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN8) + +/* PWM + * + * Eight PWM outputs are configured. + * + * Pins: + * + * CH1 : PA8 : TIM1_CH1 + * CH2 : PA9 : TIM1_CH2 + * CH3 : PA10 : TIM1_CH3 + * CH4 : PA11 : TIM1_CH4 + * CH5 : PC6 : TIM3_CH1 + * CH6 : PC7 : TIM3_CH2 + * CH7 : PC8 : TIM3_CH3 + * CH8 : PC9 : TIM3_CH4 + */ +#define GPIO_TIM1_CH1OUT GPIO_TIM1_CH1OUT_1 +#define GPIO_TIM1_CH2OUT GPIO_TIM1_CH2OUT_1 +#define GPIO_TIM1_CH3OUT GPIO_TIM1_CH3OUT_1 +#define GPIO_TIM1_CH4OUT GPIO_TIM1_CH4OUT_1 +#define GPIO_TIM3_CH1OUT GPIO_TIM3_CH1OUT_3 +#define GPIO_TIM3_CH2OUT GPIO_TIM3_CH2OUT_3 +#define GPIO_TIM3_CH3OUT GPIO_TIM3_CH3OUT_2 +#define GPIO_TIM3_CH4OUT GPIO_TIM3_CH4OUT_2 + +/* High-resolution timer */ +#define HRT_TIMER 8 /* use timer 8 for the HRT */ +#define HRT_TIMER_CHANNEL 1 /* use capture/compare channel */ + +/* Tone Alarm (no onboard speaker )*/ +#define TONE_ALARM_TIMER 2 /* timer 2 */ +#define TONE_ALARM_CHANNEL 1 /* channel 1 */ +#define GPIO_TONE_ALARM_IDLE (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTA|GPIO_PIN0) +#define GPIO_TONE_ALARM (GPIO_ALT|GPIO_AF1|GPIO_SPEED_2MHz|GPIO_PUSHPULL|GPIO_PORTA|GPIO_PIN0) + + +/**************************************************************************************************** + * Public Types + ****************************************************************************************************/ + +/**************************************************************************************************** + * Public data + ****************************************************************************************************/ + +#ifndef __ASSEMBLY__ + +/**************************************************************************************************** + * Public Functions + ****************************************************************************************************/ + +/**************************************************************************************************** + * Name: stm32_spiinitialize + * + * Description: + * Called to configure SPI chip select GPIO pins for the PX4FMU board. + * + ****************************************************************************************************/ + +extern void stm32_spiinitialize(void); + +#endif /* __ASSEMBLY__ */ + +__END_DECLS diff --git a/src/drivers/boards/aerocore/module.mk b/src/drivers/boards/aerocore/module.mk new file mode 100644 index 000000000..b53fe0a29 --- /dev/null +++ b/src/drivers/boards/aerocore/module.mk @@ -0,0 +1,8 @@ +# +# Board-specific startup code for the AeroCore +# + +SRCS = aerocore_init.c \ + aerocore_pwm_servo.c \ + aerocore_spi.c \ + aerocore_led.c diff --git a/src/drivers/boards/px4fmu-v1/board_config.h b/src/drivers/boards/px4fmu-v1/board_config.h index 02c26b5c0..58273f2d2 100644 --- a/src/drivers/boards/px4fmu-v1/board_config.h +++ b/src/drivers/boards/px4fmu-v1/board_config.h @@ -85,6 +85,8 @@ __BEGIN_DECLS #define GPIO_SPI_CS_MPU (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_50MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN0) #define GPIO_SPI_CS_SDCARD (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_50MHz|GPIO_OUTPUT_SET|GPIO_PORTA|GPIO_PIN4) +#define PX4_SPI_BUS_SENSORS 1 + /* * Use these in place of the spi_dev_e enumeration to * select a specific SPI device on SPI1 diff --git a/src/drivers/boards/px4fmu-v2/board_config.h b/src/drivers/boards/px4fmu-v2/board_config.h index 7cfca7656..c2de1bfba 100644 --- a/src/drivers/boards/px4fmu-v2/board_config.h +++ b/src/drivers/boards/px4fmu-v2/board_config.h @@ -107,6 +107,8 @@ __BEGIN_DECLS #define GPIO_SPI_CS_FRAM (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTD|GPIO_PIN10) #define GPIO_SPI_CS_MPU (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTC|GPIO_PIN2) +#define PX4_SPI_BUS_SENSORS 1 + /* Use these in place of the spi_dev_e enumeration to select a specific SPI device on SPI1 */ #define PX4_SPIDEV_GYRO 1 #define PX4_SPIDEV_ACCEL_MAG 2 diff --git a/src/drivers/drv_gpio.h b/src/drivers/drv_gpio.h index f60964c2b..5acd0d343 100644 --- a/src/drivers/drv_gpio.h +++ b/src/drivers/drv_gpio.h @@ -94,6 +94,14 @@ #endif +#ifdef CONFIG_ARCH_BOARD_AEROCORE +/* + * AeroCore GPIO numbers and configuration. + * + */ +# define PX4FMU_DEVICE_PATH "/dev/px4fmu" +#endif + #ifdef CONFIG_ARCH_BOARD_PX4IO_V1 /* no GPIO driver on the PX4IOv1 board */ #endif @@ -146,4 +154,4 @@ #define GPIO_SENSOR_RAIL_RESET GPIOC(13) -#endif /* _DRV_GPIO_H */
\ No newline at end of file +#endif /* _DRV_GPIO_H */ diff --git a/src/drivers/drv_gps.h b/src/drivers/drv_gps.h index 06e3535b3..e14f4e00d 100644 --- a/src/drivers/drv_gps.h +++ b/src/drivers/drv_gps.h @@ -43,10 +43,14 @@ #include <stdint.h> #include <sys/ioctl.h> +#include "board_config.h" + #include "drv_sensor.h" #include "drv_orb_dev.h" +#ifndef GPS_DEFAULT_UART_PORT #define GPS_DEFAULT_UART_PORT "/dev/ttyS3" +#endif #define GPS_DEVICE_PATH "/dev/gps" diff --git a/src/drivers/drv_hrt.h b/src/drivers/drv_hrt.h index d130d68b3..8bfc90c64 100644 --- a/src/drivers/drv_hrt.h +++ b/src/drivers/drv_hrt.h @@ -41,6 +41,7 @@ #include <sys/types.h> #include <stdbool.h> +#include <inttypes.h> #include <time.h> #include <queue.h> diff --git a/src/drivers/drv_pwm_output.h b/src/drivers/drv_pwm_output.h index 7a93e513e..972573f9f 100644 --- a/src/drivers/drv_pwm_output.h +++ b/src/drivers/drv_pwm_output.h @@ -199,6 +199,9 @@ ORB_DECLARE(output_pwm); /** get the lockdown override flag to enable outputs in HIL */ #define PWM_SERVO_GET_DISABLE_LOCKDOWN _IOC(_PWM_SERVO_BASE, 22) +/** force safety switch off (to disable use of safety switch) */ +#define PWM_SERVO_SET_FORCE_SAFETY_OFF _IOC(_PWM_SERVO_BASE, 23) + /* * * diff --git a/src/drivers/drv_range_finder.h b/src/drivers/drv_range_finder.h index cf91f7030..e45939b37 100644 --- a/src/drivers/drv_range_finder.h +++ b/src/drivers/drv_range_finder.h @@ -46,6 +46,10 @@ #define RANGE_FINDER_DEVICE_PATH "/dev/range_finder" +enum RANGE_FINDER_TYPE { + RANGE_FINDER_TYPE_LASER = 0, +}; + /** * range finder report structure. Reads from the device must be in multiples of this * structure. @@ -53,8 +57,11 @@ struct range_finder_report { uint64_t timestamp; uint64_t error_count; - float distance; /** in meters */ - uint8_t valid; /** 1 == within sensor range, 0 = outside sensor range */ + unsigned type; /**< type, following RANGE_FINDER_TYPE enum */ + float distance; /**< in meters */ + float minimum_distance; /**< minimum distance the sensor can measure */ + float maximum_distance; /**< maximum distance the sensor can measure */ + uint8_t valid; /**< 1 == within sensor range, 0 = outside sensor range */ }; /* diff --git a/src/drivers/drv_tone_alarm.h b/src/drivers/drv_tone_alarm.h index cb5fd53a5..b7981e9c4 100644 --- a/src/drivers/drv_tone_alarm.h +++ b/src/drivers/drv_tone_alarm.h @@ -147,6 +147,8 @@ enum { TONE_BATTERY_WARNING_SLOW_TUNE, TONE_BATTERY_WARNING_FAST_TUNE, TONE_GPS_WARNING_TUNE, + TONE_ARMING_FAILURE_TUNE, + TONE_PARACHUTE_RELEASE_TUNE, TONE_NUMBER_OF_TUNES }; diff --git a/src/drivers/ets_airspeed/ets_airspeed.cpp b/src/drivers/ets_airspeed/ets_airspeed.cpp index d27ab9727..146a06e7c 100644 --- a/src/drivers/ets_airspeed/ets_airspeed.cpp +++ b/src/drivers/ets_airspeed/ets_airspeed.cpp @@ -176,11 +176,14 @@ ETSAirspeed::collect() _max_differential_pressure_pa = diff_pres_pa; } - // XXX we may want to smooth out the readings to remove noise. differential_pressure_s report; report.timestamp = hrt_absolute_time(); report.error_count = perf_event_count(_comms_errors); report.differential_pressure_pa = (float)diff_pres_pa; + + // XXX we may want to smooth out the readings to remove noise. + report.differential_pressure_filtered_pa = (float)diff_pres_pa; + report.temperature = -1000.0f; report.voltage = 0; report.max_differential_pressure_pa = _max_differential_pressure_pa; @@ -204,14 +207,18 @@ ETSAirspeed::collect() void ETSAirspeed::cycle() { + int ret; + /* collection phase? */ if (_collect_phase) { /* perform collection */ - if (OK != collect()) { + ret = collect(); + if (OK != ret) { perf_count(_comms_errors); /* restart the measurement state machine */ start(); + _sensor_ok = false; return; } @@ -235,8 +242,12 @@ ETSAirspeed::cycle() } /* measurement phase */ - if (OK != measure()) - log("measure error"); + ret = measure(); + if (OK != ret) { + debug("measure error"); + } + + _sensor_ok = (ret == OK); /* next phase is collection */ _collect_phase = true; diff --git a/src/drivers/frsky_telemetry/frsky_data.c b/src/drivers/frsky_telemetry/frsky_data.c index cfcf91e3f..18de3f4da 100644 --- a/src/drivers/frsky_telemetry/frsky_data.c +++ b/src/drivers/frsky_telemetry/frsky_data.c @@ -53,6 +53,8 @@ #include <uORB/topics/vehicle_global_position.h> #include <uORB/topics/vehicle_status.h> +#include <drivers/drv_hrt.h> + /* FrSky sensor hub data IDs */ #define FRSKY_ID_GPS_ALT_BP 0x01 #define FRSKY_ID_TEMP1 0x02 @@ -225,7 +227,7 @@ void frsky_send_frame2(int uart) float course = 0, lat = 0, lon = 0, speed = 0, alt = 0; char lat_ns = 0, lon_ew = 0; int sec = 0; - if (global_pos.global_valid) { + if (global_pos.timestamp != 0 && hrt_absolute_time() < global_pos.timestamp + 20000) { time_t time_gps = global_pos.time_gps_usec / 1000000; struct tm *tm_gps = gmtime(&time_gps); diff --git a/src/drivers/frsky_telemetry/frsky_telemetry.c b/src/drivers/frsky_telemetry/frsky_telemetry.c index 7b08ca69e..6e0839043 100644 --- a/src/drivers/frsky_telemetry/frsky_telemetry.c +++ b/src/drivers/frsky_telemetry/frsky_telemetry.c @@ -222,7 +222,7 @@ int frsky_telemetry_main(int argc, char *argv[]) frsky_task = task_spawn_cmd("frsky_telemetry", SCHED_DEFAULT, SCHED_PRIORITY_DEFAULT, - 2048, + 2000, frsky_telemetry_thread_main, (const char **)argv); diff --git a/src/drivers/frsky_telemetry/module.mk b/src/drivers/frsky_telemetry/module.mk index 1632c74f7..9a49589ee 100644 --- a/src/drivers/frsky_telemetry/module.mk +++ b/src/drivers/frsky_telemetry/module.mk @@ -39,3 +39,5 @@ MODULE_COMMAND = frsky_telemetry SRCS = frsky_data.c \ frsky_telemetry.c + +MODULE_STACKSIZE = 1200 diff --git a/src/drivers/gps/gps.cpp b/src/drivers/gps/gps.cpp index c72f692d7..6195cd6ea 100644 --- a/src/drivers/gps/gps.cpp +++ b/src/drivers/gps/gps.cpp @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -56,6 +56,7 @@ #include <arch/board/board.h> #include <drivers/drv_hrt.h> #include <drivers/device/i2c.h> +#include <systemlib/systemlib.h> #include <systemlib/perf_counter.h> #include <systemlib/scheduling_priorities.h> #include <systemlib/err.h> @@ -63,6 +64,8 @@ #include <uORB/uORB.h> #include <uORB/topics/vehicle_gps_position.h> +#include <board_config.h> + #include "ubx.h" #include "mtk.h" @@ -76,12 +79,6 @@ #endif static const int ERROR = -1; -#ifndef CONFIG_SCHED_WORKQUEUE -# error This requires CONFIG_SCHED_WORKQUEUE. -#endif - - - class GPS : public device::CDev { public: @@ -209,7 +206,8 @@ GPS::init() goto out; /* start the GPS driver worker task */ - _task = task_create("gps", SCHED_PRIORITY_SLOW_DRIVER, 2048, (main_t)&GPS::task_main_trampoline, nullptr); + _task = task_spawn_cmd("gps", SCHED_DEFAULT, + SCHED_PRIORITY_SLOW_DRIVER, 2000, (main_t)&GPS::task_main_trampoline, nullptr); if (_task < 0) { warnx("task start failed: %d", errno); @@ -276,14 +274,14 @@ GPS::task_main() _report.timestamp_position = hrt_absolute_time(); _report.lat = (int32_t)47.378301e7f; _report.lon = (int32_t)8.538777e7f; - _report.alt = (int32_t)400e3f; + _report.alt = (int32_t)1200e3f; _report.timestamp_variance = hrt_absolute_time(); _report.s_variance_m_s = 10.0f; _report.p_variance_m = 10.0f; _report.c_variance_rad = 0.1f; _report.fix_type = 3; - _report.eph_m = 10.0f; - _report.epv_m = 10.0f; + _report.eph_m = 0.9f; + _report.epv_m = 1.8f; _report.timestamp_velocity = hrt_absolute_time(); _report.vel_n_m_s = 0.0f; _report.vel_e_m_s = 0.0f; @@ -421,7 +419,14 @@ GPS::task_main() void GPS::cmd_reset() { - //XXX add reset? +#ifdef GPIO_GPS_NRESET + warnx("Toggling GPS reset pin"); + stm32_configgpio(GPIO_GPS_NRESET); + stm32_gpiowrite(GPIO_GPS_NRESET, 0); + usleep(100); + stm32_gpiowrite(GPIO_GPS_NRESET, 1); + warnx("Toggled GPS reset pin"); +#endif } void diff --git a/src/drivers/gps/module.mk b/src/drivers/gps/module.mk index 82c67d40a..eb382c4b2 100644 --- a/src/drivers/gps/module.mk +++ b/src/drivers/gps/module.mk @@ -41,3 +41,5 @@ SRCS = gps.cpp \ gps_helper.cpp \ mtk.cpp \ ubx.cpp + +MODULE_STACKSIZE = 1200 diff --git a/src/drivers/hil/hil.cpp b/src/drivers/hil/hil.cpp index 0a047f38f..55cc077fb 100644 --- a/src/drivers/hil/hil.cpp +++ b/src/drivers/hil/hil.cpp @@ -122,7 +122,7 @@ private: actuator_controls_s _controls; static void task_main_trampoline(int argc, char *argv[]); - void task_main() __attribute__((noreturn)); + void task_main(); static int control_callback(uintptr_t handle, uint8_t control_group, diff --git a/src/drivers/hmc5883/hmc5883.cpp b/src/drivers/hmc5883/hmc5883.cpp index 4c85c0cda..fddba806e 100644 --- a/src/drivers/hmc5883/hmc5883.cpp +++ b/src/drivers/hmc5883/hmc5883.cpp @@ -158,6 +158,7 @@ private: int _class_instance; orb_advert_t _mag_topic; + orb_advert_t _subsystem_pub; perf_counter_t _sample_perf; perf_counter_t _comms_errors; @@ -169,6 +170,8 @@ private: int _bus; /**< the bus the device is connected to */ + struct mag_report _last_report; /**< used for info() */ + /** * Test whether the device supported by the driver is present at a * specific address. @@ -322,7 +325,9 @@ HMC5883::HMC5883(int bus) : _reports(nullptr), _range_scale(0), /* default range scale from counts to gauss */ _range_ga(1.3f), + _collect_phase(false), _mag_topic(-1), + _subsystem_pub(-1), _class_instance(-1), _sample_perf(perf_alloc(PC_ELAPSED, "hmc5883_read")), _comms_errors(perf_alloc(PC_COUNT, "hmc5883_comms_errors")), @@ -713,7 +718,7 @@ HMC5883::cycle() /* perform collection */ if (OK != collect()) { - log("collection error"); + debug("collection error"); /* restart the measurement state machine */ start(); return; @@ -740,7 +745,7 @@ HMC5883::cycle() /* measurement phase */ if (OK != measure()) - log("measure error"); + debug("measure error"); /* next phase is collection */ _collect_phase = true; @@ -870,6 +875,8 @@ HMC5883::collect() } } + _last_report = new_report; + /* post a report to the ring */ if (_reports->force(&new_report)) { perf_count(_buffer_overflows); @@ -1042,31 +1049,28 @@ int HMC5883::calibrate(struct file *filp, unsigned enable) warnx("axes scaling: %.6f %.6f %.6f", (double)scaling[0], (double)scaling[1], (double)scaling[2]); - /* set back to normal mode */ - /* Set to 1.1 Gauss */ - if (OK != ::ioctl(fd, MAGIOCSRANGE, 1)) { - warnx("failed to set 1.1 Ga range"); - goto out; - } - - if (OK != ::ioctl(fd, MAGIOCEXSTRAP, 0)) { - warnx("failed to disable sensor calibration mode"); - goto out; - } - /* set scaling in device */ mscale_previous.x_scale = scaling[0]; mscale_previous.y_scale = scaling[1]; mscale_previous.z_scale = scaling[2]; + ret = OK; + +out: + if (OK != ioctl(filp, MAGIOCSSCALE, (long unsigned int)&mscale_previous)) { warn("WARNING: failed to set new scale / offsets for mag"); - goto out; } - ret = OK; + /* set back to normal mode */ + /* Set to 1.1 Gauss */ + if (OK != ::ioctl(fd, MAGIOCSRANGE, 1)) { + warnx("failed to set 1.1 Ga range"); + } -out: + if (OK != ::ioctl(fd, MAGIOCEXSTRAP, 0)) { + warnx("failed to disable sensor calibration mode"); + } if (ret == OK) { if (!check_scale()) { @@ -1136,13 +1140,12 @@ int HMC5883::check_calibration() true, _calibrated, SUBSYSTEM_TYPE_MAG}; - static orb_advert_t pub = -1; if (!(_pub_blocked)) { - if (pub > 0) { - orb_publish(ORB_ID(subsystem_info), pub, &info); + if (_subsystem_pub > 0) { + orb_publish(ORB_ID(subsystem_info), _subsystem_pub, &info); } else { - pub = orb_advertise(ORB_ID(subsystem_info), &info); + _subsystem_pub = orb_advertise(ORB_ID(subsystem_info), &info); } } } @@ -1221,6 +1224,7 @@ HMC5883::print_info() perf_print_counter(_comms_errors); perf_print_counter(_buffer_overflows); printf("poll interval: %u ticks\n", _measure_ticks); + printf("output (%.2f %.2f %.2f)\n", (double)_last_report.x, (double)_last_report.y, (double)_last_report.z); printf("offsets (%.2f %.2f %.2f)\n", (double)_scale.x_offset, (double)_scale.y_offset, (double)_scale.z_offset); printf("scaling (%.2f %.2f %.2f) 1/range_scale %.2f range_ga %.2f\n", (double)_scale.x_scale, (double)_scale.y_scale, (double)_scale.z_scale, diff --git a/src/drivers/hott/messages.cpp b/src/drivers/hott/messages.cpp index 90a744015..1e779e8dc 100644 --- a/src/drivers/hott/messages.cpp +++ b/src/drivers/hott/messages.cpp @@ -51,6 +51,8 @@ #include <uORB/topics/sensor_combined.h> #include <uORB/topics/vehicle_gps_position.h> +#include <drivers/drv_hrt.h> + /* The board is very roughly 5 deg warmer than the surrounding air */ #define BOARD_TEMP_OFFSET_DEG 5 @@ -62,7 +64,6 @@ static int _airspeed_sub = -1; static int _esc_sub = -1; static orb_advert_t _esc_pub; -struct esc_status_s _esc; static bool _home_position_set = false; static double _home_lat = 0.0d; @@ -82,8 +83,6 @@ init_sub_messages(void) void init_pub_messages(void) { - memset(&_esc, 0, sizeof(_esc)); - _esc_pub = orb_advertise(ORB_ID(esc_status), &_esc); } void @@ -106,23 +105,26 @@ publish_gam_message(const uint8_t *buffer) size_t size = sizeof(msg); memset(&msg, 0, size); memcpy(&msg, buffer, size); + struct esc_status_s esc; + memset(&esc, 0, sizeof(esc)); + + // Publish it. + esc.timestamp = hrt_absolute_time(); + esc.esc_count = 1; + esc.esc_connectiontype = ESC_CONNECTION_TYPE_PPM; + + esc.esc[0].esc_vendor = ESC_VENDOR_GRAUPNER_HOTT; + esc.esc[0].esc_rpm = (uint16_t)((msg.rpm_H << 8) | (msg.rpm_L & 0xff)) * 10; + esc.esc[0].esc_temperature = msg.temperature1 - 20; + esc.esc[0].esc_voltage = (uint16_t)((msg.main_voltage_H << 8) | (msg.main_voltage_L & 0xff)); + esc.esc[0].esc_current = (uint16_t)((msg.current_H << 8) | (msg.current_L & 0xff)); /* announce the esc if needed, just publish else */ if (_esc_pub > 0) { - orb_publish(ORB_ID(esc_status), _esc_pub, &_esc); + orb_publish(ORB_ID(esc_status), _esc_pub, &esc); } else { - _esc_pub = orb_advertise(ORB_ID(esc_status), &_esc); + _esc_pub = orb_advertise(ORB_ID(esc_status), &esc); } - - // Publish it. - _esc.esc_count = 1; - _esc.esc_connectiontype = ESC_CONNECTION_TYPE_PPM; - - _esc.esc[0].esc_vendor = ESC_VENDOR_GRAUPNER_HOTT; - _esc.esc[0].esc_rpm = (uint16_t)((msg.rpm_H << 8) | (msg.rpm_L & 0xff)) * 10; - _esc.esc[0].esc_temperature = msg.temperature1 - 20; - _esc.esc[0].esc_voltage = (uint16_t)((msg.main_voltage_H << 8) | (msg.main_voltage_L & 0xff)); - _esc.esc[0].esc_current = (uint16_t)((msg.current_H << 8) | (msg.current_L & 0xff)); } void diff --git a/src/drivers/l3gd20/l3gd20.cpp b/src/drivers/l3gd20/l3gd20.cpp index 90c3db9ae..37e72388b 100644 --- a/src/drivers/l3gd20/l3gd20.cpp +++ b/src/drivers/l3gd20/l3gd20.cpp @@ -34,6 +34,9 @@ /** * @file l3gd20.cpp * Driver for the ST L3GD20 MEMS gyro connected via SPI. + * + * Note: With the exception of the self-test feature, the ST L3G4200D is + * also supported by this driver. */ #include <nuttx/config.h> @@ -89,9 +92,11 @@ static const int ERROR = -1; #define ADDR_WHO_AM_I 0x0F #define WHO_I_AM_H 0xD7 #define WHO_I_AM 0xD4 +#define WHO_I_AM_L3G4200D 0xD3 /* for L3G4200D */ #define ADDR_CTRL_REG1 0x20 #define REG1_RATE_LP_MASK 0xF0 /* Mask to guard partial register update */ + /* keep lowpass low to avoid noise issues */ #define RATE_95HZ_LP_25HZ ((0<<7) | (0<<6) | (0<<5) | (1<<4)) #define RATE_190HZ_LP_25HZ ((0<<7) | (1<<6) | (0<<5) | (1<<4)) @@ -166,9 +171,14 @@ static const int ERROR = -1; #define FIFO_CTRL_BYPASS_TO_STREAM_MODE (1<<7) #define L3GD20_DEFAULT_RATE 760 +#define L3G4200D_DEFAULT_RATE 800 #define L3GD20_DEFAULT_RANGE_DPS 2000 #define L3GD20_DEFAULT_FILTER_FREQ 30 +#ifndef SENSOR_BOARD_ROTATION_DEFAULT +#define SENSOR_BOARD_ROTATION_DEFAULT SENSOR_BOARD_ROTATION_270_DEG +#endif + extern "C" { __EXPORT int l3gd20_main(int argc, char *argv[]); } class L3GD20 : public device::SPI @@ -216,6 +226,9 @@ private: math::LowPassFilter2p _gyro_filter_y; math::LowPassFilter2p _gyro_filter_z; + /* true if an L3G4200D is detected */ + bool _is_l3g4200d; + /** * Start automatic measurement. */ @@ -324,14 +337,15 @@ L3GD20::L3GD20(int bus, const char* path, spi_dev_e device) : _gyro_topic(-1), _class_instance(-1), _current_rate(0), - _orientation(SENSOR_BOARD_ROTATION_270_DEG), + _orientation(SENSOR_BOARD_ROTATION_DEFAULT), _read(0), _sample_perf(perf_alloc(PC_ELAPSED, "l3gd20_read")), _reschedules(perf_alloc(PC_COUNT, "l3gd20_reschedules")), _errors(perf_alloc(PC_COUNT, "l3gd20_errors")), _gyro_filter_x(L3GD20_DEFAULT_RATE, L3GD20_DEFAULT_FILTER_FREQ), _gyro_filter_y(L3GD20_DEFAULT_RATE, L3GD20_DEFAULT_FILTER_FREQ), - _gyro_filter_z(L3GD20_DEFAULT_RATE, L3GD20_DEFAULT_FILTER_FREQ) + _gyro_filter_z(L3GD20_DEFAULT_RATE, L3GD20_DEFAULT_FILTER_FREQ), + _is_l3g4200d(false) { // enable debug() calls _debug_enabled = true; @@ -413,14 +427,7 @@ L3GD20::probe() /* verify that the device is attached and functioning, accept L3GD20 and L3GD20H */ if (read_reg(ADDR_WHO_AM_I) == WHO_I_AM) { - #ifdef CONFIG_ARCH_BOARD_PX4FMU_V1 - _orientation = SENSOR_BOARD_ROTATION_270_DEG; - #elif CONFIG_ARCH_BOARD_PX4FMU_V2 - _orientation = SENSOR_BOARD_ROTATION_270_DEG; - #else - #error This driver needs a board selection, either CONFIG_ARCH_BOARD_PX4FMU_V1 or CONFIG_ARCH_BOARD_PX4FMU_V2 - #endif - + _orientation = SENSOR_BOARD_ROTATION_DEFAULT; success = true; } @@ -430,6 +437,13 @@ L3GD20::probe() success = true; } + /* Detect the L3G4200D used on AeroCore */ + if (read_reg(ADDR_WHO_AM_I) == WHO_I_AM_L3G4200D) { + _is_l3g4200d = true; + _orientation = SENSOR_BOARD_ROTATION_DEFAULT; + success = true; + } + if (success) return OK; @@ -502,6 +516,9 @@ L3GD20::ioctl(struct file *filp, int cmd, unsigned long arg) /* set default/max polling rate */ case SENSOR_POLLRATE_MAX: case SENSOR_POLLRATE_DEFAULT: + if (_is_l3g4200d) { + return ioctl(filp, SENSORIOCSPOLLRATE, L3G4200D_DEFAULT_RATE); + } return ioctl(filp, SENSORIOCSPOLLRATE, L3GD20_DEFAULT_RATE); /* adjust to a legal polling interval in Hz */ @@ -683,23 +700,26 @@ L3GD20::set_samplerate(unsigned frequency) uint8_t bits = REG1_POWER_NORMAL | REG1_Z_ENABLE | REG1_Y_ENABLE | REG1_X_ENABLE; if (frequency == 0) - frequency = 760; + frequency = _is_l3g4200d ? 800 : 760; - /* use limits good for H or non-H models */ + /* + * Use limits good for H or non-H models. Rates are slightly different + * for L3G4200D part but register settings are the same. + */ if (frequency <= 100) { - _current_rate = 95; + _current_rate = _is_l3g4200d ? 100 : 95; bits |= RATE_95HZ_LP_25HZ; } else if (frequency <= 200) { - _current_rate = 190; + _current_rate = _is_l3g4200d ? 200 : 190; bits |= RATE_190HZ_LP_50HZ; } else if (frequency <= 400) { - _current_rate = 380; + _current_rate = _is_l3g4200d ? 400 : 380; bits |= RATE_380HZ_LP_50HZ; } else if (frequency <= 800) { - _current_rate = 760; + _current_rate = _is_l3g4200d ? 800 : 760; bits |= RATE_760HZ_LP_50HZ; } else { return -EINVAL; @@ -772,7 +792,7 @@ L3GD20::reset() * callback fast enough to not miss data. */ write_reg(ADDR_FIFO_CTRL_REG, FIFO_CTRL_BYPASS_MODE); - set_samplerate(0); // 760Hz + set_samplerate(0); // 760Hz or 800Hz set_range(L3GD20_DEFAULT_RANGE_DPS); set_driver_lowpass_filter(L3GD20_DEFAULT_RATE, L3GD20_DEFAULT_FILTER_FREQ); @@ -971,7 +991,7 @@ start() errx(0, "already started"); /* create the driver */ - g_dev = new L3GD20(1 /* SPI bus 1 */, L3GD20_DEVICE_PATH, (spi_dev_e)PX4_SPIDEV_GYRO); + g_dev = new L3GD20(PX4_SPI_BUS_SENSORS, L3GD20_DEVICE_PATH, (spi_dev_e)PX4_SPIDEV_GYRO); if (g_dev == nullptr) goto fail; diff --git a/src/drivers/lsm303d/lsm303d.cpp b/src/drivers/lsm303d/lsm303d.cpp index 4dee7649b..4ca8b5e42 100644 --- a/src/drivers/lsm303d/lsm303d.cpp +++ b/src/drivers/lsm303d/lsm303d.cpp @@ -1793,7 +1793,7 @@ start() errx(0, "already started"); /* create the driver */ - g_dev = new LSM303D(1 /* SPI dev 1 */, LSM303D_DEVICE_PATH_ACCEL, (spi_dev_e)PX4_SPIDEV_ACCEL_MAG); + g_dev = new LSM303D(PX4_SPI_BUS_SENSORS, LSM303D_DEVICE_PATH_ACCEL, (spi_dev_e)PX4_SPIDEV_ACCEL_MAG); if (g_dev == nullptr) { warnx("failed instantiating LSM303D obj"); diff --git a/src/drivers/meas_airspeed/meas_airspeed.cpp b/src/drivers/meas_airspeed/meas_airspeed.cpp index beca28e7a..c0f3c28e0 100644 --- a/src/drivers/meas_airspeed/meas_airspeed.cpp +++ b/src/drivers/meas_airspeed/meas_airspeed.cpp @@ -79,12 +79,15 @@ #include <systemlib/param/param.h> #include <systemlib/perf_counter.h> +#include <mathlib/math/filter/LowPassFilter2p.hpp> + #include <drivers/drv_airspeed.h> #include <drivers/drv_hrt.h> #include <uORB/uORB.h> #include <uORB/topics/differential_pressure.h> #include <uORB/topics/subsystem_info.h> +#include <uORB/topics/system_power.h> #include <drivers/airspeed/airspeed.h> @@ -99,6 +102,8 @@ #define ADDR_READ_MR 0x00 /* write to this address to start conversion */ /* Measurement rate is 100Hz */ +#define MEAS_RATE 100.0f +#define MEAS_DRIVER_FILTER_FREQ 3.0f #define CONVERSION_INTERVAL (1000000 / 100) /* microseconds */ class MEASAirspeed : public Airspeed @@ -116,6 +121,15 @@ protected: virtual int measure(); virtual int collect(); + math::LowPassFilter2p _filter; + + /** + * Correct for 5V rail voltage variations + */ + void voltage_correction(float &diff_pres_pa, float &temperature); + + int _t_system_power; + struct system_power_s system_power; }; /* @@ -124,9 +138,11 @@ protected: extern "C" __EXPORT int meas_airspeed_main(int argc, char *argv[]); MEASAirspeed::MEASAirspeed(int bus, int address, const char *path) : Airspeed(bus, address, - CONVERSION_INTERVAL, path) + CONVERSION_INTERVAL, path), + _filter(MEAS_RATE, MEAS_DRIVER_FILTER_FREQ), + _t_system_power(-1) { - + memset(&system_power, 0, sizeof(system_power)); } int @@ -188,19 +204,48 @@ MEASAirspeed::collect() dp_raw = 0x3FFF & dp_raw; dT_raw = (val[2] << 8) + val[3]; dT_raw = (0xFFE0 & dT_raw) >> 5; - float temperature = ((200 * dT_raw) / 2047) - 50; + float temperature = ((200.0f * dT_raw) / 2047) - 50; - /* calculate differential pressure. As its centered around 8000 - * and can go positive or negative, enforce absolute value - */ + // Calculate differential pressure. As its centered around 8000 + // and can go positive or negative const float P_min = -1.0f; const float P_max = 1.0f; - float diff_press_pa = fabsf((((float)dp_raw - 0.1f * 16383.0f) * (P_max - P_min) / (0.8f * 16383.0f) + P_min) * 6894.8f) - _diff_pres_offset; + const float PSI_to_Pa = 6894.757f; + /* + this equation is an inversion of the equation in the + pressure transfer function figure on page 4 of the datasheet - if (diff_press_pa < 0.0f) { - diff_press_pa = 0.0f; - } + We negate the result so that positive differential pressures + are generated when the bottom port is used as the static + port on the pitot and top port is used as the dynamic port + */ + float diff_press_PSI = -((dp_raw - 0.1f*16383) * (P_max-P_min)/(0.8f*16383) + P_min); + float diff_press_pa_raw = diff_press_PSI * PSI_to_Pa; + // correct for 5V rail voltage if possible + voltage_correction(diff_press_pa_raw, temperature); + + float diff_press_pa = fabsf(diff_press_pa_raw - _diff_pres_offset); + + /* + note that we return both the absolute value with offset + applied and a raw value without the offset applied. This + makes it possible for higher level code to detect if the + user has the tubes connected backwards, and also makes it + possible to correctly use offsets calculated by a higher + level airspeed driver. + + With the above calculation the MS4525 sensor will produce a + positive number when the top port is used as a dynamic port + and bottom port is used as the static port + + Also note that the _diff_pres_offset is applied before the + fabsf() not afterwards. It needs to be done this way to + prevent a bias at low speeds, but this also means that when + setting a offset you must set it based on the raw value, not + the offset value + */ + struct differential_pressure_s report; /* track maximum differential pressure measured (so we can work out top speed). */ @@ -212,6 +257,14 @@ MEASAirspeed::collect() report.error_count = perf_event_count(_comms_errors); report.temperature = temperature; report.differential_pressure_pa = diff_press_pa; + report.differential_pressure_filtered_pa = _filter.apply(diff_press_pa); + + /* the dynamics of the filter can make it overshoot into the negative range */ + if (report.differential_pressure_filtered_pa < 0.0f) { + report.differential_pressure_filtered_pa = _filter.reset(diff_press_pa); + } + + report.differential_pressure_raw_pa = diff_press_pa_raw; report.voltage = 0; report.max_differential_pressure_pa = _max_differential_pressure_pa; @@ -235,13 +288,17 @@ MEASAirspeed::collect() void MEASAirspeed::cycle() { + int ret; + /* collection phase? */ if (_collect_phase) { /* perform collection */ - if (OK != collect()) { + ret = collect(); + if (OK != ret) { /* restart the measurement state machine */ start(); + _sensor_ok = false; return; } @@ -265,10 +322,13 @@ MEASAirspeed::cycle() } /* measurement phase */ - if (OK != measure()) { - log("measure error"); + ret = measure(); + if (OK != ret) { + debug("measure error"); } + _sensor_ok = (ret == OK); + /* next phase is collection */ _collect_phase = true; @@ -281,6 +341,62 @@ MEASAirspeed::cycle() } /** + correct for 5V rail voltage if the system_power ORB topic is + available + + See http://uav.tridgell.net/MS4525/MS4525-offset.png for a graph of + offset versus voltage for 3 sensors + */ +void +MEASAirspeed::voltage_correction(float &diff_press_pa, float &temperature) +{ +#ifdef CONFIG_ARCH_BOARD_PX4FMU_V2 + if (_t_system_power == -1) { + _t_system_power = orb_subscribe(ORB_ID(system_power)); + } + if (_t_system_power == -1) { + // not available + return; + } + bool updated = false; + orb_check(_t_system_power, &updated); + if (updated) { + orb_copy(ORB_ID(system_power), _t_system_power, &system_power); + } + if (system_power.voltage5V_v < 3.0f || system_power.voltage5V_v > 6.0f) { + // not valid, skip correction + return; + } + + const float slope = 65.0f; + /* + apply a piecewise linear correction, flattening at 0.5V from 5V + */ + float voltage_diff = system_power.voltage5V_v - 5.0f; + if (voltage_diff > 0.5f) { + voltage_diff = 0.5f; + } + if (voltage_diff < -0.5f) { + voltage_diff = -0.5f; + } + diff_press_pa -= voltage_diff * slope; + + /* + the temperature masurement varies as well + */ + const float temp_slope = 0.887f; + voltage_diff = system_power.voltage5V_v - 5.0f; + if (voltage_diff > 0.5f) { + voltage_diff = 0.5f; + } + if (voltage_diff < -1.0f) { + voltage_diff = -1.0f; + } + temperature -= voltage_diff * temp_slope; +#endif // CONFIG_ARCH_BOARD_PX4FMU_V2 +} + +/** * Local functions in support of the shell command. */ namespace meas_airspeed @@ -402,7 +518,7 @@ test() } warnx("single read"); - warnx("diff pressure: %8.4f pa", (double)report.differential_pressure_pa); + warnx("diff pressure: %d pa", (int)report.differential_pressure_pa); /* start the sensor polling at 2Hz */ if (OK != ioctl(fd, SENSORIOCSPOLLRATE, 2)) { @@ -430,7 +546,7 @@ test() } warnx("periodic read %u", i); - warnx("diff pressure: %8.4f pa", (double)report.differential_pressure_pa); + warnx("diff pressure: %d pa", (int)report.differential_pressure_pa); warnx("temperature: %d C (0x%02x)", (int)report.temperature, (unsigned) report.temperature); } diff --git a/src/drivers/mkblctrl/mkblctrl.cpp b/src/drivers/mkblctrl/mkblctrl.cpp index 705e98eea..5954c40da 100644 --- a/src/drivers/mkblctrl/mkblctrl.cpp +++ b/src/drivers/mkblctrl/mkblctrl.cpp @@ -92,8 +92,20 @@ #define MOTOR_SPINUP_COUNTER 30 #define ESC_UORB_PUBLISH_DELAY 500000 - - +struct MotorData_t { + unsigned int Version; // the version of the BL (0 = old) + unsigned int SetPoint; // written by attitude controller + unsigned int SetPointLowerBits; // for higher Resolution of new BLs + float SetPoint_PX4; // Values from PX4 + unsigned int State; // 7 bit for I2C error counter, highest bit indicates if motor is present + unsigned int ReadMode; // select data to read + unsigned short RawPwmValue; // length of PWM pulse + // the following bytes must be exactly in that order! + unsigned int Current; // in 0.1 A steps, read back from BL + unsigned int MaxPWM; // read back from BL is less than 255 if BL is in current limit + unsigned int Temperature; // old BL-Ctrl will return a 255 here, the new version the temp. in + unsigned int RoundCount; +}; class MK : public device::I2C { @@ -154,8 +166,10 @@ private: actuator_controls_s _controls; + MotorData_t Motor[MAX_MOTORS]; + static void task_main_trampoline(int argc, char *argv[]); - void task_main() __attribute__((noreturn)); + void task_main(); static int control_callback(uintptr_t handle, uint8_t control_group, @@ -195,24 +209,6 @@ const int blctrlAddr_px4[] = { 0, 0, 0, 0, 0, 0, 0, 0}; int addrTranslator[] = {0, 0, 0, 0, 0, 0, 0, 0}; -struct MotorData_t { - unsigned int Version; // the version of the BL (0 = old) - unsigned int SetPoint; // written by attitude controller - unsigned int SetPointLowerBits; // for higher Resolution of new BLs - float SetPoint_PX4; // Values from PX4 - unsigned int State; // 7 bit for I2C error counter, highest bit indicates if motor is present - unsigned int ReadMode; // select data to read - unsigned short RawPwmValue; // length of PWM pulse - // the following bytes must be exactly in that order! - unsigned int Current; // in 0.1 A steps, read back from BL - unsigned int MaxPWM; // read back from BL is less than 255 if BL is in current limit - unsigned int Temperature; // old BL-Ctrl will return a 255 here, the new version the temp. in - unsigned int RoundCount; -}; - -MotorData_t Motor[MAX_MOTORS]; - - namespace { @@ -1015,7 +1011,7 @@ MK::pwm_ioctl(file *filp, int cmd, unsigned long arg) case PWM_SERVO_GET(0) ... PWM_SERVO_GET(_max_actuators - 1): /* copy the current output value from the channel */ - *(servo_position_t *)arg = Motor[cmd - PWM_SERVO_SET(0)].RawPwmValue; + *(servo_position_t *)arg = Motor[cmd - PWM_SERVO_GET(0)].RawPwmValue; break; diff --git a/src/drivers/ms5611/ms5611.cpp b/src/drivers/ms5611/ms5611.cpp index 0ef056273..3fe1b0abc 100644 --- a/src/drivers/ms5611/ms5611.cpp +++ b/src/drivers/ms5611/ms5611.cpp @@ -526,6 +526,7 @@ void MS5611::cycle() { int ret; + unsigned dummy; /* collection phase? */ if (_collect_phase) { @@ -542,6 +543,8 @@ MS5611::cycle() } else { //log("collection error %d", ret); } + /* issue a reset command to the sensor */ + _interface->ioctl(IOCTL_RESET, dummy); /* reset the collection state machine and try again */ start_cycle(); return; @@ -573,6 +576,8 @@ MS5611::cycle() ret = measure(); if (ret != OK) { //log("measure error %d", ret); + /* issue a reset command to the sensor */ + _interface->ioctl(IOCTL_RESET, dummy); /* reset the collection state machine and try again */ start_cycle(); return; diff --git a/src/drivers/ms5611/ms5611_spi.cpp b/src/drivers/ms5611/ms5611_spi.cpp index 26216e840..8759d16a1 100644 --- a/src/drivers/ms5611/ms5611_spi.cpp +++ b/src/drivers/ms5611/ms5611_spi.cpp @@ -117,7 +117,7 @@ private: device::Device * MS5611_spi_interface(ms5611::prom_u &prom_buf) { - return new MS5611_SPI(1 /* XXX MAGIC NUMBER */, (spi_dev_e)PX4_SPIDEV_BARO, prom_buf); + return new MS5611_SPI(PX4_SPI_BUS_SENSORS, (spi_dev_e)PX4_SPIDEV_BARO, prom_buf); } MS5611_SPI::MS5611_SPI(int bus, spi_dev_e device, ms5611::prom_u &prom_buf) : diff --git a/src/drivers/px4fmu/fmu.cpp b/src/drivers/px4fmu/fmu.cpp index a70ff6c5c..fd69cf795 100644 --- a/src/drivers/px4fmu/fmu.cpp +++ b/src/drivers/px4fmu/fmu.cpp @@ -92,6 +92,7 @@ public: MODE_2PWM, MODE_4PWM, MODE_6PWM, + MODE_8PWM, }; PX4FMU(); virtual ~PX4FMU(); @@ -113,6 +114,9 @@ private: #if defined(CONFIG_ARCH_BOARD_PX4FMU_V2) static const unsigned _max_actuators = 6; #endif +#if defined(CONFIG_ARCH_BOARD_AEROCORE) + static const unsigned _max_actuators = 8; +#endif Mode _mode; unsigned _pwm_default_rate; @@ -120,19 +124,25 @@ private: uint32_t _pwm_alt_rate_channels; unsigned _current_update_rate; int _task; - int _t_actuators; - int _t_actuator_armed; - orb_advert_t _t_outputs; + int _armed_sub; + orb_advert_t _outputs_pub; + actuator_armed_s _armed; unsigned _num_outputs; bool _primary_pwm_device; volatile bool _task_should_exit; - bool _armed; + bool _servo_armed; bool _pwm_on; MixerGroup *_mixers; - actuator_controls_s _controls; + uint32_t _groups_required; + uint32_t _groups_subscribed; + int _control_subs[NUM_ACTUATOR_CONTROL_GROUPS]; + actuator_controls_s _controls[NUM_ACTUATOR_CONTROL_GROUPS]; + orb_id_t _control_topics[NUM_ACTUATOR_CONTROL_GROUPS]; + pollfd _poll_fds[NUM_ACTUATOR_CONTROL_GROUPS]; + unsigned _poll_fds_num; pwm_limit_t _pwm_limit; uint16_t _failsafe_pwm[_max_actuators]; @@ -143,13 +153,13 @@ private: unsigned _num_disarmed_set; static void task_main_trampoline(int argc, char *argv[]); - void task_main() __attribute__((noreturn)); + void task_main(); static int control_callback(uintptr_t handle, uint8_t control_group, uint8_t control_index, float &input); - + void subscribe(); int set_pwm_rate(unsigned rate_map, unsigned default_rate, unsigned alt_rate); int pwm_ioctl(file *filp, int cmd, unsigned long arg); @@ -197,6 +207,20 @@ const PX4FMU::GPIOConfig PX4FMU::_gpio_tab[] = { {GPIO_VDD_5V_HIPOWER_OC, 0, 0}, {GPIO_VDD_5V_PERIPH_OC, 0, 0}, #endif +#if defined(CONFIG_ARCH_BOARD_AEROCORE) + /* AeroCore breaks out User GPIOs on J11 */ + {GPIO_GPIO0_INPUT, GPIO_GPIO0_OUTPUT, 0}, + {GPIO_GPIO1_INPUT, GPIO_GPIO1_OUTPUT, 0}, + {GPIO_GPIO3_INPUT, GPIO_GPIO3_OUTPUT, 0}, + {GPIO_GPIO4_INPUT, GPIO_GPIO4_OUTPUT, 0}, + {GPIO_GPIO5_INPUT, GPIO_GPIO5_OUTPUT, 0}, + {GPIO_GPIO6_INPUT, GPIO_GPIO6_OUTPUT, 0}, + {GPIO_GPIO7_INPUT, GPIO_GPIO7_OUTPUT, 0}, + {GPIO_GPIO8_INPUT, GPIO_GPIO8_OUTPUT, 0}, + {GPIO_GPIO9_INPUT, GPIO_GPIO9_OUTPUT, 0}, + {GPIO_GPIO10_INPUT, GPIO_GPIO10_OUTPUT, 0}, + {GPIO_GPIO11_INPUT, GPIO_GPIO11_OUTPUT, 0}, +#endif }; const unsigned PX4FMU::_ngpio = sizeof(PX4FMU::_gpio_tab) / sizeof(PX4FMU::_gpio_tab[0]); @@ -216,15 +240,18 @@ PX4FMU::PX4FMU() : _pwm_alt_rate_channels(0), _current_update_rate(0), _task(-1), - _t_actuators(-1), - _t_actuator_armed(-1), - _t_outputs(0), + _control_subs({-1}), + _poll_fds_num(0), + _armed_sub(-1), + _outputs_pub(-1), _num_outputs(0), _primary_pwm_device(false), _task_should_exit(false), - _armed(false), + _servo_armed(false), _pwm_on(false), _mixers(nullptr), + _groups_required(0), + _groups_subscribed(0), _failsafe_pwm({0}), _disarmed_pwm({0}), _num_failsafe_set(0), @@ -235,6 +262,14 @@ PX4FMU::PX4FMU() : _max_pwm[i] = PWM_DEFAULT_MAX; } + _control_topics[0] = ORB_ID(actuator_controls_0); + _control_topics[1] = ORB_ID(actuator_controls_1); + _control_topics[2] = ORB_ID(actuator_controls_2); + _control_topics[3] = ORB_ID(actuator_controls_3); + + memset(_controls, 0, sizeof(_controls)); + memset(_poll_fds, 0, sizeof(_poll_fds)); + _debug_enabled = true; } @@ -365,6 +400,20 @@ PX4FMU::set_mode(Mode mode) break; +#ifdef CONFIG_ARCH_BOARD_AEROCORE + case MODE_8PWM: // AeroCore PWMs as 8 PWM outs + debug("MODE_8PWM"); + /* default output rates */ + _pwm_default_rate = 50; + _pwm_alt_rate = 50; + _pwm_alt_rate_channels = 0; + + /* XXX magic numbers */ + up_pwm_servo_init(0xff); + set_pwm_rate(_pwm_alt_rate_channels, _pwm_default_rate, _pwm_alt_rate); + break; +#endif + case MODE_NONE: debug("MODE_NONE"); @@ -448,32 +497,42 @@ PX4FMU::set_pwm_alt_channels(uint32_t channels) } void +PX4FMU::subscribe() +{ + /* subscribe/unsubscribe to required actuator control groups */ + uint32_t sub_groups = _groups_required & ~_groups_subscribed; + uint32_t unsub_groups = _groups_subscribed & ~_groups_required; + _poll_fds_num = 0; + for (unsigned i = 0; i < NUM_ACTUATOR_CONTROL_GROUPS; i++) { + if (sub_groups & (1 << i)) { + warnx("subscribe to actuator_controls_%d", i); + _control_subs[i] = orb_subscribe(_control_topics[i]); + } + if (unsub_groups & (1 << i)) { + warnx("unsubscribe from actuator_controls_%d", i); + ::close(_control_subs[i]); + _control_subs[i] = -1; + } + + if (_control_subs[i] > 0) { + _poll_fds[_poll_fds_num].fd = _control_subs[i]; + _poll_fds[_poll_fds_num].events = POLLIN; + _poll_fds_num++; + } + } +} + +void PX4FMU::task_main() { - /* - * Subscribe to the appropriate PWM output topic based on whether we are the - * primary PWM output or not. - */ - _t_actuators = orb_subscribe(_primary_pwm_device ? ORB_ID_VEHICLE_ATTITUDE_CONTROLS : - ORB_ID(actuator_controls_1)); /* force a reset of the update rate */ _current_update_rate = 0; - _t_actuator_armed = orb_subscribe(ORB_ID(actuator_armed)); - orb_set_interval(_t_actuator_armed, 200); /* 5Hz update rate */ + _armed_sub = orb_subscribe(ORB_ID(actuator_armed)); /* advertise the mixed control outputs */ actuator_outputs_s outputs; memset(&outputs, 0, sizeof(outputs)); - /* advertise the mixed control outputs */ - _t_outputs = orb_advertise(_primary_pwm_device ? ORB_ID_VEHICLE_CONTROLS : ORB_ID(actuator_outputs_1), - &outputs); - - pollfd fds[2]; - fds[0].fd = _t_actuators; - fds[0].events = POLLIN; - fds[1].fd = _t_actuator_armed; - fds[1].events = POLLIN; #ifdef HRT_PPM_CHANNEL // rc input, published to ORB @@ -491,6 +550,12 @@ PX4FMU::task_main() /* loop until killed */ while (!_task_should_exit) { + if (_groups_subscribed != _groups_required) { + subscribe(); + _groups_subscribed = _groups_required; + /* force setting update rate */ + _current_update_rate = 0; + } /* * Adjust actuator topic update rate to keep up with @@ -515,20 +580,23 @@ PX4FMU::task_main() } debug("adjusted actuator update interval to %ums", update_rate_in_ms); - orb_set_interval(_t_actuators, update_rate_in_ms); + for (unsigned i = 0; i < NUM_ACTUATOR_CONTROL_GROUPS; i++) { + if (_control_subs[i] > 0) { + orb_set_interval(_control_subs[i], update_rate_in_ms); + } + } // set to current max rate, even if we are actually checking slower/faster _current_update_rate = max_rate; } /* sleep waiting for data, stopping to check for PPM - * input at 100Hz */ - int ret = ::poll(&fds[0], 2, CONTROL_INPUT_DROP_LIMIT_MS); + * input at 50Hz */ + int ret = ::poll(_poll_fds, _poll_fds_num, CONTROL_INPUT_DROP_LIMIT_MS); /* this would be bad... */ if (ret < 0) { log("poll error %d", errno); - usleep(1000000); continue; } else if (ret == 0) { @@ -537,89 +605,101 @@ PX4FMU::task_main() } else { - /* do we have a control update? */ - if (fds[0].revents & POLLIN) { + /* get controls for required topics */ + unsigned poll_id = 0; + for (unsigned i = 0; i < NUM_ACTUATOR_CONTROL_GROUPS; i++) { + if (_control_subs[i] > 0) { + if (_poll_fds[poll_id].revents & POLLIN) { + orb_copy(_control_topics[i], _control_subs[i], &_controls[i]); + } + poll_id++; + } + } - /* get controls - must always do this to avoid spinning */ - orb_copy(_primary_pwm_device ? ORB_ID_VEHICLE_ATTITUDE_CONTROLS : ORB_ID(actuator_controls_1), _t_actuators, &_controls); + /* can we mix? */ + if (_mixers != nullptr) { - /* can we mix? */ - if (_mixers != nullptr) { + unsigned num_outputs; - unsigned num_outputs; + switch (_mode) { + case MODE_2PWM: + num_outputs = 2; + break; - switch (_mode) { - case MODE_2PWM: - num_outputs = 2; - break; + case MODE_4PWM: + num_outputs = 4; + break; - case MODE_4PWM: - num_outputs = 4; - break; + case MODE_6PWM: + num_outputs = 6; + break; - case MODE_6PWM: - num_outputs = 6; - break; + case MODE_8PWM: + num_outputs = 8; + break; + default: + num_outputs = 0; + break; + } - default: - num_outputs = 0; - break; + /* do mixing */ + outputs.noutputs = _mixers->mix(&outputs.output[0], num_outputs); + outputs.timestamp = hrt_absolute_time(); + + /* iterate actuators */ + for (unsigned i = 0; i < num_outputs; i++) { + /* last resort: catch NaN, INF and out-of-band errors */ + if (i >= outputs.noutputs || + !isfinite(outputs.output[i]) || + outputs.output[i] < -1.0f || + outputs.output[i] > 1.0f) { + /* + * Value is NaN, INF or out of band - set to the minimum value. + * This will be clearly visible on the servo status and will limit the risk of accidentally + * spinning motors. It would be deadly in flight. + */ + outputs.output[i] = -1.0f; } + } - /* do mixing */ - outputs.noutputs = _mixers->mix(&outputs.output[0], num_outputs); - outputs.timestamp = hrt_absolute_time(); - - /* iterate actuators */ - for (unsigned i = 0; i < num_outputs; i++) { - /* last resort: catch NaN, INF and out-of-band errors */ - if (i >= outputs.noutputs || - !isfinite(outputs.output[i]) || - outputs.output[i] < -1.0f || - outputs.output[i] > 1.0f) { - /* - * Value is NaN, INF or out of band - set to the minimum value. - * This will be clearly visible on the servo status and will limit the risk of accidentally - * spinning motors. It would be deadly in flight. - */ - outputs.output[i] = -1.0f; - } - } + uint16_t pwm_limited[num_outputs]; - uint16_t pwm_limited[num_outputs]; + pwm_limit_calc(_servo_armed, num_outputs, _disarmed_pwm, _min_pwm, _max_pwm, outputs.output, pwm_limited, &_pwm_limit); - pwm_limit_calc(_armed, num_outputs, _disarmed_pwm, _min_pwm, _max_pwm, outputs.output, pwm_limited, &_pwm_limit); + /* output to the servos */ + for (unsigned i = 0; i < num_outputs; i++) { + up_pwm_servo_set(i, pwm_limited[i]); + } - /* output to the servos */ - for (unsigned i = 0; i < num_outputs; i++) { - up_pwm_servo_set(i, pwm_limited[i]); - } + /* publish mixed control outputs */ + if (_outputs_pub < 0) { + _outputs_pub = orb_advertise(_primary_pwm_device ? ORB_ID_VEHICLE_CONTROLS : ORB_ID(actuator_outputs_1), &outputs); + } else { - /* and publish for anyone that cares to see */ - orb_publish(_primary_pwm_device ? ORB_ID_VEHICLE_CONTROLS : ORB_ID(actuator_outputs_1), _t_outputs, &outputs); + orb_publish(_primary_pwm_device ? ORB_ID_VEHICLE_CONTROLS : ORB_ID(actuator_outputs_1), _outputs_pub, &outputs); } } + } - /* how about an arming update? */ - if (fds[1].revents & POLLIN) { - actuator_armed_s aa; + /* check arming state */ + bool updated = false; + orb_check(_armed_sub, &updated); - /* get new value */ - orb_copy(ORB_ID(actuator_armed), _t_actuator_armed, &aa); + if (updated) { + orb_copy(ORB_ID(actuator_armed), _armed_sub, &_armed); - /* update the armed status and check that we're not locked down */ - bool set_armed = aa.armed && !aa.lockdown; + /* update the armed status and check that we're not locked down */ + bool set_armed = _armed.armed && !_armed.lockdown; - if (_armed != set_armed) - _armed = set_armed; + if (_servo_armed != set_armed) + _servo_armed = set_armed; - /* update PWM status if armed or if disarmed PWM values are set */ - bool pwm_on = (aa.armed || _num_disarmed_set > 0); + /* update PWM status if armed or if disarmed PWM values are set */ + bool pwm_on = (_armed.armed || _num_disarmed_set > 0); - if (_pwm_on != pwm_on) { - _pwm_on = pwm_on; - up_pwm_servo_arm(pwm_on); - } + if (_pwm_on != pwm_on) { + _pwm_on = pwm_on; + up_pwm_servo_arm(pwm_on); } } @@ -661,8 +741,13 @@ PX4FMU::task_main() } - ::close(_t_actuators); - ::close(_t_actuator_armed); + for (unsigned i = 0; i < NUM_ACTUATOR_CONTROL_GROUPS; i++) { + if (_control_subs > 0) { + ::close(_control_subs[i]); + _control_subs[i] = -1; + } + } + ::close(_armed_sub); /* make sure servos are off */ up_pwm_servo_deinit(); @@ -684,7 +769,7 @@ PX4FMU::control_callback(uintptr_t handle, { const actuator_controls_s *controls = (actuator_controls_s *)handle; - input = controls->control[control_index]; + input = controls[control_group].control[control_index]; return 0; } @@ -707,6 +792,9 @@ PX4FMU::ioctl(file *filp, int cmd, unsigned long arg) case MODE_2PWM: case MODE_4PWM: case MODE_6PWM: +#ifdef CONFIG_ARCH_BOARD_AEROCORE + case MODE_8PWM: +#endif ret = pwm_ioctl(filp, cmd, arg); break; @@ -736,6 +824,7 @@ PX4FMU::pwm_ioctl(file *filp, int cmd, unsigned long arg) case PWM_SERVO_SET_ARM_OK: case PWM_SERVO_CLEAR_ARM_OK: + case PWM_SERVO_SET_FORCE_SAFETY_OFF: // these are no-ops, as no safety switch break; @@ -935,6 +1024,15 @@ PX4FMU::pwm_ioctl(file *filp, int cmd, unsigned long arg) break; } +#ifdef CONFIG_ARCH_BOARD_AEROCORE + case PWM_SERVO_SET(7): + case PWM_SERVO_SET(6): + if (_mode < MODE_8PWM) { + ret = -EINVAL; + break; + } +#endif + case PWM_SERVO_SET(5): case PWM_SERVO_SET(4): if (_mode < MODE_6PWM) { @@ -962,6 +1060,15 @@ PX4FMU::pwm_ioctl(file *filp, int cmd, unsigned long arg) break; +#ifdef CONFIG_ARCH_BOARD_AEROCORE + case PWM_SERVO_GET(7): + case PWM_SERVO_GET(6): + if (_mode < MODE_8PWM) { + ret = -EINVAL; + break; + } +#endif + case PWM_SERVO_GET(5): case PWM_SERVO_GET(4): if (_mode < MODE_6PWM) { @@ -989,12 +1096,22 @@ PX4FMU::pwm_ioctl(file *filp, int cmd, unsigned long arg) case PWM_SERVO_GET_RATEGROUP(3): case PWM_SERVO_GET_RATEGROUP(4): case PWM_SERVO_GET_RATEGROUP(5): +#ifdef CONFIG_ARCH_BOARD_AEROCORE + case PWM_SERVO_GET_RATEGROUP(6): + case PWM_SERVO_GET_RATEGROUP(7): +#endif *(uint32_t *)arg = up_pwm_servo_get_rate_group(cmd - PWM_SERVO_GET_RATEGROUP(0)); break; case PWM_SERVO_GET_COUNT: case MIXERIOCGETOUTPUTCOUNT: switch (_mode) { +#ifdef CONFIG_ARCH_BOARD_AEROCORE + case MODE_8PWM: + *(unsigned *)arg = 8; + break; +#endif + case MODE_6PWM: *(unsigned *)arg = 6; break; @@ -1040,6 +1157,11 @@ PX4FMU::pwm_ioctl(file *filp, int cmd, unsigned long arg) set_mode(MODE_6PWM); break; #endif +#if defined(CONFIG_ARCH_BOARD_AEROCORE) + case 8: + set_mode(MODE_8PWM); + break; +#endif default: ret = -EINVAL; @@ -1052,6 +1174,7 @@ PX4FMU::pwm_ioctl(file *filp, int cmd, unsigned long arg) if (_mixers != nullptr) { delete _mixers; _mixers = nullptr; + _groups_required = 0; } break; @@ -1060,18 +1183,20 @@ PX4FMU::pwm_ioctl(file *filp, int cmd, unsigned long arg) mixer_simple_s *mixinfo = (mixer_simple_s *)arg; SimpleMixer *mixer = new SimpleMixer(control_callback, - (uintptr_t)&_controls, mixinfo); + (uintptr_t)_controls, mixinfo); if (mixer->check()) { delete mixer; + _groups_required = 0; ret = -EINVAL; } else { if (_mixers == nullptr) _mixers = new MixerGroup(control_callback, - (uintptr_t)&_controls); + (uintptr_t)_controls); _mixers->add_mixer(mixer); + _mixers->groups_required(_groups_required); } break; @@ -1082,9 +1207,10 @@ PX4FMU::pwm_ioctl(file *filp, int cmd, unsigned long arg) unsigned buflen = strnlen(buf, 1024); if (_mixers == nullptr) - _mixers = new MixerGroup(control_callback, (uintptr_t)&_controls); + _mixers = new MixerGroup(control_callback, (uintptr_t)_controls); if (_mixers == nullptr) { + _groups_required = 0; ret = -ENOMEM; } else { @@ -1095,7 +1221,11 @@ PX4FMU::pwm_ioctl(file *filp, int cmd, unsigned long arg) debug("mixer load failed with %d", ret); delete _mixers; _mixers = nullptr; + _groups_required = 0; ret = -EINVAL; + } else { + + _mixers->groups_required(_groups_required); } } @@ -1122,10 +1252,17 @@ PX4FMU::write(file *filp, const char *buffer, size_t len) unsigned count = len / 2; uint16_t values[6]; +#ifdef CONFIG_ARCH_BOARD_AEROCORE + if (count > 8) { + // we have at most 8 outputs + count = 8; + } +#else if (count > 6) { // we have at most 6 outputs count = 6; } +#endif // allow for misaligned values memcpy(values, buffer, count * 2); @@ -1400,6 +1537,9 @@ fmu_new_mode(PortMode new_mode) #if defined(CONFIG_ARCH_BOARD_PX4FMU_V2) servo_mode = PX4FMU::MODE_6PWM; #endif +#if defined(CONFIG_ARCH_BOARD_AEROCORE) + servo_mode = PX4FMU::MODE_8PWM; +#endif break; /* mixed modes supported on v1 board only */ @@ -1717,7 +1857,7 @@ fmu_main(int argc, char *argv[]) fprintf(stderr, "FMU: unrecognised command %s, try:\n", verb); #if defined(CONFIG_ARCH_BOARD_PX4FMU_V1) fprintf(stderr, " mode_gpio, mode_serial, mode_pwm, mode_gpio_serial, mode_pwm_serial, mode_pwm_gpio, test\n"); -#elif defined(CONFIG_ARCH_BOARD_PX4FMU_V2) +#elif defined(CONFIG_ARCH_BOARD_PX4FMU_V2) || defined(CONFIG_ARCH_BOARD_AEROCORE) fprintf(stderr, " mode_gpio, mode_pwm, test, sensor_reset [milliseconds]\n"); #endif exit(1); diff --git a/src/drivers/px4fmu/module.mk b/src/drivers/px4fmu/module.mk index 05bc7a5b3..eeb59e1a1 100644 --- a/src/drivers/px4fmu/module.mk +++ b/src/drivers/px4fmu/module.mk @@ -4,3 +4,5 @@ MODULE_COMMAND = fmu SRCS = fmu.cpp + +MODULE_STACKSIZE = 1200 diff --git a/src/drivers/px4io/module.mk b/src/drivers/px4io/module.mk index 2054faa12..c14f1f783 100644 --- a/src/drivers/px4io/module.mk +++ b/src/drivers/px4io/module.mk @@ -44,3 +44,5 @@ SRCS = px4io.cpp \ # XXX prune to just get UART registers INCLUDE_DIRS += $(NUTTX_SRC)/arch/arm/src/stm32 $(NUTTX_SRC)/arch/arm/src/common + +MODULE_STACKSIZE = 1200 diff --git a/src/drivers/px4io/px4io.cpp b/src/drivers/px4io/px4io.cpp index 82f3ba044..4099e5522 100644 --- a/src/drivers/px4io/px4io.cpp +++ b/src/drivers/px4io/px4io.cpp @@ -91,6 +91,8 @@ #include "uploader.h" +#include "modules/dataman/dataman.h" + extern device::Device *PX4IO_i2c_interface() weak_function; extern device::Device *PX4IO_serial_interface() weak_function; @@ -527,6 +529,11 @@ PX4IO::~PX4IO() if (_interface != nullptr) delete _interface; + /* deallocate perfs */ + perf_free(_perf_update); + perf_free(_perf_write); + perf_free(_perf_chan_count); + g_dev = nullptr; } @@ -568,9 +575,15 @@ int PX4IO::init() { int ret; + param_t sys_restart_param; + int sys_restart_val = DM_INIT_REASON_VOLATILE; ASSERT(_task == -1); + sys_restart_param = param_find("SYS_RESTART_TYPE"); + /* Indicate restart type is unknown */ + param_set(sys_restart_param, &sys_restart_val); + /* do regular cdev init */ ret = CDev::init(); @@ -675,6 +688,25 @@ PX4IO::init() /* send command to arm system via command API */ vehicle_command_s cmd; + /* send this to itself */ + param_t sys_id_param = param_find("MAV_SYS_ID"); + param_t comp_id_param = param_find("MAV_COMP_ID"); + + int32_t sys_id; + int32_t comp_id; + + if (param_get(sys_id_param, &sys_id)) { + errx(1, "PRM SYSID"); + } + + if (param_get(comp_id_param, &comp_id)) { + errx(1, "PRM CMPID"); + } + + cmd.target_system = sys_id; + cmd.target_component = comp_id; + cmd.source_system = sys_id; + cmd.source_component = comp_id; /* request arming */ cmd.param1 = 1.0f; cmd.param2 = 0; @@ -684,10 +716,7 @@ PX4IO::init() cmd.param6 = 0; cmd.param7 = 0; cmd.command = VEHICLE_CMD_COMPONENT_ARM_DISARM; - // cmd.target_system = status.system_id; - // cmd.target_component = status.component_id; - // cmd.source_system = status.system_id; - // cmd.source_component = status.component_id; + /* ask to confirm command */ cmd.confirmation = 1; @@ -720,6 +749,11 @@ PX4IO::init() /* keep waiting for state change for 2 s */ } while (!safety.armed); + /* Indicate restart type is in-flight */ + sys_restart_val = DM_INIT_REASON_IN_FLIGHT; + param_set(sys_restart_param, &sys_restart_val); + + /* regular boot, no in-air restart, init IO */ } else { @@ -745,6 +779,10 @@ PX4IO::init() } } + /* Indicate restart type is power on */ + sys_restart_val = DM_INIT_REASON_POWER_ON; + param_set(sys_restart_param, &sys_restart_val); + } /* try to claim the generic PWM output device node as well - it's OK if we fail at this */ @@ -756,7 +794,12 @@ PX4IO::init() } /* start the IO interface task */ - _task = task_create("px4io", SCHED_PRIORITY_ACTUATOR_OUTPUTS, 2048, (main_t)&PX4IO::task_main_trampoline, nullptr); + _task = task_spawn_cmd("px4io", + SCHED_DEFAULT, + SCHED_PRIORITY_ACTUATOR_OUTPUTS, + 2000, + (main_t)&PX4IO::task_main_trampoline, + nullptr); if (_task < 0) { debug("task start failed: %d", errno); @@ -944,8 +987,27 @@ PX4IO::task_main() int pret = io_reg_set(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_VBATT_SCALE, &scaling, 1); if (pret != OK) { - log("voltage scaling upload failed"); + log("vscale upload failed"); + } + + /* send RC throttle failsafe value to IO */ + int32_t failsafe_param_val; + param_t failsafe_param = param_find("RC_FAILS_THR"); + + if (failsafe_param != PARAM_INVALID) { + + param_get(failsafe_param, &failsafe_param_val); + + if (failsafe_param_val > 0) { + + uint16_t failsafe_thr = failsafe_param_val; + pret = io_reg_set(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_RC_THR_FAILSAFE_US, &failsafe_thr, 1); + if (pret != OK) { + log("failsafe upload failed, FS: %d us", (int)failsafe_thr); + } + } } + } } @@ -1400,7 +1462,7 @@ PX4IO::io_get_raw_rc_input(rc_input_values &input_rc) /* we don't have the status bits, so input_source has to be set elsewhere */ input_rc.input_source = RC_INPUT_SOURCE_UNKNOWN; - static const unsigned prolog = (PX4IO_P_RAW_RC_BASE - PX4IO_P_RAW_RC_COUNT); + const unsigned prolog = (PX4IO_P_RAW_RC_BASE - PX4IO_P_RAW_RC_COUNT); uint16_t regs[RC_INPUT_MAX_CHANNELS + prolog]; /* @@ -1408,8 +1470,6 @@ PX4IO::io_get_raw_rc_input(rc_input_values &input_rc) * * This should be the common case (9 channel R/C control being a reasonable upper bound). */ - input_rc.timestamp_publication = hrt_absolute_time(); - ret = io_reg_get(PX4IO_PAGE_RAW_RC_INPUT, PX4IO_P_RAW_RC_COUNT, ®s[0], prolog + 9); if (ret != OK) @@ -1421,23 +1481,38 @@ PX4IO::io_get_raw_rc_input(rc_input_values &input_rc) */ channel_count = regs[PX4IO_P_RAW_RC_COUNT]; - if (channel_count != _rc_chan_count) + /* limit the channel count */ + if (channel_count > RC_INPUT_MAX_CHANNELS) { + channel_count = RC_INPUT_MAX_CHANNELS; + } + + /* count channel count changes to identify signal integrity issues */ + if (channel_count != _rc_chan_count) { perf_count(_perf_chan_count); + } _rc_chan_count = channel_count; + input_rc.timestamp_publication = hrt_absolute_time(); + input_rc.rc_ppm_frame_length = regs[PX4IO_P_RAW_RC_DATA]; input_rc.rssi = regs[PX4IO_P_RAW_RC_NRSSI]; input_rc.rc_failsafe = (regs[PX4IO_P_RAW_RC_FLAGS] & PX4IO_P_RAW_RC_FLAGS_FAILSAFE); + input_rc.rc_lost = !(regs[PX4IO_P_RAW_RC_FLAGS] & PX4IO_P_RAW_RC_FLAGS_RC_OK); input_rc.rc_lost_frame_count = regs[PX4IO_P_RAW_LOST_FRAME_COUNT]; input_rc.rc_total_frame_count = regs[PX4IO_P_RAW_FRAME_COUNT]; + input_rc.channel_count = channel_count; /* rc_lost has to be set before the call to this function */ - if (!input_rc.rc_lost && !input_rc.rc_failsafe) + if (!input_rc.rc_lost && !input_rc.rc_failsafe) { _rc_last_valid = input_rc.timestamp_publication; + } input_rc.timestamp_last_signal = _rc_last_valid; + /* FIELDS NOT SET HERE */ + /* input_rc.input_source is set after this call XXX we might want to mirror the flags in the RC struct */ + if (channel_count > 9) { ret = io_reg_get(PX4IO_PAGE_RAW_RC_INPUT, PX4IO_P_RAW_RC_BASE + 9, ®s[prolog + 9], channel_count - 9); @@ -1445,8 +1520,10 @@ PX4IO::io_get_raw_rc_input(rc_input_values &input_rc) return ret; } - input_rc.channel_count = channel_count; - memcpy(input_rc.values, ®s[prolog], channel_count * 2); + /* last thing set are the actual channel values as 16 bit values */ + for (unsigned i = 0; i < channel_count; i++) { + input_rc.values[i] = regs[prolog + i]; + } return ret; } @@ -1479,10 +1556,11 @@ PX4IO::io_publish_raw_rc() } else { rc_val.input_source = RC_INPUT_SOURCE_UNKNOWN; - /* we do not know the RC input, only publish if RC OK flag is set */ - /* if no raw RC, just don't publish */ - if (!(_status & PX4IO_P_STATUS_FLAGS_RC_OK)) + /* only keep publishing RC input if we ever got a valid input */ + if (_rc_last_valid == 0) { + /* we have never seen valid RC signals, abort */ return OK; + } } /* lazily advertise on first publication */ @@ -2113,6 +2191,10 @@ PX4IO::ioctl(file * filep, int cmd, unsigned long arg) case PWM_SERVO_GET_DISABLE_LOCKDOWN: *(unsigned *)arg = _lockdown_override; + + case PWM_SERVO_SET_FORCE_SAFETY_OFF: + /* force safety swith off */ + ret = io_reg_set(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FORCE_SAFETY_OFF, PX4IO_FORCE_SAFETY_MAGIC); break; case DSM_BIND_START: diff --git a/src/drivers/px4io/px4io_uploader.cpp b/src/drivers/px4io/px4io_uploader.cpp index dd8abbac5..28ec62356 100644 --- a/src/drivers/px4io/px4io_uploader.cpp +++ b/src/drivers/px4io/px4io_uploader.cpp @@ -201,9 +201,14 @@ PX4IO_Uploader::upload(const char *filenames[]) continue; } - if (bl_rev <= 2) + if (bl_rev <= 2) { ret = verify_rev2(fw_size); - else if(bl_rev == 3) { + } else if(bl_rev == 3) { + ret = verify_rev3(fw_size); + } else { + /* verify rev 4 and higher still uses the same approach and + * every version *needs* to be verified. + */ ret = verify_rev3(fw_size); } diff --git a/src/drivers/sf0x/sf0x.cpp b/src/drivers/sf0x/sf0x.cpp index 70cd1ab1e..a0cf98340 100644 --- a/src/drivers/sf0x/sf0x.cpp +++ b/src/drivers/sf0x/sf0x.cpp @@ -124,6 +124,8 @@ private: orb_advert_t _range_finder_topic; + unsigned _consecutive_fail_count; + perf_counter_t _sample_perf; perf_counter_t _comms_errors; perf_counter_t _buffer_overflows; @@ -186,6 +188,7 @@ SF0X::SF0X(const char *port) : _linebuf_index(0), _last_read(0), _range_finder_topic(-1), + _consecutive_fail_count(0), _sample_perf(perf_alloc(PC_ELAPSED, "sf0x_read")), _comms_errors(perf_alloc(PC_COUNT, "sf0x_comms_errors")), _buffer_overflows(perf_alloc(PC_COUNT, "sf0x_buffer_overflows")) @@ -276,34 +279,11 @@ SF0X::init() warnx("advert err"); } - /* attempt to get a measurement 5 times */ - while (ret != OK && i < 5) { - - if (measure()) { - ret = ERROR; - _sensor_ok = false; - } - - usleep(100000); - - if (collect()) { - ret = ERROR; - _sensor_ok = false; - - } else { - ret = OK; - /* sensor is ok, but we don't really know if it is within range */ - _sensor_ok = true; - } - - i++; - } - /* close the fd */ ::close(_fd); _fd = -1; out: - return ret; + return OK; } int @@ -376,6 +356,7 @@ SF0X::ioctl(struct file *filp, int cmd, unsigned long arg) /* adjust to a legal polling interval in Hz */ default: { + /* do we need to start internal polling? */ bool want_start = (_measure_ticks == 0); @@ -544,10 +525,16 @@ SF0X::collect() if (read_elapsed > (SF0X_CONVERSION_INTERVAL * 2)) { _linebuf_index = 0; + } else if (_linebuf_index > 0) { + /* increment to next read position */ + _linebuf_index++; } + /* the buffer for read chars is buflen minus null termination */ + unsigned readlen = sizeof(_linebuf) - 1; + /* read from the sensor (uart buffer) */ - ret = ::read(_fd, &_linebuf[_linebuf_index], sizeof(_linebuf) - _linebuf_index); + ret = ::read(_fd, &_linebuf[_linebuf_index], readlen - _linebuf_index); if (ret < 0) { _linebuf[sizeof(_linebuf) - 1] = '\0'; @@ -562,19 +549,30 @@ SF0X::collect() } else { return -EAGAIN; } + } else if (ret == 0) { + return -EAGAIN; } - _linebuf_index += ret; - - if (_linebuf_index >= sizeof(_linebuf)) { - _linebuf_index = 0; - } + /* we did increment the index to the next position already, so just add the additional fields */ + _linebuf_index += (ret - 1); _last_read = hrt_absolute_time(); - if (_linebuf[_linebuf_index - 2] != '\r' || _linebuf[_linebuf_index - 1] != '\n') { - /* incomplete read, reschedule ourselves */ + if (_linebuf_index < 1) { + /* we need at least the two end bytes to make sense of this string */ return -EAGAIN; + + } else if (_linebuf[_linebuf_index - 1] != '\r' || _linebuf[_linebuf_index] != '\n') { + + if (_linebuf_index >= readlen - 1) { + /* we have a full buffer, but no line ending - abort */ + _linebuf_index = 0; + perf_count(_comms_errors); + return -ENOMEM; + } else { + /* incomplete read, reschedule ourselves */ + return -EAGAIN; + } } char *end; @@ -582,22 +580,56 @@ SF0X::collect() bool valid; /* enforce line ending */ - _linebuf[sizeof(_linebuf) - 1] = '\0'; + unsigned lend = (_linebuf_index < (sizeof(_linebuf) - 1)) ? _linebuf_index : (sizeof(_linebuf) - 1); + + _linebuf[lend] = '\0'; if (_linebuf[0] == '-' && _linebuf[1] == '-' && _linebuf[2] == '.') { si_units = -1.0f; valid = false; } else { - si_units = strtod(_linebuf, &end); - valid = true; + + /* we need to find a dot in the string, as we're missing the meters part else */ + valid = false; + + /* wipe out partially read content from last cycle(s), check for dot */ + for (int i = 0; i < (lend - 2); i++) { + if (_linebuf[i] == '\n') { + char buf[sizeof(_linebuf)]; + memcpy(buf, &_linebuf[i+1], (lend + 1) - (i + 1)); + memcpy(_linebuf, buf, (lend + 1) - (i + 1)); + } + + if (_linebuf[i] == '.') { + valid = true; + } + } + + if (valid) { + si_units = strtod(_linebuf, &end); + + /* we require at least 3 characters for a valid number */ + if (end > _linebuf + 3) { + valid = true; + } else { + si_units = -1.0f; + valid = false; + } + } } - debug("val (float): %8.4f, raw: %s\n", si_units, _linebuf); + debug("val (float): %8.4f, raw: %s, valid: %s\n", si_units, _linebuf, ((valid) ? "OK" : "NO")); - /* done with this chunk, resetting */ + /* done with this chunk, resetting - even if invalid */ _linebuf_index = 0; + /* if its invalid, there is no reason to forward the value */ + if (!valid) { + perf_count(_comms_errors); + return -EINVAL; + } + struct range_finder_report report; /* this should be fairly close to the end of the measurement, so the best approximation of the time */ @@ -689,10 +721,19 @@ SF0X::cycle() } if (OK != collect_ret) { - log("collection error"); + + /* we know the sensor needs about four seconds to initialize */ + if (hrt_absolute_time() > 5 * 1000 * 1000LL && _consecutive_fail_count < 5) { + log("collection error #%u", _consecutive_fail_count); + } + _consecutive_fail_count++; + /* restart the measurement state machine */ start(); return; + } else { + /* apparently success */ + _consecutive_fail_count = 0; } /* next phase is measurement */ @@ -848,10 +889,10 @@ test() } warnx("single read"); - warnx("measurement: %0.2f m", (double)report.distance); - warnx("time: %lld", report.timestamp); + warnx("val: %0.2f m", (double)report.distance); + warnx("time: %lld", report.timestamp); - /* start the sensor polling at 2Hz */ + /* start the sensor polling at 2 Hz rate */ if (OK != ioctl(fd, SENSORIOCSPOLLRATE, 2)) { errx(1, "failed to set 2Hz poll rate"); } @@ -866,24 +907,26 @@ test() int ret = poll(&fds, 1, 2000); if (ret != 1) { - errx(1, "timed out waiting for sensor data"); + warnx("timed out"); + break; } /* now go get it */ sz = read(fd, &report, sizeof(report)); if (sz != sizeof(report)) { - err(1, "periodic read failed"); + warnx("read failed: got %d vs exp. %d", sz, sizeof(report)); + break; } - warnx("periodic read %u", i); - warnx("measurement: %0.3f", (double)report.distance); - warnx("time: %lld", report.timestamp); + warnx("read #%u", i); + warnx("val: %0.3f m", (double)report.distance); + warnx("time: %lld", report.timestamp); } - /* reset the sensor polling to default rate */ + /* reset the sensor polling to the default rate */ if (OK != ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_DEFAULT)) { - errx(1, "failed to set default poll rate"); + errx(1, "ERR: DEF RATE"); } errx(0, "PASS"); diff --git a/src/drivers/stm32/adc/adc.cpp b/src/drivers/stm32/adc/adc.cpp index 00e46d6b8..de13b8969 100644 --- a/src/drivers/stm32/adc/adc.cpp +++ b/src/drivers/stm32/adc/adc.cpp @@ -41,6 +41,7 @@ */ #include <nuttx/config.h> +#include <board_config.h> #include <drivers/device/device.h> #include <sys/types.h> @@ -64,6 +65,8 @@ #include <systemlib/err.h> #include <systemlib/perf_counter.h> +#include <uORB/topics/system_power.h> + /* * Register accessors. * For now, no reason not to just use ADC1. @@ -119,6 +122,8 @@ private: unsigned _channel_count; adc_msg_s *_samples; /**< sample buffer */ + orb_advert_t _to_system_power; + /** work trampoline */ static void _tick_trampoline(void *arg); @@ -134,13 +139,16 @@ private: */ uint16_t _sample(unsigned channel); + // update system_power ORB topic, only on FMUv2 + void update_system_power(void); }; ADC::ADC(uint32_t channels) : CDev("adc", ADC_DEVICE_PATH), _sample_perf(perf_alloc(PC_ELAPSED, "ADC samples")), _channel_count(0), - _samples(nullptr) + _samples(nullptr), + _to_system_power(0) { _debug_enabled = true; @@ -290,6 +298,43 @@ ADC::_tick() /* scan the channel set and sample each */ for (unsigned i = 0; i < _channel_count; i++) _samples[i].am_data = _sample(_samples[i].am_channel); + update_system_power(); +} + +void +ADC::update_system_power(void) +{ +#ifdef CONFIG_ARCH_BOARD_PX4FMU_V2 + system_power_s system_power; + system_power.timestamp = hrt_absolute_time(); + + system_power.voltage5V_v = 0; + for (unsigned i = 0; i < _channel_count; i++) { + if (_samples[i].am_channel == 4) { + // it is 2:1 scaled + system_power.voltage5V_v = _samples[i].am_data * (6.6f / 4096); + } + } + + // these are not ADC related, but it is convenient to + // publish these to the same topic + system_power.usb_connected = stm32_gpioread(GPIO_OTGFS_VBUS); + + // note that the valid pins are active low + system_power.brick_valid = !stm32_gpioread(GPIO_VDD_BRICK_VALID); + system_power.servo_valid = !stm32_gpioread(GPIO_VDD_SERVO_VALID); + + // OC pins are active low + system_power.periph_5V_OC = !stm32_gpioread(GPIO_VDD_5V_PERIPH_OC); + system_power.hipower_5V_OC = !stm32_gpioread(GPIO_VDD_5V_HIPOWER_OC); + + /* lazily publish */ + if (_to_system_power > 0) { + orb_publish(ORB_ID(system_power), _to_system_power, &system_power); + } else { + _to_system_power = orb_advertise(ORB_ID(system_power), &system_power); + } +#endif // CONFIG_ARCH_BOARD_PX4FMU_V2 } uint16_t @@ -341,7 +386,7 @@ test(void) err(1, "can't open ADC device"); for (unsigned i = 0; i < 50; i++) { - adc_msg_s data[10]; + adc_msg_s data[12]; ssize_t count = read(fd, data, sizeof(data)); if (count < 0) @@ -374,6 +419,10 @@ adc_main(int argc, char *argv[]) g_adc = new ADC((1 << 2) | (1 << 3) | (1 << 4) | (1 << 10) | (1 << 11) | (1 << 12) | (1 << 13) | (1 << 14) | (1 << 15)); #endif +#ifdef CONFIG_ARCH_BOARD_AEROCORE + /* XXX this hardcodes the default channel set for AeroCore - should be configurable */ + g_adc = new ADC((1 << 10) | (1 << 11) | (1 << 12) | (1 << 13)); +#endif if (g_adc == nullptr) errx(1, "couldn't allocate the ADC driver"); diff --git a/src/drivers/stm32/drv_hrt.c b/src/drivers/stm32/drv_hrt.c index b7c9b89a4..281f918d7 100644 --- a/src/drivers/stm32/drv_hrt.c +++ b/src/drivers/stm32/drv_hrt.c @@ -94,7 +94,7 @@ #elif HRT_TIMER == 3 # define HRT_TIMER_BASE STM32_TIM3_BASE # define HRT_TIMER_POWER_REG STM32_RCC_APB1ENR -# define HRT_TIMER_POWER_BIT RCC_APB2ENR_TIM3EN +# define HRT_TIMER_POWER_BIT RCC_APB1ENR_TIM3EN # define HRT_TIMER_VECTOR STM32_IRQ_TIM3 # define HRT_TIMER_CLOCK STM32_APB1_TIM3_CLKIN # if CONFIG_STM32_TIM3 @@ -141,7 +141,7 @@ # define HRT_TIMER_POWER_REG STM32_RCC_APB1ENR # define HRT_TIMER_POWER_BIT RCC_APB2ENR_TIM10EN # define HRT_TIMER_VECTOR STM32_IRQ_TIM1UP -# define HRT_TIMER_CLOCK STM32_APB1_TIM10_CLKIN +# define HRT_TIMER_CLOCK STM32_APB2_TIM10_CLKIN # if CONFIG_STM32_TIM10 # error must not set CONFIG_STM32_TIM11=y and HRT_TIMER=10 # endif @@ -150,7 +150,7 @@ # define HRT_TIMER_POWER_REG STM32_RCC_APB1ENR # define HRT_TIMER_POWER_BIT RCC_APB2ENR_TIM11EN # define HRT_TIMER_VECTOR STM32_IRQ_TIM1TRGCOM -# define HRT_TIMER_CLOCK STM32_APB1_TIM11_CLKIN +# define HRT_TIMER_CLOCK STM32_APB2_TIM11_CLKIN # if CONFIG_STM32_TIM11 # error must not set CONFIG_STM32_TIM11=y and HRT_TIMER=11 # endif @@ -354,6 +354,9 @@ __EXPORT uint16_t ppm_frame_length = 0; __EXPORT unsigned ppm_decoded_channels = 0; __EXPORT uint64_t ppm_last_valid_decode = 0; +#define PPM_DEBUG 0 + +#if PPM_DEBUG /* PPM edge history */ __EXPORT uint16_t ppm_edge_history[32]; unsigned ppm_edge_next; @@ -361,6 +364,7 @@ unsigned ppm_edge_next; /* PPM pulse history */ __EXPORT uint16_t ppm_pulse_history[32]; unsigned ppm_pulse_next; +#endif static uint16_t ppm_temp_buffer[PPM_MAX_CHANNELS]; @@ -455,10 +459,12 @@ hrt_ppm_decode(uint32_t status) /* how long since the last edge? - this handles counter wrapping implicitely. */ width = count - ppm.last_edge; +#if PPM_DEBUG ppm_edge_history[ppm_edge_next++] = width; if (ppm_edge_next >= 32) ppm_edge_next = 0; +#endif /* * if this looks like a start pulse, then push the last set of values @@ -546,10 +552,12 @@ hrt_ppm_decode(uint32_t status) interval = count - ppm.last_mark; ppm.last_mark = count; +#if PPM_DEBUG ppm_pulse_history[ppm_pulse_next++] = interval; if (ppm_pulse_next >= 32) ppm_pulse_next = 0; +#endif /* if the mark-mark timing is out of bounds, abandon the frame */ if ((interval < PPM_MIN_CHANNEL_VALUE) || (interval > PPM_MAX_CHANNEL_VALUE)) diff --git a/src/drivers/stm32/tone_alarm/tone_alarm.cpp b/src/drivers/stm32/tone_alarm/tone_alarm.cpp index f36f2091e..810f4aacc 100644 --- a/src/drivers/stm32/tone_alarm/tone_alarm.cpp +++ b/src/drivers/stm32/tone_alarm/tone_alarm.cpp @@ -334,6 +334,8 @@ ToneAlarm::ToneAlarm() : _default_tunes[TONE_BATTERY_WARNING_SLOW_TUNE] = "MBNT100a8"; //battery warning slow _default_tunes[TONE_BATTERY_WARNING_FAST_TUNE] = "MBNT255a8a8a8a8a8a8a8a8a8a8a8a8a8a8a8a8"; //battery warning fast _default_tunes[TONE_GPS_WARNING_TUNE] = "MFT255L4AAAL1F#"; //gps warning slow + _default_tunes[TONE_ARMING_FAILURE_TUNE] = "MFT255L4<<<BAP"; + _default_tunes[TONE_PARACHUTE_RELEASE_TUNE] = "MFT255L16agagagag"; // parachute release _tune_names[TONE_STARTUP_TUNE] = "startup"; // startup tune _tune_names[TONE_ERROR_TUNE] = "error"; // ERROR tone @@ -344,6 +346,8 @@ ToneAlarm::ToneAlarm() : _tune_names[TONE_BATTERY_WARNING_SLOW_TUNE] = "slow_bat"; // battery warning slow _tune_names[TONE_BATTERY_WARNING_FAST_TUNE] = "fast_bat"; // battery warning fast _tune_names[TONE_GPS_WARNING_TUNE] = "gps_warning"; // gps warning + _tune_names[TONE_ARMING_FAILURE_TUNE] = "arming_failure"; //fail to arm + _tune_names[TONE_PARACHUTE_RELEASE_TUNE] = "parachute_release"; // parachute release } ToneAlarm::~ToneAlarm() diff --git a/src/examples/fixedwing_control/module.mk b/src/examples/fixedwing_control/module.mk index d2c48934f..a2a9eb113 100644 --- a/src/examples/fixedwing_control/module.mk +++ b/src/examples/fixedwing_control/module.mk @@ -39,3 +39,5 @@ MODULE_COMMAND = ex_fixedwing_control SRCS = main.c \ params.c + +MODULE_STACKSIZE = 1200 diff --git a/src/examples/flow_position_estimator/flow_position_estimator_main.c b/src/examples/flow_position_estimator/flow_position_estimator_main.c index 495c415f2..c775428ef 100644 --- a/src/examples/flow_position_estimator/flow_position_estimator_main.c +++ b/src/examples/flow_position_estimator/flow_position_estimator_main.c @@ -65,6 +65,7 @@ #include <uORB/topics/optical_flow.h> #include <uORB/topics/filtered_bottom_flow.h> #include <systemlib/perf_counter.h> +#include <systemlib/systemlib.h> #include <poll.h> #include "flow_position_estimator_params.h" @@ -109,9 +110,9 @@ int flow_position_estimator_main(int argc, char *argv[]) thread_should_exit = false; daemon_task = task_spawn_cmd("flow_position_estimator", - SCHED_RR, + SCHED_DEFAULT, SCHED_PRIORITY_MAX - 5, - 4096, + 4000, flow_position_estimator_thread_main, (argv) ? (const char **)&argv[2] : (const char **)NULL); exit(0); diff --git a/src/examples/px4_daemon_app/module.mk b/src/examples/px4_daemon_app/module.mk index 5f8aa73d5..fc4223142 100644 --- a/src/examples/px4_daemon_app/module.mk +++ b/src/examples/px4_daemon_app/module.mk @@ -38,3 +38,5 @@ MODULE_COMMAND = px4_daemon_app SRCS = px4_daemon_app.c + +MODULE_STACKSIZE = 1200 diff --git a/src/examples/px4_daemon_app/px4_daemon_app.c b/src/examples/px4_daemon_app/px4_daemon_app.c index 53f1b4a9a..3eaf14148 100644 --- a/src/examples/px4_daemon_app/px4_daemon_app.c +++ b/src/examples/px4_daemon_app/px4_daemon_app.c @@ -98,7 +98,7 @@ int px4_daemon_app_main(int argc, char *argv[]) daemon_task = task_spawn_cmd("daemon", SCHED_DEFAULT, SCHED_PRIORITY_DEFAULT, - 4096, + 2000, px4_daemon_thread_main, (argv) ? (const char **)&argv[2] : (const char **)NULL); exit(0); diff --git a/src/examples/px4_mavlink_debug/module.mk b/src/examples/px4_mavlink_debug/module.mk index fefd61496..c7ef97fc4 100644 --- a/src/examples/px4_mavlink_debug/module.mk +++ b/src/examples/px4_mavlink_debug/module.mk @@ -37,4 +37,6 @@ MODULE_COMMAND = px4_mavlink_debug -SRCS = px4_mavlink_debug.c
\ No newline at end of file +SRCS = px4_mavlink_debug.c + +MODULE_STACKSIZE = 2000 diff --git a/src/lib/geo/geo.c b/src/lib/geo/geo.c index 59c04f0e3..9a24ff50e 100644 --- a/src/lib/geo/geo.c +++ b/src/lib/geo/geo.c @@ -1,9 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: Thomas Gubler <thomasgubler@student.ethz.ch> - * Julian Oes <joes@student.ethz.ch> - * Lorenz Meier <lm@inf.ethz.ch> + * Copyright (C) 2012, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -42,6 +39,7 @@ * @author Thomas Gubler <thomasgubler@student.ethz.ch> * @author Julian Oes <joes@student.ethz.ch> * @author Lorenz Meier <lm@inf.ethz.ch> + * @author Anton Babushkin <anton.babushkin@me.com> */ #include <geo/geo.h> @@ -52,124 +50,58 @@ #include <math.h> #include <stdbool.h> +/* + * Azimuthal Equidistant Projection + * formulas according to: http://mathworld.wolfram.com/AzimuthalEquidistantProjection.html + */ -/* values for map projection */ -static double phi_1; -static double sin_phi_1; -static double cos_phi_1; -static double lambda_0; -static double scale; - -__EXPORT void map_projection_init(double lat_0, double lon_0) //lat_0, lon_0 are expected to be in correct format: -> 47.1234567 and not 471234567 +__EXPORT void map_projection_init(struct map_projection_reference_s *ref, double lat_0, double lon_0) //lat_0, lon_0 are expected to be in correct format: -> 47.1234567 and not 471234567 { - /* notation and formulas according to: http://mathworld.wolfram.com/AzimuthalEquidistantProjection.html */ - phi_1 = lat_0 / 180.0 * M_PI; - lambda_0 = lon_0 / 180.0 * M_PI; - - sin_phi_1 = sin(phi_1); - cos_phi_1 = cos(phi_1); - - /* calculate local scale by using the relation of true distance and the distance on plane */ //TODO: this is a quick solution, there are probably easier ways to determine the scale - - /* 1) calculate true distance d on sphere to a point: http://www.movable-type.co.uk/scripts/latlong.html */ - - double lat1 = phi_1; - double lon1 = lambda_0; - - double lat2 = phi_1 + 0.5 / 180 * M_PI; - double lon2 = lambda_0 + 0.5 / 180 * M_PI; - double sin_lat_2 = sin(lat2); - double cos_lat_2 = cos(lat2); - double d = acos(sin(lat1) * sin_lat_2 + cos(lat1) * cos_lat_2 * cos(lon2 - lon1)) * CONSTANTS_RADIUS_OF_EARTH; - - /* 2) calculate distance rho on plane */ - double k_bar = 0; - double c = acos(sin_phi_1 * sin_lat_2 + cos_phi_1 * cos_lat_2 * cos(lon2 - lambda_0)); - - if (0 != c) - k_bar = c / sin(c); - - double x2 = k_bar * (cos_lat_2 * sin(lon2 - lambda_0)); //Projection of point 2 on plane - double y2 = k_bar * ((cos_phi_1 * sin_lat_2 - sin_phi_1 * cos_lat_2 * cos(lon2 - lambda_0))); - double rho = sqrt(pow(x2, 2) + pow(y2, 2)); - - scale = d / rho; + ref->lat = lat_0 / 180.0 * M_PI; + ref->lon = lon_0 / 180.0 * M_PI; + ref->sin_lat = sin(ref->lat); + ref->cos_lat = cos(ref->lat); } -__EXPORT void map_projection_project(double lat, double lon, float *x, float *y) +__EXPORT void map_projection_project(struct map_projection_reference_s *ref, double lat, double lon, float *x, float *y) { - /* notation and formulas accoring to: http://mathworld.wolfram.com/AzimuthalEquidistantProjection.html */ - double phi = lat / 180.0 * M_PI; - double lambda = lon / 180.0 * M_PI; - - double sin_phi = sin(phi); - double cos_phi = cos(phi); - - double k_bar = 0; - /* using small angle approximation (formula in comment is without aproximation) */ - double c = acos(sin_phi_1 * sin_phi + cos_phi_1 * cos_phi * (1 - pow((lambda - lambda_0), 2) / 2)); //double c = acos( sin_phi_1 * sin_phi + cos_phi_1 * cos_phi * cos(lambda - lambda_0) ); + double lat_rad = lat / 180.0 * M_PI; + double lon_rad = lon / 180.0 * M_PI; - if (0 != c) - k_bar = c / sin(c); + double sin_lat = sin(lat_rad); + double cos_lat = cos(lat_rad); + double cos_d_lon = cos(lon_rad - ref->lon); - /* using small angle approximation (formula in comment is without aproximation) */ - *y = k_bar * (cos_phi * (lambda - lambda_0)) * scale;//*y = k_bar * (cos_phi * sin(lambda - lambda_0)) * scale; - *x = k_bar * ((cos_phi_1 * sin_phi - sin_phi_1 * cos_phi * (1 - pow((lambda - lambda_0), 2) / 2))) * scale; // *x = k_bar * ((cos_phi_1 * sin_phi - sin_phi_1 * cos_phi * cos(lambda - lambda_0))) * scale; + double c = acos(ref->sin_lat * sin_lat + ref->cos_lat * cos_lat * cos_d_lon); + double k = (c == 0.0) ? 1.0 : (c / sin(c)); -// printf("%phi_1=%.10f, lambda_0 =%.10f\n", phi_1, lambda_0); + *x = k * (ref->cos_lat * sin_lat - ref->sin_lat * cos_lat * cos_d_lon) * CONSTANTS_RADIUS_OF_EARTH; + *y = k * cos_lat * sin(lon_rad - ref->lon) * CONSTANTS_RADIUS_OF_EARTH; } -__EXPORT void map_projection_reproject(float x, float y, double *lat, double *lon) +__EXPORT void map_projection_reproject(struct map_projection_reference_s *ref, float x, float y, double *lat, double *lon) { - /* notation and formulas accoring to: http://mathworld.wolfram.com/AzimuthalEquidistantProjection.html */ - - double x_descaled = x / scale; - double y_descaled = y / scale; - - double c = sqrt(pow(x_descaled, 2) + pow(y_descaled, 2)); + float x_rad = x / CONSTANTS_RADIUS_OF_EARTH; + float y_rad = y / CONSTANTS_RADIUS_OF_EARTH; + double c = sqrtf(x_rad * x_rad + y_rad * y_rad); double sin_c = sin(c); double cos_c = cos(c); - double lat_sphere = 0; + double lat_rad; + double lon_rad; - if (c != 0) - lat_sphere = asin(cos_c * sin_phi_1 + (x_descaled * sin_c * cos_phi_1) / c); - else - lat_sphere = asin(cos_c * sin_phi_1); - -// printf("lat_sphere = %.10f\n",lat_sphere); - - double lon_sphere = 0; - - if (phi_1 == M_PI / 2) { - //using small angle approximation (formula in comment is without aproximation) - lon_sphere = (lambda_0 - y_descaled / x_descaled); //lon_sphere = (lambda_0 + atan2(-y_descaled, x_descaled)); - - } else if (phi_1 == -M_PI / 2) { - //using small angle approximation (formula in comment is without aproximation) - lon_sphere = (lambda_0 + y_descaled / x_descaled); //lon_sphere = (lambda_0 + atan2(y_descaled, x_descaled)); + if (c != 0.0) { + lat_rad = asin(cos_c * ref->sin_lat + (x_rad * sin_c * ref->cos_lat) / c); + lon_rad = (ref->lon + atan2(y_rad * sin_c, c * ref->cos_lat * cos_c - x_rad * ref->sin_lat * sin_c)); } else { - - lon_sphere = (lambda_0 + atan2(y_descaled * sin_c , c * cos_phi_1 * cos_c - x_descaled * sin_phi_1 * sin_c)); - //using small angle approximation -// double denominator = (c * cos_phi_1 * cos_c - x_descaled * sin_phi_1 * sin_c); -// if(denominator != 0) -// { -// lon_sphere = (lambda_0 + (y_descaled * sin_c) / denominator); -// } -// else -// { -// ... -// } + lat_rad = ref->lat; + lon_rad = ref->lon; } -// printf("lon_sphere = %.10f\n",lon_sphere); - - *lat = lat_sphere * 180.0 / M_PI; - *lon = lon_sphere * 180.0 / M_PI; - + *lat = lat_rad * 180.0 / M_PI; + *lon = lon_rad * 180.0 / M_PI; } @@ -197,7 +129,6 @@ __EXPORT float get_bearing_to_next_waypoint(double lat_now, double lon_now, doub double lat_next_rad = lat_next * M_DEG_TO_RAD; double lon_next_rad = lon_next * M_DEG_TO_RAD; - double d_lat = lat_next_rad - lat_now_rad; double d_lon = lon_next_rad - lon_now_rad; /* conscious mix of double and float trig function to maximize speed and efficiency */ @@ -208,7 +139,7 @@ __EXPORT float get_bearing_to_next_waypoint(double lat_now, double lon_now, doub return theta; } -__EXPORT void get_vector_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next, float* v_n, float* v_e) +__EXPORT void get_vector_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next, float *v_n, float *v_e) { double lat_now_rad = lat_now * M_DEG_TO_RAD; double lon_now_rad = lon_now * M_DEG_TO_RAD; @@ -223,7 +154,7 @@ __EXPORT void get_vector_to_next_waypoint(double lat_now, double lon_now, double *v_e = CONSTANTS_RADIUS_OF_EARTH * sin(d_lon) * cos(lat_next_rad); } -__EXPORT void get_vector_to_next_waypoint_fast(double lat_now, double lon_now, double lat_next, double lon_next, float* v_n, float* v_e) +__EXPORT void get_vector_to_next_waypoint_fast(double lat_now, double lon_now, double lat_next, double lon_next, float *v_n, float *v_e) { double lat_now_rad = lat_now * M_DEG_TO_RAD; double lon_now_rad = lon_now * M_DEG_TO_RAD; @@ -249,7 +180,7 @@ __EXPORT void add_vector_to_global_position(double lat_now, double lon_now, floa // Additional functions - @author Doug Weibel <douglas.weibel@colorado.edu> -__EXPORT int get_distance_to_line(struct crosstrack_error_s * crosstrack_error, double lat_now, double lon_now, double lat_start, double lon_start, double lat_end, double lon_end) +__EXPORT int get_distance_to_line(struct crosstrack_error_s *crosstrack_error, double lat_now, double lon_now, double lat_start, double lon_start, double lat_end, double lon_end) { // This function returns the distance to the nearest point on the track line. Distance is positive if current // position is right of the track and negative if left of the track as seen from a point on the track line @@ -266,7 +197,7 @@ __EXPORT int get_distance_to_line(struct crosstrack_error_s * crosstrack_error, crosstrack_error->bearing = 0.0f; // Return error if arguments are bad - if (lat_now == 0.0d || lon_now == 0.0d || lat_start == 0.0d || lon_start == 0.0d || lat_end == 0.0d || lon_end == 0.0d) return return_value; + if (lat_now == 0.0d || lon_now == 0.0d || lat_start == 0.0d || lon_start == 0.0d || lat_end == 0.0d || lon_end == 0.0d) { return return_value; } bearing_end = get_bearing_to_next_waypoint(lat_now, lon_now, lat_end, lon_end); bearing_track = get_bearing_to_next_waypoint(lat_start, lon_start, lat_end, lon_end); @@ -297,8 +228,8 @@ __EXPORT int get_distance_to_line(struct crosstrack_error_s * crosstrack_error, } -__EXPORT int get_distance_to_arc(struct crosstrack_error_s * crosstrack_error, double lat_now, double lon_now, double lat_center, double lon_center, - float radius, float arc_start_bearing, float arc_sweep) +__EXPORT int get_distance_to_arc(struct crosstrack_error_s *crosstrack_error, double lat_now, double lon_now, double lat_center, double lon_center, + float radius, float arc_start_bearing, float arc_sweep) { // This function returns the distance to the nearest point on the track arc. Distance is positive if current // position is right of the arc and negative if left of the arc as seen from the closest point on the arc and @@ -317,29 +248,29 @@ __EXPORT int get_distance_to_arc(struct crosstrack_error_s * crosstrack_error, d crosstrack_error->bearing = 0.0f; // Return error if arguments are bad - if (lat_now == 0.0d || lon_now == 0.0d || lat_center == 0.0d || lon_center == 0.0d || radius == 0.0d) return return_value; + if (lat_now == 0.0d || lon_now == 0.0d || lat_center == 0.0d || lon_center == 0.0d || radius == 0.0d) { return return_value; } if (arc_sweep >= 0) { bearing_sector_start = arc_start_bearing; bearing_sector_end = arc_start_bearing + arc_sweep; - if (bearing_sector_end > 2.0f * M_PI_F) bearing_sector_end -= M_TWOPI_F; + if (bearing_sector_end > 2.0f * M_PI_F) { bearing_sector_end -= M_TWOPI_F; } } else { bearing_sector_end = arc_start_bearing; bearing_sector_start = arc_start_bearing - arc_sweep; - if (bearing_sector_start < 0.0f) bearing_sector_start += M_TWOPI_F; + if (bearing_sector_start < 0.0f) { bearing_sector_start += M_TWOPI_F; } } in_sector = false; // Case where sector does not span zero - if (bearing_sector_end >= bearing_sector_start && bearing_now >= bearing_sector_start && bearing_now <= bearing_sector_end) in_sector = true; + if (bearing_sector_end >= bearing_sector_start && bearing_now >= bearing_sector_start && bearing_now <= bearing_sector_end) { in_sector = true; } // Case where sector does span zero - if (bearing_sector_end < bearing_sector_start && (bearing_now > bearing_sector_start || bearing_now < bearing_sector_end)) in_sector = true; + if (bearing_sector_end < bearing_sector_start && (bearing_now > bearing_sector_start || bearing_now < bearing_sector_end)) { in_sector = true; } // If in the sector then calculate distance and bearing to closest point if (in_sector) { @@ -395,8 +326,8 @@ __EXPORT int get_distance_to_arc(struct crosstrack_error_s * crosstrack_error, d } __EXPORT float get_distance_to_point_global_wgs84(double lat_now, double lon_now, float alt_now, - double lat_next, double lon_next, float alt_next, - float *dist_xy, float *dist_z) + double lat_next, double lon_next, float alt_next, + float *dist_xy, float *dist_z) { double current_x_rad = lat_next / 180.0 * M_PI; double current_y_rad = lon_next / 180.0 * M_PI; @@ -420,8 +351,8 @@ __EXPORT float get_distance_to_point_global_wgs84(double lat_now, double lon_now __EXPORT float mavlink_wpm_distance_to_point_local(float x_now, float y_now, float z_now, - float x_next, float y_next, float z_next, - float *dist_xy, float *dist_z) + float x_next, float y_next, float z_next, + float *dist_xy, float *dist_z) { float dx = x_now - x_next; float dy = y_now - y_next; @@ -443,15 +374,19 @@ __EXPORT float _wrap_pi(float bearing) int c = 0; while (bearing >= M_PI_F) { bearing -= M_TWOPI_F; - if (c++ > 3) + + if (c++ > 3) { return NAN; + } } c = 0; while (bearing < -M_PI_F) { bearing += M_TWOPI_F; - if (c++ > 3) + + if (c++ > 3) { return NAN; + } } return bearing; @@ -467,15 +402,19 @@ __EXPORT float _wrap_2pi(float bearing) int c = 0; while (bearing >= M_TWOPI_F) { bearing -= M_TWOPI_F; - if (c++ > 3) + + if (c++ > 3) { return NAN; + } } c = 0; while (bearing < 0.0f) { bearing += M_TWOPI_F; - if (c++ > 3) + + if (c++ > 3) { return NAN; + } } return bearing; @@ -491,15 +430,19 @@ __EXPORT float _wrap_180(float bearing) int c = 0; while (bearing >= 180.0f) { bearing -= 360.0f; - if (c++ > 3) + + if (c++ > 3) { return NAN; + } } c = 0; while (bearing < -180.0f) { bearing += 360.0f; - if (c++ > 3) + + if (c++ > 3) { return NAN; + } } return bearing; @@ -515,15 +458,19 @@ __EXPORT float _wrap_360(float bearing) int c = 0; while (bearing >= 360.0f) { bearing -= 360.0f; - if (c++ > 3) + + if (c++ > 3) { return NAN; + } } c = 0; while (bearing < 0.0f) { bearing += 360.0f; - if (c++ > 3) + + if (c++ > 3) { return NAN; + } } return bearing; diff --git a/src/lib/geo/geo.h b/src/lib/geo/geo.h index 94afb4df0..e2f3da6f8 100644 --- a/src/lib/geo/geo.h +++ b/src/lib/geo/geo.h @@ -1,9 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: Thomas Gubler <thomasgubler@student.ethz.ch> - * Julian Oes <joes@student.ethz.ch> - * Lorenz Meier <lm@inf.ethz.ch> + * Copyright (C) 2012, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -42,6 +39,7 @@ * @author Thomas Gubler <thomasgubler@student.ethz.ch> * @author Julian Oes <joes@student.ethz.ch> * @author Lorenz Meier <lm@inf.ethz.ch> + * @author Anton Babushkin <anton.babushkin@me.com> * Additional functions - @author Doug Weibel <douglas.weibel@colorado.edu> */ @@ -52,6 +50,8 @@ __BEGIN_DECLS +#include "geo/geo_mag_declination.h" + #include <stdbool.h> #define CONSTANTS_ONE_G 9.80665f /* m/s^2 */ @@ -67,6 +67,14 @@ struct crosstrack_error_s { float bearing; // Bearing in radians to closest point on line/arc } ; +/* lat/lon are in radians */ +struct map_projection_reference_s { + double lat; + double lon; + double sin_lat; + double cos_lat; +}; + /** * Initializes the map transformation. * @@ -74,7 +82,7 @@ struct crosstrack_error_s { * @param lat in degrees (47.1234567°, not 471234567°) * @param lon in degrees (8.1234567°, not 81234567°) */ -__EXPORT void map_projection_init(double lat_0, double lon_0); +__EXPORT void map_projection_init(struct map_projection_reference_s *ref, double lat_0, double lon_0); /** * Transforms a point in the geographic coordinate system to the local azimuthal equidistant plane @@ -83,7 +91,7 @@ __EXPORT void map_projection_init(double lat_0, double lon_0); * @param lat in degrees (47.1234567°, not 471234567°) * @param lon in degrees (8.1234567°, not 81234567°) */ -__EXPORT void map_projection_project(double lat, double lon, float *x, float *y); +__EXPORT void map_projection_project(struct map_projection_reference_s *ref, double lat, double lon, float *x, float *y); /** * Transforms a point in the local azimuthal equidistant plane to the geographic coordinate system @@ -93,7 +101,7 @@ __EXPORT void map_projection_project(double lat, double lon, float *x, float *y) * @param lat in degrees (47.1234567°, not 471234567°) * @param lon in degrees (8.1234567°, not 81234567°) */ -__EXPORT void map_projection_reproject(float x, float y, double *lat, double *lon); +__EXPORT void map_projection_reproject(struct map_projection_reference_s *ref, float x, float y, double *lat, double *lon); /** * Returns the distance to the next waypoint in meters. @@ -115,30 +123,30 @@ __EXPORT float get_distance_to_next_waypoint(double lat_now, double lon_now, dou */ __EXPORT float get_bearing_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next); -__EXPORT void get_vector_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next, float* v_n, float* v_e); +__EXPORT void get_vector_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next, float *v_n, float *v_e); -__EXPORT void get_vector_to_next_waypoint_fast(double lat_now, double lon_now, double lat_next, double lon_next, float* v_n, float* v_e); +__EXPORT void get_vector_to_next_waypoint_fast(double lat_now, double lon_now, double lat_next, double lon_next, float *v_n, float *v_e); __EXPORT void add_vector_to_global_position(double lat_now, double lon_now, float v_n, float v_e, double *lat_res, double *lon_res); -__EXPORT int get_distance_to_line(struct crosstrack_error_s * crosstrack_error, double lat_now, double lon_now, double lat_start, double lon_start, double lat_end, double lon_end); +__EXPORT int get_distance_to_line(struct crosstrack_error_s *crosstrack_error, double lat_now, double lon_now, double lat_start, double lon_start, double lat_end, double lon_end); -__EXPORT int get_distance_to_arc(struct crosstrack_error_s * crosstrack_error, double lat_now, double lon_now, double lat_center, double lon_center, - float radius, float arc_start_bearing, float arc_sweep); +__EXPORT int get_distance_to_arc(struct crosstrack_error_s *crosstrack_error, double lat_now, double lon_now, double lat_center, double lon_center, + float radius, float arc_start_bearing, float arc_sweep); /* * Calculate distance in global frame */ __EXPORT float get_distance_to_point_global_wgs84(double lat_now, double lon_now, float alt_now, - double lat_next, double lon_next, float alt_next, - float *dist_xy, float *dist_z); + double lat_next, double lon_next, float alt_next, + float *dist_xy, float *dist_z); /* * Calculate distance in local frame (NED) */ __EXPORT float mavlink_wpm_distance_to_point_local(float x_now, float y_now, float z_now, - float x_next, float y_next, float z_next, - float *dist_xy, float *dist_z); + float x_next, float y_next, float z_next, + float *dist_xy, float *dist_z); __EXPORT float _wrap_180(float bearing); __EXPORT float _wrap_360(float bearing); diff --git a/src/lib/geo/geo_mag_declination.c b/src/lib/geo/geo_mag_declination.c new file mode 100644 index 000000000..09eac38f4 --- /dev/null +++ b/src/lib/geo/geo_mag_declination.c @@ -0,0 +1,136 @@ +/**************************************************************************** + * + * Copyright (c) 2014 MAV GEO Library (MAVGEO). All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name MAVGEO nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** +* @file geo_mag_declination.c +* +* Calculation / lookup table for earth magnetic field declination. +* +* Lookup table from Scott Ferguson <scottfromscott@gmail.com> +* +* XXX Lookup table currently too coarse in resolution (only full degrees) +* and lat/lon res - needs extension medium term. +* +*/ + +#include <geo/geo.h> + +/** set this always to the sampling in degrees for the table below */ +#define SAMPLING_RES 10.0f +#define SAMPLING_MIN_LAT -60.0f +#define SAMPLING_MAX_LAT 60.0f +#define SAMPLING_MIN_LON -180.0f +#define SAMPLING_MAX_LON 180.0f + +static const int8_t declination_table[13][37] = \ +{ + 46, 45, 44, 42, 41, 40, 38, 36, 33, 28, 23, 16, 10, 4, -1, -5, -9, -14, -19, -26, -33, -40, -48, -55, -61, \ + -66, -71, -74, -75, -72, -61, -25, 22, 40, 45, 47, 46, 30, 30, 30, 30, 29, 29, 29, 29, 27, 24, 18, 11, 3, \ + -3, -9, -12, -15, -17, -21, -26, -32, -39, -45, -51, -55, -57, -56, -53, -44, -31, -14, 0, 13, 21, 26, \ + 29, 30, 21, 22, 22, 22, 22, 22, 22, 22, 21, 18, 13, 5, -3, -11, -17, -20, -21, -22, -23, -25, -29, -35, \ + -40, -44, -45, -44, -40, -32, -22, -12, -3, 3, 9, 14, 18, 20, 21, 16, 17, 17, 17, 17, 17, 16, 16, 16, 13, \ + 8, 0, -9, -16, -21, -24, -25, -25, -23, -20, -21, -24, -28, -31, -31, -29, -24, -17, -9, -3, 0, 4, 7, \ + 10, 13, 15, 16, 12, 13, 13, 13, 13, 13, 12, 12, 11, 9, 3, -4, -12, -19, -23, -24, -24, -22, -17, -12, -9, \ + -10, -13, -17, -18, -16, -13, -8, -3, 0, 1, 3, 6, 8, 10, 12, 12, 10, 10, 10, 10, 10, 10, 10, 9, 9, 6, 0, -6, \ + -14, -20, -22, -22, -19, -15, -10, -6, -2, -2, -4, -7, -8, -8, -7, -4, 0, 1, 1, 2, 4, 6, 8, 10, 10, 9, 9, 9, \ + 9, 9, 9, 8, 8, 7, 4, -1, -8, -15, -19, -20, -18, -14, -9, -5, -2, 0, 1, 0, -2, -3, -4, -3, -2, 0, 0, 0, 1, 3, 5, \ + 7, 8, 9, 8, 8, 8, 9, 9, 9, 8, 8, 6, 2, -3, -9, -15, -18, -17, -14, -10, -6, -2, 0, 1, 2, 2, 0, -1, -1, -2, -1, 0, \ + 0, 0, 0, 1, 3, 5, 7, 8, 8, 9, 9, 10, 10, 10, 10, 8, 5, 0, -5, -11, -15, -16, -15, -12, -8, -4, -1, 0, 2, 3, 2, 1, 0, \ + 0, 0, 0, 0, -1, -2, -2, -1, 0, 3, 6, 8, 6, 9, 10, 11, 12, 12, 11, 9, 5, 0, -7, -12, -15, -15, -13, -10, -7, -3, \ + 0, 1, 2, 3, 3, 3, 2, 1, 0, 0, -1, -3, -4, -5, -5, -2, 0, 3, 6, 5, 8, 11, 13, 15, 15, 14, 11, 5, -1, -9, -14, -17, \ + -16, -14, -11, -7, -3, 0, 1, 3, 4, 5, 5, 5, 4, 3, 1, -1, -4, -7, -8, -8, -6, -2, 1, 5, 4, 8, 12, 15, 17, 18, 16, \ + 12, 5, -3, -12, -18, -20, -19, -16, -13, -8, -4, -1, 1, 4, 6, 8, 9, 9, 9, 7, 3, -1, -6, -10, -12, -11, -9, -5, \ + 0, 4, 3, 9, 14, 17, 20, 21, 19, 14, 4, -8, -19, -25, -26, -25, -21, -17, -12, -7, -2, 1, 5, 9, 13, 15, 16, 16, \ + 13, 7, 0, -7, -12, -15, -14, -11, -6, -1, 3 +}; + +static float get_lookup_table_val(unsigned lat, unsigned lon); + +__EXPORT float get_mag_declination(float lat, float lon) +{ + /* + * If the values exceed valid ranges, return zero as default + * as we have no way of knowing what the closest real value + * would be. + */ + if (lat < -90.0f || lat > 90.0f || + lon < -180.0f || lon > 180.0f) { + return 0.0f; + } + + /* round down to nearest sampling resolution */ + int min_lat = (int)(lat / SAMPLING_RES) * SAMPLING_RES; + int min_lon = (int)(lon / SAMPLING_RES) * SAMPLING_RES; + + /* for the rare case of hitting the bounds exactly + * the rounding logic wouldn't fit, so enforce it. + */ + + /* limit to table bounds - required for maxima even when table spans full globe range */ + if (lat <= SAMPLING_MIN_LAT) { + min_lat = SAMPLING_MIN_LAT; + } + + if (lat >= SAMPLING_MAX_LAT) { + min_lat = (int)(lat / SAMPLING_RES) * SAMPLING_RES - SAMPLING_RES; + } + + if (lon <= SAMPLING_MIN_LON) { + min_lon = SAMPLING_MIN_LON; + } + + if (lon >= SAMPLING_MAX_LON) { + min_lon = (int)(lon / SAMPLING_RES) * SAMPLING_RES - SAMPLING_RES; + } + + /* find index of nearest low sampling point */ + unsigned min_lat_index = (-(SAMPLING_MIN_LAT) + min_lat) / SAMPLING_RES; + unsigned min_lon_index = (-(SAMPLING_MIN_LON) + min_lon) / SAMPLING_RES; + + float declination_sw = get_lookup_table_val(min_lat_index, min_lon_index); + float declination_se = get_lookup_table_val(min_lat_index, min_lon_index + 1); + float declination_ne = get_lookup_table_val(min_lat_index + 1, min_lon_index + 1); + float declination_nw = get_lookup_table_val(min_lat_index + 1, min_lon_index); + + /* perform bilinear interpolation on the four grid corners */ + + float declination_min = ((lon - min_lon) / SAMPLING_RES) * (declination_se - declination_sw) + declination_sw; + float declination_max = ((lon - min_lon) / SAMPLING_RES) * (declination_ne - declination_nw) + declination_nw; + + return ((lat - min_lat) / SAMPLING_RES) * (declination_max - declination_min) + declination_min; +} + +float get_lookup_table_val(unsigned lat_index, unsigned lon_index) +{ + return declination_table[lat_index][lon_index]; +}
\ No newline at end of file diff --git a/src/modules/att_pos_estimator_ekf/params.c b/src/lib/geo/geo_mag_declination.h index 4af5edead..0ac062d6d 100644 --- a/src/modules/att_pos_estimator_ekf/params.c +++ b/src/lib/geo/geo_mag_declination.h @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved. + * Copyright (c) 2014 MAV GEO Library (MAVGEO). All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -12,7 +12,7 @@ * notice, this list of conditions and the following disclaimer in * the documentation and/or other materials provided with the * distribution. - * 3. Neither the name PX4 nor the names of its contributors may be + * 3. Neither the name MAVGEO nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * @@ -31,19 +31,17 @@ * ****************************************************************************/ -#include <systemlib/param/param.h> +/** +* @file geo_mag_declination.h +* +* Calculation / lookup table for earth magnetic field declination. +* +*/ -/*PARAM_DEFINE_FLOAT(NAME,0.0f);*/ -PARAM_DEFINE_FLOAT(KF_V_GYRO, 0.008f); -PARAM_DEFINE_FLOAT(KF_V_ACCEL, 1.0f); -PARAM_DEFINE_FLOAT(KF_R_MAG, 0.8f); -PARAM_DEFINE_FLOAT(KF_R_GPS_VEL, 0.5f); -PARAM_DEFINE_FLOAT(KF_R_GPS_POS, 2.0f); -PARAM_DEFINE_FLOAT(KF_R_GPS_ALT, 3.0f); -PARAM_DEFINE_FLOAT(KF_R_PRESS_ALT, 0.1f); -PARAM_DEFINE_FLOAT(KF_R_ACCEL, 1.0f); -PARAM_DEFINE_FLOAT(KF_FAULT_POS, 10.0f); -PARAM_DEFINE_FLOAT(KF_FAULT_ATT, 10.0f); -PARAM_DEFINE_FLOAT(KF_ENV_G, 9.765f); -PARAM_DEFINE_FLOAT(KF_ENV_MAG_DIP, 60.0f); -PARAM_DEFINE_FLOAT(KF_ENV_MAG_DEC, 0.0f); +#pragma once + +__BEGIN_DECLS + +__EXPORT float get_mag_declination(float lat, float lon); + +__END_DECLS diff --git a/src/lib/geo/module.mk b/src/lib/geo/module.mk index 30a2dc99f..9500a2bcc 100644 --- a/src/lib/geo/module.mk +++ b/src/lib/geo/module.mk @@ -35,4 +35,5 @@ # Geo library # -SRCS = geo.c +SRCS = geo.c \ + geo_mag_declination.c diff --git a/src/lib/launchdetection/CatapultLaunchMethod.cpp b/src/lib/launchdetection/CatapultLaunchMethod.cpp index 12f80c4a3..c555a0a69 100644 --- a/src/lib/launchdetection/CatapultLaunchMethod.cpp +++ b/src/lib/launchdetection/CatapultLaunchMethod.cpp @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2013 Estimation and Control Library (ECL). All rights reserved. + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -10,9 +10,9 @@ * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in - * the documentation4 and/or other materials provided with the + * the documentation and/or other materials provided with the * distribution. - * 3. Neither the name ECL nor the names of its contributors may be + * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * @@ -33,9 +33,10 @@ /** * @file CatapultLaunchMethod.cpp - * Catpult Launch detection + * Catapult Launch detection + * + * @author Thomas Gubler <thomasgubler@gmail.com> * - * Authors and acknowledgements in header. */ #include "CatapultLaunchMethod.h" diff --git a/src/lib/launchdetection/CatapultLaunchMethod.h b/src/lib/launchdetection/CatapultLaunchMethod.h index 55c46ff3f..23757f6f3 100644 --- a/src/lib/launchdetection/CatapultLaunchMethod.h +++ b/src/lib/launchdetection/CatapultLaunchMethod.h @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2013 Estimation and Control Library (ECL). All rights reserved. + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -10,9 +10,9 @@ * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in - * the documentation4 and/or other materials provided with the + * the documentation and/or other materials provided with the * distribution. - * 3. Neither the name ECL nor the names of its contributors may be + * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * diff --git a/src/lib/launchdetection/LaunchDetector.cpp b/src/lib/launchdetection/LaunchDetector.cpp index bf539701b..3bf47bbb0 100644 --- a/src/lib/launchdetection/LaunchDetector.cpp +++ b/src/lib/launchdetection/LaunchDetector.cpp @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2013 Estimation and Control Library (ECL). All rights reserved. + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -12,7 +12,7 @@ * notice, this list of conditions and the following disclaimer in * the documentation and/or other materials provided with the * distribution. - * 3. Neither the name ECL nor the names of its contributors may be + * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * @@ -30,12 +30,11 @@ * POSSIBILITY OF SUCH DAMAGE. * ****************************************************************************/ - /** * @file launchDetection.cpp * Auto Detection for different launch methods (e.g. catapult) * - * Authors and acknowledgements in header. + * @author Thomas Gubler <thomasgubler@gmail.com> */ #include "LaunchDetector.h" diff --git a/src/lib/launchdetection/LaunchDetector.h b/src/lib/launchdetection/LaunchDetector.h index 8066ebab3..1a214b66e 100644 --- a/src/lib/launchdetection/LaunchDetector.h +++ b/src/lib/launchdetection/LaunchDetector.h @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2013 Estimation and Control Library (ECL). All rights reserved. + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -10,9 +10,9 @@ * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in - * the documentation4 and/or other materials provided with the + * the documentation and/or other materials provided with the * distribution. - * 3. Neither the name ECL nor the names of its contributors may be + * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * diff --git a/src/lib/launchdetection/LaunchMethod.h b/src/lib/launchdetection/LaunchMethod.h index 01fa7050e..e04467f6a 100644 --- a/src/lib/launchdetection/LaunchMethod.h +++ b/src/lib/launchdetection/LaunchMethod.h @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2013 Estimation and Control Library (ECL). All rights reserved. + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -10,9 +10,9 @@ * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in - * the documentation4 and/or other materials provided with the + * the documentation and/or other materials provided with the * distribution. - * 3. Neither the name ECL nor the names of its contributors may be + * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * diff --git a/src/lib/launchdetection/launchdetection_params.c b/src/lib/launchdetection/launchdetection_params.c index 45d7957f1..8df8c696c 100644 --- a/src/lib/launchdetection/launchdetection_params.c +++ b/src/lib/launchdetection/launchdetection_params.c @@ -1,7 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2013 PX4 Development Team. All rights reserved. - * Author: Lorenz Meier <lm@inf.ethz.ch> + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -18,7 +17,7 @@ * without specific prior written permission. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS - * AS IS AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, diff --git a/src/lib/launchdetection/module.mk b/src/lib/launchdetection/module.mk index 13648b74c..de0174e37 100644 --- a/src/lib/launchdetection/module.mk +++ b/src/lib/launchdetection/module.mk @@ -1,6 +1,6 @@ ############################################################################ # -# Copyright (c) 2013 Estimation and Control Library (ECL). All rights reserved. +# Copyright (c) 2012, 2013, 2014 PX4 Development Team. All rights reserved. # # Redistribution and use in source and binary forms, with or without # modification, are permitted provided that the following conditions diff --git a/src/lib/mathlib/CMSIS/Include/arm_math.h b/src/lib/mathlib/CMSIS/Include/arm_math.h index 6f66f9ee3..61d3a3b61 100644 --- a/src/lib/mathlib/CMSIS/Include/arm_math.h +++ b/src/lib/mathlib/CMSIS/Include/arm_math.h @@ -5193,7 +5193,7 @@ void arm_rfft_fast_f32( *pIa = Ialpha;
/* Calculating pIb from Ialpha and Ibeta by equation pIb = -(1/2) * Ialpha + (sqrt(3)/2) * Ibeta */
- *pIb = -0.5 * Ialpha + (float32_t) 0.8660254039 *Ibeta;
+ *pIb = (float32_t)-0.5 * Ialpha + (float32_t) 0.8660254039 *Ibeta;
}
diff --git a/src/lib/mathlib/math/filter/LowPassFilter2p.cpp b/src/lib/mathlib/math/filter/LowPassFilter2p.cpp index 3699d9bce..6f640c9f9 100644 --- a/src/lib/mathlib/math/filter/LowPassFilter2p.cpp +++ b/src/lib/mathlib/math/filter/LowPassFilter2p.cpp @@ -69,7 +69,7 @@ float LowPassFilter2p::apply(float sample) // do the filtering float delay_element_0 = sample - _delay_element_1 * _a1 - _delay_element_2 * _a2; if (isnan(delay_element_0) || isinf(delay_element_0)) { - // don't allow bad values to propogate via the filter + // don't allow bad values to propagate via the filter delay_element_0 = sample; } float output = delay_element_0 * _b0 + _delay_element_1 * _b1 + _delay_element_2 * _b2; @@ -81,5 +81,10 @@ float LowPassFilter2p::apply(float sample) return output; } +float LowPassFilter2p::reset(float sample) { + _delay_element_1 = _delay_element_2 = sample; + return apply(sample); +} + } // namespace math diff --git a/src/lib/mathlib/math/filter/LowPassFilter2p.hpp b/src/lib/mathlib/math/filter/LowPassFilter2p.hpp index 208ec98d4..74cd5d78c 100644 --- a/src/lib/mathlib/math/filter/LowPassFilter2p.hpp +++ b/src/lib/mathlib/math/filter/LowPassFilter2p.hpp @@ -52,18 +52,30 @@ public: _delay_element_1 = _delay_element_2 = 0; } - // change parameters + /** + * Change filter parameters + */ void set_cutoff_frequency(float sample_freq, float cutoff_freq); - // apply - Add a new raw value to the filter - // and retrieve the filtered result + /** + * Add a new raw value to the filter + * + * @return retrieve the filtered result + */ float apply(float sample); - // return the cutoff frequency + /** + * Return the cutoff frequency + */ float get_cutoff_freq(void) const { return _cutoff_freq; } + /** + * Reset the filter state to this value + */ + float reset(float sample); + private: float _cutoff_freq; float _a1; diff --git a/src/lib/version/version.h b/src/lib/version/version.h index af733aaf0..d8ccb6774 100644 --- a/src/lib/version/version.h +++ b/src/lib/version/version.h @@ -59,4 +59,8 @@ #define HW_ARCH "PX4FMU_V2" #endif +#ifdef CONFIG_ARCH_BOARD_AEROCORE +#define HW_ARCH "AEROCORE" +#endif + #endif /* VERSION_H_ */ diff --git a/src/modules/att_pos_estimator_ekf/KalmanNav.cpp b/src/modules/att_pos_estimator_ekf/KalmanNav.cpp deleted file mode 100644 index 668bac5d9..000000000 --- a/src/modules/att_pos_estimator_ekf/KalmanNav.cpp +++ /dev/null @@ -1,815 +0,0 @@ -/**************************************************************************** - * - * Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved. - * - * Redistribution and use in source and binary forms, with or without - * modification, are permitted provided that the following conditions - * are met: - * - * 1. Redistributions of source code must retain the above copyright - * notice, this list of conditions and the following disclaimer. - * 2. Redistributions in binary form must reproduce the above copyright - * notice, this list of conditions and the following disclaimer in - * the documentation and/or other materials provided with the - * distribution. - * 3. Neither the name PX4 nor the names of its contributors may be - * used to endorse or promote products derived from this software - * without specific prior written permission. - * - * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS - * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT - * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS - * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE - * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, - * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, - * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS - * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED - * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT - * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN - * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE - * POSSIBILITY OF SUCH DAMAGE. - * - ****************************************************************************/ - -/** - * @file KalmanNav.cpp - * - * Kalman filter navigation code - */ - -#include <poll.h> - -#include "KalmanNav.hpp" -#include <systemlib/err.h> -#include <geo/geo.h> - -// constants -// Titterton pg. 52 -static const float omega = 7.2921150e-5f; // earth rotation rate, rad/s -static const float R0 = 6378137.0f; // earth radius, m -static const float g0 = 9.806f; // standard gravitational accel. m/s^2 -static const int8_t ret_ok = 0; // no error in function -static const int8_t ret_error = -1; // error occurred - -KalmanNav::KalmanNav(SuperBlock *parent, const char *name) : - SuperBlock(parent, name), - // subscriptions - _sensors(&getSubscriptions(), ORB_ID(sensor_combined), 5), // limit to 200 Hz - _gps(&getSubscriptions(), ORB_ID(vehicle_gps_position), 100), // limit to 10 Hz - _param_update(&getSubscriptions(), ORB_ID(parameter_update), 1000), // limit to 1 Hz - // publications - _pos(&getPublications(), ORB_ID(vehicle_global_position)), - _localPos(&getPublications(), ORB_ID(vehicle_local_position)), - _att(&getPublications(), ORB_ID(vehicle_attitude)), - // timestamps - _pubTimeStamp(hrt_absolute_time()), - _predictTimeStamp(hrt_absolute_time()), - _attTimeStamp(hrt_absolute_time()), - _outTimeStamp(hrt_absolute_time()), - // frame count - _navFrames(0), - // miss counts - _miss(0), - // accelerations - fN(0), fE(0), fD(0), - // state - phi(0), theta(0), psi(0), - vN(0), vE(0), vD(0), - lat(0), lon(0), alt(0), - lat0(0), lon0(0), alt0(0), - // parameters for ground station - _vGyro(this, "V_GYRO"), - _vAccel(this, "V_ACCEL"), - _rMag(this, "R_MAG"), - _rGpsVel(this, "R_GPS_VEL"), - _rGpsPos(this, "R_GPS_POS"), - _rGpsAlt(this, "R_GPS_ALT"), - _rPressAlt(this, "R_PRESS_ALT"), - _rAccel(this, "R_ACCEL"), - _magDip(this, "ENV_MAG_DIP"), - _magDec(this, "ENV_MAG_DEC"), - _g(this, "ENV_G"), - _faultPos(this, "FAULT_POS"), - _faultAtt(this, "FAULT_ATT"), - _attitudeInitialized(false), - _positionInitialized(false), - _attitudeInitCounter(0) -{ - using namespace math; - - F.zero(); - G.zero(); - V.zero(); - HAtt.zero(); - RAtt.zero(); - HPos.zero(); - RPos.zero(); - - // initial state covariance matrix - P0.identity(); - P0 *= 0.01f; - P = P0; - - // initial state - phi = 0.0f; - theta = 0.0f; - psi = 0.0f; - vN = 0.0f; - vE = 0.0f; - vD = 0.0f; - lat = 0.0f; - lon = 0.0f; - alt = 0.0f; - - // initialize rotation quaternion with a single raw sensor measurement - _sensors.update(); - q = init( - _sensors.accelerometer_m_s2[0], - _sensors.accelerometer_m_s2[1], - _sensors.accelerometer_m_s2[2], - _sensors.magnetometer_ga[0], - _sensors.magnetometer_ga[1], - _sensors.magnetometer_ga[2]); - - // initialize dcm - C_nb = q.to_dcm(); - - // HPos is constant - HPos(0, 3) = 1.0f; - HPos(1, 4) = 1.0f; - HPos(2, 6) = 1.0e7f * M_RAD_TO_DEG_F; - HPos(3, 7) = 1.0e7f * M_RAD_TO_DEG_F; - HPos(4, 8) = 1.0f; - HPos(5, 8) = 1.0f; - - // initialize all parameters - updateParams(); -} - -math::Quaternion KalmanNav::init(float ax, float ay, float az, float mx, float my, float mz) -{ - float initialRoll, initialPitch; - float cosRoll, sinRoll, cosPitch, sinPitch; - float magX, magY; - float initialHdg, cosHeading, sinHeading; - - initialRoll = atan2(-ay, -az); - initialPitch = atan2(ax, -az); - - cosRoll = cosf(initialRoll); - sinRoll = sinf(initialRoll); - cosPitch = cosf(initialPitch); - sinPitch = sinf(initialPitch); - - magX = mx * cosPitch + my * sinRoll * sinPitch + mz * cosRoll * sinPitch; - - magY = my * cosRoll - mz * sinRoll; - - initialHdg = atan2f(-magY, magX); - - cosRoll = cosf(initialRoll * 0.5f); - sinRoll = sinf(initialRoll * 0.5f); - - cosPitch = cosf(initialPitch * 0.5f); - sinPitch = sinf(initialPitch * 0.5f); - - cosHeading = cosf(initialHdg * 0.5f); - sinHeading = sinf(initialHdg * 0.5f); - - float q0 = cosRoll * cosPitch * cosHeading + sinRoll * sinPitch * sinHeading; - float q1 = sinRoll * cosPitch * cosHeading - cosRoll * sinPitch * sinHeading; - float q2 = cosRoll * sinPitch * cosHeading + sinRoll * cosPitch * sinHeading; - float q3 = cosRoll * cosPitch * sinHeading - sinRoll * sinPitch * cosHeading; - - return math::Quaternion(q0, q1, q2, q3); - -} - -void KalmanNav::update() -{ - using namespace math; - - struct pollfd fds[1]; - fds[0].fd = _sensors.getHandle(); - fds[0].events = POLLIN; - - // poll for new data - int ret = poll(fds, 1, 1000); - - if (ret < 0) { - // XXX this is seriously bad - should be an emergency - return; - - } else if (ret == 0) { // timeout - return; - } - - // get new timestamp - uint64_t newTimeStamp = hrt_absolute_time(); - - // check updated subscriptions - if (_param_update.updated()) updateParams(); - - bool gpsUpdate = _gps.updated(); - bool sensorsUpdate = _sensors.updated(); - - // get new information from subscriptions - // this clears update flag - updateSubscriptions(); - - // initialize attitude when sensors online - if (!_attitudeInitialized && sensorsUpdate) { - if (correctAtt() == ret_ok) _attitudeInitCounter++; - - if (_attitudeInitCounter > 100) { - warnx("initialized EKF attitude"); - warnx("phi: %8.4f, theta: %8.4f, psi: %8.4f", - double(phi), double(theta), double(psi)); - _attitudeInitialized = true; - } - } - - // initialize position when gps received - if (!_positionInitialized && - _attitudeInitialized && // wait for attitude first - gpsUpdate && - _gps.fix_type > 2 - //&& _gps.counter_pos_valid > 10 - ) { - vN = _gps.vel_n_m_s; - vE = _gps.vel_e_m_s; - vD = _gps.vel_d_m_s; - setLatDegE7(_gps.lat); - setLonDegE7(_gps.lon); - setAltE3(_gps.alt); - // set reference position for - // local position - lat0 = lat; - lon0 = lon; - alt0 = alt; - // XXX map_projection has internal global - // states that multiple things could change, - // should make map_projection take reference - // lat/lon and not have init - map_projection_init(lat0, lon0); - _positionInitialized = true; - warnx("initialized EKF state with GPS"); - warnx("vN: %8.4f, vE: %8.4f, vD: %8.4f, lat: %8.4f, lon: %8.4f, alt: %8.4f", - double(vN), double(vE), double(vD), - lat, lon, double(alt)); - } - - // prediction step - // using sensors timestamp so we can account for packet lag - float dt = (_sensors.timestamp - _predictTimeStamp) / 1.0e6f; - //printf("dt: %15.10f\n", double(dt)); - _predictTimeStamp = _sensors.timestamp; - - // don't predict if time greater than a second - if (dt < 1.0f) { - predictState(dt); - predictStateCovariance(dt); - // count fast frames - _navFrames += 1; - } - - // count times 100 Hz rate isn't met - if (dt > 0.01f) _miss++; - - // gps correction step - if (_positionInitialized && gpsUpdate) { - correctPos(); - } - - // attitude correction step - if (_attitudeInitialized // initialized - && sensorsUpdate // new data - && _sensors.timestamp - _attTimeStamp > 1e6 / 50 // 50 Hz - ) { - _attTimeStamp = _sensors.timestamp; - correctAtt(); - } - - // publication - if (newTimeStamp - _pubTimeStamp > 1e6 / 50) { // 50 Hz - _pubTimeStamp = newTimeStamp; - - updatePublications(); - } - - // output - if (newTimeStamp - _outTimeStamp > 10e6) { // 0.1 Hz - _outTimeStamp = newTimeStamp; - //printf("nav: %4d Hz, miss #: %4d\n", - // _navFrames / 10, _miss / 10); - _navFrames = 0; - _miss = 0; - } -} - -void KalmanNav::updatePublications() -{ - using namespace math; - - // global position publication - _pos.timestamp = _pubTimeStamp; - _pos.time_gps_usec = _gps.timestamp_position; - _pos.global_valid = true; - _pos.lat = lat * M_RAD_TO_DEG; - _pos.lon = lon * M_RAD_TO_DEG; - _pos.alt = float(alt); - _pos.vel_n = vN; - _pos.vel_e = vE; - _pos.vel_d = vD; - _pos.yaw = psi; - - // local position publication - float x; - float y; - bool landed = alt < (alt0 + 0.1); // XXX improve? - map_projection_project(lat, lon, &x, &y); - _localPos.timestamp = _pubTimeStamp; - _localPos.xy_valid = true; - _localPos.z_valid = true; - _localPos.v_xy_valid = true; - _localPos.v_z_valid = true; - _localPos.x = x; - _localPos.y = y; - _localPos.z = alt0 - alt; - _localPos.vx = vN; - _localPos.vy = vE; - _localPos.vz = vD; - _localPos.yaw = psi; - _localPos.xy_global = true; - _localPos.z_global = true; - _localPos.ref_timestamp = _pubTimeStamp; - _localPos.ref_lat = getLatDegE7(); - _localPos.ref_lon = getLonDegE7(); - _localPos.ref_alt = 0; - _localPos.landed = landed; - - // attitude publication - _att.timestamp = _pubTimeStamp; - _att.roll = phi; - _att.pitch = theta; - _att.yaw = psi; - _att.rollspeed = _sensors.gyro_rad_s[0]; - _att.pitchspeed = _sensors.gyro_rad_s[1]; - _att.yawspeed = _sensors.gyro_rad_s[2]; - // TODO, add gyro offsets to filter - _att.rate_offsets[0] = 0.0f; - _att.rate_offsets[1] = 0.0f; - _att.rate_offsets[2] = 0.0f; - - for (int i = 0; i < 3; i++) for (int j = 0; j < 3; j++) - _att.R[i][j] = C_nb(i, j); - - for (int i = 0; i < 4; i++) _att.q[i] = q(i); - - _att.R_valid = true; - _att.q_valid = true; - - // selectively update publications, - // do NOT call superblock do-all method - if (_positionInitialized) { - _pos.update(); - _localPos.update(); - } - - if (_attitudeInitialized) - _att.update(); -} - -int KalmanNav::predictState(float dt) -{ - using namespace math; - - // trig - float sinL = sinf(lat); - float cosL = cosf(lat); - float cosLSing = cosf(lat); - - // prevent singularity - if (fabsf(cosLSing) < 0.01f) { - if (cosLSing > 0) cosLSing = 0.01; - else cosLSing = -0.01; - } - - // attitude prediction - if (_attitudeInitialized) { - Vector<3> w(_sensors.gyro_rad_s); - - // attitude - q = q + q.derivative(w) * dt; - - // renormalize quaternion if needed - if (fabsf(q.length() - 1.0f) > 1e-4f) { - q.normalize(); - } - - // C_nb update - C_nb = q.to_dcm(); - - // euler update - Vector<3> euler = C_nb.to_euler(); - phi = euler.data[0]; - theta = euler.data[1]; - psi = euler.data[2]; - - // specific acceleration in nav frame - Vector<3> accelB(_sensors.accelerometer_m_s2); - Vector<3> accelN = C_nb * accelB; - fN = accelN(0); - fE = accelN(1); - fD = accelN(2); - } - - // position prediction - if (_positionInitialized) { - // neglects angular deflections in local gravity - // see Titerton pg. 70 - float R = R0 + float(alt); - float LDot = vN / R; - float lDot = vE / (cosLSing * R); - float rotRate = 2 * omega + lDot; - - // XXX position prediction using speed - float vNDot = fN - vE * rotRate * sinL + - vD * LDot; - float vDDot = fD - vE * rotRate * cosL - - vN * LDot + _g.get(); - float vEDot = fE + vN * rotRate * sinL + - vDDot * rotRate * cosL; - - // rectangular integration - vN += vNDot * dt; - vE += vEDot * dt; - vD += vDDot * dt; - lat += double(LDot * dt); - lon += double(lDot * dt); - alt += double(-vD * dt); - } - - return ret_ok; -} - -int KalmanNav::predictStateCovariance(float dt) -{ - using namespace math; - - // trig - float sinL = sinf(lat); - float cosL = cosf(lat); - float cosLSq = cosL * cosL; - float tanL = tanf(lat); - - // prepare for matrix - float R = R0 + float(alt); - float RSq = R * R; - - // F Matrix - // Titterton pg. 291 - - F(0, 1) = -(omega * sinL + vE * tanL / R); - F(0, 2) = vN / R; - F(0, 4) = 1.0f / R; - F(0, 6) = -omega * sinL; - F(0, 8) = -vE / RSq; - - F(1, 0) = omega * sinL + vE * tanL / R; - F(1, 2) = omega * cosL + vE / R; - F(1, 3) = -1.0f / R; - F(1, 8) = vN / RSq; - - F(2, 0) = -vN / R; - F(2, 1) = -omega * cosL - vE / R; - F(2, 4) = -tanL / R; - F(2, 6) = -omega * cosL - vE / (R * cosLSq); - F(2, 8) = vE * tanL / RSq; - - F(3, 1) = -fD; - F(3, 2) = fE; - F(3, 3) = vD / R; - F(3, 4) = -2 * (omega * sinL + vE * tanL / R); - F(3, 5) = vN / R; - F(3, 6) = -vE * (2 * omega * cosL + vE / (R * cosLSq)); - F(3, 8) = (vE * vE * tanL - vN * vD) / RSq; - - F(4, 0) = fD; - F(4, 2) = -fN; - F(4, 3) = 2 * omega * sinL + vE * tanL / R; - F(4, 4) = (vN * tanL + vD) / R; - F(4, 5) = 2 * omega * cosL + vE / R; - F(4, 6) = 2 * omega * (vN * cosL - vD * sinL) + - vN * vE / (R * cosLSq); - F(4, 8) = -vE * (vN * tanL + vD) / RSq; - - F(5, 0) = -fE; - F(5, 1) = fN; - F(5, 3) = -2 * vN / R; - F(5, 4) = -2 * (omega * cosL + vE / R); - F(5, 6) = 2 * omega * vE * sinL; - F(5, 8) = (vN * vN + vE * vE) / RSq; - - F(6, 3) = 1 / R; - F(6, 8) = -vN / RSq; - - F(7, 4) = 1 / (R * cosL); - F(7, 6) = vE * tanL / (R * cosL); - F(7, 8) = -vE / (cosL * RSq); - - F(8, 5) = -1; - - // G Matrix - // Titterton pg. 291 - G(0, 0) = -C_nb(0, 0); - G(0, 1) = -C_nb(0, 1); - G(0, 2) = -C_nb(0, 2); - G(1, 0) = -C_nb(1, 0); - G(1, 1) = -C_nb(1, 1); - G(1, 2) = -C_nb(1, 2); - G(2, 0) = -C_nb(2, 0); - G(2, 1) = -C_nb(2, 1); - G(2, 2) = -C_nb(2, 2); - - G(3, 3) = C_nb(0, 0); - G(3, 4) = C_nb(0, 1); - G(3, 5) = C_nb(0, 2); - G(4, 3) = C_nb(1, 0); - G(4, 4) = C_nb(1, 1); - G(4, 5) = C_nb(1, 2); - G(5, 3) = C_nb(2, 0); - G(5, 4) = C_nb(2, 1); - G(5, 5) = C_nb(2, 2); - - // continuous prediction equations - // for discrete time EKF - // http://en.wikipedia.org/wiki/Extended_Kalman_filter - P = P + (F * P + P * F.transposed() + G * V * G.transposed()) * dt; - - return ret_ok; -} - -int KalmanNav::correctAtt() -{ - using namespace math; - - // trig - float cosPhi = cosf(phi); - float cosTheta = cosf(theta); - // float cosPsi = cosf(psi); - float sinPhi = sinf(phi); - float sinTheta = sinf(theta); - // float sinPsi = sinf(psi); - - // mag predicted measurement - // choosing some typical magnetic field properties, - // TODO dip/dec depend on lat/ lon/ time - //float dip = _magDip.get() / M_RAD_TO_DEG_F; // dip, inclination with level - float dec = _magDec.get() / M_RAD_TO_DEG_F; // declination, clockwise rotation from north - - // compensate roll and pitch, but not yaw - // XXX take the vectors out of the C_nb matrix to avoid singularities - math::Matrix<3,3> C_rp; - C_rp.from_euler(phi, theta, 0.0f);//C_nb.transposed(); - - // mag measurement - Vector<3> magBody(_sensors.magnetometer_ga); - - // transform to earth frame - Vector<3> magNav = C_rp * magBody; - - // calculate error between estimate and measurement - // apply declination correction for true heading as well. - float yMag = -atan2f(magNav(1),magNav(0)) - psi - dec; - if (yMag > M_PI_F) yMag -= 2*M_PI_F; - if (yMag < -M_PI_F) yMag += 2*M_PI_F; - - // accel measurement - Vector<3> zAccel(_sensors.accelerometer_m_s2); - float accelMag = zAccel.length(); - zAccel.normalize(); - - // ignore accel correction when accel mag not close to g - Matrix<4,4> RAttAdjust = RAtt; - - bool ignoreAccel = fabsf(accelMag - _g.get()) > 1.1f; - - if (ignoreAccel) { - RAttAdjust(1, 1) = 1.0e10; - RAttAdjust(2, 2) = 1.0e10; - RAttAdjust(3, 3) = 1.0e10; - - } else { - //printf("correcting attitude with accel\n"); - } - - // accel predicted measurement - Vector<3> zAccelHat = (C_nb.transposed() * Vector<3>(0, 0, -_g.get())).normalized(); - - // calculate residual - Vector<4> y(yMag, zAccel(0) - zAccelHat(0), zAccel(1) - zAccelHat(1), zAccel(2) - zAccelHat(2)); - - // HMag - HAtt(0, 2) = 1; - - // HAccel - HAtt(1, 1) = cosTheta; - HAtt(2, 0) = -cosPhi * cosTheta; - HAtt(2, 1) = sinPhi * sinTheta; - HAtt(3, 0) = sinPhi * cosTheta; - HAtt(3, 1) = cosPhi * sinTheta; - - // compute correction - // http://en.wikipedia.org/wiki/Extended_Kalman_filter - Matrix<4, 4> S = HAtt * P * HAtt.transposed() + RAttAdjust; // residual covariance - Matrix<9, 4> K = P * HAtt.transposed() * S.inversed(); - Vector<9> xCorrect = K * y; - - // check correciton is sane - for (size_t i = 0; i < xCorrect.get_size(); i++) { - float val = xCorrect(i); - - if (isnan(val) || isinf(val)) { - // abort correction and return - warnx("numerical failure in att correction"); - // reset P matrix to P0 - P = P0; - return ret_error; - } - } - - // correct state - if (!ignoreAccel) { - phi += xCorrect(PHI); - theta += xCorrect(THETA); - } - - psi += xCorrect(PSI); - - // attitude also affects nav velocities - if (_positionInitialized) { - vN += xCorrect(VN); - vE += xCorrect(VE); - vD += xCorrect(VD); - } - - // update state covariance - // http://en.wikipedia.org/wiki/Extended_Kalman_filter - P = P - K * HAtt * P; - - // fault detection - float beta = y * (S.inversed() * y); - - if (beta > _faultAtt.get()) { - warnx("fault in attitude: beta = %8.4f", (double)beta); - warnx("y:"); y.print(); - } - - // update quaternions from euler - // angle correction - q.from_euler(phi, theta, psi); - - return ret_ok; -} - -int KalmanNav::correctPos() -{ - using namespace math; - - // residual - Vector<6> y; - y(0) = _gps.vel_n_m_s - vN; - y(1) = _gps.vel_e_m_s - vE; - y(2) = double(_gps.lat) - double(lat) * 1.0e7 * M_RAD_TO_DEG; - y(3) = double(_gps.lon) - double(lon) * 1.0e7 * M_RAD_TO_DEG; - y(4) = _gps.alt / 1.0e3f - alt; - y(5) = _sensors.baro_alt_meter - alt; - - // compute correction - // http://en.wikipedia.org/wiki/Extended_Kalman_filter - Matrix<6,6> S = HPos * P * HPos.transposed() + RPos; // residual covariance - Matrix<9,6> K = P * HPos.transposed() * S.inversed(); - Vector<9> xCorrect = K * y; - - // check correction is sane - for (size_t i = 0; i < xCorrect.get_size(); i++) { - float val = xCorrect(i); - - if (!isfinite(val)) { - // abort correction and return - warnx("numerical failure in gps correction"); - // fallback to GPS - vN = _gps.vel_n_m_s; - vE = _gps.vel_e_m_s; - vD = _gps.vel_d_m_s; - setLatDegE7(_gps.lat); - setLonDegE7(_gps.lon); - setAltE3(_gps.alt); - // reset P matrix to P0 - P = P0; - return ret_error; - } - } - - // correct state - vN += xCorrect(VN); - vE += xCorrect(VE); - vD += xCorrect(VD); - lat += double(xCorrect(LAT)); - lon += double(xCorrect(LON)); - alt += xCorrect(ALT); - - // update state covariance - // http://en.wikipedia.org/wiki/Extended_Kalman_filter - P = P - K * HPos * P; - - // fault detetcion - float beta = y * (S.inversed() * y); - - static int counter = 0; - if (beta > _faultPos.get() && (counter % 10 == 0)) { - warnx("fault in gps: beta = %8.4f", (double)beta); - warnx("Y/N: vN: %8.4f, vE: %8.4f, lat: %8.4f, lon: %8.4f, alt: %8.4f, baro: %8.4f", - double(y(0) / sqrtf(RPos(0, 0))), - double(y(1) / sqrtf(RPos(1, 1))), - double(y(2) / sqrtf(RPos(2, 2))), - double(y(3) / sqrtf(RPos(3, 3))), - double(y(4) / sqrtf(RPos(4, 4))), - double(y(5) / sqrtf(RPos(5, 5)))); - } - counter++; - - return ret_ok; -} - -void KalmanNav::updateParams() -{ - using namespace math; - using namespace control; - SuperBlock::updateParams(); - - // gyro noise - V(0, 0) = _vGyro.get(); // gyro x, rad/s - V(1, 1) = _vGyro.get(); // gyro y - V(2, 2) = _vGyro.get(); // gyro z - - // accel noise - V(3, 3) = _vAccel.get(); // accel x, m/s^2 - V(4, 4) = _vAccel.get(); // accel y - V(5, 5) = _vAccel.get(); // accel z - - // magnetometer noise - float noiseMin = 1e-6f; - float noiseMagSq = _rMag.get() * _rMag.get(); - - if (noiseMagSq < noiseMin) noiseMagSq = noiseMin; - - RAtt(0, 0) = noiseMagSq; // normalized direction - - // accelerometer noise - float noiseAccelSq = _rAccel.get() * _rAccel.get(); - - // bound noise to prevent singularities - if (noiseAccelSq < noiseMin) noiseAccelSq = noiseMin; - - RAtt(1, 1) = noiseAccelSq; // normalized direction - RAtt(2, 2) = noiseAccelSq; - RAtt(3, 3) = noiseAccelSq; - - // gps noise - float R = R0 + float(alt); - float cosLSing = cosf(lat); - - // prevent singularity - if (fabsf(cosLSing) < 0.01f) { - if (cosLSing > 0) cosLSing = 0.01; - else cosLSing = -0.01; - } - - float noiseVel = _rGpsVel.get(); - float noiseLatDegE7 = 1.0e7f * M_RAD_TO_DEG_F * _rGpsPos.get() / R; - float noiseLonDegE7 = noiseLatDegE7 / cosLSing; - float noiseGpsAlt = _rGpsAlt.get(); - float noisePressAlt = _rPressAlt.get(); - - // bound noise to prevent singularities - if (noiseVel < noiseMin) noiseVel = noiseMin; - - if (noiseLatDegE7 < noiseMin) noiseLatDegE7 = noiseMin; - - if (noiseLonDegE7 < noiseMin) noiseLonDegE7 = noiseMin; - - if (noiseGpsAlt < noiseMin) noiseGpsAlt = noiseMin; - - if (noisePressAlt < noiseMin) noisePressAlt = noiseMin; - - RPos(0, 0) = noiseVel * noiseVel; // vn - RPos(1, 1) = noiseVel * noiseVel; // ve - RPos(2, 2) = noiseLatDegE7 * noiseLatDegE7; // lat - RPos(3, 3) = noiseLonDegE7 * noiseLonDegE7; // lon - RPos(4, 4) = noiseGpsAlt * noiseGpsAlt; // h - RPos(5, 5) = noisePressAlt * noisePressAlt; // h - // XXX, note that RPos depends on lat, so updateParams should - // be called if lat changes significantly -} diff --git a/src/modules/att_pos_estimator_ekf/KalmanNav.hpp b/src/modules/att_pos_estimator_ekf/KalmanNav.hpp deleted file mode 100644 index caf93bc78..000000000 --- a/src/modules/att_pos_estimator_ekf/KalmanNav.hpp +++ /dev/null @@ -1,192 +0,0 @@ -/**************************************************************************** - * - * Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved. - * - * Redistribution and use in source and binary forms, with or without - * modification, are permitted provided that the following conditions - * are met: - * - * 1. Redistributions of source code must retain the above copyright - * notice, this list of conditions and the following disclaimer. - * 2. Redistributions in binary form must reproduce the above copyright - * notice, this list of conditions and the following disclaimer in - * the documentation and/or other materials provided with the - * distribution. - * 3. Neither the name PX4 nor the names of its contributors may be - * used to endorse or promote products derived from this software - * without specific prior written permission. - * - * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS - * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT - * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS - * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE - * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, - * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, - * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS - * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED - * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT - * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN - * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE - * POSSIBILITY OF SUCH DAMAGE. - * - ****************************************************************************/ - -/** - * @file KalmanNav.hpp - * - * kalman filter navigation code - */ - -#pragma once - -//#define MATRIX_ASSERT -//#define VECTOR_ASSERT - -#include <nuttx/config.h> - -#include <mathlib/mathlib.h> -#include <controllib/blocks.hpp> -#include <controllib/block/BlockParam.hpp> -#include <uORB/Subscription.hpp> -#include <uORB/Publication.hpp> - -#include <uORB/topics/vehicle_attitude.h> -#include <uORB/topics/vehicle_global_position.h> -#include <uORB/topics/vehicle_local_position.h> -#include <uORB/topics/sensor_combined.h> -#include <uORB/topics/vehicle_gps_position.h> -#include <uORB/topics/parameter_update.h> - -#include <drivers/drv_accel.h> -#include <drivers/drv_gyro.h> -#include <drivers/drv_mag.h> - -#include <drivers/drv_hrt.h> -#include <poll.h> -#include <unistd.h> - -/** - * Kalman filter navigation class - * http://en.wikipedia.org/wiki/Extended_Kalman_filter - * Discrete-time extended Kalman filter - */ -class KalmanNav : public control::SuperBlock -{ -public: - /** - * Constructor - */ - KalmanNav(SuperBlock *parent, const char *name); - - /** - * Deconstuctor - */ - - virtual ~KalmanNav() {}; - - math::Quaternion init(float ax, float ay, float az, float mx, float my, float mz); - - /** - * The main callback function for the class - */ - void update(); - - - /** - * Publication update - */ - virtual void updatePublications(); - - /** - * State prediction - * Continuous, non-linear - */ - int predictState(float dt); - - /** - * State covariance prediction - * Continuous, linear - */ - int predictStateCovariance(float dt); - - /** - * Attitude correction - */ - int correctAtt(); - - /** - * Position correction - */ - int correctPos(); - - /** - * Overloaded update parameters - */ - virtual void updateParams(); -protected: - // kalman filter - math::Matrix<9,9> F; /**< Jacobian(f,x), where dx/dt = f(x,u) */ - math::Matrix<9,6> G; /**< noise shaping matrix for gyro/accel */ - math::Matrix<9,9> P; /**< state covariance matrix */ - math::Matrix<9,9> P0; /**< initial state covariance matrix */ - math::Matrix<6,6> V; /**< gyro/ accel noise matrix */ - math::Matrix<4,9> HAtt; /**< attitude measurement matrix */ - math::Matrix<4,4> RAtt; /**< attitude measurement noise matrix */ - math::Matrix<6,9> HPos; /**< position measurement jacobian matrix */ - math::Matrix<6,6> RPos; /**< position measurement noise matrix */ - // attitude - math::Matrix<3,3> C_nb; /**< direction cosine matrix from body to nav frame */ - math::Quaternion q; /**< quaternion from body to nav frame */ - // subscriptions - uORB::Subscription<sensor_combined_s> _sensors; /**< sensors sub. */ - uORB::Subscription<vehicle_gps_position_s> _gps; /**< gps sub. */ - uORB::Subscription<parameter_update_s> _param_update; /**< parameter update sub. */ - // publications - uORB::Publication<vehicle_global_position_s> _pos; /**< position pub. */ - uORB::Publication<vehicle_local_position_s> _localPos; /**< local position pub. */ - uORB::Publication<vehicle_attitude_s> _att; /**< attitude pub. */ - // time stamps - uint64_t _pubTimeStamp; /**< output data publication time stamp */ - uint64_t _predictTimeStamp; /**< prediction time stamp */ - uint64_t _attTimeStamp; /**< attitude correction time stamp */ - uint64_t _outTimeStamp; /**< output time stamp */ - // frame count - uint16_t _navFrames; /**< navigation frames completed in output cycle */ - // miss counts - uint16_t _miss; /**< number of times fast prediction loop missed */ - // accelerations - float fN, fE, fD; /**< navigation frame acceleration */ - // states - enum {PHI = 0, THETA, PSI, VN, VE, VD, LAT, LON, ALT}; /**< state enumeration */ - float phi, theta, psi; /**< 3-2-1 euler angles */ - float vN, vE, vD; /**< navigation velocity, m/s */ - double lat, lon; /**< lat, lon radians */ - // parameters - float alt; /**< altitude, meters */ - double lat0, lon0; /**< reference latitude and longitude */ - float alt0; /**< refeerence altitude (ground height) */ - control::BlockParamFloat _vGyro; /**< gyro process noise */ - control::BlockParamFloat _vAccel; /**< accelerometer process noise */ - control::BlockParamFloat _rMag; /**< magnetometer measurement noise */ - control::BlockParamFloat _rGpsVel; /**< gps velocity measurement noise */ - control::BlockParamFloat _rGpsPos; /**< gps position measurement noise */ - control::BlockParamFloat _rGpsAlt; /**< gps altitude measurement noise */ - control::BlockParamFloat _rPressAlt; /**< press altitude measurement noise */ - control::BlockParamFloat _rAccel; /**< accelerometer measurement noise */ - control::BlockParamFloat _magDip; /**< magnetic inclination with level */ - control::BlockParamFloat _magDec; /**< magnetic declination, clockwise rotation */ - control::BlockParamFloat _g; /**< gravitational constant */ - control::BlockParamFloat _faultPos; /**< fault detection threshold for position */ - control::BlockParamFloat _faultAtt; /**< fault detection threshold for attitude */ - // status - bool _attitudeInitialized; - bool _positionInitialized; - uint16_t _attitudeInitCounter; - // accessors - int32_t getLatDegE7() { return int32_t(lat * 1.0e7 * M_RAD_TO_DEG); } - void setLatDegE7(int32_t val) { lat = val / 1.0e7 / M_RAD_TO_DEG; } - int32_t getLonDegE7() { return int32_t(lon * 1.0e7 * M_RAD_TO_DEG); } - void setLonDegE7(int32_t val) { lon = val / 1.0e7 / M_RAD_TO_DEG; } - int32_t getAltE3() { return int32_t(alt * 1.0e3); } - void setAltE3(int32_t val) { alt = double(val) / 1.0e3; } -}; diff --git a/src/modules/att_pos_estimator_ekf/kalman_main.cpp b/src/modules/att_pos_estimator_ekf/kalman_main.cpp deleted file mode 100644 index 3d20d4d2d..000000000 --- a/src/modules/att_pos_estimator_ekf/kalman_main.cpp +++ /dev/null @@ -1,157 +0,0 @@ -/**************************************************************************** - * - * Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved. - * Author: James Goppert - * - * Redistribution and use in source and binary forms, with or without - * modification, are permitted provided that the following conditions - * are met: - * - * 1. Redistributions of source code must retain the above copyright - * notice, this list of conditions and the following disclaimer. - * 2. Redistributions in binary form must reproduce the above copyright - * notice, this list of conditions and the following disclaimer in - * the documentation and/or other materials provided with the - * distribution. - * 3. Neither the name PX4 nor the names of its contributors may be - * used to endorse or promote products derived from this software - * without specific prior written permission. - * - * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS - * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT - * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS - * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE - * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, - * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, - * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS - * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED - * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT - * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN - * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE - * POSSIBILITY OF SUCH DAMAGE. - * - ****************************************************************************/ - -/** - * @file kalman_main.cpp - * Combined attitude / position estimator. - * - * @author James Goppert - */ - -#include <nuttx/config.h> -#include <unistd.h> -#include <stdio.h> -#include <stdlib.h> -#include <string.h> -#include <systemlib/systemlib.h> -#include <systemlib/param/param.h> -#include <systemlib/err.h> -#include <drivers/drv_hrt.h> -#include <math.h> -#include "KalmanNav.hpp" - -static bool thread_should_exit = false; /**< Deamon exit flag */ -static bool thread_running = false; /**< Deamon status flag */ -static int daemon_task; /**< Handle of deamon task / thread */ - -/** - * Deamon management function. - */ -extern "C" __EXPORT int att_pos_estimator_ekf_main(int argc, char *argv[]); - -/** - * Mainloop of deamon. - */ -int kalman_demo_thread_main(int argc, char *argv[]); - -/** - * Print the correct usage. - */ -static void usage(const char *reason); - -static void -usage(const char *reason) -{ - if (reason) - fprintf(stderr, "%s\n", reason); - - warnx("usage: att_pos_estimator_ekf {start|stop|status} [-p <additional params>]"); - exit(1); -} - -/** - * The deamon app only briefly exists to start - * the background job. The stack size assigned in the - * Makefile does only apply to this management task. - * - * The actual stack size should be set in the call - * to task_create(). - */ -int att_pos_estimator_ekf_main(int argc, char *argv[]) -{ - - if (argc < 1) - usage("missing command"); - - if (!strcmp(argv[1], "start")) { - - if (thread_running) { - warnx("already running"); - /* this is not an error */ - exit(0); - } - - thread_should_exit = false; - - daemon_task = task_spawn_cmd("att_pos_estimator_ekf", - SCHED_DEFAULT, - SCHED_PRIORITY_MAX - 30, - 8192, - kalman_demo_thread_main, - (argv) ? (const char **)&argv[2] : (const char **)NULL); - exit(0); - } - - if (!strcmp(argv[1], "stop")) { - thread_should_exit = true; - exit(0); - } - - if (!strcmp(argv[1], "status")) { - if (thread_running) { - warnx("is running\n"); - exit(0); - - } else { - warnx("not started\n"); - exit(1); - } - - } - - usage("unrecognized command"); - exit(1); -} - -int kalman_demo_thread_main(int argc, char *argv[]) -{ - - warnx("starting"); - - using namespace math; - - thread_running = true; - - KalmanNav nav(NULL, "KF"); - - while (!thread_should_exit) { - nav.update(); - } - - warnx("exiting."); - - thread_running = false; - - return 0; -} diff --git a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp index 10a6cd2c5..2ec889efe 100755 --- a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp +++ b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp @@ -1,8 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: Tobias Naegeli <naegelit@student.ethz.ch> - * Lorenz Meier <lm@inf.ethz.ch> + * Copyright (c) 2012-2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -34,9 +32,12 @@ ****************************************************************************/ /* - * @file attitude_estimator_ekf_main.c + * @file attitude_estimator_ekf_main.cpp * * Extended Kalman Filter for Attitude Estimation. + * + * @author Tobias Naegeli <naegelit@student.ethz.ch> + * @author Lorenz Meier <lm@inf.ethz.ch> */ #include <nuttx/config.h> @@ -111,7 +112,7 @@ usage(const char *reason) * Makefile does only apply to this management task. * * The actual stack size should be set in the call - * to task_create(). + * to task_spawn_cmd(). */ int attitude_estimator_ekf_main(int argc, char *argv[]) { @@ -407,7 +408,7 @@ const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds vel(2) = gps.vel_d_m_s; } - } else if (ekf_params.acc_comp == 2 && global_pos.global_valid && hrt_absolute_time() < global_pos.timestamp + 500000) { + } else if (ekf_params.acc_comp == 2 && gps.eph_m < 5.0f && global_pos.timestamp != 0 && hrt_absolute_time() < global_pos.timestamp + 20000) { vel_valid = true; if (global_pos_updated) { vel_t = global_pos.timestamp; diff --git a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c index 4154e3db4..3ff3d9922 100755 --- a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c +++ b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c @@ -40,6 +40,7 @@ */ #include "attitude_estimator_ekf_params.h" +#include <math.h> /* Extended Kalman Filter covariances */ @@ -113,6 +114,7 @@ int parameters_update(const struct attitude_estimator_ekf_param_handles *h, stru param_get(h->yaw_off, &(p->yaw_off)); param_get(h->mag_decl, &(p->mag_decl)); + p->mag_decl *= M_PI / 180.0f; param_get(h->acc_comp, &(p->acc_comp)); diff --git a/src/modules/attitude_estimator_ekf/module.mk b/src/modules/attitude_estimator_ekf/module.mk index d98647f99..99d0c5bf2 100644 --- a/src/modules/attitude_estimator_ekf/module.mk +++ b/src/modules/attitude_estimator_ekf/module.mk @@ -50,3 +50,5 @@ SRCS = attitude_estimator_ekf_main.cpp \ codegen/rtGetNaN.c \ codegen/norm.c \ codegen/cross.c + +MODULE_STACKSIZE = 1200 diff --git a/src/modules/attitude_estimator_so3/attitude_estimator_so3_main.cpp b/src/modules/attitude_estimator_so3/attitude_estimator_so3_main.cpp index 3653defa6..e55b01160 100755 --- a/src/modules/attitude_estimator_so3/attitude_estimator_so3_main.cpp +++ b/src/modules/attitude_estimator_so3/attitude_estimator_so3_main.cpp @@ -1,8 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. - * Author: Hyon Lim <limhyon@gmail.com> - * Anton Babushkin <anton.babushkin@me.com> + * Copyright (c) 2013 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -36,6 +34,9 @@ /* * @file attitude_estimator_so3_main.cpp * + * @author Hyon Lim <limhyon@gmail.com> + * @author Anton Babushkin <anton.babushkin@me.com> + * * Implementation of nonlinear complementary filters on the SO(3). * This code performs attitude estimation by using accelerometer, gyroscopes and magnetometer. * Result is provided as quaternion, 1-2-3 Euler angle and rotation matrix. @@ -131,7 +132,7 @@ usage(const char *reason) * Makefile does only apply to this management task. * * The actual stack size should be set in the call - * to task_create(). + * to task_spawn_cmd(). */ int attitude_estimator_so3_main(int argc, char *argv[]) { diff --git a/src/modules/attitude_estimator_so3/module.mk b/src/modules/attitude_estimator_so3/module.mk index e29bb16a6..f52715abb 100644 --- a/src/modules/attitude_estimator_so3/module.mk +++ b/src/modules/attitude_estimator_so3/module.mk @@ -6,3 +6,5 @@ MODULE_COMMAND = attitude_estimator_so3 SRCS = attitude_estimator_so3_main.cpp \ attitude_estimator_so3_params.c + +MODULE_STACKSIZE = 1200 diff --git a/src/modules/commander/accelerometer_calibration.cpp b/src/modules/commander/accelerometer_calibration.cpp index 1cbdf9bf8..7180048ff 100644 --- a/src/modules/commander/accelerometer_calibration.cpp +++ b/src/modules/commander/accelerometer_calibration.cpp @@ -194,13 +194,13 @@ int do_accel_calibration(int mavlink_fd) int32_t board_rotation_int; param_get(board_rotation_h, &(board_rotation_int)); enum Rotation board_rotation_id = (enum Rotation)board_rotation_int; - math::Matrix<3,3> board_rotation; + math::Matrix<3, 3> board_rotation; get_rot_matrix(board_rotation_id, &board_rotation); - math::Matrix<3,3> board_rotation_t = board_rotation.transposed(); + math::Matrix<3, 3> board_rotation_t = board_rotation.transposed(); math::Vector<3> accel_offs_vec(&accel_offs[0]); - math::Vector<3> accel_offs_rotated = board_rotation_t * accel_offs_vec; - math::Matrix<3,3> accel_T_mat(&accel_T[0][0]); - math::Matrix<3,3> accel_T_rotated = board_rotation_t * accel_T_mat * board_rotation; + math::Vector<3> accel_offs_rotated = board_rotation_t *accel_offs_vec; + math::Matrix<3, 3> accel_T_mat(&accel_T[0][0]); + math::Matrix<3, 3> accel_T_rotated = board_rotation_t *accel_T_mat * board_rotation; accel_scale.x_offset = accel_offs_rotated(0); accel_scale.x_scale = accel_T_rotated(0, 0); @@ -277,11 +277,13 @@ int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float } } - if (old_done_count != done_count) + if (old_done_count != done_count) { mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 17 * done_count); + } - if (done) + if (done) { break; + } mavlink_log_info(mavlink_fd, "directions left: %s%s%s%s%s%s", (!data_collected[0]) ? "x+ " : "", @@ -380,11 +382,13 @@ int detect_orientation(int mavlink_fd, int sub_sensor_combined) d = d * d; accel_disp[i] = accel_disp[i] * (1.0f - w); - if (d > still_thr2 * 8.0f) + if (d > still_thr2 * 8.0f) { d = still_thr2 * 8.0f; + } - if (d > accel_disp[i]) + if (d > accel_disp[i]) { accel_disp[i] = d; + } } /* still detector with hysteresis */ @@ -432,33 +436,39 @@ int detect_orientation(int mavlink_fd, int sub_sensor_combined) if (fabsf(accel_ema[0] - CONSTANTS_ONE_G) < accel_err_thr && fabsf(accel_ema[1]) < accel_err_thr && - fabsf(accel_ema[2]) < accel_err_thr) - return 0; // [ g, 0, 0 ] + fabsf(accel_ema[2]) < accel_err_thr) { + return 0; // [ g, 0, 0 ] + } if (fabsf(accel_ema[0] + CONSTANTS_ONE_G) < accel_err_thr && fabsf(accel_ema[1]) < accel_err_thr && - fabsf(accel_ema[2]) < accel_err_thr) - return 1; // [ -g, 0, 0 ] + fabsf(accel_ema[2]) < accel_err_thr) { + return 1; // [ -g, 0, 0 ] + } if (fabsf(accel_ema[0]) < accel_err_thr && fabsf(accel_ema[1] - CONSTANTS_ONE_G) < accel_err_thr && - fabsf(accel_ema[2]) < accel_err_thr) - return 2; // [ 0, g, 0 ] + fabsf(accel_ema[2]) < accel_err_thr) { + return 2; // [ 0, g, 0 ] + } if (fabsf(accel_ema[0]) < accel_err_thr && fabsf(accel_ema[1] + CONSTANTS_ONE_G) < accel_err_thr && - fabsf(accel_ema[2]) < accel_err_thr) - return 3; // [ 0, -g, 0 ] + fabsf(accel_ema[2]) < accel_err_thr) { + return 3; // [ 0, -g, 0 ] + } if (fabsf(accel_ema[0]) < accel_err_thr && fabsf(accel_ema[1]) < accel_err_thr && - fabsf(accel_ema[2] - CONSTANTS_ONE_G) < accel_err_thr) - return 4; // [ 0, 0, g ] + fabsf(accel_ema[2] - CONSTANTS_ONE_G) < accel_err_thr) { + return 4; // [ 0, 0, g ] + } if (fabsf(accel_ema[0]) < accel_err_thr && fabsf(accel_ema[1]) < accel_err_thr && - fabsf(accel_ema[2] + CONSTANTS_ONE_G) < accel_err_thr) - return 5; // [ 0, 0, -g ] + fabsf(accel_ema[2] + CONSTANTS_ONE_G) < accel_err_thr) { + return 5; // [ 0, 0, -g ] + } mavlink_log_critical(mavlink_fd, "ERROR: invalid orientation"); @@ -485,8 +495,9 @@ int read_accelerometer_avg(int sensor_combined_sub, float accel_avg[3], int samp struct sensor_combined_s sensor; orb_copy(ORB_ID(sensor_combined), sensor_combined_sub, &sensor); - for (int i = 0; i < 3; i++) + for (int i = 0; i < 3; i++) { accel_sum[i] += sensor.accelerometer_m_s2[i]; + } count++; @@ -495,8 +506,9 @@ int read_accelerometer_avg(int sensor_combined_sub, float accel_avg[3], int samp continue; } - if (errcount > samples_num / 10) + if (errcount > samples_num / 10) { return ERROR; + } } for (int i = 0; i < 3; i++) { @@ -512,8 +524,9 @@ int mat_invert3(float src[3][3], float dst[3][3]) src[0][1] * (src[1][0] * src[2][2] - src[1][2] * src[2][0]) + src[0][2] * (src[1][0] * src[2][1] - src[1][1] * src[2][0]); - if (det == 0.0f) - return ERROR; // Singular matrix + if (det == 0.0f) { + return ERROR; // Singular matrix + } dst[0][0] = (src[1][1] * src[2][2] - src[1][2] * src[2][1]) / det; dst[1][0] = (src[1][2] * src[2][0] - src[1][0] * src[2][2]) / det; @@ -549,8 +562,9 @@ int calculate_calibration_values(float accel_ref[6][3], float accel_T[3][3], flo /* calculate inverse matrix for A */ float mat_A_inv[3][3]; - if (mat_invert3(mat_A, mat_A_inv) != OK) + if (mat_invert3(mat_A, mat_A_inv) != OK) { return ERROR; + } /* copy results to accel_T */ for (int i = 0; i < 3; i++) { diff --git a/src/modules/commander/airspeed_calibration.cpp b/src/modules/commander/airspeed_calibration.cpp index 6039d92a7..5d21d89d0 100644 --- a/src/modules/commander/airspeed_calibration.cpp +++ b/src/modules/commander/airspeed_calibration.cpp @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -64,9 +64,9 @@ int do_airspeed_calibration(int mavlink_fd) { /* give directions */ mavlink_log_info(mavlink_fd, CAL_STARTED_MSG, sensor_name); - mavlink_log_info(mavlink_fd, "don't move system"); + mavlink_log_info(mavlink_fd, "ensure airspeed sensor is not registering wind"); - const int calibration_count = 2500; + const int calibration_count = 2000; int diff_pres_sub = orb_subscribe(ORB_ID(differential_pressure)); struct differential_pressure_s diff_pres; @@ -82,16 +82,21 @@ int do_airspeed_calibration(int mavlink_fd) bool paramreset_successful = false; int fd = open(AIRSPEED_DEVICE_PATH, 0); + if (fd > 0) { if (OK == ioctl(fd, AIRSPEEDIOCSSCALE, (long unsigned int)&airscale)) { paramreset_successful = true; + + } else { + mavlink_log_critical(mavlink_fd, "airspeed offset zero failed"); } + close(fd); } if (!paramreset_successful) { - warn("WARNING: failed to set scale / offsets for airspeed sensor"); - mavlink_log_critical(mavlink_fd, "could not reset dpress sensor"); + warn("FAILED to set scale / offsets for airspeed"); + mavlink_log_critical(mavlink_fd, "dpress reset failed"); mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name); return ERROR; } @@ -107,11 +112,12 @@ int do_airspeed_calibration(int mavlink_fd) if (poll_ret) { orb_copy(ORB_ID(differential_pressure), diff_pres_sub, &diff_pres); - diff_pres_offset += diff_pres.differential_pressure_pa; + diff_pres_offset += diff_pres.differential_pressure_raw_pa; calibration_counter++; - if (calibration_counter % (calibration_count / 20) == 0) + if (calibration_counter % (calibration_count / 20) == 0) { mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, (calibration_counter * 100) / calibration_count); + } } else if (poll_ret == 0) { /* any poll failure for 1s is a reason to abort */ diff --git a/src/modules/commander/commander.cpp b/src/modules/commander/commander.cpp index d114a2e5c..504696ff9 100644 --- a/src/modules/commander/commander.cpp +++ b/src/modules/commander/commander.cpp @@ -67,6 +67,7 @@ #include <uORB/topics/home_position.h> #include <uORB/topics/vehicle_global_position.h> #include <uORB/topics/vehicle_local_position.h> +#include <uORB/topics/position_setpoint_triplet.h> #include <uORB/topics/vehicle_gps_position.h> #include <uORB/topics/vehicle_command.h> #include <uORB/topics/subsystem_info.h> @@ -112,14 +113,14 @@ extern struct system_load_s system_load; #define MAVLINK_OPEN_INTERVAL 50000 -#define STICK_ON_OFF_LIMIT 0.75f -#define STICK_THRUST_RANGE 1.0f +#define STICK_ON_OFF_LIMIT 0.9f #define STICK_ON_OFF_HYSTERESIS_TIME_MS 1000 #define STICK_ON_OFF_COUNTER_LIMIT (STICK_ON_OFF_HYSTERESIS_TIME_MS*COMMANDER_MONITORING_LOOPSPERMSEC) -#define POSITION_TIMEOUT 1000000 /**< consider the local or global position estimate invalid after 1s */ -#define RC_TIMEOUT 100000 -#define DIFFPRESS_TIMEOUT 2000000 +#define POSITION_TIMEOUT (600 * 1000) /**< consider the local or global position estimate invalid after 600ms */ +#define FAILSAFE_DEFAULT_TIMEOUT (3 * 1000 * 1000) /**< hysteresis time - the failsafe will trigger after 3 seconds in this state */ +#define RC_TIMEOUT 500000 +#define DIFFPRESS_TIMEOUT 2000000 #define PRINT_INTERVAL 5000000 #define PRINT_MODE_REJECT_INTERVAL 2000000 @@ -137,7 +138,7 @@ enum MAV_MODE_FLAG { }; /* Mavlink file descriptors */ -static int mavlink_fd; +static int mavlink_fd = 0; /* flags */ static bool commander_initialized = false; @@ -153,6 +154,7 @@ static bool on_usb_power = false; static float takeoff_alt = 5.0f; static int parachute_enabled = 0; +static float eph_epv_threshold = 5.0f; static struct vehicle_status_s status; static struct actuator_armed_s armed; @@ -194,7 +196,7 @@ void usage(const char *reason); /** * React to commands that are sent e.g. from the mavlink module. */ -bool handle_command(struct vehicle_status_s *status, struct vehicle_command_s *cmd, struct actuator_armed_s *armed); +bool handle_command(struct vehicle_status_s *status, const struct safety_s *safety, struct vehicle_command_s *cmd, struct actuator_armed_s *armed, struct home_position_s *home, struct vehicle_global_position_s *global_pos, orb_advert_t *home_pub); /** * Mainloop of commander. @@ -207,7 +209,7 @@ void check_valid(hrt_abstime timestamp, hrt_abstime timeout, bool valid_in, bool void check_mode_switches(struct manual_control_setpoint_s *sp_man, struct vehicle_status_s *status); -transition_result_t set_main_state_rc(struct vehicle_status_s *status); +transition_result_t set_main_state_rc(struct vehicle_status_s *status, struct manual_control_setpoint_s *sp_man); void set_control_mode(); @@ -217,11 +219,10 @@ void print_reject_arm(const char *msg); void print_status(); -int arm(); -int disarm(); - transition_result_t check_navigation_state_machine(struct vehicle_status_s *status, struct vehicle_control_mode_s *control_mode, struct vehicle_local_position_s *local_pos); +transition_result_t arm_disarm(bool arm, const int mavlink_fd, const char *armedBy); + /** * Loop that runs at a lower rate and priority for calibration and parameter tasks. */ @@ -232,8 +233,9 @@ void answer_command(struct vehicle_command_s &cmd, enum VEHICLE_CMD_RESULT resul int commander_main(int argc, char *argv[]) { - if (argc < 1) + if (argc < 1) { usage("missing command"); + } if (!strcmp(argv[1], "start")) { @@ -247,7 +249,7 @@ int commander_main(int argc, char *argv[]) daemon_task = task_spawn_cmd("commander", SCHED_DEFAULT, SCHED_PRIORITY_MAX - 40, - 3000, + 2950, commander_thread_main, (argv) ? (const char **)&argv[2] : (const char **)NULL); @@ -260,8 +262,9 @@ int commander_main(int argc, char *argv[]) if (!strcmp(argv[1], "stop")) { - if (!thread_running) + if (!thread_running) { errx(0, "commander already stopped"); + } thread_should_exit = true; @@ -288,12 +291,12 @@ int commander_main(int argc, char *argv[]) } if (!strcmp(argv[1], "arm")) { - arm(); + arm_disarm(true, mavlink_fd, "command line"); exit(0); } - if (!strcmp(argv[1], "disarm")) { - disarm(); + if (!strcmp(argv[1], "2")) { + arm_disarm(false, mavlink_fd, "command line"); exit(0); } @@ -303,8 +306,9 @@ int commander_main(int argc, char *argv[]) void usage(const char *reason) { - if (reason) + if (reason) { fprintf(stderr, "%s\n", reason); + } fprintf(stderr, "usage: daemon {start|stop|status} [-p <additional params>]\n\n"); exit(1); @@ -363,38 +367,35 @@ void print_status() static orb_advert_t status_pub; -int arm() +transition_result_t arm_disarm(bool arm, const int mavlink_fd, const char *armedBy) { - int arming_res = arming_state_transition(&status, &safety, ARMING_STATE_ARMED, &armed); + transition_result_t arming_res = TRANSITION_NOT_CHANGED; - if (arming_res == TRANSITION_CHANGED) { - mavlink_log_info(mavlink_fd, "[cmd] ARMED by commandline"); - return 0; + // Transition the armed state. By passing mavlink_fd to arming_state_transition it will + // output appropriate error messages if the state cannot transition. + arming_res = arming_state_transition(&status, &safety, arm ? ARMING_STATE_ARMED : ARMING_STATE_STANDBY, &armed, mavlink_fd); - } else { - return 1; - } -} - -int disarm() -{ - int arming_res = arming_state_transition(&status, &safety, ARMING_STATE_STANDBY, &armed); + if (arming_res == TRANSITION_CHANGED && mavlink_fd) { + mavlink_log_info(mavlink_fd, "[cmd] %s by %s", arm ? "ARMED" : "DISARMED", armedBy); - if (arming_res == TRANSITION_CHANGED) { - mavlink_log_info(mavlink_fd, "[cmd] ARMED by commandline"); - return 0; - - } else { - return 1; + } else if (arming_res == TRANSITION_DENIED) { + tune_negative(true); } + + return arming_res; } -bool handle_command(struct vehicle_status_s *status, const struct safety_s *safety, struct vehicle_command_s *cmd, struct actuator_armed_s *armed) +bool handle_command(struct vehicle_status_s *status, const struct safety_s *safety, struct vehicle_command_s *cmd, struct actuator_armed_s *armed, struct home_position_s *home, struct vehicle_global_position_s *global_pos, orb_advert_t *home_pub) { /* result of the command */ enum VEHICLE_CMD_RESULT result = VEHICLE_CMD_RESULT_UNSUPPORTED; bool ret = false; + /* only handle commands that are meant to be handled by this system and component */ + if (cmd->target_system != status->system_id || ((cmd->target_component != status->component_id) && (cmd->target_component != 0))) { // component_id 0: valid for all components + return false; + } + /* only handle high-priority commands here */ /* request to set different system mode */ @@ -421,43 +422,16 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe } } - if (hil_ret == OK) + if (hil_ret == OK) { ret = true; - - // TODO remove debug code - //mavlink_log_critical(mavlink_fd, "#audio: command setmode: %d %d", base_mode, custom_main_mode); - /* set arming state */ - arming_res = TRANSITION_NOT_CHANGED; - - if (base_mode & MAV_MODE_FLAG_SAFETY_ARMED) { - if (safety->safety_switch_available && !safety->safety_off && status->hil_state == HIL_STATE_OFF) { - print_reject_arm("NOT ARMING: Press safety switch first."); - arming_res = TRANSITION_DENIED; - - } else { - arming_res = arming_state_transition(status, safety, ARMING_STATE_ARMED, armed); - } - - if (arming_res == TRANSITION_CHANGED) { - mavlink_log_info(mavlink_fd, "[cmd] ARMED by command"); - } - - } else { - if (status->arming_state == ARMING_STATE_ARMED || status->arming_state == ARMING_STATE_ARMED_ERROR) { - arming_state_t new_arming_state = (status->arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY : ARMING_STATE_STANDBY_ERROR); - arming_res = arming_state_transition(status, safety, new_arming_state, armed); - - if (arming_res == TRANSITION_CHANGED) { - mavlink_log_info(mavlink_fd, "[cmd] DISARMED by command"); - } - - } else { - arming_res = TRANSITION_NOT_CHANGED; - } } - if (arming_res == TRANSITION_CHANGED) + // Transition the arming state + arming_res = arm_disarm(base_mode & MAV_MODE_FLAG_SAFETY_ARMED, mavlink_fd, "set mode command"); + + if (arming_res == TRANSITION_CHANGED) { ret = true; + } /* set main state */ transition_result_t main_res = TRANSITION_DENIED; @@ -468,13 +442,13 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe /* MANUAL */ main_res = main_state_transition(status, MAIN_STATE_MANUAL); - } else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_SEATBELT) { - /* SEATBELT */ - main_res = main_state_transition(status, MAIN_STATE_SEATBELT); + } else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_ALTCTL) { + /* ALTCTL */ + main_res = main_state_transition(status, MAIN_STATE_ALTCTL); - } else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_EASY) { - /* EASY */ - main_res = main_state_transition(status, MAIN_STATE_EASY); + } else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_POSCTL) { + /* POSCTL */ + main_res = main_state_transition(status, MAIN_STATE_POSCTL); } else if (custom_main_mode == PX4_CUSTOM_MAIN_MODE_AUTO) { /* AUTO */ @@ -489,8 +463,8 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe } else if (base_mode & MAV_MODE_FLAG_MANUAL_INPUT_ENABLED) { if (base_mode & MAV_MODE_FLAG_GUIDED_ENABLED) { - /* EASY */ - main_res = main_state_transition(status, MAIN_STATE_EASY); + /* POSCTL */ + main_res = main_state_transition(status, MAIN_STATE_POSCTL); } else if (base_mode & MAV_MODE_FLAG_STABILIZE_ENABLED) { /* MANUAL */ @@ -499,8 +473,9 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe } } - if (main_res == TRANSITION_CHANGED) + if (main_res == TRANSITION_CHANGED) { ret = true; + } if (arming_res != TRANSITION_DENIED && main_res != TRANSITION_DENIED) { result = VEHICLE_CMD_RESULT_ACCEPTED; @@ -513,25 +488,26 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe } case VEHICLE_CMD_COMPONENT_ARM_DISARM: { - transition_result_t arming_res = TRANSITION_NOT_CHANGED; + // Follow exactly what the mavlink spec says for values: 0.0f for disarm, 1.0f for arm. + // We use an float epsilon delta to test float equality. + if (cmd->param1 != 0.0f && (fabsf(cmd->param1 - 1.0f) > 2.0f * FLT_EPSILON)) { + mavlink_log_info(mavlink_fd, "Unsupported ARM_DISARM parameter: %.6f", cmd->param1); - if (!armed->armed && ((int)(cmd->param1 + 0.5f)) == 1) { - if (safety->safety_switch_available && !safety->safety_off && status->hil_state == HIL_STATE_OFF) { - print_reject_arm("NOT ARMING: Press safety switch first."); - arming_res = TRANSITION_DENIED; + } else { - } else { - arming_res = arming_state_transition(status, safety, ARMING_STATE_ARMED, armed); + // Flick to inair restore first if this comes from an onboard system + if (cmd->source_system == status->system_id && cmd->source_component == status->component_id) { + status->arming_state = ARMING_STATE_IN_AIR_RESTORE; } - if (arming_res == TRANSITION_CHANGED) { - mavlink_log_critical(mavlink_fd, "#audio: ARMED by component arm cmd"); - result = VEHICLE_CMD_RESULT_ACCEPTED; - ret = true; + transition_result_t arming_res = arm_disarm(cmd->param1 != 0.0f, mavlink_fd, "arm/disarm component command"); - } else { + if (arming_res == TRANSITION_DENIED) { mavlink_log_critical(mavlink_fd, "#audio: REJECTING component arm cmd"); result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED; + + } else { + result = VEHICLE_CMD_RESULT_ACCEPTED; } } } @@ -561,7 +537,7 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe } break; - /* Flight termination */ + /* Flight termination */ case VEHICLE_CMD_DO_SET_SERVO: { //xxx: needs its own mavlink command //XXX: to enable the parachute, a param needs to be set @@ -579,6 +555,53 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe } break; + case VEHICLE_CMD_DO_SET_HOME: { + bool use_current = cmd->param1 > 0.5f; + + if (use_current) { + /* use current position */ + if (status->condition_global_position_valid) { + home->lat = global_pos->lat; + home->lon = global_pos->lon; + home->alt = global_pos->alt; + + home->timestamp = hrt_absolute_time(); + + result = VEHICLE_CMD_RESULT_ACCEPTED; + + } else { + result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED; + } + + } else { + /* use specified position */ + home->lat = cmd->param5; + home->lon = cmd->param6; + home->alt = cmd->param7; + + home->timestamp = hrt_absolute_time(); + + result = VEHICLE_CMD_RESULT_ACCEPTED; + } + + if (result == VEHICLE_CMD_RESULT_ACCEPTED) { + warnx("home: lat = %.7f, lon = %.7f, alt = %.2f ", home->lat, home->lon, (double)home->alt); + mavlink_log_info(mavlink_fd, "[cmd] home: %.7f, %.7f, %.2f", home->lat, home->lon, (double)home->alt); + + /* announce new home position */ + if (*home_pub > 0) { + orb_publish(ORB_ID(home_position), *home_pub, home); + + } else { + *home_pub = orb_advertise(ORB_ID(home_position), home); + } + + /* mark home position as set */ + status->condition_home_position_valid = true; + } + } + break; + case VEHICLE_CMD_PREFLIGHT_REBOOT_SHUTDOWN: case VEHICLE_CMD_PREFLIGHT_CALIBRATION: case VEHICLE_CMD_PREFLIGHT_SET_SENSOR_OFFSETS: @@ -587,7 +610,8 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe break; default: - /* warn about unsupported commands */ + /* Warn about unsupported commands, this makes sense because only commands + * to this component ID (or all) are passed by mavlink. */ answer_command(*cmd, VEHICLE_CMD_RESULT_UNSUPPORTED); break; } @@ -611,6 +635,7 @@ int commander_thread_main(int argc, char *argv[]) commander_initialized = false; bool arm_tune_played = false; + bool was_armed = false; /* set parameters */ param_t _param_sys_type = param_find("MAV_TYPE"); @@ -624,8 +649,8 @@ int commander_thread_main(int argc, char *argv[]) char *main_states_str[MAIN_STATE_MAX]; main_states_str[0] = "MANUAL"; - main_states_str[1] = "SEATBELT"; - main_states_str[2] = "EASY"; + main_states_str[1] = "ALTCTL"; + main_states_str[2] = "POSCTL"; main_states_str[3] = "AUTO"; char *arming_states_str[ARMING_STATE_MAX]; @@ -718,7 +743,7 @@ int commander_thread_main(int argc, char *argv[]) pthread_attr_t commander_low_prio_attr; pthread_attr_init(&commander_low_prio_attr); - pthread_attr_setstacksize(&commander_low_prio_attr, 2992); + pthread_attr_setstacksize(&commander_low_prio_attr, 2900); struct sched_param param; (void)pthread_attr_getschedparam(&commander_low_prio_attr, ¶m); @@ -737,8 +762,9 @@ int commander_thread_main(int argc, char *argv[]) bool low_battery_voltage_actions_done = false; bool critical_battery_voltage_actions_done = false; - uint64_t last_idle_time = 0; - uint64_t start_time = 0; + hrt_abstime last_idle_time = 0; + hrt_abstime start_time = 0; + hrt_abstime last_auto_state_valid = 0; bool status_changed = true; bool param_init_forced = true; @@ -767,6 +793,9 @@ int commander_thread_main(int argc, char *argv[]) int global_position_sub = orb_subscribe(ORB_ID(vehicle_global_position)); struct vehicle_global_position_s global_position; memset(&global_position, 0, sizeof(global_position)); + /* Init EPH and EPV */ + global_position.eph = 1000.0f; + global_position.epv = 1000.0f; /* Subscribe to local position data */ int local_position_sub = orb_subscribe(ORB_ID(vehicle_local_position)); @@ -814,6 +843,11 @@ int commander_thread_main(int argc, char *argv[]) struct subsystem_info_s info; memset(&info, 0, sizeof(info)); + /* Subscribe to position setpoint triplet */ + int pos_sp_triplet_sub = orb_subscribe(ORB_ID(position_setpoint_triplet)); + struct position_setpoint_triplet_s pos_sp_triplet; + memset(&pos_sp_triplet, 0, sizeof(pos_sp_triplet)); + control_status_leds(&status, &armed, true); /* now initialized */ @@ -864,6 +898,7 @@ int commander_thread_main(int argc, char *argv[]) /* re-check RC calibration */ rc_calibration_ok = (OK == rc_calibration_check(mavlink_fd)); } + /* navigation parameters */ param_get(_param_takeoff_alt, &takeoff_alt); param_get(_param_enable_parachute, ¶chute_enabled); @@ -904,6 +939,7 @@ int commander_thread_main(int argc, char *argv[]) /* disarm if safety is now on and still armed */ if (status.hil_state == HIL_STATE_OFF && safety.safety_switch_available && !safety.safety_off && armed.armed) { arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY : ARMING_STATE_STANDBY_ERROR); + if (TRANSITION_CHANGED == arming_state_transition(&status, &safety, new_arming_state, &armed)) { mavlink_log_info(mavlink_fd, "[cmd] DISARMED by safety switch"); } @@ -919,7 +955,53 @@ int commander_thread_main(int argc, char *argv[]) } /* update condition_global_position_valid */ - check_valid(global_position.timestamp, POSITION_TIMEOUT, global_position.global_valid, &(status.condition_global_position_valid), &status_changed); + /* hysteresis for EPH/EPV */ + bool eph_epv_good; + + if (status.condition_global_position_valid) { + if (global_position.eph > eph_epv_threshold * 2.0f || global_position.epv > eph_epv_threshold * 2.0f) { + eph_epv_good = false; + + } else { + eph_epv_good = true; + } + + } else { + if (global_position.eph < eph_epv_threshold && global_position.epv < eph_epv_threshold) { + eph_epv_good = true; + + } else { + eph_epv_good = false; + } + } + + check_valid(global_position.timestamp, POSITION_TIMEOUT, eph_epv_good, &(status.condition_global_position_valid), &status_changed); + + /* check if GPS fix is ok */ + + /* update home position */ + if (!status.condition_home_position_valid && status.condition_global_position_valid && !armed.armed && + (global_position.eph < eph_epv_threshold) && (global_position.epv < eph_epv_threshold)) { + + home.lat = global_position.lat; + home.lon = global_position.lon; + home.alt = global_position.alt; + + warnx("home: lat = %.7f, lon = %.7f, alt = %.2f ", home.lat, home.lon, (double)home.alt); + mavlink_log_info(mavlink_fd, "[cmd] home: %.7f, %.7f, %.2f", home.lat, home.lon, (double)home.alt); + + /* announce new home position */ + if (home_pub > 0) { + orb_publish(ORB_ID(home_position), home_pub, &home); + + } else { + home_pub = orb_advertise(ORB_ID(home_position), &home); + } + + /* mark home position as set */ + status.condition_home_position_valid = true; + tune_positive(true); + } /* update local position estimate */ orb_check(local_position_sub, &updated); @@ -930,10 +1012,11 @@ int commander_thread_main(int argc, char *argv[]) } /* update condition_local_position_valid and condition_local_altitude_valid */ - check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.xy_valid, &(status.condition_local_position_valid), &status_changed); + check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.xy_valid && eph_epv_good, &(status.condition_local_position_valid), &status_changed); check_valid(local_position.timestamp, POSITION_TIMEOUT, local_position.z_valid, &(status.condition_local_altitude_valid), &status_changed); static bool published_condition_landed_fw = false; + if (status.is_rotary_wing && status.condition_local_altitude_valid) { if (status.condition_landed != local_position.landed) { status.condition_landed = local_position.landed; @@ -947,6 +1030,7 @@ int commander_thread_main(int argc, char *argv[]) mavlink_log_critical(mavlink_fd, "#audio: IN AIR"); } } + } else { if (!published_condition_landed_fw) { status.condition_landed = false; // Fixedwing does not have a landing detector currently @@ -962,7 +1046,7 @@ int commander_thread_main(int argc, char *argv[]) orb_copy(ORB_ID(battery_status), battery_sub, &battery); /* only consider battery voltage if system has been running 2s and battery voltage is valid */ - if (status.hil_state == HIL_STATE_OFF && hrt_absolute_time() > start_time + 2000000 && battery.voltage_filtered_v > 0.0f) { + if (hrt_absolute_time() > start_time + 2000000 && battery.voltage_filtered_v > 0.0f) { status.battery_voltage = battery.voltage_filtered_v; status.battery_current = battery.current_a; status.condition_battery_voltage_valid = true; @@ -1005,12 +1089,20 @@ int commander_thread_main(int argc, char *argv[]) status_changed = true; } + /* update position setpoint triplet */ + orb_check(pos_sp_triplet_sub, &updated); + + if (updated) { + orb_copy(ORB_ID(position_setpoint_triplet), pos_sp_triplet_sub, &pos_sp_triplet); + } + if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0) { /* compute system load */ uint64_t interval_runtime = system_load.tasks[0].total_runtime - last_idle_time; - if (last_idle_time > 0) - status.load = 1.0f - ((float)interval_runtime / 1e6f); //system load is time spent in non-idle + if (last_idle_time > 0) { + status.load = 1.0f - ((float)interval_runtime / 1e6f); //system load is time spent in non-idle + } last_idle_time = system_load.tasks[0].total_runtime; @@ -1067,45 +1159,6 @@ int commander_thread_main(int argc, char *argv[]) if (updated) { orb_copy(ORB_ID(vehicle_gps_position), gps_sub, &gps_position); - /* check if GPS fix is ok */ - float hdop_threshold_m = 4.0f; - float vdop_threshold_m = 8.0f; - - /* - * If horizontal dilution of precision (hdop / eph) - * and vertical diluation of precision (vdop / epv) - * are below a certain threshold (e.g. 4 m), AND - * home position is not yet set AND the last GPS - * GPS measurement is not older than two seconds AND - * the system is currently not armed, set home - * position to the current position. - */ - - if (!status.condition_home_position_valid && gps_position.fix_type >= 3 && - (gps_position.eph_m < hdop_threshold_m) && (gps_position.epv_m < vdop_threshold_m) && - (hrt_absolute_time() < gps_position.timestamp_position + POSITION_TIMEOUT) && !armed.armed - && global_position.global_valid) { - - /* copy position data to uORB home message, store it locally as well */ - home.lat = global_position.lat; - home.lon = global_position.lon; - home.alt = global_position.alt; - - warnx("home: lat = %.7f, lon = %.7f, alt = %.4f ", home.lat, home.lon, (double)home.alt); - mavlink_log_info(mavlink_fd, "[cmd] home: %.7f, %.7f, %.4f", home.lat, home.lon, (double)home.alt); - - /* announce new home position */ - if (home_pub > 0) { - orb_publish(ORB_ID(home_position), home_pub, &home); - - } else { - home_pub = orb_advertise(ORB_ID(home_position), &home); - } - - /* mark home position as set */ - status.condition_home_position_valid = true; - tune_positive(true); - } } /* start RC input check */ @@ -1125,22 +1178,22 @@ int commander_thread_main(int argc, char *argv[]) status.rc_signal_lost = false; - transition_result_t res; // store all transitions results here + transition_result_t arming_res; // store all transitions results here /* arm/disarm by RC */ - res = TRANSITION_NOT_CHANGED; + arming_res = TRANSITION_NOT_CHANGED; - /* check if left stick is in lower left position and we are in MANUAL or AUTO_READY mode or (ASSISTED mode and landed) -> disarm + /* check if left stick is in lower left position and we are in MANUAL or AUTO_READY mode or (ASSIST mode and landed) -> disarm * do it only for rotary wings */ if (status.is_rotary_wing && (status.arming_state == ARMING_STATE_ARMED || status.arming_state == ARMING_STATE_ARMED_ERROR) && (status.main_state == MAIN_STATE_MANUAL || status.condition_landed) && - sp_man.yaw < -STICK_ON_OFF_LIMIT && sp_man.throttle < STICK_THRUST_RANGE * 0.1f) { + sp_man.r < -STICK_ON_OFF_LIMIT && sp_man.z < 0.1f) { if (stick_off_counter > STICK_ON_OFF_COUNTER_LIMIT) { /* disarm to STANDBY if ARMED or to STANDBY_ERROR if ARMED_ERROR */ arming_state_t new_arming_state = (status.arming_state == ARMING_STATE_ARMED ? ARMING_STATE_STANDBY : ARMING_STATE_STANDBY_ERROR); - res = arming_state_transition(&status, &safety, new_arming_state, &armed); + arming_res = arming_state_transition(&status, &safety, new_arming_state, &armed); stick_off_counter = 0; } else { @@ -1153,7 +1206,7 @@ int commander_thread_main(int argc, char *argv[]) /* check if left stick is in lower right position and we're in MANUAL mode -> arm */ if (status.arming_state == ARMING_STATE_STANDBY && - sp_man.yaw > STICK_ON_OFF_LIMIT && sp_man.throttle < STICK_THRUST_RANGE * 0.1f) { + sp_man.r > STICK_ON_OFF_LIMIT && sp_man.z < 0.1f) { if (stick_on_counter > STICK_ON_OFF_COUNTER_LIMIT) { if (safety.safety_switch_available && !safety.safety_off && status.hil_state == HIL_STATE_OFF) { print_reject_arm("NOT ARMING: Press safety switch first."); @@ -1162,7 +1215,7 @@ int commander_thread_main(int argc, char *argv[]) print_reject_arm("NOT ARMING: Switch to MANUAL mode first."); } else { - res = arming_state_transition(&status, &safety, ARMING_STATE_ARMED, &armed); + arming_res = arming_state_transition(&status, &safety, ARMING_STATE_ARMED, &armed); } stick_on_counter = 0; @@ -1175,7 +1228,7 @@ int commander_thread_main(int argc, char *argv[]) stick_on_counter = 0; } - if (res == TRANSITION_CHANGED) { + if (arming_res == TRANSITION_CHANGED) { if (status.arming_state == ARMING_STATE_ARMED) { mavlink_log_info(mavlink_fd, "[cmd] ARMED by RC"); @@ -1183,31 +1236,56 @@ int commander_thread_main(int argc, char *argv[]) mavlink_log_info(mavlink_fd, "[cmd] DISARMED by RC"); } - } else if (res == TRANSITION_DENIED) { + } else if (arming_res == TRANSITION_DENIED) { /* DENIED here indicates bug in the commander */ mavlink_log_critical(mavlink_fd, "ERROR: arming state transition denied"); } if (status.failsafe_state != FAILSAFE_STATE_NORMAL) { /* recover from failsafe */ - transition_result_t res = failsafe_state_transition(&status, FAILSAFE_STATE_NORMAL); + (void)failsafe_state_transition(&status, FAILSAFE_STATE_NORMAL); } - /* fill status according to mode switches */ - check_mode_switches(&sp_man, &status); - /* evaluate the main state machine according to mode switches */ - res = set_main_state_rc(&status); + transition_result_t main_res = set_main_state_rc(&status, &sp_man); /* play tune on mode change only if armed, blink LED always */ - if (res == TRANSITION_CHANGED) { + if (main_res == TRANSITION_CHANGED) { tune_positive(armed.armed); - } else if (res == TRANSITION_DENIED) { + } else if (main_res == TRANSITION_DENIED) { /* DENIED here indicates bug in the commander */ mavlink_log_critical(mavlink_fd, "ERROR: main state transition denied"); } + /* set navigation state */ + /* RETURN switch, overrides MISSION switch */ + if (sp_man.return_switch == SWITCH_POS_ON) { + /* switch to RTL if not already landed after RTL and home position set */ + status.set_nav_state = NAV_STATE_RTL; + status.set_nav_state_timestamp = hrt_absolute_time(); + + } else { + + /* LOITER switch */ + if (sp_man.loiter_switch == SWITCH_POS_ON) { + /* stick is in LOITER position */ + status.set_nav_state = NAV_STATE_LOITER; + status.set_nav_state_timestamp = hrt_absolute_time(); + + } else if (sp_man.loiter_switch != SWITCH_POS_NONE) { + /* stick is in MISSION position */ + status.set_nav_state = NAV_STATE_MISSION; + status.set_nav_state_timestamp = hrt_absolute_time(); + + } else if ((sp_man.return_switch == SWITCH_POS_OFF || sp_man.return_switch == SWITCH_POS_MIDDLE) && + pos_sp_triplet.nav_state == NAV_STATE_RTL) { + /* RETURN switch is in normal mode, no MISSION switch mapped, interrupt if in RTL state */ + status.set_nav_state = NAV_STATE_MISSION; + status.set_nav_state_timestamp = hrt_absolute_time(); + } + } + } else { if (!status.rc_signal_lost) { mavlink_log_critical(mavlink_fd, "#audio: CRITICAL: RC SIGNAL LOST"); @@ -1218,29 +1296,39 @@ int commander_thread_main(int argc, char *argv[]) if (armed.armed) { if (status.main_state == MAIN_STATE_AUTO) { /* check if AUTO mode still allowed */ - transition_result_t res = main_state_transition(&status, MAIN_STATE_AUTO); + transition_result_t auto_res = main_state_transition(&status, MAIN_STATE_AUTO); - if (res == TRANSITION_DENIED) { + if (auto_res == TRANSITION_NOT_CHANGED) { + last_auto_state_valid = hrt_absolute_time(); + } + + /* still invalid state after the timeout interval, execute failsafe */ + if ((hrt_elapsed_time(&last_auto_state_valid) > FAILSAFE_DEFAULT_TIMEOUT) && (auto_res == TRANSITION_DENIED)) { /* AUTO mode denied, don't try RTL, switch to failsafe state LAND */ - res = failsafe_state_transition(&status, FAILSAFE_STATE_LAND); + auto_res = failsafe_state_transition(&status, FAILSAFE_STATE_LAND); - if (res == TRANSITION_DENIED) { + if (auto_res == TRANSITION_DENIED) { /* LAND not allowed, set TERMINATION state */ - transition_result_t res = failsafe_state_transition(&status, FAILSAFE_STATE_TERMINATION); + (void)failsafe_state_transition(&status, FAILSAFE_STATE_TERMINATION); } } } else { /* failsafe for manual modes */ - transition_result_t res = failsafe_state_transition(&status, FAILSAFE_STATE_RTL); + transition_result_t manual_res = TRANSITION_DENIED; + + if (!status.condition_landed) { + /* vehicle is not landed, try to perform RTL */ + manual_res = failsafe_state_transition(&status, FAILSAFE_STATE_RTL); + } - if (res == TRANSITION_DENIED) { - /* RTL not allowed (no global position estimate), try LAND */ - res = failsafe_state_transition(&status, FAILSAFE_STATE_LAND); + if (manual_res == TRANSITION_DENIED) { + /* RTL not allowed (no global position estimate) or not wanted, try LAND */ + manual_res = failsafe_state_transition(&status, FAILSAFE_STATE_LAND); - if (res == TRANSITION_DENIED) { + if (manual_res == TRANSITION_DENIED) { /* LAND not allowed, set TERMINATION state */ - res = failsafe_state_transition(&status, FAILSAFE_STATE_TERMINATION); + (void)failsafe_state_transition(&status, FAILSAFE_STATE_TERMINATION); } } } @@ -1248,14 +1336,14 @@ int commander_thread_main(int argc, char *argv[]) } else { if (status.failsafe_state != FAILSAFE_STATE_NORMAL) { /* reset failsafe when disarmed */ - transition_result_t res = failsafe_state_transition(&status, FAILSAFE_STATE_NORMAL); + (void)failsafe_state_transition(&status, FAILSAFE_STATE_NORMAL); } } } // TODO remove this hack - /* flight termination in manual mode if assisted switch is on easy position */ - if (!status.is_rotary_wing && parachute_enabled && armed.armed && status.main_state == MAIN_STATE_MANUAL && sp_man.assisted_switch > STICK_ON_OFF_LIMIT) { + /* flight termination in manual mode if assist switch is on POSCTL position */ + if (!status.is_rotary_wing && parachute_enabled && armed.armed && status.main_state == MAIN_STATE_MANUAL && sp_man.posctl_switch == SWITCH_POS_ON) { if (TRANSITION_CHANGED == failsafe_state_transition(&status, FAILSAFE_STATE_TERMINATION)) { tune_positive(armed.armed); } @@ -1269,8 +1357,9 @@ int commander_thread_main(int argc, char *argv[]) orb_copy(ORB_ID(vehicle_command), cmd_sub, &cmd); /* handle it */ - if (handle_command(&status, &safety, &cmd, &armed)) + if (handle_command(&status, &safety, &cmd, &armed, &home, &global_position, &home_pub)) { status_changed = true; + } } /* check which state machines for changes, clear "changed" flag */ @@ -1284,8 +1373,34 @@ int commander_thread_main(int argc, char *argv[]) if (arming_state_changed) { status_changed = true; mavlink_log_info(mavlink_fd, "[cmd] arming state: %s", arming_states_str[status.arming_state]); + + /* update home position on arming if at least 2s from commander start spent to avoid setting home on in-air restart */ + if (armed.armed && !was_armed && hrt_absolute_time() > start_time + 2000000 && status.condition_global_position_valid && + (global_position.eph < eph_epv_threshold) && (global_position.epv < eph_epv_threshold)) { + + // TODO remove code duplication + home.lat = global_position.lat; + home.lon = global_position.lon; + home.alt = global_position.alt; + + warnx("home: lat = %.7f, lon = %.7f, alt = %.2f ", home.lat, home.lon, (double)home.alt); + mavlink_log_info(mavlink_fd, "[cmd] home: %.7f, %.7f, %.2f", home.lat, home.lon, (double)home.alt); + + /* announce new home position */ + if (home_pub > 0) { + orb_publish(ORB_ID(home_position), home_pub, &home); + + } else { + home_pub = orb_advertise(ORB_ID(home_position), &home); + } + + /* mark home position as set */ + status.condition_home_position_valid = true; + } } + was_armed = armed.armed; + if (main_state_changed) { status_changed = true; mavlink_log_info(mavlink_fd, "[cmd] main state: %s", main_states_str[status.main_state]); @@ -1447,21 +1562,24 @@ control_status_leds(vehicle_status_s *status, const actuator_armed_s *actuator_a } else if (actuator_armed->ready_to_arm) { /* ready to arm, blink at 1Hz */ - if (leds_counter % 20 == 0) + if (leds_counter % 20 == 0) { led_toggle(LED_BLUE); + } } else { /* not ready to arm, blink at 10Hz */ - if (leds_counter % 2 == 0) + if (leds_counter % 2 == 0) { led_toggle(LED_BLUE); + } } #endif /* give system warnings on error LED, XXX maybe add memory usage warning too */ if (status->load > 0.95f) { - if (leds_counter % 2 == 0) + if (leds_counter % 2 == 0) { led_toggle(LED_AMBER); + } } else { led_off(LED_AMBER); @@ -1470,106 +1588,63 @@ control_status_leds(vehicle_status_s *status, const actuator_armed_s *actuator_a leds_counter++; } -void -check_mode_switches(struct manual_control_setpoint_s *sp_man, struct vehicle_status_s *status) -{ - /* main mode switch */ - if (!isfinite(sp_man->mode_switch)) { - /* default to manual if signal is invalid */ - status->mode_switch = MODE_SWITCH_MANUAL; - - } else if (sp_man->mode_switch > STICK_ON_OFF_LIMIT) { - status->mode_switch = MODE_SWITCH_AUTO; - - } else if (sp_man->mode_switch < -STICK_ON_OFF_LIMIT) { - status->mode_switch = MODE_SWITCH_MANUAL; - - } else { - status->mode_switch = MODE_SWITCH_ASSISTED; - } - - /* return switch */ - if (!isfinite(sp_man->return_switch)) { - status->return_switch = RETURN_SWITCH_NONE; - - } else if (sp_man->return_switch > STICK_ON_OFF_LIMIT) { - status->return_switch = RETURN_SWITCH_RETURN; - - } else { - status->return_switch = RETURN_SWITCH_NORMAL; - } - - /* assisted switch */ - if (!isfinite(sp_man->assisted_switch)) { - status->assisted_switch = ASSISTED_SWITCH_SEATBELT; - - } else if (sp_man->assisted_switch > STICK_ON_OFF_LIMIT) { - status->assisted_switch = ASSISTED_SWITCH_EASY; - - } else { - status->assisted_switch = ASSISTED_SWITCH_SEATBELT; - } - - /* mission switch */ - if (!isfinite(sp_man->mission_switch)) { - status->mission_switch = MISSION_SWITCH_NONE; - - } else if (sp_man->mission_switch > STICK_ON_OFF_LIMIT) { - status->mission_switch = MISSION_SWITCH_LOITER; - - } else { - status->mission_switch = MISSION_SWITCH_MISSION; - } -} - transition_result_t -set_main_state_rc(struct vehicle_status_s *status) +set_main_state_rc(struct vehicle_status_s *status, struct manual_control_setpoint_s *sp_man) { /* set main state according to RC switches */ transition_result_t res = TRANSITION_DENIED; - switch (status->mode_switch) { - case MODE_SWITCH_MANUAL: + switch (sp_man->mode_switch) { + case SWITCH_POS_NONE: + res = TRANSITION_NOT_CHANGED; + break; + + case SWITCH_POS_OFF: // MANUAL res = main_state_transition(status, MAIN_STATE_MANUAL); // TRANSITION_DENIED is not possible here break; - case MODE_SWITCH_ASSISTED: - if (status->assisted_switch == ASSISTED_SWITCH_EASY) { - res = main_state_transition(status, MAIN_STATE_EASY); + case SWITCH_POS_MIDDLE: // ASSIST + if (sp_man->posctl_switch == SWITCH_POS_ON) { + res = main_state_transition(status, MAIN_STATE_POSCTL); - if (res != TRANSITION_DENIED) + if (res != TRANSITION_DENIED) { break; // changed successfully or already in this state + } - // else fallback to SEATBELT - print_reject_mode(status, "EASY"); + // else fallback to ALTCTL + print_reject_mode(status, "POSCTL"); } - res = main_state_transition(status, MAIN_STATE_SEATBELT); + res = main_state_transition(status, MAIN_STATE_ALTCTL); - if (res != TRANSITION_DENIED) + if (res != TRANSITION_DENIED) { break; // changed successfully or already in this mode + } - if (status->assisted_switch != ASSISTED_SWITCH_EASY) // don't print both messages - print_reject_mode(status, "SEATBELT"); + if (sp_man->posctl_switch != SWITCH_POS_ON) { + print_reject_mode(status, "ALTCTL"); + } // else fallback to MANUAL res = main_state_transition(status, MAIN_STATE_MANUAL); // TRANSITION_DENIED is not possible here break; - case MODE_SWITCH_AUTO: + case SWITCH_POS_ON: // AUTO res = main_state_transition(status, MAIN_STATE_AUTO); - if (res != TRANSITION_DENIED) + if (res != TRANSITION_DENIED) { break; // changed successfully or already in this state + } - // else fallback to SEATBELT (EASY likely will not work too) + // else fallback to ALTCTL (POSCTL likely will not work too) print_reject_mode(status, "AUTO"); - res = main_state_transition(status, MAIN_STATE_SEATBELT); + res = main_state_transition(status, MAIN_STATE_ALTCTL); - if (res != TRANSITION_DENIED) + if (res != TRANSITION_DENIED) { break; // changed successfully or already in this state + } // else fallback to MANUAL res = main_state_transition(status, MAIN_STATE_MANUAL); @@ -1611,7 +1686,7 @@ set_control_mode() control_mode.flag_control_velocity_enabled = false; break; - case MAIN_STATE_SEATBELT: + case MAIN_STATE_ALTCTL: control_mode.flag_control_manual_enabled = true; control_mode.flag_control_auto_enabled = false; control_mode.flag_control_rates_enabled = true; @@ -1622,7 +1697,7 @@ set_control_mode() control_mode.flag_control_velocity_enabled = false; break; - case MAIN_STATE_EASY: + case MAIN_STATE_POSCTL: control_mode.flag_control_manual_enabled = true; control_mode.flag_control_auto_enabled = false; control_mode.flag_control_rates_enabled = true; @@ -1635,6 +1710,7 @@ set_control_mode() case MAIN_STATE_AUTO: navigator_enabled = true; + break; default: break; @@ -1673,8 +1749,11 @@ set_control_mode() control_mode.flag_control_auto_enabled = true; control_mode.flag_control_rates_enabled = true; control_mode.flag_control_attitude_enabled = true; - control_mode.flag_control_position_enabled = true; - control_mode.flag_control_velocity_enabled = true; + + /* in failsafe LAND mode position may be not available */ + control_mode.flag_control_position_enabled = status.condition_local_position_valid; + control_mode.flag_control_velocity_enabled = status.condition_local_position_valid; + control_mode.flag_control_altitude_enabled = true; control_mode.flag_control_climb_rate_enabled = true; } @@ -1715,7 +1794,7 @@ void answer_command(struct vehicle_command_s &cmd, enum VEHICLE_CMD_RESULT resul { switch (result) { case VEHICLE_CMD_RESULT_ACCEPTED: - tune_positive(true); + tune_positive(true); break; case VEHICLE_CMD_RESULT_DENIED: @@ -1765,8 +1844,9 @@ void *commander_low_prio_loop(void *arg) int pret = poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 200); /* timed out - periodic check for thread_should_exit, etc. */ - if (pret == 0) + if (pret == 0) { continue; + } /* this is undesirable but not much we can do - might want to flag unhappy status */ if (pret < 0) { @@ -1781,8 +1861,9 @@ void *commander_low_prio_loop(void *arg) if (cmd.command == VEHICLE_CMD_DO_SET_MODE || cmd.command == VEHICLE_CMD_COMPONENT_ARM_DISARM || cmd.command == VEHICLE_CMD_NAV_TAKEOFF || - cmd.command == VEHICLE_CMD_DO_SET_SERVO) + cmd.command == VEHICLE_CMD_DO_SET_SERVO) { continue; + } /* only handle low-priority commands here */ switch (cmd.command) { @@ -1860,6 +1941,7 @@ void *commander_low_prio_loop(void *arg) /* airspeed calibration */ answer_command(cmd, VEHICLE_CMD_RESULT_ACCEPTED); calib_ret = do_airspeed_calibration(mavlink_fd); + } else if ((int)(cmd.param4) == 0) { /* RC calibration ended - have we been in one worth confirming? */ if (status.rc_input_blocked) { @@ -1874,10 +1956,12 @@ void *commander_low_prio_loop(void *arg) } - if (calib_ret == OK) + if (calib_ret == OK) { tune_positive(true); - else + + } else { tune_negative(true); + } arming_state_transition(&status, &safety, ARMING_STATE_STANDBY, &armed); @@ -1897,11 +1981,13 @@ void *commander_low_prio_loop(void *arg) mavlink_log_critical(mavlink_fd, "#audio: parameters load ERROR"); /* convenience as many parts of NuttX use negative errno */ - if (ret < 0) + if (ret < 0) { ret = -ret; + } - if (ret < 1000) + if (ret < 1000) { mavlink_log_critical(mavlink_fd, "#audio: %s", strerror(ret)); + } answer_command(cmd, VEHICLE_CMD_RESULT_FAILED); } @@ -1917,11 +2003,13 @@ void *commander_low_prio_loop(void *arg) mavlink_log_critical(mavlink_fd, "#audio: parameters save error"); /* convenience as many parts of NuttX use negative errno */ - if (ret < 0) + if (ret < 0) { ret = -ret; + } - if (ret < 1000) + if (ret < 1000) { mavlink_log_critical(mavlink_fd, "#audio: %s", strerror(ret)); + } answer_command(cmd, VEHICLE_CMD_RESULT_FAILED); } @@ -1931,8 +2019,8 @@ void *commander_low_prio_loop(void *arg) } case VEHICLE_CMD_START_RX_PAIR: - /* handled in the IO driver */ - break; + /* handled in the IO driver */ + break; default: /* don't answer on unsupported commands, it will be done in main loop */ diff --git a/src/modules/commander/commander_helper.cpp b/src/modules/commander/commander_helper.cpp index fe6c9bfaa..940a04aa1 100644 --- a/src/modules/commander/commander_helper.cpp +++ b/src/modules/commander/commander_helper.cpp @@ -113,17 +113,22 @@ void buzzer_deinit() close(buzzer); } -void set_tune(int tune) { +void set_tune(int tune) +{ unsigned int new_tune_duration = tune_durations[tune]; + /* don't interrupt currently playing non-repeating tune by repeating */ if (tune_end == 0 || new_tune_duration != 0 || hrt_absolute_time() > tune_end) { /* allow interrupting current non-repeating tune by the same tune */ if (tune != tune_current || new_tune_duration != 0) { ioctl(buzzer, TONE_SET_ALARM, tune); } + tune_current = tune; + if (new_tune_duration != 0) { tune_end = hrt_absolute_time() + new_tune_duration; + } else { tune_end = 0; } @@ -138,6 +143,7 @@ void tune_positive(bool use_buzzer) blink_msg_end = hrt_absolute_time() + BLINK_MSG_TIME; rgbled_set_color(RGBLED_COLOR_GREEN); rgbled_set_mode(RGBLED_MODE_BLINK_FAST); + if (use_buzzer) { set_tune(TONE_NOTIFY_POSITIVE_TUNE); } @@ -151,6 +157,7 @@ void tune_neutral(bool use_buzzer) blink_msg_end = hrt_absolute_time() + BLINK_MSG_TIME; rgbled_set_color(RGBLED_COLOR_WHITE); rgbled_set_mode(RGBLED_MODE_BLINK_FAST); + if (use_buzzer) { set_tune(TONE_NOTIFY_NEUTRAL_TUNE); } @@ -164,6 +171,7 @@ void tune_negative(bool use_buzzer) blink_msg_end = hrt_absolute_time() + BLINK_MSG_TIME; rgbled_set_color(RGBLED_COLOR_RED); rgbled_set_mode(RGBLED_MODE_BLINK_FAST); + if (use_buzzer) { set_tune(TONE_NOTIFY_NEGATIVE_TUNE); } @@ -198,16 +206,10 @@ int led_init() return ERROR; } - /* the blue LED is only available on FMUv1 but not FMUv2 */ -#ifdef CONFIG_ARCH_BOARD_PX4FMU_V1 - - if (ioctl(leds, LED_ON, LED_BLUE)) { - warnx("Blue LED: ioctl fail\n"); - return ERROR; - } - -#endif + /* the blue LED is only available on FMUv1 & AeroCore but not FMUv2 */ + (void)ioctl(leds, LED_ON, LED_BLUE); + /* we consider the amber led mandatory */ if (ioctl(leds, LED_ON, LED_AMBER)) { warnx("Amber LED: ioctl fail\n"); return ERROR; @@ -217,11 +219,7 @@ int led_init() rgbleds = open(RGBLED_DEVICE_PATH, 0); if (rgbleds == -1) { -#ifdef CONFIG_ARCH_BOARD_PX4FMU_V2 - errx(1, "Unable to open " RGBLED_DEVICE_PATH); -#else - warnx("No RGB LED found"); -#endif + warnx("No RGB LED found at " RGBLED_DEVICE_PATH); } return 0; @@ -254,22 +252,25 @@ int led_off(int led) void rgbled_set_color(rgbled_color_t color) { - if (rgbleds != -1) + if (rgbleds != -1) { ioctl(rgbleds, RGBLED_SET_COLOR, (unsigned long)color); + } } void rgbled_set_mode(rgbled_mode_t mode) { - if (rgbleds != -1) + if (rgbleds != -1) { ioctl(rgbleds, RGBLED_SET_MODE, (unsigned long)mode); + } } void rgbled_set_pattern(rgbled_pattern_t *pattern) { - if (rgbleds != -1) + if (rgbleds != -1) { ioctl(rgbleds, RGBLED_SET_PATTERN, (unsigned long)pattern); + } } float battery_remaining_estimate_voltage(float voltage, float discharged) @@ -309,6 +310,7 @@ float battery_remaining_estimate_voltage(float voltage, float discharged) if (bat_capacity > 0.0f) { /* if battery capacity is known, use discharged current for estimate, but don't show more than voltage estimate */ ret = fminf(remaining_voltage, 1.0f - discharged / bat_capacity); + } else { /* else use voltage */ ret = remaining_voltage; diff --git a/src/modules/commander/commander_tests/commander_tests.cpp b/src/modules/commander/commander_tests/commander_tests.cpp index 6e72cf0d9..0abb84a82 100644 --- a/src/modules/commander/commander_tests/commander_tests.cpp +++ b/src/modules/commander/commander_tests/commander_tests.cpp @@ -48,8 +48,7 @@ extern "C" __EXPORT int commander_tests_main(int argc, char *argv[]); int commander_tests_main(int argc, char *argv[]) { - state_machine_helper_test(); - //state_machine_test(); + stateMachineHelperTest(); return 0; } diff --git a/src/modules/commander/commander_tests/state_machine_helper_test.cpp b/src/modules/commander/commander_tests/state_machine_helper_test.cpp index 40bedd9f3..ee0d08391 100644 --- a/src/modules/commander/commander_tests/state_machine_helper_test.cpp +++ b/src/modules/commander/commander_tests/state_machine_helper_test.cpp @@ -49,13 +49,12 @@ public: StateMachineHelperTest(); virtual ~StateMachineHelperTest(); - virtual const char* run_tests(); + virtual void runTests(void); private: - const char* arming_state_transition_test(); - const char* arming_state_transition_arm_disarm_test(); - const char* main_state_transition_test(); - const char* is_safe_test(); + bool armingStateTransitionTest(); + bool mainStateTransitionTest(); + bool isSafeTest(); }; StateMachineHelperTest::StateMachineHelperTest() { @@ -64,61 +63,242 @@ StateMachineHelperTest::StateMachineHelperTest() { StateMachineHelperTest::~StateMachineHelperTest() { } -const char* -StateMachineHelperTest::arming_state_transition_test() +bool StateMachineHelperTest::armingStateTransitionTest(void) { + // These are the critical values from vehicle_status_s and actuator_armed_s which must be primed + // to simulate machine state prior to testing an arming state transition. This structure is also + // use to represent the expected machine state after the transition has been requested. + typedef struct { + arming_state_t arming_state; // vehicle_status_s.arming_state + bool armed; // actuator_armed_s.armed + bool ready_to_arm; // actuator_armed_s.ready_to_arm + } ArmingTransitionVolatileState_t; + + // This structure represents a test case for arming_state_transition. It contains the machine + // state prior to transtion, the requested state to transition to and finally the expected + // machine state after transition. + typedef struct { + const char* assertMsg; // Text to show when test case fails + ArmingTransitionVolatileState_t current_state; // Machine state prior to transtion + hil_state_t hil_state; // Current vehicle_status_s.hil_state + bool condition_system_sensors_initialized; // Current vehicle_status_s.condition_system_sensors_initialized + bool safety_switch_available; // Current safety_s.safety_switch_available + bool safety_off; // Current safety_s.safety_off + arming_state_t requested_state; // Requested arming state to transition to + ArmingTransitionVolatileState_t expected_state; // Expected machine state after transition + transition_result_t expected_transition_result; // Expected result from arming_state_transition + } ArmingTransitionTest_t; + + // We use these defines so that our test cases are more readable + #define ATT_ARMED true + #define ATT_DISARMED false + #define ATT_READY_TO_ARM true + #define ATT_NOT_READY_TO_ARM false + #define ATT_SENSORS_INITIALIZED true + #define ATT_SENSORS_NOT_INITIALIZED false + #define ATT_SAFETY_AVAILABLE true + #define ATT_SAFETY_NOT_AVAILABLE true + #define ATT_SAFETY_OFF true + #define ATT_SAFETY_ON false + + // These are test cases for arming_state_transition + static const ArmingTransitionTest_t rgArmingTransitionTests[] = { + // TRANSITION_NOT_CHANGED tests + + { "no transition: identical states", + { ARMING_STATE_INIT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_INIT, + { ARMING_STATE_INIT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_NOT_CHANGED }, + + // TRANSITION_CHANGED tests + + // Check all basic valid transitions, these don't require special state in vehicle_status_t or safety_s + + { "transition: init to standby", + { ARMING_STATE_INIT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_STANDBY, + { ARMING_STATE_STANDBY, ATT_DISARMED, ATT_READY_TO_ARM }, TRANSITION_CHANGED }, + + { "transition: init to standby error", + { ARMING_STATE_INIT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_STANDBY_ERROR, + { ARMING_STATE_STANDBY_ERROR, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_CHANGED }, + + { "transition: init to reboot", + { ARMING_STATE_INIT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_REBOOT, + { ARMING_STATE_REBOOT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_CHANGED }, + + { "transition: standby to init", + { ARMING_STATE_STANDBY, ATT_DISARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_INIT, + { ARMING_STATE_INIT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_CHANGED }, + + { "transition: standby to standby error", + { ARMING_STATE_STANDBY, ATT_DISARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_STANDBY_ERROR, + { ARMING_STATE_STANDBY_ERROR, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_CHANGED }, + + { "transition: standby to reboot", + { ARMING_STATE_STANDBY, ATT_DISARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_REBOOT, + { ARMING_STATE_REBOOT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_CHANGED }, + + { "transition: armed to standby", + { ARMING_STATE_ARMED, ATT_ARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_STANDBY, + { ARMING_STATE_STANDBY, ATT_DISARMED, ATT_READY_TO_ARM }, TRANSITION_CHANGED }, + + { "transition: armed to armed error", + { ARMING_STATE_ARMED, ATT_ARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_ARMED_ERROR, + { ARMING_STATE_ARMED_ERROR, ATT_ARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_CHANGED }, + + { "transition: armed error to standby error", + { ARMING_STATE_ARMED_ERROR, ATT_ARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_STANDBY_ERROR, + { ARMING_STATE_STANDBY_ERROR, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_CHANGED }, + + { "transition: standby error to reboot", + { ARMING_STATE_STANDBY_ERROR, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_REBOOT, + { ARMING_STATE_REBOOT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_CHANGED }, + + { "transition: in air restore to armed", + { ARMING_STATE_IN_AIR_RESTORE, ATT_DISARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_ARMED, + { ARMING_STATE_ARMED, ATT_ARMED, ATT_READY_TO_ARM }, TRANSITION_CHANGED }, + + { "transition: in air restore to reboot", + { ARMING_STATE_IN_AIR_RESTORE, ATT_DISARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_REBOOT, + { ARMING_STATE_REBOOT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_CHANGED }, + + // hil on tests, standby error to standby not normally allowed + + { "transition: standby error to standby, hil on", + { ARMING_STATE_STANDBY_ERROR, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_ON, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_STANDBY, + { ARMING_STATE_STANDBY, ATT_DISARMED, ATT_READY_TO_ARM }, TRANSITION_CHANGED }, + + // Safety switch arming tests + + { "transition: init to standby, no safety switch", + { ARMING_STATE_STANDBY, ATT_DISARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_NOT_AVAILABLE, ATT_SAFETY_OFF, + ARMING_STATE_ARMED, + { ARMING_STATE_ARMED, ATT_ARMED, ATT_READY_TO_ARM }, TRANSITION_CHANGED }, + + { "transition: init to standby, safety switch off", + { ARMING_STATE_STANDBY, ATT_DISARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_OFF, + ARMING_STATE_ARMED, + { ARMING_STATE_ARMED, ATT_ARMED, ATT_READY_TO_ARM }, TRANSITION_CHANGED }, + + // standby error + { "transition: armed error to standby error requested standby", + { ARMING_STATE_ARMED_ERROR, ATT_ARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_STANDBY, + { ARMING_STATE_STANDBY_ERROR, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_CHANGED }, + + // TRANSITION_DENIED tests + + // Check some important basic invalid transitions, these don't require special state in vehicle_status_t or safety_s + + { "no transition: init to armed", + { ARMING_STATE_INIT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_ARMED, + { ARMING_STATE_INIT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_DENIED }, + + { "no transition: standby to armed error", + { ARMING_STATE_STANDBY, ATT_DISARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_ARMED_ERROR, + { ARMING_STATE_STANDBY, ATT_DISARMED, ATT_READY_TO_ARM }, TRANSITION_DENIED }, + + { "no transition: armed to init", + { ARMING_STATE_ARMED, ATT_ARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_INIT, + { ARMING_STATE_ARMED, ATT_ARMED, ATT_READY_TO_ARM }, TRANSITION_DENIED }, + + { "no transition: armed to reboot", + { ARMING_STATE_ARMED, ATT_ARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_REBOOT, + { ARMING_STATE_ARMED, ATT_ARMED, ATT_READY_TO_ARM }, TRANSITION_DENIED }, + + { "no transition: armed error to armed", + { ARMING_STATE_ARMED_ERROR, ATT_ARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_ARMED, + { ARMING_STATE_ARMED_ERROR, ATT_ARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_DENIED }, + + { "no transition: armed error to reboot", + { ARMING_STATE_ARMED_ERROR, ATT_ARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_REBOOT, + { ARMING_STATE_ARMED_ERROR, ATT_ARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_DENIED }, + + { "no transition: standby error to armed", + { ARMING_STATE_STANDBY_ERROR, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_ARMED, + { ARMING_STATE_STANDBY_ERROR, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_DENIED }, + + { "no transition: standby error to standby", + { ARMING_STATE_STANDBY_ERROR, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_STANDBY, + { ARMING_STATE_STANDBY_ERROR, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_DENIED }, + + { "no transition: reboot to armed", + { ARMING_STATE_REBOOT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_ARMED, + { ARMING_STATE_REBOOT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_DENIED }, + + { "no transition: in air restore to standby", + { ARMING_STATE_IN_AIR_RESTORE, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_STANDBY, + { ARMING_STATE_IN_AIR_RESTORE, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_DENIED }, + + // Sensor tests + + { "no transition: init to standby - sensors not initialized", + { ARMING_STATE_INIT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_NOT_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_STANDBY, + { ARMING_STATE_INIT, ATT_DISARMED, ATT_NOT_READY_TO_ARM }, TRANSITION_DENIED }, + + // Safety switch arming tests + + { "no transition: init to standby, safety switch on", + { ARMING_STATE_STANDBY, ATT_DISARMED, ATT_READY_TO_ARM }, HIL_STATE_OFF, ATT_SENSORS_INITIALIZED, ATT_SAFETY_AVAILABLE, ATT_SAFETY_ON, + ARMING_STATE_ARMED, + { ARMING_STATE_STANDBY, ATT_DISARMED, ATT_READY_TO_ARM }, TRANSITION_DENIED }, + }; + struct vehicle_status_s status; - struct safety_s safety; - arming_state_t new_arming_state; - struct actuator_armed_s armed; - - // Identical states. - status.arming_state = ARMING_STATE_INIT; - new_arming_state = ARMING_STATE_INIT; - mu_assert("no transition: identical states", - TRANSITION_NOT_CHANGED == arming_state_transition(&status, &safety, new_arming_state, &armed)); - - // INIT to STANDBY. - armed.armed = false; - armed.ready_to_arm = false; - status.arming_state = ARMING_STATE_INIT; - status.condition_system_sensors_initialized = true; - new_arming_state = ARMING_STATE_STANDBY; - mu_assert("transition: init to standby", - TRANSITION_CHANGED == arming_state_transition(&status, &safety, new_arming_state, &armed)); - mu_assert("current state: standby", ARMING_STATE_STANDBY == status.arming_state); - mu_assert("not armed", !armed.armed); - mu_assert("ready to arm", armed.ready_to_arm); - - // INIT to STANDBY, sensors not initialized. - armed.armed = false; - armed.ready_to_arm = false; - status.arming_state = ARMING_STATE_INIT; - status.condition_system_sensors_initialized = false; - new_arming_state = ARMING_STATE_STANDBY; - mu_assert("no transition: sensors not initialized", - TRANSITION_DENIED == arming_state_transition(&status, &safety, new_arming_state, &armed)); - mu_assert("current state: init", ARMING_STATE_INIT == status.arming_state); - mu_assert("not armed", !armed.armed); - mu_assert("not ready to arm", !armed.ready_to_arm); - - return 0; -} - -const char* -StateMachineHelperTest::arming_state_transition_arm_disarm_test() -{ - struct vehicle_status_s status; - struct safety_s safety; - arming_state_t new_arming_state; + struct safety_s safety; struct actuator_armed_s armed; - - // TODO(sjwilks): ARM then DISARM. - return 0; + + size_t cArmingTransitionTests = sizeof(rgArmingTransitionTests) / sizeof(rgArmingTransitionTests[0]); + for (size_t i=0; i<cArmingTransitionTests; i++) { + const ArmingTransitionTest_t* test = &rgArmingTransitionTests[i]; + + // Setup initial machine state + status.arming_state = test->current_state.arming_state; + status.condition_system_sensors_initialized = test->condition_system_sensors_initialized; + status.hil_state = test->hil_state; + safety.safety_switch_available = test->safety_switch_available; + safety.safety_off = test->safety_off; + armed.armed = test->current_state.armed; + armed.ready_to_arm = test->current_state.ready_to_arm; + + // Attempt transition + transition_result_t result = arming_state_transition(&status, &safety, test->requested_state, &armed); + + // Validate result of transition + ut_assert(test->assertMsg, test->expected_transition_result == result); + ut_assert(test->assertMsg, status.arming_state == test->expected_state.arming_state); + ut_assert(test->assertMsg, armed.armed == test->expected_state.armed); + ut_assert(test->assertMsg, armed.ready_to_arm == test->expected_state.ready_to_arm); + } + + return true; } -const char* -StateMachineHelperTest::main_state_transition_test() +bool StateMachineHelperTest::mainStateTransitionTest(void) { struct vehicle_status_s current_state; main_state_t new_main_state; @@ -126,70 +306,69 @@ StateMachineHelperTest::main_state_transition_test() // Identical states. current_state.main_state = MAIN_STATE_MANUAL; new_main_state = MAIN_STATE_MANUAL; - mu_assert("no transition: identical states", + ut_assert("no transition: identical states", TRANSITION_NOT_CHANGED == main_state_transition(¤t_state, new_main_state)); - mu_assert("current state: manual", MAIN_STATE_MANUAL == current_state.main_state); + ut_assert("current state: manual", MAIN_STATE_MANUAL == current_state.main_state); // AUTO to MANUAL. current_state.main_state = MAIN_STATE_AUTO; new_main_state = MAIN_STATE_MANUAL; - mu_assert("transition changed: auto to manual", + ut_assert("transition changed: auto to manual", TRANSITION_CHANGED == main_state_transition(¤t_state, new_main_state)); - mu_assert("new state: manual", MAIN_STATE_MANUAL == current_state.main_state); + ut_assert("new state: manual", MAIN_STATE_MANUAL == current_state.main_state); - // MANUAL to SEATBELT. + // MANUAL to ALTCTRL. current_state.main_state = MAIN_STATE_MANUAL; current_state.condition_local_altitude_valid = true; - new_main_state = MAIN_STATE_SEATBELT; - mu_assert("tranisition: manual to seatbelt", + new_main_state = MAIN_STATE_ALTCTL; + ut_assert("tranisition: manual to altctrl", TRANSITION_CHANGED == main_state_transition(¤t_state, new_main_state)); - mu_assert("new state: seatbelt", MAIN_STATE_SEATBELT == current_state.main_state); + ut_assert("new state: altctrl", MAIN_STATE_ALTCTL == current_state.main_state); - // MANUAL to SEATBELT, invalid local altitude. + // MANUAL to ALTCTRL, invalid local altitude. current_state.main_state = MAIN_STATE_MANUAL; current_state.condition_local_altitude_valid = false; - new_main_state = MAIN_STATE_SEATBELT; - mu_assert("no transition: invalid local altitude", + new_main_state = MAIN_STATE_ALTCTL; + ut_assert("no transition: invalid local altitude", TRANSITION_DENIED == main_state_transition(¤t_state, new_main_state)); - mu_assert("current state: manual", MAIN_STATE_MANUAL == current_state.main_state); + ut_assert("current state: manual", MAIN_STATE_MANUAL == current_state.main_state); - // MANUAL to EASY. + // MANUAL to POSCTRL. current_state.main_state = MAIN_STATE_MANUAL; current_state.condition_local_position_valid = true; - new_main_state = MAIN_STATE_EASY; - mu_assert("transition: manual to easy", + new_main_state = MAIN_STATE_POSCTL; + ut_assert("transition: manual to posctrl", TRANSITION_CHANGED == main_state_transition(¤t_state, new_main_state)); - mu_assert("current state: easy", MAIN_STATE_EASY == current_state.main_state); + ut_assert("current state: posctrl", MAIN_STATE_POSCTL == current_state.main_state); - // MANUAL to EASY, invalid local position. + // MANUAL to POSCTRL, invalid local position. current_state.main_state = MAIN_STATE_MANUAL; current_state.condition_local_position_valid = false; - new_main_state = MAIN_STATE_EASY; - mu_assert("no transition: invalid position", + new_main_state = MAIN_STATE_POSCTL; + ut_assert("no transition: invalid position", TRANSITION_DENIED == main_state_transition(¤t_state, new_main_state)); - mu_assert("current state: manual", MAIN_STATE_MANUAL == current_state.main_state); + ut_assert("current state: manual", MAIN_STATE_MANUAL == current_state.main_state); // MANUAL to AUTO. current_state.main_state = MAIN_STATE_MANUAL; current_state.condition_global_position_valid = true; new_main_state = MAIN_STATE_AUTO; - mu_assert("transition: manual to auto", + ut_assert("transition: manual to auto", TRANSITION_CHANGED == main_state_transition(¤t_state, new_main_state)); - mu_assert("current state: auto", MAIN_STATE_AUTO == current_state.main_state); + ut_assert("current state: auto", MAIN_STATE_AUTO == current_state.main_state); // MANUAL to AUTO, invalid global position. current_state.main_state = MAIN_STATE_MANUAL; current_state.condition_global_position_valid = false; new_main_state = MAIN_STATE_AUTO; - mu_assert("no transition: invalid global position", + ut_assert("no transition: invalid global position", TRANSITION_DENIED == main_state_transition(¤t_state, new_main_state)); - mu_assert("current state: manual", MAIN_STATE_MANUAL == current_state.main_state); + ut_assert("current state: manual", MAIN_STATE_MANUAL == current_state.main_state); - return 0; + return true; } -const char* -StateMachineHelperTest::is_safe_test() +bool StateMachineHelperTest::isSafeTest(void) { struct vehicle_status_s current_state; struct safety_s safety; @@ -199,49 +378,45 @@ StateMachineHelperTest::is_safe_test() armed.lockdown = false; safety.safety_switch_available = true; safety.safety_off = false; - mu_assert("is safe: not armed", is_safe(¤t_state, &safety, &armed)); + ut_assert("is safe: not armed", is_safe(¤t_state, &safety, &armed)); armed.armed = false; armed.lockdown = true; safety.safety_switch_available = true; safety.safety_off = true; - mu_assert("is safe: software lockdown", is_safe(¤t_state, &safety, &armed)); + ut_assert("is safe: software lockdown", is_safe(¤t_state, &safety, &armed)); armed.armed = true; armed.lockdown = false; safety.safety_switch_available = true; safety.safety_off = true; - mu_assert("not safe: safety off", !is_safe(¤t_state, &safety, &armed)); + ut_assert("not safe: safety off", !is_safe(¤t_state, &safety, &armed)); armed.armed = true; armed.lockdown = false; safety.safety_switch_available = true; safety.safety_off = false; - mu_assert("is safe: safety off", is_safe(¤t_state, &safety, &armed)); + ut_assert("is safe: safety off", is_safe(¤t_state, &safety, &armed)); armed.armed = true; armed.lockdown = false; safety.safety_switch_available = false; safety.safety_off = false; - mu_assert("not safe: no safety switch", !is_safe(¤t_state, &safety, &armed)); + ut_assert("not safe: no safety switch", !is_safe(¤t_state, &safety, &armed)); - return 0; + return true; } -const char* -StateMachineHelperTest::run_tests() +void StateMachineHelperTest::runTests(void) { - mu_run_test(arming_state_transition_test); - mu_run_test(arming_state_transition_arm_disarm_test); - mu_run_test(main_state_transition_test); - mu_run_test(is_safe_test); - - return 0; + ut_run_test(armingStateTransitionTest); + ut_run_test(mainStateTransitionTest); + ut_run_test(isSafeTest); } -void -state_machine_helper_test() +void stateMachineHelperTest(void) { StateMachineHelperTest* test = new StateMachineHelperTest(); - test->UnitTest::print_results(test->run_tests()); + test->runTests(); + test->printResults(); } diff --git a/src/modules/commander/commander_tests/state_machine_helper_test.h b/src/modules/commander/commander_tests/state_machine_helper_test.h index 10a68e602..bbf66255e 100644 --- a/src/modules/commander/commander_tests/state_machine_helper_test.h +++ b/src/modules/commander/commander_tests/state_machine_helper_test.h @@ -39,6 +39,6 @@ #ifndef STATE_MACHINE_HELPER_TEST_H_ #define STATE_MACHINE_HELPER_TEST_ -void state_machine_helper_test(); +void stateMachineHelperTest(void); #endif /* STATE_MACHINE_HELPER_TEST_H_ */ diff --git a/src/modules/commander/gyro_calibration.cpp b/src/modules/commander/gyro_calibration.cpp index 30cd0d48d..cbc2844c1 100644 --- a/src/modules/commander/gyro_calibration.cpp +++ b/src/modules/commander/gyro_calibration.cpp @@ -110,8 +110,9 @@ int do_gyro_calibration(int mavlink_fd) gyro_scale.z_offset += gyro_report.z; calibration_counter++; - if (calibration_counter % (calibration_count / 20) == 0) + if (calibration_counter % (calibration_count / 20) == 0) { mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, (calibration_counter * 100) / calibration_count); + } } else { poll_errcount++; @@ -163,8 +164,9 @@ int do_gyro_calibration(int mavlink_fd) /* apply new offsets */ fd = open(GYRO_DEVICE_PATH, 0); - if (OK != ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gyro_scale)) + if (OK != ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gyro_scale)) { warn("WARNING: failed to apply new offsets for gyro"); + } close(fd); @@ -178,9 +180,9 @@ int do_gyro_calibration(int mavlink_fd) float mag_last = -atan2f(raw.magnetometer_ga[1], raw.magnetometer_ga[0]); - if (mag_last > M_PI_F) mag_last -= 2 * M_PI_F; + if (mag_last > M_PI_F) { mag_last -= 2 * M_PI_F; } - if (mag_last < -M_PI_F) mag_last += 2 * M_PI_F; + if (mag_last < -M_PI_F) { mag_last += 2 * M_PI_F; } uint64_t last_time = hrt_absolute_time(); @@ -220,15 +222,15 @@ int do_gyro_calibration(int mavlink_fd) //float mag = -atan2f(magNav(1),magNav(0)); float mag = -atan2f(raw.magnetometer_ga[1], raw.magnetometer_ga[0]); - if (mag > M_PI_F) mag -= 2 * M_PI_F; + if (mag > M_PI_F) { mag -= 2 * M_PI_F; } - if (mag < -M_PI_F) mag += 2 * M_PI_F; + if (mag < -M_PI_F) { mag += 2 * M_PI_F; } float diff = mag - mag_last; - if (diff > M_PI_F) diff -= 2 * M_PI_F; + if (diff > M_PI_F) { diff -= 2 * M_PI_F; } - if (diff < -M_PI_F) diff += 2 * M_PI_F; + if (diff < -M_PI_F) { diff += 2 * M_PI_F; } baseline_integral += diff; mag_last = mag; diff --git a/src/modules/commander/mag_calibration.cpp b/src/modules/commander/mag_calibration.cpp index 4ebf266f4..0ead22f77 100644 --- a/src/modules/commander/mag_calibration.cpp +++ b/src/modules/commander/mag_calibration.cpp @@ -72,7 +72,7 @@ int do_mag_calibration(int mavlink_fd) uint64_t calibration_interval = 45 * 1000 * 1000; /* maximum 500 values */ - const unsigned int calibration_maxcount = 500; + const unsigned int calibration_maxcount = 240; unsigned int calibration_counter; struct mag_scale mscale_null = { @@ -121,9 +121,24 @@ int do_mag_calibration(int mavlink_fd) if (x == NULL || y == NULL || z == NULL) { mavlink_log_critical(mavlink_fd, "ERROR: out of memory"); + + /* clean up */ + if (x != NULL) { + free(x); + } + + if (y != NULL) { + free(y); + } + + if (z != NULL) { + free(z); + } + res = ERROR; return res; } + } else { /* exit */ return ERROR; @@ -163,8 +178,9 @@ int do_mag_calibration(int mavlink_fd) calibration_counter++; - if (calibration_counter % (calibration_maxcount / 20) == 0) + if (calibration_counter % (calibration_maxcount / 20) == 0) { mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 20 + (calibration_counter * 50) / calibration_maxcount); + } } else { poll_errcount++; @@ -198,14 +214,17 @@ int do_mag_calibration(int mavlink_fd) } } - if (x != NULL) + if (x != NULL) { free(x); + } - if (y != NULL) + if (y != NULL) { free(y); + } - if (z != NULL) + if (z != NULL) { free(z); + } if (res == OK) { /* apply calibration and set parameters */ @@ -234,23 +253,29 @@ int do_mag_calibration(int mavlink_fd) if (res == OK) { /* set parameters */ - if (param_set(param_find("SENS_MAG_XOFF"), &(mscale.x_offset))) + if (param_set(param_find("SENS_MAG_XOFF"), &(mscale.x_offset))) { res = ERROR; + } - if (param_set(param_find("SENS_MAG_YOFF"), &(mscale.y_offset))) + if (param_set(param_find("SENS_MAG_YOFF"), &(mscale.y_offset))) { res = ERROR; + } - if (param_set(param_find("SENS_MAG_ZOFF"), &(mscale.z_offset))) + if (param_set(param_find("SENS_MAG_ZOFF"), &(mscale.z_offset))) { res = ERROR; + } - if (param_set(param_find("SENS_MAG_XSCALE"), &(mscale.x_scale))) + if (param_set(param_find("SENS_MAG_XSCALE"), &(mscale.x_scale))) { res = ERROR; + } - if (param_set(param_find("SENS_MAG_YSCALE"), &(mscale.y_scale))) + if (param_set(param_find("SENS_MAG_YSCALE"), &(mscale.y_scale))) { res = ERROR; + } - if (param_set(param_find("SENS_MAG_ZSCALE"), &(mscale.z_scale))) + if (param_set(param_find("SENS_MAG_ZSCALE"), &(mscale.z_scale))) { res = ERROR; + } if (res != OK) { mavlink_log_critical(mavlink_fd, CAL_FAILED_SET_PARAMS_MSG); diff --git a/src/modules/commander/module.mk b/src/modules/commander/module.mk index 554dfcb08..27ca5c182 100644 --- a/src/modules/commander/module.mk +++ b/src/modules/commander/module.mk @@ -47,3 +47,7 @@ SRCS = commander.cpp \ baro_calibration.cpp \ rc_calibration.cpp \ airspeed_calibration.cpp + +MODULE_STACKSIZE = 1200 + +MAXOPTIMIZATION = -Os diff --git a/src/modules/commander/px4_custom_mode.h b/src/modules/commander/px4_custom_mode.h index 2144d3460..a83c81850 100644 --- a/src/modules/commander/px4_custom_mode.h +++ b/src/modules/commander/px4_custom_mode.h @@ -12,8 +12,8 @@ enum PX4_CUSTOM_MAIN_MODE { PX4_CUSTOM_MAIN_MODE_MANUAL = 1, - PX4_CUSTOM_MAIN_MODE_SEATBELT, - PX4_CUSTOM_MAIN_MODE_EASY, + PX4_CUSTOM_MAIN_MODE_ALTCTL, + PX4_CUSTOM_MAIN_MODE_POSCTL, PX4_CUSTOM_MAIN_MODE_AUTO, }; diff --git a/src/modules/commander/rc_calibration.cpp b/src/modules/commander/rc_calibration.cpp index 41f3ca0aa..0776894fb 100644 --- a/src/modules/commander/rc_calibration.cpp +++ b/src/modules/commander/rc_calibration.cpp @@ -69,11 +69,11 @@ int do_trim_calibration(int mavlink_fd) orb_copy(ORB_ID(manual_control_setpoint), sub_man, &sp); /* set parameters */ - float p = sp.roll; + float p = sp.y; param_set(param_find("TRIM_ROLL"), &p); - p = sp.pitch; + p = sp.x; param_set(param_find("TRIM_PITCH"), &p); - p = sp.yaw; + p = sp.r; param_set(param_find("TRIM_YAW"), &p); /* store to permanent storage */ diff --git a/src/modules/commander/state_machine_helper.cpp b/src/modules/commander/state_machine_helper.cpp index e6f245cf9..abcf72717 100644 --- a/src/modules/commander/state_machine_helper.cpp +++ b/src/modules/commander/state_machine_helper.cpp @@ -69,10 +69,44 @@ static bool arming_state_changed = true; static bool main_state_changed = true; static bool failsafe_state_changed = true; +// This array defines the arming state transitions. The rows are the new state, and the columns +// are the current state. Using new state and current state you can index into the array which +// will be true for a valid transition or false for a invalid transition. In some cases even +// though the transition is marked as true additional checks must be made. See arming_state_transition +// code for those checks. +static const bool arming_transitions[ARMING_STATE_MAX][ARMING_STATE_MAX] = { + // INIT, STANDBY, ARMED, ARMED_ERROR, STANDBY_ERROR, REBOOT, IN_AIR_RESTORE + { /* ARMING_STATE_INIT */ true, true, false, false, false, false, false }, + { /* ARMING_STATE_STANDBY */ true, true, true, true, false, false, false }, + { /* ARMING_STATE_ARMED */ false, true, true, false, false, false, true }, + { /* ARMING_STATE_ARMED_ERROR */ false, false, true, true, false, false, false }, + { /* ARMING_STATE_STANDBY_ERROR */ true, true, false, true, true, false, false }, + { /* ARMING_STATE_REBOOT */ true, true, false, false, true, true, true }, + { /* ARMING_STATE_IN_AIR_RESTORE */ false, false, false, false, false, false, false }, // NYI +}; + +// You can index into the array with an arming_state_t in order to get it's textual representation +static const char *state_names[ARMING_STATE_MAX] = { + "ARMING_STATE_INIT", + "ARMING_STATE_STANDBY", + "ARMING_STATE_ARMED", + "ARMING_STATE_ARMED_ERROR", + "ARMING_STATE_STANDBY_ERROR", + "ARMING_STATE_REBOOT", + "ARMING_STATE_IN_AIR_RESTORE", +}; + transition_result_t -arming_state_transition(struct vehicle_status_s *status, const struct safety_s *safety, - arming_state_t new_arming_state, struct actuator_armed_s *armed) +arming_state_transition(struct vehicle_status_s *status, /// current vehicle status + const struct safety_s *safety, /// current safety settings + arming_state_t new_arming_state, /// arming state requested + struct actuator_armed_s *armed, /// current armed status + const int mavlink_fd) /// mavlink fd for error reporting, 0 for none { + // Double check that our static arrays are still valid + ASSERT(ARMING_STATE_INIT == 0); + ASSERT(ARMING_STATE_IN_AIR_RESTORE == ARMING_STATE_MAX - 1); + /* * Perform an atomic state update */ @@ -85,7 +119,6 @@ arming_state_transition(struct vehicle_status_s *status, const struct safety_s * ret = TRANSITION_NOT_CHANGED; } else { - /* enforce lockdown in HIL */ if (status->hil_state == HIL_STATE_ON) { armed->lockdown = true; @@ -94,95 +127,43 @@ arming_state_transition(struct vehicle_status_s *status, const struct safety_s * armed->lockdown = false; } - switch (new_arming_state) { - case ARMING_STATE_INIT: - - /* allow going back from INIT for calibration */ - if (status->arming_state == ARMING_STATE_STANDBY) { - ret = TRANSITION_CHANGED; - armed->armed = false; - armed->ready_to_arm = false; - } - - break; - - case ARMING_STATE_STANDBY: - - /* allow coming from INIT and disarming from ARMED */ - if (status->arming_state == ARMING_STATE_INIT - || status->arming_state == ARMING_STATE_ARMED - || status->hil_state == HIL_STATE_ON) { + // Check that we have a valid state transition + bool valid_transition = arming_transitions[new_arming_state][status->arming_state]; + + if (valid_transition) { + // We have a good transition. Now perform any secondary validation. + if (new_arming_state == ARMING_STATE_ARMED) { + // Fail transition if we need safety switch press + // Allow if coming from in air restore + // Allow if HIL_STATE_ON + if (status->arming_state != ARMING_STATE_IN_AIR_RESTORE && status->hil_state == HIL_STATE_OFF && safety->safety_switch_available && !safety->safety_off) { + if (mavlink_fd) { + mavlink_log_critical(mavlink_fd, "NOT ARMING: Press safety switch first."); + } - /* sensors need to be initialized for STANDBY state */ - if (status->condition_system_sensors_initialized) { - ret = TRANSITION_CHANGED; - armed->armed = false; - armed->ready_to_arm = true; + valid_transition = false; } - } - - break; - - case ARMING_STATE_ARMED: - - /* allow arming from STANDBY and IN-AIR-RESTORE */ - if ((status->arming_state == ARMING_STATE_STANDBY - || status->arming_state == ARMING_STATE_IN_AIR_RESTORE) - && (!safety->safety_switch_available || safety->safety_off || status->hil_state == HIL_STATE_ON)) { /* only allow arming if safety is off */ - ret = TRANSITION_CHANGED; - armed->armed = true; - armed->ready_to_arm = true; - } - - break; - - case ARMING_STATE_ARMED_ERROR: - - /* an armed error happens when ARMED obviously */ - if (status->arming_state == ARMING_STATE_ARMED) { - ret = TRANSITION_CHANGED; - armed->armed = true; - armed->ready_to_arm = false; - } - - break; - - case ARMING_STATE_STANDBY_ERROR: - - /* a disarmed error happens when in STANDBY or in INIT or after ARMED_ERROR */ - if (status->arming_state == ARMING_STATE_STANDBY - || status->arming_state == ARMING_STATE_INIT - || status->arming_state == ARMING_STATE_ARMED_ERROR) { - ret = TRANSITION_CHANGED; - armed->armed = false; - armed->ready_to_arm = false; - } - - break; - case ARMING_STATE_REBOOT: - - /* an armed error happens when ARMED obviously */ - if (status->arming_state == ARMING_STATE_INIT - || status->arming_state == ARMING_STATE_STANDBY - || status->arming_state == ARMING_STATE_STANDBY_ERROR) { - ret = TRANSITION_CHANGED; - armed->armed = false; - armed->ready_to_arm = false; + } else if (new_arming_state == ARMING_STATE_STANDBY && status->arming_state == ARMING_STATE_ARMED_ERROR) { + new_arming_state = ARMING_STATE_STANDBY_ERROR; } + } - break; - - case ARMING_STATE_IN_AIR_RESTORE: - - /* XXX implement */ - break; + // HIL can always go to standby + if (status->hil_state == HIL_STATE_ON && new_arming_state == ARMING_STATE_STANDBY) { + valid_transition = true; + } - default: - break; + /* Sensors need to be initialized for STANDBY state */ + if (new_arming_state == ARMING_STATE_STANDBY && !status->condition_system_sensors_initialized) { + valid_transition = false; } - if (ret == TRANSITION_CHANGED) { + // Finish up the state transition + if (valid_transition) { + armed->armed = new_arming_state == ARMING_STATE_ARMED || new_arming_state == ARMING_STATE_ARMED_ERROR; + armed->ready_to_arm = new_arming_state == ARMING_STATE_ARMED || new_arming_state == ARMING_STATE_STANDBY; + ret = TRANSITION_CHANGED; status->arming_state = new_arming_state; arming_state_changed = true; } @@ -191,8 +172,15 @@ arming_state_transition(struct vehicle_status_s *status, const struct safety_s * /* end of atomic state update */ irqrestore(flags); - if (ret == TRANSITION_DENIED) - warnx("arming transition rejected"); + if (ret == TRANSITION_DENIED) { + static const char *errMsg = "Invalid arming transition from %s to %s"; + + if (mavlink_fd) { + mavlink_log_critical(mavlink_fd, errMsg, state_names[status->arming_state], state_names[new_arming_state]); + } + + warnx(errMsg, state_names[status->arming_state], state_names[new_arming_state]); + } return ret; } @@ -234,7 +222,7 @@ main_state_transition(struct vehicle_status_s *status, main_state_t new_main_sta ret = TRANSITION_CHANGED; break; - case MAIN_STATE_SEATBELT: + case MAIN_STATE_ALTCTL: /* need at minimum altitude estimate */ if (!status->is_rotary_wing || @@ -245,7 +233,7 @@ main_state_transition(struct vehicle_status_s *status, main_state_t new_main_sta break; - case MAIN_STATE_EASY: + case MAIN_STATE_POSCTL: /* need at minimum local position estimate */ if (status->condition_local_position_valid || @@ -339,6 +327,7 @@ int hil_state_transition(hil_state_t new_state, int status_pub, struct vehicle_s /* list directory */ DIR *d; d = opendir("/dev"); + if (d) { struct dirent *direntry; @@ -350,26 +339,32 @@ int hil_state_transition(hil_state_t new_state, int status_pub, struct vehicle_s if (!strncmp("tty", direntry->d_name, 3)) { continue; } + /* skip mtd devices */ if (!strncmp("mtd", direntry->d_name, 3)) { continue; } + /* skip ram devices */ if (!strncmp("ram", direntry->d_name, 3)) { continue; } + /* skip MMC devices */ if (!strncmp("mmc", direntry->d_name, 3)) { continue; } + /* skip mavlink */ if (!strcmp("mavlink", direntry->d_name)) { continue; } + /* skip console */ if (!strcmp("console", direntry->d_name)) { continue; } + /* skip null */ if (!strcmp("null", direntry->d_name)) { continue; diff --git a/src/modules/commander/state_machine_helper.h b/src/modules/commander/state_machine_helper.h index f04879ff9..0ddd4f05a 100644 --- a/src/modules/commander/state_machine_helper.h +++ b/src/modules/commander/state_machine_helper.h @@ -57,7 +57,7 @@ typedef enum { } transition_result_t; transition_result_t arming_state_transition(struct vehicle_status_s *current_state, const struct safety_s *safety, - arming_state_t new_arming_state, struct actuator_armed_s *armed); + arming_state_t new_arming_state, struct actuator_armed_s *armed, const int mavlink_fd = 0); bool is_safe(const struct vehicle_status_s *current_state, const struct safety_s *safety, const struct actuator_armed_s *armed); diff --git a/src/modules/dataman/dataman.c b/src/modules/dataman/dataman.c index fa88dfaff..1a65313e8 100644 --- a/src/modules/dataman/dataman.c +++ b/src/modules/dataman/dataman.c @@ -1,8 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2013 PX4 Development Team. All rights reserved. - * Author: Lorenz Meier - * Jean Cyr + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -35,22 +33,21 @@ /** * @file dataman.c * DATAMANAGER driver. + * + * @author Jean Cyr + * @author Lorenz Meier + * @author Julian Oes + * @author Thomas Gubler */ #include <nuttx/config.h> #include <stdio.h> #include <stdlib.h> -#include <string.h> -#include <unistd.h> #include <fcntl.h> -#include <errno.h> -#include <math.h> -#include <poll.h> -#include <time.h> -#include <sys/ioctl.h> #include <systemlib/systemlib.h> #include <systemlib/err.h> #include <queue.h> +#include <string.h> #include "dataman.h" @@ -66,7 +63,7 @@ __EXPORT ssize_t dm_write(dm_item_t item, unsigned char index, dm_persitence_t __EXPORT int dm_clear(dm_item_t item); __EXPORT int dm_restart(dm_reset_reason restart_type); -/* Types of function calls supported by the worker task */ +/** Types of function calls supported by the worker task */ typedef enum { dm_write_func = 0, dm_read_func, @@ -75,11 +72,12 @@ typedef enum { dm_number_of_funcs } dm_function_t; -/* Work task work item */ +/** Work task work item */ typedef struct { sq_entry_t link; /**< list linkage */ sem_t wait_sem; - dm_function_t func; + unsigned char first; + unsigned char func; ssize_t result; union { struct { @@ -104,6 +102,8 @@ typedef struct { }; } work_q_item_t; +const size_t k_work_item_allocation_chunk_size = 8; + /* Usage statistics */ static unsigned g_func_counts[dm_number_of_funcs]; @@ -175,13 +175,29 @@ create_work_item(void) /* Try to reuse item from free item queue */ lock_queue(&g_free_q); + if ((item = (work_q_item_t *)sq_remfirst(&(g_free_q.q)))) g_free_q.size--; + unlock_queue(&g_free_q); - /* If we there weren't any free items then obtain memory for a new one */ - if (item == NULL) - item = (work_q_item_t *)malloc(sizeof(work_q_item_t)); + /* If we there weren't any free items then obtain memory for a new ones */ + if (item == NULL) { + item = (work_q_item_t *)malloc(k_work_item_allocation_chunk_size * sizeof(work_q_item_t)); + if (item) { + item->first = 1; + lock_queue(&g_free_q); + for (int i = 1; i < k_work_item_allocation_chunk_size; i++) { + (item + i)->first = 0; + sq_addfirst(&(item + i)->link, &(g_free_q.q)); + } + /* Update the queue size and potentially the maximum queue size */ + g_free_q.size += k_work_item_allocation_chunk_size - 1; + if (g_free_q.size > g_free_q.max_size) + g_free_q.max_size = g_free_q.size; + unlock_queue(&g_free_q); + } + } /* If we got one then lock the item*/ if (item) @@ -289,11 +305,11 @@ _write(dm_item_t item, unsigned char index, dm_persitence_t persistence, const v offset = calculate_offset(item, index); /* If item type or index out of range, return error */ - if (offset < 0) + if (offset < 0) return -1; /* Make sure caller has not given us more data than we can handle */ - if (count > DM_MAX_DATA_SIZE) + if (count > DM_MAX_DATA_SIZE) return -1; /* Write out the data, prefixed with length and persistence level */ @@ -339,6 +355,7 @@ _read(dm_item_t item, unsigned char index, void *buf, size_t count) /* Read the prefix and data */ len = -1; + if (lseek(g_task_fd, offset, SEEK_SET) == offset) len = read(g_task_fd, buffer, count + DM_SECTOR_HDR_SIZE); @@ -412,31 +429,31 @@ _clear(dm_item_t item) return result; } -/* Tell the data manager about the type of the last reset */ +/** Tell the data manager about the type of the last reset */ static int _restart(dm_reset_reason reason) { unsigned char buffer[2]; - int offset, result = 0; + int offset = 0, result = 0; /* We need to scan the entire file and invalidate and data that should not persist after the last reset */ /* Loop through all of the data segments and delete those that are not persistent */ - offset = 0; - while (1) { size_t len; /* Get data segment at current offset */ if (lseek(g_task_fd, offset, SEEK_SET) != offset) { - result = -1; + /* must be at eof */ break; } len = read(g_task_fd, buffer, sizeof(buffer)); - if (len == 0) + if (len != sizeof(buffer)) { + /* must be at eof */ break; + } /* check if segment contains data */ if (buffer[0]) { @@ -444,12 +461,12 @@ _restart(dm_reset_reason reason) /* Whether data gets deleted depends on reset type and data segment's persistence setting */ if (reason == DM_INIT_REASON_POWER_ON) { - if (buffer[1] != DM_PERSIST_POWER_ON_RESET) { + if (buffer[1] > DM_PERSIST_POWER_ON_RESET) { clear_entry = 1; } } else { - if ((buffer[1] != DM_PERSIST_POWER_ON_RESET) && (buffer[1] != DM_PERSIST_IN_FLIGHT_RESET)) { + if (buffer[1] > DM_PERSIST_IN_FLIGHT_RESET) { clear_entry = 1; } } @@ -481,7 +498,7 @@ _restart(dm_reset_reason reason) return result; } -/* write to the data manager file */ +/** Write to the data manager file */ __EXPORT ssize_t dm_write(dm_item_t item, unsigned char index, dm_persitence_t persistence, const void *buf, size_t count) { @@ -492,7 +509,7 @@ dm_write(dm_item_t item, unsigned char index, dm_persitence_t persistence, const return -1; /* get a work item and queue up a write request */ - if ((work = create_work_item()) == NULL) + if ((work = create_work_item()) == NULL) return -1; work->func = dm_write_func; @@ -506,7 +523,7 @@ dm_write(dm_item_t item, unsigned char index, dm_persitence_t persistence, const return (ssize_t)enqueue_work_item_and_wait_for_result(work); } -/* Retrieve from the data manager file */ +/** Retrieve from the data manager file */ __EXPORT ssize_t dm_read(dm_item_t item, unsigned char index, void *buf, size_t count) { @@ -597,21 +614,55 @@ task_main(int argc, char *argv[]) sem_init(&g_work_queued_sema, 1, 0); + /* See if the data manage file exists and is a multiple of the sector size */ + g_task_fd = open(k_data_manager_device_path, O_RDONLY | O_BINARY); + if (g_task_fd >= 0) { + /* File exists, check its size */ + int file_size = lseek(g_task_fd, 0, SEEK_END); + if ((file_size % k_sector_size) != 0) { + warnx("Incompatible data manager file %s, resetting it", k_data_manager_device_path); + close(g_task_fd); + unlink(k_data_manager_device_path); + } + else + close(g_task_fd); + } + /* Open or create the data manager file */ g_task_fd = open(k_data_manager_device_path, O_RDWR | O_CREAT | O_BINARY); + if (g_task_fd < 0) { warnx("Could not open data manager file %s", k_data_manager_device_path); sem_post(&g_init_sema); /* Don't want to hang startup */ return -1; } - if (lseek(g_task_fd, max_offset, SEEK_SET) != max_offset) { + + if ((unsigned)lseek(g_task_fd, max_offset, SEEK_SET) != max_offset) { close(g_task_fd); warnx("Could not seek data manager file %s", k_data_manager_device_path); sem_post(&g_init_sema); /* Don't want to hang startup */ return -1; } + fsync(g_task_fd); + /* see if we need to erase any items based on restart type */ + int sys_restart_val; + if (param_get(param_find("SYS_RESTART_TYPE"), &sys_restart_val) == OK) { + if (sys_restart_val == DM_INIT_REASON_POWER_ON) { + warnx("Power on restart"); + _restart(DM_INIT_REASON_POWER_ON); + } + else if (sys_restart_val == DM_INIT_REASON_IN_FLIGHT) { + warnx("In flight restart"); + _restart(DM_INIT_REASON_IN_FLIGHT); + } + else + warnx("Unknown restart"); + } + else + warnx("Unknown restart"); + /* We use two file descriptors, one for the caller context and one for the worker thread */ /* They are actually the same but we need to some way to reject caller request while the */ /* worker thread is shutting down but still processing requests */ @@ -684,8 +735,8 @@ task_main(int argc, char *argv[]) for (;;) { if ((work = (work_q_item_t *)sq_remfirst(&(g_free_q.q))) == NULL) break; - - free(work); + if (work->first) + free(work); } destroy_q(&g_work_q); @@ -703,12 +754,12 @@ start(void) sem_init(&g_init_sema, 1, 0); /* start the worker thread */ - if ((task = task_spawn_cmd("dataman", SCHED_DEFAULT, SCHED_PRIORITY_MAX - 5, 2048, task_main, NULL)) <= 0) { + if ((task = task_spawn_cmd("dataman", SCHED_DEFAULT, SCHED_PRIORITY_MAX - 5, 2000, task_main, NULL)) <= 0) { warn("task start failed"); return -1; } - /* wait for the thread to actuall initialize */ + /* wait for the thread to actually initialize */ sem_wait(&g_init_sema); sem_destroy(&g_init_sema); @@ -767,13 +818,12 @@ dataman_main(int argc, char *argv[]) stop(); else if (!strcmp(argv[1], "status")) status(); - else if (!strcmp(argv[1], "poweronrestart")) - dm_restart(DM_INIT_REASON_POWER_ON); - else if (!strcmp(argv[1], "inflightrestart")) - dm_restart(DM_INIT_REASON_IN_FLIGHT); + else if (!strcmp(argv[1], "poweronrestart")) + dm_restart(DM_INIT_REASON_POWER_ON); + else if (!strcmp(argv[1], "inflightrestart")) + dm_restart(DM_INIT_REASON_IN_FLIGHT); else usage(); exit(1); } - diff --git a/src/modules/dataman/dataman.h b/src/modules/dataman/dataman.h index a70638ccc..1dfb26f73 100644 --- a/src/modules/dataman/dataman.h +++ b/src/modules/dataman/dataman.h @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2013 PX4 Development Team. All rights reserved. + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -46,7 +46,7 @@ extern "C" { #endif - /* Types of items that the data manager can store */ + /** Types of items that the data manager can store */ typedef enum { DM_KEY_SAFE_POINTS = 0, /* Safe points coordinates, safe point 0 is home point */ DM_KEY_FENCE_POINTS, /* Fence vertex coordinates */ @@ -56,7 +56,7 @@ extern "C" { DM_KEY_NUM_KEYS /* Total number of item types defined */ } dm_item_t; - /* The maximum number of instances for each item type */ + /** The maximum number of instances for each item type */ enum { DM_KEY_SAFE_POINTS_MAX = 8, DM_KEY_FENCE_POINTS_MAX = GEOFENCE_MAX_VERTICES, @@ -65,23 +65,24 @@ extern "C" { DM_KEY_WAYPOINTS_ONBOARD_MAX = NUM_MISSIONS_SUPPORTED }; - /* Data persistence levels */ + /** Data persistence levels */ typedef enum { DM_PERSIST_POWER_ON_RESET = 0, /* Data survives all resets */ DM_PERSIST_IN_FLIGHT_RESET, /* Data survives in-flight resets only */ DM_PERSIST_VOLATILE /* Data does not survive resets */ } dm_persitence_t; - /* The reason for the last reset */ + /** The reason for the last reset */ typedef enum { DM_INIT_REASON_POWER_ON = 0, /* Data survives resets */ - DM_INIT_REASON_IN_FLIGHT /* Data survives in-flight resets only */ + DM_INIT_REASON_IN_FLIGHT, /* Data survives in-flight resets only */ + DM_INIT_REASON_VOLATILE /* Data does not survive reset */ } dm_reset_reason; - /* Maximum size in bytes of a single item instance */ - #define DM_MAX_DATA_SIZE 126 + /** Maximum size in bytes of a single item instance */ + #define DM_MAX_DATA_SIZE 124 - /* Retrieve from the data manager store */ + /** Retrieve from the data manager store */ __EXPORT ssize_t dm_read( dm_item_t item, /* The item type to retrieve */ @@ -90,7 +91,7 @@ extern "C" { size_t buflen /* Length in bytes of data to retrieve */ ); - /* write to the data manager store */ + /** write to the data manager store */ __EXPORT ssize_t dm_write( dm_item_t item, /* The item type to store */ @@ -100,13 +101,13 @@ extern "C" { size_t buflen /* Length in bytes of data to retrieve */ ); - /* Retrieve from the data manager store */ + /** Erase all items of this type */ __EXPORT int dm_clear( dm_item_t item /* The item type to clear */ ); - /* Tell the data manager about the type of the last reset */ + /** Tell the data manager about the type of the last reset */ __EXPORT int dm_restart( dm_reset_reason restart_type /* The last reset type */ diff --git a/src/modules/dataman/module.mk b/src/modules/dataman/module.mk index dce7a6235..234607b3d 100644 --- a/src/modules/dataman/module.mk +++ b/src/modules/dataman/module.mk @@ -39,4 +39,4 @@ MODULE_COMMAND = dataman SRCS = dataman.c -INCLUDE_DIRS += $(MAVLINK_SRC)/include/mavlink +MODULE_STACKSIZE = 1200 diff --git a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp new file mode 100644 index 000000000..7a71894ed --- /dev/null +++ b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp @@ -0,0 +1,1523 @@ +/**************************************************************************** + * + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file ekf_att_pos_estimator_main.cpp + * Implementation of the attitude and position estimator. + * + * @author Paul Riseborough <p_riseborough@live.com.au> + * @author Lorenz Meier <lm@inf.ethz.ch> + */ + +#include <nuttx/config.h> +#include <stdio.h> +#include <stdlib.h> +#include <string.h> +#include <unistd.h> +#include <fcntl.h> +#include <errno.h> +#include <math.h> +#include <poll.h> +#include <time.h> +#include <drivers/drv_hrt.h> + +#define SENSOR_COMBINED_SUB + + +#include <drivers/drv_gyro.h> +#include <drivers/drv_accel.h> +#include <drivers/drv_mag.h> +#include <drivers/drv_baro.h> +#ifdef SENSOR_COMBINED_SUB +#include <uORB/topics/sensor_combined.h> +#endif +#include <arch/board/board.h> +#include <uORB/uORB.h> +#include <uORB/topics/airspeed.h> +#include <uORB/topics/vehicle_global_position.h> +#include <uORB/topics/vehicle_local_position.h> +#include <uORB/topics/vehicle_gps_position.h> +#include <uORB/topics/vehicle_attitude.h> +#include <uORB/topics/actuator_controls.h> +#include <uORB/topics/vehicle_status.h> +#include <uORB/topics/parameter_update.h> +#include <uORB/topics/estimator_status.h> +#include <uORB/topics/actuator_armed.h> +#include <uORB/topics/home_position.h> +#include <systemlib/param/param.h> +#include <systemlib/err.h> +#include <geo/geo.h> +#include <systemlib/perf_counter.h> +#include <systemlib/systemlib.h> +#include <mathlib/mathlib.h> +#include <mavlink/mavlink_log.h> + +#include "estimator.h" + + + +/** + * estimator app start / stop handling function + * + * @ingroup apps + */ +extern "C" __EXPORT int ekf_att_pos_estimator_main(int argc, char *argv[]); + +__EXPORT uint32_t millis(); + +static uint64_t last_run = 0; +static uint64_t IMUmsec = 0; +static const uint64_t FILTER_INIT_DELAY = 1 * 1000 * 1000; + +uint32_t millis() +{ + return IMUmsec; +} + +class FixedwingEstimator +{ +public: + /** + * Constructor + */ + FixedwingEstimator(); + + /** + * Destructor, also kills the sensors task. + */ + ~FixedwingEstimator(); + + /** + * Start the sensors task. + * + * @return OK on success. + */ + int start(); + + /** + * Print the current status. + */ + void print_status(); + + /** + * Trip the filter by feeding it NaN values. + */ + int trip_nan(); + +private: + + bool _task_should_exit; /**< if true, sensor task should exit */ + int _estimator_task; /**< task handle for sensor task */ +#ifndef SENSOR_COMBINED_SUB + int _gyro_sub; /**< gyro sensor subscription */ + int _accel_sub; /**< accel sensor subscription */ + int _mag_sub; /**< mag sensor subscription */ +#else + int _sensor_combined_sub; +#endif + int _airspeed_sub; /**< airspeed subscription */ + int _baro_sub; /**< barometer subscription */ + int _gps_sub; /**< GPS subscription */ + int _vstatus_sub; /**< vehicle status subscription */ + int _params_sub; /**< notification of parameter updates */ + int _manual_control_sub; /**< notification of manual control updates */ + int _mission_sub; + int _home_sub; /**< home position as defined by commander / user */ + + orb_advert_t _att_pub; /**< vehicle attitude */ + orb_advert_t _global_pos_pub; /**< global position */ + orb_advert_t _local_pos_pub; /**< position in local frame */ + orb_advert_t _estimator_status_pub; /**< status of the estimator */ + + struct vehicle_attitude_s _att; /**< vehicle attitude */ + struct gyro_report _gyro; + struct accel_report _accel; + struct mag_report _mag; + struct airspeed_s _airspeed; /**< airspeed */ + struct baro_report _baro; /**< baro readings */ + struct vehicle_status_s _vstatus; /**< vehicle status */ + struct vehicle_global_position_s _global_pos; /**< global vehicle position */ + struct vehicle_local_position_s _local_pos; /**< local vehicle position */ + struct vehicle_gps_position_s _gps; /**< GPS position */ + + struct gyro_scale _gyro_offsets; + struct accel_scale _accel_offsets; + struct mag_scale _mag_offsets; + +#ifdef SENSOR_COMBINED_SUB + struct sensor_combined_s _sensor_combined; +#endif + + struct map_projection_reference_s _pos_ref; + + float _baro_ref; /**< barometer reference altitude */ + float _baro_gps_offset; /**< offset between GPS and baro */ + + perf_counter_t _loop_perf; /**< loop performance counter */ + perf_counter_t _perf_gyro; ///<local performance counter for gyro updates + perf_counter_t _perf_accel; ///<local performance counter for accel updates + perf_counter_t _perf_mag; ///<local performance counter for mag updates + perf_counter_t _perf_gps; ///<local performance counter for gps updates + perf_counter_t _perf_baro; ///<local performance counter for baro updates + perf_counter_t _perf_airspeed; ///<local performance counter for airspeed updates + + bool _initialized; + bool _baro_init; + bool _gps_initialized; + uint64_t _gps_start_time; + uint64_t _filter_start_time; + bool _gyro_valid; + bool _accel_valid; + bool _mag_valid; + + int _mavlink_fd; + + struct { + int32_t vel_delay_ms; + int32_t pos_delay_ms; + int32_t height_delay_ms; + int32_t mag_delay_ms; + int32_t tas_delay_ms; + float velne_noise; + float veld_noise; + float posne_noise; + float posd_noise; + float mag_noise; + float gyro_pnoise; + float acc_pnoise; + float gbias_pnoise; + float abias_pnoise; + float mage_pnoise; + float magb_pnoise; + float eas_noise; + float pos_stddev_threshold; + } _parameters; /**< local copies of interesting parameters */ + + struct { + param_t vel_delay_ms; + param_t pos_delay_ms; + param_t height_delay_ms; + param_t mag_delay_ms; + param_t tas_delay_ms; + param_t velne_noise; + param_t veld_noise; + param_t posne_noise; + param_t posd_noise; + param_t mag_noise; + param_t gyro_pnoise; + param_t acc_pnoise; + param_t gbias_pnoise; + param_t abias_pnoise; + param_t mage_pnoise; + param_t magb_pnoise; + param_t eas_noise; + param_t pos_stddev_threshold; + } _parameter_handles; /**< handles for interesting parameters */ + + AttPosEKF *_ekf; + + /** + * Update our local parameter cache. + */ + int parameters_update(); + + /** + * Update control outputs + * + */ + void control_update(); + + /** + * Check for changes in vehicle status. + */ + void vehicle_status_poll(); + + /** + * Shim for calling task_main from task_create. + */ + static void task_main_trampoline(int argc, char *argv[]); + + /** + * Main sensor collection task. + */ + void task_main(); +}; + +namespace estimator +{ + +/* oddly, ERROR is not defined for c++ */ +#ifdef ERROR +# undef ERROR +#endif +static const int ERROR = -1; + +FixedwingEstimator *g_estimator; +} + +FixedwingEstimator::FixedwingEstimator() : + + _task_should_exit(false), + _estimator_task(-1), + +/* subscriptions */ +#ifndef SENSOR_COMBINED_SUB + _gyro_sub(-1), + _accel_sub(-1), + _mag_sub(-1), +#else + _sensor_combined_sub(-1), +#endif + _airspeed_sub(-1), + _baro_sub(-1), + _gps_sub(-1), + _vstatus_sub(-1), + _params_sub(-1), + _manual_control_sub(-1), + _mission_sub(-1), + _home_sub(-1), + +/* publications */ + _att_pub(-1), + _global_pos_pub(-1), + _local_pos_pub(-1), + _estimator_status_pub(-1), + + _att({}), + _gyro({}), + _accel({}), + _mag({}), + _airspeed({}), + _baro({}), + _vstatus({}), + _global_pos({}), + _local_pos({}), + _gps({}), + + _gyro_offsets({}), + _accel_offsets({}), + _mag_offsets({}), + + #ifdef SENSOR_COMBINED_SUB + _sensor_combined({}), + #endif + + _baro_ref(0.0f), + _baro_gps_offset(0.0f), + +/* performance counters */ + _loop_perf(perf_alloc(PC_COUNT, "ekf_att_pos_estimator")), + _perf_gyro(perf_alloc(PC_COUNT, "ekf_att_pos_gyro_upd")), + _perf_accel(perf_alloc(PC_COUNT, "ekf_att_pos_accel_upd")), + _perf_mag(perf_alloc(PC_COUNT, "ekf_att_pos_mag_upd")), + _perf_gps(perf_alloc(PC_COUNT, "ekf_att_pos_gps_upd")), + _perf_baro(perf_alloc(PC_COUNT, "ekf_att_pos_baro_upd")), + _perf_airspeed(perf_alloc(PC_COUNT, "ekf_att_pos_aspd_upd")), + +/* states */ + _initialized(false), + _baro_init(false), + _gps_initialized(false), + _gyro_valid(false), + _accel_valid(false), + _mag_valid(false), + _mavlink_fd(-1), + _ekf(nullptr) +{ + + last_run = hrt_absolute_time(); + + _parameter_handles.vel_delay_ms = param_find("PE_VEL_DELAY_MS"); + _parameter_handles.pos_delay_ms = param_find("PE_POS_DELAY_MS"); + _parameter_handles.height_delay_ms = param_find("PE_HGT_DELAY_MS"); + _parameter_handles.mag_delay_ms = param_find("PE_MAG_DELAY_MS"); + _parameter_handles.tas_delay_ms = param_find("PE_TAS_DELAY_MS"); + _parameter_handles.velne_noise = param_find("PE_VELNE_NOISE"); + _parameter_handles.veld_noise = param_find("PE_VELD_NOISE"); + _parameter_handles.posne_noise = param_find("PE_POSNE_NOISE"); + _parameter_handles.posd_noise = param_find("PE_POSD_NOISE"); + _parameter_handles.mag_noise = param_find("PE_MAG_NOISE"); + _parameter_handles.gyro_pnoise = param_find("PE_GYRO_PNOISE"); + _parameter_handles.acc_pnoise = param_find("PE_ACC_PNOISE"); + _parameter_handles.gbias_pnoise = param_find("PE_GBIAS_PNOISE"); + _parameter_handles.abias_pnoise = param_find("PE_ABIAS_PNOISE"); + _parameter_handles.mage_pnoise = param_find("PE_MAGE_PNOISE"); + _parameter_handles.magb_pnoise = param_find("PE_MAGB_PNOISE"); + _parameter_handles.eas_noise = param_find("PE_EAS_NOISE"); + _parameter_handles.pos_stddev_threshold = param_find("PE_POSDEV_INIT"); + + /* fetch initial parameter values */ + parameters_update(); + + /* get offsets */ + + int fd, res; + + fd = open(GYRO_DEVICE_PATH, O_RDONLY); + + if (fd > 0) { + res = ioctl(fd, GYROIOCGSCALE, (long unsigned int)&_gyro_offsets); + close(fd); + + if (res) { + warnx("G SCALE FAIL"); + } + } + + fd = open(ACCEL_DEVICE_PATH, O_RDONLY); + + if (fd > 0) { + res = ioctl(fd, ACCELIOCGSCALE, (long unsigned int)&_accel_offsets); + close(fd); + + if (res) { + warnx("A SCALE FAIL"); + } + } + + fd = open(MAG_DEVICE_PATH, O_RDONLY); + + if (fd > 0) { + res = ioctl(fd, MAGIOCGSCALE, (long unsigned int)&_mag_offsets); + close(fd); + + if (res) { + warnx("M SCALE FAIL"); + } + } +} + +FixedwingEstimator::~FixedwingEstimator() +{ + if (_estimator_task != -1) { + + /* task wakes up every 100ms or so at the longest */ + _task_should_exit = true; + + /* wait for a second for the task to quit at our request */ + unsigned i = 0; + + do { + /* wait 20ms */ + usleep(20000); + + /* if we have given up, kill it */ + if (++i > 50) { + task_delete(_estimator_task); + break; + } + } while (_estimator_task != -1); + } + + estimator::g_estimator = nullptr; +} + +int +FixedwingEstimator::parameters_update() +{ + + param_get(_parameter_handles.vel_delay_ms, &(_parameters.vel_delay_ms)); + param_get(_parameter_handles.pos_delay_ms, &(_parameters.pos_delay_ms)); + param_get(_parameter_handles.height_delay_ms, &(_parameters.height_delay_ms)); + param_get(_parameter_handles.mag_delay_ms, &(_parameters.mag_delay_ms)); + param_get(_parameter_handles.tas_delay_ms, &(_parameters.tas_delay_ms)); + param_get(_parameter_handles.velne_noise, &(_parameters.velne_noise)); + param_get(_parameter_handles.veld_noise, &(_parameters.veld_noise)); + param_get(_parameter_handles.posne_noise, &(_parameters.posne_noise)); + param_get(_parameter_handles.posd_noise, &(_parameters.posd_noise)); + param_get(_parameter_handles.mag_noise, &(_parameters.mag_noise)); + param_get(_parameter_handles.gyro_pnoise, &(_parameters.gyro_pnoise)); + param_get(_parameter_handles.acc_pnoise, &(_parameters.acc_pnoise)); + param_get(_parameter_handles.gbias_pnoise, &(_parameters.gbias_pnoise)); + param_get(_parameter_handles.abias_pnoise, &(_parameters.abias_pnoise)); + param_get(_parameter_handles.mage_pnoise, &(_parameters.mage_pnoise)); + param_get(_parameter_handles.magb_pnoise, &(_parameters.magb_pnoise)); + param_get(_parameter_handles.eas_noise, &(_parameters.eas_noise)); + param_get(_parameter_handles.pos_stddev_threshold, &(_parameters.pos_stddev_threshold)); + + if (_ekf) { + // _ekf->yawVarScale = 1.0f; + // _ekf->windVelSigma = 0.1f; + _ekf->dAngBiasSigma = _parameters.gbias_pnoise; + _ekf->dVelBiasSigma = _parameters.abias_pnoise; + _ekf->magEarthSigma = _parameters.mage_pnoise; + _ekf->magBodySigma = _parameters.magb_pnoise; + // _ekf->gndHgtSigma = 0.02f; + _ekf->vneSigma = _parameters.velne_noise; + _ekf->vdSigma = _parameters.veld_noise; + _ekf->posNeSigma = _parameters.posne_noise; + _ekf->posDSigma = _parameters.posd_noise; + _ekf->magMeasurementSigma = _parameters.mag_noise; + _ekf->gyroProcessNoise = _parameters.gyro_pnoise; + _ekf->accelProcessNoise = _parameters.acc_pnoise; + _ekf->airspeedMeasurementSigma = _parameters.eas_noise; + } + + return OK; +} + +void +FixedwingEstimator::vehicle_status_poll() +{ + bool vstatus_updated; + + /* Check HIL state if vehicle status has changed */ + orb_check(_vstatus_sub, &vstatus_updated); + + if (vstatus_updated) { + + orb_copy(ORB_ID(vehicle_status), _vstatus_sub, &_vstatus); + } +} + +void +FixedwingEstimator::task_main_trampoline(int argc, char *argv[]) +{ + estimator::g_estimator->task_main(); +} + +void +FixedwingEstimator::task_main() +{ + _mavlink_fd = open(MAVLINK_LOG_DEVICE, 0); + + _ekf = new AttPosEKF(); + float dt = 0.0f; // time lapsed since last covariance prediction + _filter_start_time = hrt_absolute_time(); + + if (!_ekf) { + errx(1, "failed allocating EKF filter - out of RAM!"); + } + + /* + * do subscriptions + */ + _baro_sub = orb_subscribe(ORB_ID(sensor_baro)); + _airspeed_sub = orb_subscribe(ORB_ID(airspeed)); + _gps_sub = orb_subscribe(ORB_ID(vehicle_gps_position)); + _vstatus_sub = orb_subscribe(ORB_ID(vehicle_status)); + _params_sub = orb_subscribe(ORB_ID(parameter_update)); + _home_sub = orb_subscribe(ORB_ID(home_position)); + + /* rate limit vehicle status updates to 5Hz */ + orb_set_interval(_vstatus_sub, 200); + +#ifndef SENSOR_COMBINED_SUB + + _gyro_sub = orb_subscribe(ORB_ID(sensor_gyro)); + _accel_sub = orb_subscribe(ORB_ID(sensor_accel)); + _mag_sub = orb_subscribe(ORB_ID(sensor_mag)); + + /* rate limit gyro updates to 50 Hz */ + /* XXX remove this!, BUT increase the data buffer size! */ + orb_set_interval(_gyro_sub, 4); +#else + _sensor_combined_sub = orb_subscribe(ORB_ID(sensor_combined)); + /* XXX remove this!, BUT increase the data buffer size! */ + orb_set_interval(_sensor_combined_sub, 4); +#endif + + /* sets also parameters in the EKF object */ + parameters_update(); + + Vector3f lastAngRate = {0.0f, 0.0f, 0.0f}; + Vector3f lastAccel = {0.0f, 0.0f, 0.0f}; + + /* wakeup source(s) */ + struct pollfd fds[2]; + + /* Setup of loop */ + fds[0].fd = _params_sub; + fds[0].events = POLLIN; +#ifndef SENSOR_COMBINED_SUB + fds[1].fd = _gyro_sub; + fds[1].events = POLLIN; +#else + fds[1].fd = _sensor_combined_sub; + fds[1].events = POLLIN; +#endif + + bool newDataGps = false; + bool newHgtData = false; + bool newAdsData = false; + bool newDataMag = false; + + while (!_task_should_exit) { + + /* wait for up to 500ms for data */ + int pret = poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 100); + + /* timed out - periodic check for _task_should_exit, etc. */ + if (pret == 0) + continue; + + /* this is undesirable but not much we can do - might want to flag unhappy status */ + if (pret < 0) { + warn("poll error %d, %d", pret, errno); + continue; + } + + perf_begin(_loop_perf); + + /* only update parameters if they changed */ + if (fds[0].revents & POLLIN) { + /* read from param to clear updated flag */ + struct parameter_update_s update; + orb_copy(ORB_ID(parameter_update), _params_sub, &update); + + /* update parameters from storage */ + parameters_update(); + } + + /* only run estimator if gyro updated */ + if (fds[1].revents & POLLIN) { + + /* check vehicle status for changes to publication state */ + bool prev_hil = (_vstatus.hil_state == HIL_STATE_ON); + vehicle_status_poll(); + + bool accel_updated; + bool mag_updated; + + hrt_abstime last_sensor_timestamp; + + perf_count(_perf_gyro); + + /* Reset baro reference if switching to HIL, reset sensor states */ + if (!prev_hil && (_vstatus.hil_state == HIL_STATE_ON)) { + /* system is in HIL now, wait for measurements to come in one last round */ + usleep(60000); + +#ifndef SENSOR_COMBINED_SUB + orb_copy(ORB_ID(sensor_gyro), _gyro_sub, &_gyro); + orb_copy(ORB_ID(sensor_accel), _accel_sub, &_accel); + orb_copy(ORB_ID(sensor_mag), _mag_sub, &_mag); +#else + /* now read all sensor publications to ensure all real sensor data is purged */ + orb_copy(ORB_ID(sensor_combined), _sensor_combined_sub, &_sensor_combined); +#endif + + /* set sensors to de-initialized state */ + _gyro_valid = false; + _accel_valid = false; + _mag_valid = false; + + _baro_init = false; + _gps_initialized = false; + last_sensor_timestamp = hrt_absolute_time(); + last_run = last_sensor_timestamp; + + _ekf->ZeroVariables(); + _ekf->dtIMU = 0.01f; + _filter_start_time = last_sensor_timestamp; + + /* now skip this loop and get data on the next one, which will also re-init the filter */ + continue; + } + + /** + * PART ONE: COLLECT ALL DATA + **/ + + /* load local copies */ +#ifndef SENSOR_COMBINED_SUB + orb_copy(ORB_ID(sensor_gyro), _gyro_sub, &_gyro); + + + orb_check(_accel_sub, &accel_updated); + + if (accel_updated) { + perf_count(_perf_accel); + orb_copy(ORB_ID(sensor_accel), _accel_sub, &_accel); + } + + last_sensor_timestamp = _gyro.timestamp; + IMUmsec = _gyro.timestamp / 1e3f; + + float deltaT = (_gyro.timestamp - last_run) / 1e6f; + last_run = _gyro.timestamp; + + /* guard against too large deltaT's */ + if (!isfinite(deltaT) || deltaT > 1.0f || deltaT < 0.000001f) { + deltaT = 0.01f; + } + + + // Always store data, independent of init status + /* fill in last data set */ + _ekf->dtIMU = deltaT; + + if (isfinite(_gyro.x) && + isfinite(_gyro.y) && + isfinite(_gyro.z)) { + _ekf->angRate.x = _gyro.x; + _ekf->angRate.y = _gyro.y; + _ekf->angRate.z = _gyro.z; + + if (!_gyro_valid) { + lastAngRate = _ekf->angRate; + } + + _gyro_valid = true; + } + + if (accel_updated) { + _ekf->accel.x = _accel.x; + _ekf->accel.y = _accel.y; + _ekf->accel.z = _accel.z; + + if (!_accel_valid) { + lastAccel = _ekf->accel; + } + + _accel_valid = true; + } + + _ekf->dAngIMU = 0.5f * (angRate + lastAngRate) * dtIMU; + _ekf->lastAngRate = angRate; + _ekf->dVelIMU = 0.5f * (accel + lastAccel) * dtIMU; + _ekf->lastAccel = accel; + + +#else + orb_copy(ORB_ID(sensor_combined), _sensor_combined_sub, &_sensor_combined); + + static hrt_abstime last_accel = 0; + static hrt_abstime last_mag = 0; + + if (last_accel != _sensor_combined.accelerometer_timestamp) { + accel_updated = true; + } else { + accel_updated = false; + } + + last_accel = _sensor_combined.accelerometer_timestamp; + + + // Copy gyro and accel + last_sensor_timestamp = _sensor_combined.timestamp; + IMUmsec = _sensor_combined.timestamp / 1e3f; + + float deltaT = (_sensor_combined.timestamp - last_run) / 1e6f; + + /* guard against too large deltaT's */ + if (!isfinite(deltaT) || deltaT > 1.0f || deltaT < 0.000001f) { + deltaT = 0.01f; + } + + last_run = _sensor_combined.timestamp; + + // Always store data, independent of init status + /* fill in last data set */ + _ekf->dtIMU = deltaT; + + if (isfinite(_sensor_combined.gyro_rad_s[0]) && + isfinite(_sensor_combined.gyro_rad_s[1]) && + isfinite(_sensor_combined.gyro_rad_s[2])) { + _ekf->angRate.x = _sensor_combined.gyro_rad_s[0]; + _ekf->angRate.y = _sensor_combined.gyro_rad_s[1]; + _ekf->angRate.z = _sensor_combined.gyro_rad_s[2]; + + if (!_gyro_valid) { + lastAngRate = _ekf->angRate; + } + + _gyro_valid = true; + } + + if (accel_updated) { + _ekf->accel.x = _sensor_combined.accelerometer_m_s2[0]; + _ekf->accel.y = _sensor_combined.accelerometer_m_s2[1]; + _ekf->accel.z = _sensor_combined.accelerometer_m_s2[2]; + + if (!_accel_valid) { + lastAccel = _ekf->accel; + } + + _accel_valid = true; + } + + _ekf->dAngIMU = 0.5f * (_ekf->angRate + lastAngRate) * _ekf->dtIMU; + lastAngRate = _ekf->angRate; + _ekf->dVelIMU = 0.5f * (_ekf->accel + lastAccel) * _ekf->dtIMU; + lastAccel = _ekf->accel; + + if (last_mag != _sensor_combined.magnetometer_timestamp) { + mag_updated = true; + newDataMag = true; + + } else { + newDataMag = false; + } + + last_mag = _sensor_combined.magnetometer_timestamp; + +#endif + + bool airspeed_updated; + orb_check(_airspeed_sub, &airspeed_updated); + + if (airspeed_updated) { + orb_copy(ORB_ID(airspeed), _airspeed_sub, &_airspeed); + perf_count(_perf_airspeed); + + _ekf->VtasMeas = _airspeed.true_airspeed_m_s; + newAdsData = true; + + } else { + newAdsData = false; + } + + bool gps_updated; + orb_check(_gps_sub, &gps_updated); + + if (gps_updated) { + + uint64_t last_gps = _gps.timestamp_position; + + orb_copy(ORB_ID(vehicle_gps_position), _gps_sub, &_gps); + perf_count(_perf_gps); + + if (_gps.fix_type < 3) { + newDataGps = false; + + } else { + + /* store time of valid GPS measurement */ + _gps_start_time = hrt_absolute_time(); + + /* check if we had a GPS outage for a long time */ + if (hrt_elapsed_time(&last_gps) > 5 * 1000 * 1000) { + _ekf->ResetPosition(); + _ekf->ResetVelocity(); + _ekf->ResetStoredStates(); + } + + /* fuse GPS updates */ + + //_gps.timestamp / 1e3; + _ekf->GPSstatus = _gps.fix_type; + _ekf->velNED[0] = _gps.vel_n_m_s; + _ekf->velNED[1] = _gps.vel_e_m_s; + _ekf->velNED[2] = _gps.vel_d_m_s; + + // warnx("GPS updated: status: %d, vel: %8.4f %8.4f %8.4f", (int)GPSstatus, velNED[0], velNED[1], velNED[2]); + + _ekf->gpsLat = math::radians(_gps.lat / (double)1e7); + _ekf->gpsLon = math::radians(_gps.lon / (double)1e7) - M_PI; + _ekf->gpsHgt = _gps.alt / 1e3f; + + // if (_gps.s_variance_m_s > 0.25f && _gps.s_variance_m_s < 100.0f * 100.0f) { + // _ekf->vneSigma = sqrtf(_gps.s_variance_m_s); + // } else { + // _ekf->vneSigma = _parameters.velne_noise; + // } + + // if (_gps.p_variance_m > 0.25f && _gps.p_variance_m < 100.0f * 100.0f) { + // _ekf->posNeSigma = sqrtf(_gps.p_variance_m); + // } else { + // _ekf->posNeSigma = _parameters.posne_noise; + // } + + // warnx("vel: %8.4f pos: %8.4f", _gps.s_variance_m_s, _gps.p_variance_m); + + newDataGps = true; + + } + + } + + bool baro_updated; + orb_check(_baro_sub, &baro_updated); + + if (baro_updated) { + orb_copy(ORB_ID(sensor_baro), _baro_sub, &_baro); + + _ekf->baroHgt = _baro.altitude; + + if (!_baro_init) { + _baro_ref = _baro.altitude; + _baro_init = true; + warnx("ALT REF INIT"); + } + + newHgtData = true; + } else { + newHgtData = false; + } + +#ifndef SENSOR_COMBINED_SUB + orb_check(_mag_sub, &mag_updated); +#endif + + if (mag_updated) { + + _mag_valid = true; + + perf_count(_perf_mag); + +#ifndef SENSOR_COMBINED_SUB + orb_copy(ORB_ID(sensor_mag), _mag_sub, &_mag); + + // XXX we compensate the offsets upfront - should be close to zero. + // 0.001f + _ekf->magData.x = _mag.x; + _ekf->magBias.x = 0.000001f; // _mag_offsets.x_offset + + _ekf->magData.y = _mag.y; + _ekf->magBias.y = 0.000001f; // _mag_offsets.y_offset + + _ekf->magData.z = _mag.z; + _ekf->magBias.z = 0.000001f; // _mag_offsets.y_offset + +#else + + // XXX we compensate the offsets upfront - should be close to zero. + // 0.001f + _ekf->magData.x = _sensor_combined.magnetometer_ga[0]; + _ekf->magBias.x = 0.000001f; // _mag_offsets.x_offset + + _ekf->magData.y = _sensor_combined.magnetometer_ga[1]; + _ekf->magBias.y = 0.000001f; // _mag_offsets.y_offset + + _ekf->magData.z = _sensor_combined.magnetometer_ga[2]; + _ekf->magBias.z = 0.000001f; // _mag_offsets.y_offset + +#endif + + newDataMag = true; + + } else { + newDataMag = false; + } + + + /** + * CHECK IF THE INPUT DATA IS SANE + */ + int check = _ekf->CheckAndBound(); + + const char* ekfname = "[ekf] "; + + switch (check) { + case 0: + /* all ok */ + break; + case 1: + { + const char* str = "NaN in states, resetting"; + warnx("%s", str); + mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str); + break; + } + case 2: + { + const char* str = "stale IMU data, resetting"; + warnx("%s", str); + mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str); + break; + } + case 3: + { + const char* str = "switching to dynamic state"; + warnx("%s", str); + mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); + break; + } + + default: + { + const char* str = "unknown reset condition"; + warnx("%s", str); + mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str); + } + } + + // warn on fatal resets + if (check == 1) { + warnx("NUMERIC ERROR IN FILTER"); + } + + // If non-zero, we got a filter reset + if (check) { + + struct ekf_status_report ekf_report; + + _ekf->GetLastErrorState(&ekf_report); + + struct estimator_status_report rep; + memset(&rep, 0, sizeof(rep)); + rep.timestamp = hrt_absolute_time(); + + rep.states_nan = ekf_report.statesNaN; + rep.covariance_nan = ekf_report.covarianceNaN; + rep.kalman_gain_nan = ekf_report.kalmanGainsNaN; + + // Copy all states or at least all that we can fit + unsigned i = 0; + unsigned ekf_n_states = (sizeof(ekf_report.states) / sizeof(ekf_report.states[0])); + unsigned max_states = (sizeof(rep.states) / sizeof(rep.states[0])); + rep.n_states = (ekf_n_states < max_states) ? ekf_n_states : max_states; + + while ((i < ekf_n_states) && (i < max_states)) { + + rep.states[i] = ekf_report.states[i]; + i++; + } + + if (_estimator_status_pub > 0) { + orb_publish(ORB_ID(estimator_status), _estimator_status_pub, &rep); + } else { + _estimator_status_pub = orb_advertise(ORB_ID(estimator_status), &rep); + } + + /* set sensors to de-initialized state */ + _gyro_valid = false; + _accel_valid = false; + _mag_valid = false; + + _baro_init = false; + _gps_initialized = false; + last_sensor_timestamp = hrt_absolute_time(); + last_run = last_sensor_timestamp; + + _ekf->ZeroVariables(); + _ekf->dtIMU = 0.01f; + + // Let the system re-initialize itself + continue; + + } + + + /** + * PART TWO: EXECUTE THE FILTER + **/ + + if ((hrt_elapsed_time(&_filter_start_time) > FILTER_INIT_DELAY) && _baro_init && _gyro_valid && _accel_valid && _mag_valid) { + + float initVelNED[3]; + + if (!_gps_initialized && _gps.fix_type > 2 && _gps.eph_m < _parameters.pos_stddev_threshold && _gps.epv_m < _parameters.pos_stddev_threshold) { + + initVelNED[0] = _gps.vel_n_m_s; + initVelNED[1] = _gps.vel_e_m_s; + initVelNED[2] = _gps.vel_d_m_s; + + // GPS is in scaled integers, convert + double lat = _gps.lat / 1.0e7; + double lon = _gps.lon / 1.0e7; + float gps_alt = _gps.alt / 1e3f; + + // Set up height correctly + orb_copy(ORB_ID(sensor_baro), _baro_sub, &_baro); + _baro_gps_offset = _baro_ref - _baro.altitude; + _ekf->baroHgt = _baro.altitude; + _ekf->hgtMea = 1.0f * (_ekf->baroHgt - (_baro_ref)); + + // Set up position variables correctly + _ekf->GPSstatus = _gps.fix_type; + + _ekf->gpsLat = math::radians(lat); + _ekf->gpsLon = math::radians(lon) - M_PI; + _ekf->gpsHgt = gps_alt; + + // Look up mag declination based on current position + float declination = math::radians(get_mag_declination(lat, lon)); + + _ekf->InitialiseFilter(initVelNED, math::radians(lat), math::radians(lon) - M_PI, gps_alt, declination); + + // Initialize projection + _local_pos.ref_lat = lat; + _local_pos.ref_lon = lon; + _local_pos.ref_alt = gps_alt; + _local_pos.ref_timestamp = _gps.timestamp_position; + + map_projection_init(&_pos_ref, lat, lon); + mavlink_log_info(_mavlink_fd, "[ekf] ref: LA %.4f,LO %.4f,ALT %.2f", lat, lon, (double)gps_alt); + warnx("HOME/REF: LA %8.4f,LO %8.4f,ALT %8.2f V: %8.4f %8.4f %8.4f", lat, lon, (double)gps_alt, + (double)_ekf->velNED[0], (double)_ekf->velNED[1], (double)_ekf->velNED[2]); + warnx("BARO: %8.4f m / ref: %8.4f m / gps offs: %8.4f m", _ekf->baroHgt, _baro_ref, _baro_gps_offset); + warnx("GPS: eph: %8.4f, epv: %8.4f, declination: %8.4f", (double)_gps.eph_m, (double)_gps.epv_m, (double)math::degrees(declination)); + + _gps_initialized = true; + + } else if (!_ekf->statesInitialised) { + + initVelNED[0] = 0.0f; + initVelNED[1] = 0.0f; + initVelNED[2] = 0.0f; + _ekf->posNED[0] = 0.0f; + _ekf->posNED[1] = 0.0f; + _ekf->posNED[2] = 0.0f; + + _ekf->posNE[0] = _ekf->posNED[0]; + _ekf->posNE[1] = _ekf->posNED[1]; + + _local_pos.ref_alt = _baro_ref; + _baro_gps_offset = 0.0f; + + _ekf->InitialiseFilter(initVelNED, 0.0, 0.0, 0.0f, 0.0f); + } + } + + // If valid IMU data and states initialised, predict states and covariances + if (_ekf->statesInitialised) { + // Run the strapdown INS equations every IMU update + _ekf->UpdateStrapdownEquationsNED(); +#if 0 + // debug code - could be tunred into a filter mnitoring/watchdog function + float tempQuat[4]; + + for (uint8_t j = 0; j <= 3; j++) tempQuat[j] = states[j]; + + quat2eul(eulerEst, tempQuat); + + for (uint8_t j = 0; j <= 2; j++) eulerDif[j] = eulerEst[j] - ahrsEul[j]; + + if (eulerDif[2] > pi) eulerDif[2] -= 2 * pi; + + if (eulerDif[2] < -pi) eulerDif[2] += 2 * pi; + +#endif + // store the predicted states for subsequent use by measurement fusion + _ekf->StoreStates(IMUmsec); + // Check if on ground - status is used by covariance prediction + _ekf->OnGroundCheck(); + // sum delta angles and time used by covariance prediction + _ekf->summedDelAng = _ekf->summedDelAng + _ekf->correctedDelAng; + _ekf->summedDelVel = _ekf->summedDelVel + _ekf->dVelIMU; + dt += _ekf->dtIMU; + + // perform a covariance prediction if the total delta angle has exceeded the limit + // or the time limit will be exceeded at the next IMU update + if ((dt >= (_ekf->covTimeStepMax - _ekf->dtIMU)) || (_ekf->summedDelAng.length() > _ekf->covDelAngMax)) { + _ekf->CovariancePrediction(dt); + _ekf->summedDelAng.zero(); + _ekf->summedDelVel.zero(); + dt = 0.0f; + } + + _initialized = true; + } + + // Fuse GPS Measurements + if (newDataGps && _gps_initialized) { + // Convert GPS measurements to Pos NE, hgt and Vel NED + _ekf->velNED[0] = _gps.vel_n_m_s; + _ekf->velNED[1] = _gps.vel_e_m_s; + _ekf->velNED[2] = _gps.vel_d_m_s; + _ekf->calcposNED(_ekf->posNED, _ekf->gpsLat, _ekf->gpsLon, _ekf->gpsHgt, _ekf->latRef, _ekf->lonRef, _ekf->hgtRef); + + _ekf->posNE[0] = _ekf->posNED[0]; + _ekf->posNE[1] = _ekf->posNED[1]; + // set fusion flags + _ekf->fuseVelData = true; + _ekf->fusePosData = true; + // recall states stored at time of measurement after adjusting for delays + _ekf->RecallStates(_ekf->statesAtVelTime, (IMUmsec - _parameters.vel_delay_ms)); + _ekf->RecallStates(_ekf->statesAtPosTime, (IMUmsec - _parameters.pos_delay_ms)); + // run the fusion step + _ekf->FuseVelposNED(); + + } else if (_ekf->statesInitialised) { + // Convert GPS measurements to Pos NE, hgt and Vel NED + _ekf->velNED[0] = 0.0f; + _ekf->velNED[1] = 0.0f; + _ekf->velNED[2] = 0.0f; + _ekf->posNED[0] = 0.0f; + _ekf->posNED[1] = 0.0f; + _ekf->posNED[2] = 0.0f; + + _ekf->posNE[0] = _ekf->posNED[0]; + _ekf->posNE[1] = _ekf->posNED[1]; + // set fusion flags + _ekf->fuseVelData = true; + _ekf->fusePosData = true; + // recall states stored at time of measurement after adjusting for delays + _ekf->RecallStates(_ekf->statesAtVelTime, (IMUmsec - _parameters.vel_delay_ms)); + _ekf->RecallStates(_ekf->statesAtPosTime, (IMUmsec - _parameters.pos_delay_ms)); + // run the fusion step + _ekf->FuseVelposNED(); + + } else { + _ekf->fuseVelData = false; + _ekf->fusePosData = false; + } + + if (newHgtData && _ekf->statesInitialised) { + // Could use a blend of GPS and baro alt data if desired + _ekf->hgtMea = 1.0f * (_ekf->baroHgt - _baro_ref); + _ekf->fuseHgtData = true; + // recall states stored at time of measurement after adjusting for delays + _ekf->RecallStates(_ekf->statesAtHgtTime, (IMUmsec - _parameters.height_delay_ms)); + // run the fusion step + _ekf->FuseVelposNED(); + + } else { + _ekf->fuseHgtData = false; + } + + // Fuse Magnetometer Measurements + if (newDataMag && _ekf->statesInitialised) { + _ekf->fuseMagData = true; + _ekf->RecallStates(_ekf->statesAtMagMeasTime, (IMUmsec - _parameters.mag_delay_ms)); // Assume 50 msec avg delay for magnetometer data + + } else { + _ekf->fuseMagData = false; + } + + if (_ekf->statesInitialised) _ekf->FuseMagnetometer(); + + // Fuse Airspeed Measurements + if (newAdsData && _ekf->statesInitialised && _ekf->VtasMeas > 8.0f) { + _ekf->fuseVtasData = true; + _ekf->RecallStates(_ekf->statesAtVtasMeasTime, (IMUmsec - _parameters.tas_delay_ms)); // assume 100 msec avg delay for airspeed data + _ekf->FuseAirspeed(); + + } else { + _ekf->fuseVtasData = false; + } + + // Publish results + if (_initialized && (check == OK)) { + + + + // State vector: + // 0-3: quaternions (q0, q1, q2, q3) + // 4-6: Velocity - m/sec (North, East, Down) + // 7-9: Position - m (North, East, Down) + // 10-12: Delta Angle bias - rad (X,Y,Z) + // 13-14: Wind Vector - m/sec (North,East) + // 15-17: Earth Magnetic Field Vector - milligauss (North, East, Down) + // 18-20: Body Magnetic Field Vector - milligauss (X,Y,Z) + + math::Quaternion q(_ekf->states[0], _ekf->states[1], _ekf->states[2], _ekf->states[3]); + math::Matrix<3, 3> R = q.to_dcm(); + math::Vector<3> euler = R.to_euler(); + + for (int i = 0; i < 3; i++) for (int j = 0; j < 3; j++) + _att.R[i][j] = R(i, j); + + _att.timestamp = last_sensor_timestamp; + _att.q[0] = _ekf->states[0]; + _att.q[1] = _ekf->states[1]; + _att.q[2] = _ekf->states[2]; + _att.q[3] = _ekf->states[3]; + _att.q_valid = true; + _att.R_valid = true; + + _att.timestamp = last_sensor_timestamp; + _att.roll = euler(0); + _att.pitch = euler(1); + _att.yaw = euler(2); + + _att.rollspeed = _ekf->angRate.x - _ekf->states[10]; + _att.pitchspeed = _ekf->angRate.y - _ekf->states[11]; + _att.yawspeed = _ekf->angRate.z - _ekf->states[12]; + // gyro offsets + _att.rate_offsets[0] = _ekf->states[10]; + _att.rate_offsets[1] = _ekf->states[11]; + _att.rate_offsets[2] = _ekf->states[12]; + + /* lazily publish the attitude only once available */ + if (_att_pub > 0) { + /* publish the attitude setpoint */ + orb_publish(ORB_ID(vehicle_attitude), _att_pub, &_att); + + } else { + /* advertise and publish */ + _att_pub = orb_advertise(ORB_ID(vehicle_attitude), &_att); + } + } + + if (_gps_initialized) { + _local_pos.timestamp = last_sensor_timestamp; + _local_pos.x = _ekf->states[7]; + _local_pos.y = _ekf->states[8]; + // XXX need to announce change of Z reference somehow elegantly + _local_pos.z = _ekf->states[9] - _baro_gps_offset; + + _local_pos.vx = _ekf->states[4]; + _local_pos.vy = _ekf->states[5]; + _local_pos.vz = _ekf->states[6]; + + _local_pos.xy_valid = _gps_initialized; + _local_pos.z_valid = true; + _local_pos.v_xy_valid = _gps_initialized; + _local_pos.v_z_valid = true; + _local_pos.xy_global = true; + + _local_pos.z_global = false; + _local_pos.yaw = _att.yaw; + + /* lazily publish the local position only once available */ + if (_local_pos_pub > 0) { + /* publish the attitude setpoint */ + orb_publish(ORB_ID(vehicle_local_position), _local_pos_pub, &_local_pos); + + } else { + /* advertise and publish */ + _local_pos_pub = orb_advertise(ORB_ID(vehicle_local_position), &_local_pos); + } + + _global_pos.timestamp = _local_pos.timestamp; + + if (_local_pos.xy_global) { + double est_lat, est_lon; + map_projection_reproject(&_pos_ref, _local_pos.x, _local_pos.y, &est_lat, &est_lon); + _global_pos.lat = est_lat; + _global_pos.lon = est_lon; + _global_pos.time_gps_usec = _gps.time_gps_usec; + _global_pos.eph = _gps.eph_m; + _global_pos.epv = _gps.epv_m; + } + + if (_local_pos.v_xy_valid) { + _global_pos.vel_n = _local_pos.vx; + _global_pos.vel_e = _local_pos.vy; + } else { + _global_pos.vel_n = 0.0f; + _global_pos.vel_e = 0.0f; + } + + /* local pos alt is negative, change sign and add alt offsets */ + _global_pos.alt = _local_pos.ref_alt + _baro_gps_offset + (-_local_pos.z); + + if (_local_pos.v_z_valid) { + _global_pos.vel_d = _local_pos.vz; + } + + _global_pos.yaw = _local_pos.yaw; + + _global_pos.eph = _gps.eph_m; + _global_pos.epv = _gps.epv_m; + + _global_pos.timestamp = _local_pos.timestamp; + + /* lazily publish the global position only once available */ + if (_global_pos_pub > 0) { + /* publish the attitude setpoint */ + orb_publish(ORB_ID(vehicle_global_position), _global_pos_pub, &_global_pos); + + } else { + /* advertise and publish */ + _global_pos_pub = orb_advertise(ORB_ID(vehicle_global_position), &_global_pos); + } + } + + } + + perf_end(_loop_perf); + } + + warnx("exiting.\n"); + + _estimator_task = -1; + _exit(0); +} + +int +FixedwingEstimator::start() +{ + ASSERT(_estimator_task == -1); + + /* start the task */ + _estimator_task = task_spawn_cmd("ekf_att_pos_estimator", + SCHED_DEFAULT, + SCHED_PRIORITY_MAX - 40, + 6000, + (main_t)&FixedwingEstimator::task_main_trampoline, + nullptr); + + if (_estimator_task < 0) { + warn("task start failed"); + return -errno; + } + + return OK; +} + +void +FixedwingEstimator::print_status() +{ + math::Quaternion q(_ekf->states[0], _ekf->states[1], _ekf->states[2], _ekf->states[3]); + math::Matrix<3, 3> R = q.to_dcm(); + math::Vector<3> euler = R.to_euler(); + + printf("attitude: roll: %8.4f, pitch %8.4f, yaw: %8.4f degrees\n", + (double)math::degrees(euler(0)), (double)math::degrees(euler(1)), (double)math::degrees(euler(2))); + + // State vector: + // 0-3: quaternions (q0, q1, q2, q3) + // 4-6: Velocity - m/sec (North, East, Down) + // 7-9: Position - m (North, East, Down) + // 10-12: Delta Angle bias - rad (X,Y,Z) + // 13-14: Wind Vector - m/sec (North,East) + // 15-17: Earth Magnetic Field Vector - gauss (North, East, Down) + // 18-20: Body Magnetic Field Vector - gauss (X,Y,Z) + + printf("dtIMU: %8.6f IMUmsec: %d\n", (double)_ekf->dtIMU, (int)IMUmsec); + printf("ref alt: %8.6f\n", (double)_local_pos.ref_alt); + printf("dvel: %8.6f %8.6f %8.6f accel: %8.6f %8.6f %8.6f\n", (double)_ekf->dVelIMU.x, (double)_ekf->dVelIMU.y, (double)_ekf->dVelIMU.z, (double)_ekf->accel.x, (double)_ekf->accel.y, (double)_ekf->accel.z); + printf("dang: %8.4f %8.4f %8.4f dang corr: %8.4f %8.4f %8.4f\n" , (double)_ekf->dAngIMU.x, (double)_ekf->dAngIMU.y, (double)_ekf->dAngIMU.z, (double)_ekf->correctedDelAng.x, (double)_ekf->correctedDelAng.y, (double)_ekf->correctedDelAng.z); + printf("states (quat) [1-4]: %8.4f, %8.4f, %8.4f, %8.4f\n", (double)_ekf->states[0], (double)_ekf->states[1], (double)_ekf->states[2], (double)_ekf->states[3]); + printf("states (vel m/s) [5-7]: %8.4f, %8.4f, %8.4f\n", (double)_ekf->states[4], (double)_ekf->states[5], (double)_ekf->states[6]); + printf("states (pos m) [8-10]: %8.4f, %8.4f, %8.4f\n", (double)_ekf->states[7], (double)_ekf->states[8], (double)_ekf->states[9]); + printf("states (delta ang) [11-13]: %8.4f, %8.4f, %8.4f\n", (double)_ekf->states[10], (double)_ekf->states[11], (double)_ekf->states[12]); + printf("states (wind) [14-15]: %8.4f, %8.4f\n", (double)_ekf->states[13], (double)_ekf->states[14]); + printf("states (earth mag) [16-18]: %8.4f, %8.4f, %8.4f\n", (double)_ekf->states[15], (double)_ekf->states[16], (double)_ekf->states[17]); + printf("states (body mag) [19-21]: %8.4f, %8.4f, %8.4f\n", (double)_ekf->states[18], (double)_ekf->states[19], (double)_ekf->states[20]); + printf("states: %s %s %s %s %s %s %s %s %s %s\n", + (_ekf->statesInitialised) ? "INITIALIZED" : "NON_INIT", + (_ekf->onGround) ? "ON_GROUND" : "AIRBORNE", + (_ekf->fuseVelData) ? "FUSE_VEL" : "INH_VEL", + (_ekf->fusePosData) ? "FUSE_POS" : "INH_POS", + (_ekf->fuseHgtData) ? "FUSE_HGT" : "INH_HGT", + (_ekf->fuseMagData) ? "FUSE_MAG" : "INH_MAG", + (_ekf->fuseVtasData) ? "FUSE_VTAS" : "INH_VTAS", + (_ekf->useAirspeed) ? "USE_AIRSPD" : "IGN_AIRSPD", + (_ekf->useCompass) ? "USE_COMPASS" : "IGN_COMPASS", + (_ekf->staticMode) ? "STATIC_MODE" : "DYNAMIC_MODE"); +} + +int FixedwingEstimator::trip_nan() { + + int ret = 0; + + // If system is not armed, inject a NaN value into the filter + int armed_sub = orb_subscribe(ORB_ID(actuator_armed)); + + struct actuator_armed_s armed; + orb_copy(ORB_ID(actuator_armed), armed_sub, &armed); + + if (armed.armed) { + warnx("ACTUATORS ARMED! NOT TRIPPING SYSTEM"); + ret = 1; + } else { + + float nan_val = 0.0f / 0.0f; + + warnx("system not armed, tripping state vector with NaN values"); + _ekf->states[5] = nan_val; + usleep(100000); + + warnx("tripping covariance #1 with NaN values"); + _ekf->KH[2][2] = nan_val; // intermediate result used for covariance updates + usleep(100000); + + warnx("tripping covariance #2 with NaN values"); + _ekf->KHP[5][5] = nan_val; // intermediate result used for covariance updates + usleep(100000); + + warnx("tripping covariance #3 with NaN values"); + _ekf->P[3][3] = nan_val; // covariance matrix + usleep(100000); + + warnx("tripping Kalman gains with NaN values"); + _ekf->Kfusion[0] = nan_val; // Kalman gains + usleep(100000); + + warnx("tripping stored states[0] with NaN values"); + _ekf->storedStates[0][0] = nan_val; + usleep(100000); + + warnx("\nDONE - FILTER STATE:"); + print_status(); + } + + close(armed_sub); + return ret; +} + +int ekf_att_pos_estimator_main(int argc, char *argv[]) +{ + if (argc < 1) + errx(1, "usage: ekf_att_pos_estimator {start|stop|status}"); + + if (!strcmp(argv[1], "start")) { + + if (estimator::g_estimator != nullptr) + errx(1, "already running"); + + estimator::g_estimator = new FixedwingEstimator; + + if (estimator::g_estimator == nullptr) + errx(1, "alloc failed"); + + if (OK != estimator::g_estimator->start()) { + delete estimator::g_estimator; + estimator::g_estimator = nullptr; + err(1, "start failed"); + } + + exit(0); + } + + if (!strcmp(argv[1], "stop")) { + if (estimator::g_estimator == nullptr) + errx(1, "not running"); + + delete estimator::g_estimator; + estimator::g_estimator = nullptr; + exit(0); + } + + if (!strcmp(argv[1], "status")) { + if (estimator::g_estimator) { + warnx("running"); + + estimator::g_estimator->print_status(); + + exit(0); + + } else { + errx(1, "not running"); + } + } + + if (!strcmp(argv[1], "trip")) { + if (estimator::g_estimator) { + int ret = estimator::g_estimator->trip_nan(); + + exit(ret); + + } else { + errx(1, "not running"); + } + } + + warnx("unrecognized command"); + return 1; +} diff --git a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_params.c b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_params.c new file mode 100644 index 000000000..1d9ae4623 --- /dev/null +++ b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_params.c @@ -0,0 +1,271 @@ +/**************************************************************************** + * + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file ekf_att_pos_estimator_params.c + * + * Parameters defined by the attitude and position estimator task + * + * @author Lorenz Meier <lm@inf.ethz.ch> + */ + +#include <nuttx/config.h> + +#include <systemlib/param/param.h> + +/* + * Estimator parameters, accessible via MAVLink + * + */ + +/** + * Velocity estimate delay + * + * The delay in milliseconds of the velocity estimate from GPS. + * + * @min 0 + * @max 1000 + * @group Position Estimator + */ +PARAM_DEFINE_INT32(PE_VEL_DELAY_MS, 230); + +/** + * Position estimate delay + * + * The delay in milliseconds of the position estimate from GPS. + * + * @min 0 + * @max 1000 + * @group Position Estimator + */ +PARAM_DEFINE_INT32(PE_POS_DELAY_MS, 210); + +/** + * Height estimate delay + * + * The delay in milliseconds of the height estimate from the barometer. + * + * @min 0 + * @max 1000 + * @group Position Estimator + */ +PARAM_DEFINE_INT32(PE_HGT_DELAY_MS, 350); + +/** + * Mag estimate delay + * + * The delay in milliseconds of the magnetic field estimate from + * the magnetometer. + * + * @min 0 + * @max 1000 + * @group Position Estimator + */ +PARAM_DEFINE_INT32(PE_MAG_DELAY_MS, 30); + +/** + * True airspeeed estimate delay + * + * The delay in milliseconds of the airspeed estimate. + * + * @min 0 + * @max 1000 + * @group Position Estimator + */ +PARAM_DEFINE_INT32(PE_TAS_DELAY_MS, 210); + +/** + * GPS vs. barometric altitude update weight + * + * RE-CHECK this. + * + * @min 0.0 + * @max 1.0 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_GPS_ALT_WGT, 0.9f); + +/** + * Airspeed measurement noise. + * + * Increasing this value will make the filter trust this sensor + * less and trust other sensors more. + * + * @min 0.5 + * @max 5.0 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_EAS_NOISE, 1.4f); + +/** + * Velocity measurement noise in north-east (horizontal) direction. + * + * Generic default: 0.3, multicopters: 0.5, ground vehicles: 0.5 + * + * @min 0.05 + * @max 5.0 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_VELNE_NOISE, 0.3f); + +/** + * Velocity noise in down (vertical) direction + * + * Generic default: 0.5, multicopters: 0.7, ground vehicles: 0.7 + * + * @min 0.05 + * @max 5.0 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_VELD_NOISE, 0.5f); + +/** + * Position noise in north-east (horizontal) direction + * + * Generic defaults: 0.5, multicopters: 0.5, ground vehicles: 0.5 + * + * @min 0.1 + * @max 10.0 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_POSNE_NOISE, 0.5f); + +/** + * Position noise in down (vertical) direction + * + * Generic defaults: 0.5, multicopters: 1.0, ground vehicles: 1.0 + * + * @min 0.1 + * @max 10.0 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_POSD_NOISE, 0.5f); + +/** + * Magnetometer measurement noise + * + * Generic defaults: 0.05, multicopters: 0.05, ground vehicles: 0.05 + * + * @min 0.1 + * @max 10.0 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_MAG_NOISE, 0.05f); + +/** + * Gyro process noise + * + * Generic defaults: 0.015, multicopters: 0.015, ground vehicles: 0.015. + * This noise controls how much the filter trusts the gyro measurements. + * Increasing it makes the filter trust the gyro less and other sensors more. + * + * @min 0.001 + * @max 0.05 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_GYRO_PNOISE, 0.015f); + +/** + * Accelerometer process noise + * + * Generic defaults: 0.25, multicopters: 0.25, ground vehicles: 0.25. + * Increasing this value makes the filter trust the accelerometer less + * and other sensors more. + * + * @min 0.05 + * @max 1.0 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_ACC_PNOISE, 0.25f); + +/** + * Gyro bias estimate process noise + * + * Generic defaults: 1e-07f, multicopters: 1e-07f, ground vehicles: 1e-07f. + * Increasing this value will make the gyro bias converge faster but noisier. + * + * @min 0.0000001 + * @max 0.00001 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_GBIAS_PNOISE, 1e-07f); + +/** + * Accelerometer bias estimate process noise + * + * Generic defaults: 0.0001f, multicopters: 0.0001f, ground vehicles: 0.0001f. + * Increasing this value makes the bias estimation faster and noisier. + * + * @min 0.0001 + * @max 0.001 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_ABIAS_PNOISE, 0.0001f); + +/** + * Magnetometer earth frame offsets process noise + * + * Generic defaults: 0.0001, multicopters: 0.0001, ground vehicles: 0.0001. + * Increasing this value makes the magnetometer earth bias estimate converge + * faster but also noisier. + * + * @min 0.0001 + * @max 0.01 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_MAGE_PNOISE, 0.0003f); + +/** + * Magnetometer body frame offsets process noise + * + * Generic defaults: 0.0003, multicopters: 0.0003, ground vehicles: 0.0003. + * Increasing this value makes the magnetometer body bias estimate converge faster + * but also noisier. + * + * @min 0.0001 + * @max 0.01 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_MAGB_PNOISE, 0.0003f); + +/** + * Threshold for filter initialization. + * + * If the standard deviation of the GPS position estimate is below this threshold + * in meters, the filter will initialize. + * + * @min 0.3 + * @max 10.0 + * @group Position Estimator + */ +PARAM_DEFINE_FLOAT(PE_POSDEV_INIT, 5.0f); diff --git a/src/modules/ekf_att_pos_estimator/estimator.cpp b/src/modules/ekf_att_pos_estimator/estimator.cpp new file mode 100644 index 000000000..23ecd89ac --- /dev/null +++ b/src/modules/ekf_att_pos_estimator/estimator.cpp @@ -0,0 +1,2609 @@ +#include "estimator.h" +#include <string.h> +#include <stdarg.h> + +// Define EKF_DEBUG here to enable the debug print calls +// if the macro is not set, these will be completely +// optimized out by the compiler. +#define EKF_DEBUG + +#ifdef EKF_DEBUG +#include <stdio.h> + +static void +ekf_debug_print(const char *fmt, va_list args) +{ + fprintf(stderr, "%s: ", "[ekf]"); + vfprintf(stderr, fmt, args); + + fprintf(stderr, "\n"); +} + +static void +ekf_debug(const char *fmt, ...) +{ + va_list args; + + va_start(args, fmt); + ekf_debug_print(fmt, args); +} + +#else + +static void ekf_debug(const char *fmt, ...) { while(0){} } +#endif + +float Vector3f::length(void) const +{ + return sqrt(x*x + y*y + z*z); +} + +void Vector3f::zero(void) +{ + x = 0.0f; + y = 0.0f; + z = 0.0f; +} + +Mat3f::Mat3f() { + identity(); +} + +void Mat3f::identity() { + x.x = 1.0f; + x.y = 0.0f; + x.z = 0.0f; + + y.x = 0.0f; + y.y = 1.0f; + y.z = 0.0f; + + z.x = 0.0f; + z.y = 0.0f; + z.z = 1.0f; +} + +Mat3f Mat3f::transpose(void) const +{ + Mat3f ret = *this; + swap_var(ret.x.y, ret.y.x); + swap_var(ret.x.z, ret.z.x); + swap_var(ret.y.z, ret.z.y); + return ret; +} + +// overload + operator to provide a vector addition +Vector3f operator+( Vector3f vecIn1, Vector3f vecIn2) +{ + Vector3f vecOut; + vecOut.x = vecIn1.x + vecIn2.x; + vecOut.y = vecIn1.y + vecIn2.y; + vecOut.z = vecIn1.z + vecIn2.z; + return vecOut; +} + +// overload - operator to provide a vector subtraction +Vector3f operator-( Vector3f vecIn1, Vector3f vecIn2) +{ + Vector3f vecOut; + vecOut.x = vecIn1.x - vecIn2.x; + vecOut.y = vecIn1.y - vecIn2.y; + vecOut.z = vecIn1.z - vecIn2.z; + return vecOut; +} + +// overload * operator to provide a matrix vector product +Vector3f operator*( Mat3f matIn, Vector3f vecIn) +{ + Vector3f vecOut; + vecOut.x = matIn.x.x*vecIn.x + matIn.x.y*vecIn.y + matIn.x.z*vecIn.z; + vecOut.y = matIn.y.x*vecIn.x + matIn.y.y*vecIn.y + matIn.y.z*vecIn.z; + vecOut.z = matIn.x.x*vecIn.x + matIn.z.y*vecIn.y + matIn.z.z*vecIn.z; + return vecOut; +} + +// overload % operator to provide a vector cross product +Vector3f operator%( Vector3f vecIn1, Vector3f vecIn2) +{ + Vector3f vecOut; + vecOut.x = vecIn1.y*vecIn2.z - vecIn1.z*vecIn2.y; + vecOut.y = vecIn1.z*vecIn2.x - vecIn1.x*vecIn2.z; + vecOut.z = vecIn1.x*vecIn2.y - vecIn1.y*vecIn2.x; + return vecOut; +} + +// overload * operator to provide a vector scaler product +Vector3f operator*(Vector3f vecIn1, float sclIn1) +{ + Vector3f vecOut; + vecOut.x = vecIn1.x * sclIn1; + vecOut.y = vecIn1.y * sclIn1; + vecOut.z = vecIn1.z * sclIn1; + return vecOut; +} + +// overload * operator to provide a vector scaler product +Vector3f operator*(float sclIn1, Vector3f vecIn1) +{ + Vector3f vecOut; + vecOut.x = vecIn1.x * sclIn1; + vecOut.y = vecIn1.y * sclIn1; + vecOut.z = vecIn1.z * sclIn1; + return vecOut; +} + +void swap_var(float &d1, float &d2) +{ + float tmp = d1; + d1 = d2; + d2 = tmp; +} + +AttPosEKF::AttPosEKF() + + /* NOTE: DO NOT initialize class members here. Use ZeroVariables() + * instead to allow clean in-air re-initialization. + */ +{ + + ZeroVariables(); + InitialiseParameters(); +} + +AttPosEKF::~AttPosEKF() +{ +} + +void AttPosEKF::UpdateStrapdownEquationsNED() +{ + Vector3f delVelNav; + float q00; + float q11; + float q22; + float q33; + float q01; + float q02; + float q03; + float q12; + float q13; + float q23; + float rotationMag; + float qUpdated[4]; + float quatMag; + float deltaQuat[4]; + const Vector3f gravityNED = {0.0,0.0,GRAVITY_MSS}; + +// Remove sensor bias errors + correctedDelAng.x = dAngIMU.x - states[10]; + correctedDelAng.y = dAngIMU.y - states[11]; + correctedDelAng.z = dAngIMU.z - states[12]; + dVelIMU.x = dVelIMU.x; + dVelIMU.y = dVelIMU.y; + dVelIMU.z = dVelIMU.z - states[13]; + +// Save current measurements + Vector3f prevDelAng = correctedDelAng; + +// Apply corrections for earths rotation rate and coning errors +// * and + operators have been overloaded + correctedDelAng = correctedDelAng - Tnb*earthRateNED*dtIMU + 8.333333333333333e-2f*(prevDelAng % correctedDelAng); + +// Convert the rotation vector to its equivalent quaternion + rotationMag = correctedDelAng.length(); + if (rotationMag < 1e-12f) + { + deltaQuat[0] = 1.0; + deltaQuat[1] = 0.0; + deltaQuat[2] = 0.0; + deltaQuat[3] = 0.0; + } + else + { + deltaQuat[0] = cosf(0.5f*rotationMag); + float rotScaler = (sinf(0.5f*rotationMag))/rotationMag; + deltaQuat[1] = correctedDelAng.x*rotScaler; + deltaQuat[2] = correctedDelAng.y*rotScaler; + deltaQuat[3] = correctedDelAng.z*rotScaler; + } + +// Update the quaternions by rotating from the previous attitude through +// the delta angle rotation quaternion + qUpdated[0] = states[0]*deltaQuat[0] - states[1]*deltaQuat[1] - states[2]*deltaQuat[2] - states[3]*deltaQuat[3]; + qUpdated[1] = states[0]*deltaQuat[1] + states[1]*deltaQuat[0] + states[2]*deltaQuat[3] - states[3]*deltaQuat[2]; + qUpdated[2] = states[0]*deltaQuat[2] + states[2]*deltaQuat[0] + states[3]*deltaQuat[1] - states[1]*deltaQuat[3]; + qUpdated[3] = states[0]*deltaQuat[3] + states[3]*deltaQuat[0] + states[1]*deltaQuat[2] - states[2]*deltaQuat[1]; + +// Normalise the quaternions and update the quaternion states + quatMag = sqrtf(sq(qUpdated[0]) + sq(qUpdated[1]) + sq(qUpdated[2]) + sq(qUpdated[3])); + if (quatMag > 1e-16f) + { + float quatMagInv = 1.0f/quatMag; + states[0] = quatMagInv*qUpdated[0]; + states[1] = quatMagInv*qUpdated[1]; + states[2] = quatMagInv*qUpdated[2]; + states[3] = quatMagInv*qUpdated[3]; + } + +// Calculate the body to nav cosine matrix + q00 = sq(states[0]); + q11 = sq(states[1]); + q22 = sq(states[2]); + q33 = sq(states[3]); + q01 = states[0]*states[1]; + q02 = states[0]*states[2]; + q03 = states[0]*states[3]; + q12 = states[1]*states[2]; + q13 = states[1]*states[3]; + q23 = states[2]*states[3]; + + Tbn.x.x = q00 + q11 - q22 - q33; + Tbn.y.y = q00 - q11 + q22 - q33; + Tbn.z.z = q00 - q11 - q22 + q33; + Tbn.x.y = 2*(q12 - q03); + Tbn.x.z = 2*(q13 + q02); + Tbn.y.x = 2*(q12 + q03); + Tbn.y.z = 2*(q23 - q01); + Tbn.z.x = 2*(q13 - q02); + Tbn.z.y = 2*(q23 + q01); + + Tnb = Tbn.transpose(); + +// transform body delta velocities to delta velocities in the nav frame +// * and + operators have been overloaded + //delVelNav = Tbn*dVelIMU + gravityNED*dtIMU; + delVelNav.x = Tbn.x.x*dVelIMU.x + Tbn.x.y*dVelIMU.y + Tbn.x.z*dVelIMU.z + gravityNED.x*dtIMU; + delVelNav.y = Tbn.y.x*dVelIMU.x + Tbn.y.y*dVelIMU.y + Tbn.y.z*dVelIMU.z + gravityNED.y*dtIMU; + delVelNav.z = Tbn.z.x*dVelIMU.x + Tbn.z.y*dVelIMU.y + Tbn.z.z*dVelIMU.z + gravityNED.z*dtIMU; + +// calculate the magnitude of the nav acceleration (required for GPS +// variance estimation) + accNavMag = delVelNav.length()/dtIMU; + +// If calculating position save previous velocity + float lastVelocity[3]; + lastVelocity[0] = states[4]; + lastVelocity[1] = states[5]; + lastVelocity[2] = states[6]; + +// Sum delta velocities to get velocity + states[4] = states[4] + delVelNav.x; + states[5] = states[5] + delVelNav.y; + states[6] = states[6] + delVelNav.z; + +// If calculating postions, do a trapezoidal integration for position + states[7] = states[7] + 0.5f*(states[4] + lastVelocity[0])*dtIMU; + states[8] = states[8] + 0.5f*(states[5] + lastVelocity[1])*dtIMU; + states[9] = states[9] + 0.5f*(states[6] + lastVelocity[2])*dtIMU; + + // Constrain states (to protect against filter divergence) + ConstrainStates(); +} + +void AttPosEKF::CovariancePrediction(float dt) +{ + // scalars + float daxCov; + float dayCov; + float dazCov; + float dvxCov; + float dvyCov; + float dvzCov; + float dvx; + float dvy; + float dvz; + float dax; + float day; + float daz; + float q0; + float q1; + float q2; + float q3; + float dax_b; + float day_b; + float daz_b; + float dvz_b; + + // arrays + float processNoise[n_states]; + float SF[15]; + float SG[8]; + float SQ[11]; + float SPP[8] = {0}; + float nextP[n_states][n_states]; + + // calculate covariance prediction process noise + for (uint8_t i= 0; i<=9; i++) processNoise[i] = 1.0e-9f; + for (uint8_t i=10; i<=12; i++) processNoise[i] = dt * dAngBiasSigma; + // scale gyro bias noise when on ground to allow for faster bias estimation + for (uint8_t i=10; i<=12; i++) processNoise[i] = dt * dAngBiasSigma; + processNoise[13] = dVelBiasSigma; + for (uint8_t i=14; i<=15; i++) processNoise[i] = dt * windVelSigma; + for (uint8_t i=16; i<=18; i++) processNoise[i] = dt * magEarthSigma; + for (uint8_t i=19; i<=21; i++) processNoise[i] = dt * magBodySigma; + processNoise[22] = dt * sqrtf(sq(states[4]) + sq(states[5])) * gndHgtSigma; + + // square all sigmas + for (unsigned i = 0; i < n_states; i++) processNoise[i] = sq(processNoise[i]); + + // set variables used to calculate covariance growth + dvx = summedDelVel.x; + dvy = summedDelVel.y; + dvz = summedDelVel.z; + dax = summedDelAng.x; + day = summedDelAng.y; + daz = summedDelAng.z; + q0 = states[0]; + q1 = states[1]; + q2 = states[2]; + q3 = states[3]; + dax_b = states[10]; + day_b = states[11]; + daz_b = states[12]; + dvz_b = states[13]; + gyroProcessNoise = ConstrainFloat(gyroProcessNoise, 1e-3f, 5e-2f); + daxCov = sq(dt*gyroProcessNoise); + dayCov = sq(dt*gyroProcessNoise); + dazCov = sq(dt*gyroProcessNoise); + if (onGround) dazCov = dazCov * sq(yawVarScale); + accelProcessNoise = ConstrainFloat(accelProcessNoise, 5e-2, 1.0f); + dvxCov = sq(dt*accelProcessNoise); + dvyCov = sq(dt*accelProcessNoise); + dvzCov = sq(dt*accelProcessNoise); + + // Predicted covariance calculation + SF[0] = dvz - dvz_b; + SF[1] = 2*q3*SF[0] + 2*dvx*q1 + 2*dvy*q2; + SF[2] = 2*dvx*q3 - 2*q1*SF[0] + 2*dvy*q0; + SF[3] = 2*q2*SF[0] + 2*dvx*q0 - 2*dvy*q3; + SF[4] = day/2 - day_b/2; + SF[5] = daz/2 - daz_b/2; + SF[6] = dax/2 - dax_b/2; + SF[7] = dax_b/2 - dax/2; + SF[8] = daz_b/2 - daz/2; + SF[9] = day_b/2 - day/2; + SF[10] = 2*q0*SF[0]; + SF[11] = q1/2; + SF[12] = q2/2; + SF[13] = q3/2; + SF[14] = 2*dvy*q1; + + SG[0] = q0/2; + SG[1] = sq(q3); + SG[2] = sq(q2); + SG[3] = sq(q1); + SG[4] = sq(q0); + SG[5] = 2*q2*q3; + SG[6] = 2*q1*q3; + SG[7] = 2*q1*q2; + + SQ[0] = dvzCov*(SG[5] - 2*q0*q1)*(SG[1] - SG[2] - SG[3] + SG[4]) - dvyCov*(SG[5] + 2*q0*q1)*(SG[1] - SG[2] + SG[3] - SG[4]) + dvxCov*(SG[6] - 2*q0*q2)*(SG[7] + 2*q0*q3); + SQ[1] = dvzCov*(SG[6] + 2*q0*q2)*(SG[1] - SG[2] - SG[3] + SG[4]) - dvxCov*(SG[6] - 2*q0*q2)*(SG[1] + SG[2] - SG[3] - SG[4]) + dvyCov*(SG[5] + 2*q0*q1)*(SG[7] - 2*q0*q3); + SQ[2] = dvzCov*(SG[5] - 2*q0*q1)*(SG[6] + 2*q0*q2) - dvyCov*(SG[7] - 2*q0*q3)*(SG[1] - SG[2] + SG[3] - SG[4]) - dvxCov*(SG[7] + 2*q0*q3)*(SG[1] + SG[2] - SG[3] - SG[4]); + SQ[3] = (dayCov*q1*SG[0])/2 - (dazCov*q1*SG[0])/2 - (daxCov*q2*q3)/4; + SQ[4] = (dazCov*q2*SG[0])/2 - (daxCov*q2*SG[0])/2 - (dayCov*q1*q3)/4; + SQ[5] = (daxCov*q3*SG[0])/2 - (dayCov*q3*SG[0])/2 - (dazCov*q1*q2)/4; + SQ[6] = (daxCov*q1*q2)/4 - (dazCov*q3*SG[0])/2 - (dayCov*q1*q2)/4; + SQ[7] = (dazCov*q1*q3)/4 - (daxCov*q1*q3)/4 - (dayCov*q2*SG[0])/2; + SQ[8] = (dayCov*q2*q3)/4 - (daxCov*q1*SG[0])/2 - (dazCov*q2*q3)/4; + SQ[9] = sq(SG[0]); + SQ[10] = sq(q1); + + SPP[0] = SF[10] + SF[14] - 2*dvx*q2; + SPP[1] = 2*q2*SF[0] + 2*dvx*q0 - 2*dvy*q3; + SPP[2] = 2*dvx*q3 - 2*q1*SF[0] + 2*dvy*q0; + SPP[3] = 2*q0*q1 - 2*q2*q3; + SPP[4] = 2*q0*q2 + 2*q1*q3; + SPP[5] = sq(q0) - sq(q1) - sq(q2) + sq(q3); + SPP[6] = SF[13]; + SPP[7] = SF[12]; + + nextP[0][0] = P[0][0] + P[1][0]*SF[7] + P[2][0]*SF[9] + P[3][0]*SF[8] + P[10][0]*SF[11] + P[11][0]*SPP[7] + P[12][0]*SPP[6] + (daxCov*SQ[10])/4 + SF[7]*(P[0][1] + P[1][1]*SF[7] + P[2][1]*SF[9] + P[3][1]*SF[8] + P[10][1]*SF[11] + P[11][1]*SPP[7] + P[12][1]*SPP[6]) + SF[9]*(P[0][2] + P[1][2]*SF[7] + P[2][2]*SF[9] + P[3][2]*SF[8] + P[10][2]*SF[11] + P[11][2]*SPP[7] + P[12][2]*SPP[6]) + SF[8]*(P[0][3] + P[1][3]*SF[7] + P[2][3]*SF[9] + P[3][3]*SF[8] + P[10][3]*SF[11] + P[11][3]*SPP[7] + P[12][3]*SPP[6]) + SF[11]*(P[0][10] + P[1][10]*SF[7] + P[2][10]*SF[9] + P[3][10]*SF[8] + P[10][10]*SF[11] + P[11][10]*SPP[7] + P[12][10]*SPP[6]) + SPP[7]*(P[0][11] + P[1][11]*SF[7] + P[2][11]*SF[9] + P[3][11]*SF[8] + P[10][11]*SF[11] + P[11][11]*SPP[7] + P[12][11]*SPP[6]) + SPP[6]*(P[0][12] + P[1][12]*SF[7] + P[2][12]*SF[9] + P[3][12]*SF[8] + P[10][12]*SF[11] + P[11][12]*SPP[7] + P[12][12]*SPP[6]) + (dayCov*sq(q2))/4 + (dazCov*sq(q3))/4; + nextP[0][1] = P[0][1] + SQ[8] + P[1][1]*SF[7] + P[2][1]*SF[9] + P[3][1]*SF[8] + P[10][1]*SF[11] + P[11][1]*SPP[7] + P[12][1]*SPP[6] + SF[6]*(P[0][0] + P[1][0]*SF[7] + P[2][0]*SF[9] + P[3][0]*SF[8] + P[10][0]*SF[11] + P[11][0]*SPP[7] + P[12][0]*SPP[6]) + SF[5]*(P[0][2] + P[1][2]*SF[7] + P[2][2]*SF[9] + P[3][2]*SF[8] + P[10][2]*SF[11] + P[11][2]*SPP[7] + P[12][2]*SPP[6]) + SF[9]*(P[0][3] + P[1][3]*SF[7] + P[2][3]*SF[9] + P[3][3]*SF[8] + P[10][3]*SF[11] + P[11][3]*SPP[7] + P[12][3]*SPP[6]) + SPP[6]*(P[0][11] + P[1][11]*SF[7] + P[2][11]*SF[9] + P[3][11]*SF[8] + P[10][11]*SF[11] + P[11][11]*SPP[7] + P[12][11]*SPP[6]) - SPP[7]*(P[0][12] + P[1][12]*SF[7] + P[2][12]*SF[9] + P[3][12]*SF[8] + P[10][12]*SF[11] + P[11][12]*SPP[7] + P[12][12]*SPP[6]) - (q0*(P[0][10] + P[1][10]*SF[7] + P[2][10]*SF[9] + P[3][10]*SF[8] + P[10][10]*SF[11] + P[11][10]*SPP[7] + P[12][10]*SPP[6]))/2; + nextP[0][2] = P[0][2] + SQ[7] + P[1][2]*SF[7] + P[2][2]*SF[9] + P[3][2]*SF[8] + P[10][2]*SF[11] + P[11][2]*SPP[7] + P[12][2]*SPP[6] + SF[4]*(P[0][0] + P[1][0]*SF[7] + P[2][0]*SF[9] + P[3][0]*SF[8] + P[10][0]*SF[11] + P[11][0]*SPP[7] + P[12][0]*SPP[6]) + SF[8]*(P[0][1] + P[1][1]*SF[7] + P[2][1]*SF[9] + P[3][1]*SF[8] + P[10][1]*SF[11] + P[11][1]*SPP[7] + P[12][1]*SPP[6]) + SF[6]*(P[0][3] + P[1][3]*SF[7] + P[2][3]*SF[9] + P[3][3]*SF[8] + P[10][3]*SF[11] + P[11][3]*SPP[7] + P[12][3]*SPP[6]) + SF[11]*(P[0][12] + P[1][12]*SF[7] + P[2][12]*SF[9] + P[3][12]*SF[8] + P[10][12]*SF[11] + P[11][12]*SPP[7] + P[12][12]*SPP[6]) - SPP[6]*(P[0][10] + P[1][10]*SF[7] + P[2][10]*SF[9] + P[3][10]*SF[8] + P[10][10]*SF[11] + P[11][10]*SPP[7] + P[12][10]*SPP[6]) - (q0*(P[0][11] + P[1][11]*SF[7] + P[2][11]*SF[9] + P[3][11]*SF[8] + P[10][11]*SF[11] + P[11][11]*SPP[7] + P[12][11]*SPP[6]))/2; + nextP[0][3] = P[0][3] + SQ[6] + P[1][3]*SF[7] + P[2][3]*SF[9] + P[3][3]*SF[8] + P[10][3]*SF[11] + P[11][3]*SPP[7] + P[12][3]*SPP[6] + SF[5]*(P[0][0] + P[1][0]*SF[7] + P[2][0]*SF[9] + P[3][0]*SF[8] + P[10][0]*SF[11] + P[11][0]*SPP[7] + P[12][0]*SPP[6]) + SF[4]*(P[0][1] + P[1][1]*SF[7] + P[2][1]*SF[9] + P[3][1]*SF[8] + P[10][1]*SF[11] + P[11][1]*SPP[7] + P[12][1]*SPP[6]) + SF[7]*(P[0][2] + P[1][2]*SF[7] + P[2][2]*SF[9] + P[3][2]*SF[8] + P[10][2]*SF[11] + P[11][2]*SPP[7] + P[12][2]*SPP[6]) - SF[11]*(P[0][11] + P[1][11]*SF[7] + P[2][11]*SF[9] + P[3][11]*SF[8] + P[10][11]*SF[11] + P[11][11]*SPP[7] + P[12][11]*SPP[6]) + SPP[7]*(P[0][10] + P[1][10]*SF[7] + P[2][10]*SF[9] + P[3][10]*SF[8] + P[10][10]*SF[11] + P[11][10]*SPP[7] + P[12][10]*SPP[6]) - (q0*(P[0][12] + P[1][12]*SF[7] + P[2][12]*SF[9] + P[3][12]*SF[8] + P[10][12]*SF[11] + P[11][12]*SPP[7] + P[12][12]*SPP[6]))/2; + nextP[0][4] = P[0][4] + P[1][4]*SF[7] + P[2][4]*SF[9] + P[3][4]*SF[8] + P[10][4]*SF[11] + P[11][4]*SPP[7] + P[12][4]*SPP[6] + SF[3]*(P[0][0] + P[1][0]*SF[7] + P[2][0]*SF[9] + P[3][0]*SF[8] + P[10][0]*SF[11] + P[11][0]*SPP[7] + P[12][0]*SPP[6]) + SF[1]*(P[0][1] + P[1][1]*SF[7] + P[2][1]*SF[9] + P[3][1]*SF[8] + P[10][1]*SF[11] + P[11][1]*SPP[7] + P[12][1]*SPP[6]) + SPP[0]*(P[0][2] + P[1][2]*SF[7] + P[2][2]*SF[9] + P[3][2]*SF[8] + P[10][2]*SF[11] + P[11][2]*SPP[7] + P[12][2]*SPP[6]) - SPP[2]*(P[0][3] + P[1][3]*SF[7] + P[2][3]*SF[9] + P[3][3]*SF[8] + P[10][3]*SF[11] + P[11][3]*SPP[7] + P[12][3]*SPP[6]) - SPP[4]*(P[0][13] + P[1][13]*SF[7] + P[2][13]*SF[9] + P[3][13]*SF[8] + P[10][13]*SF[11] + P[11][13]*SPP[7] + P[12][13]*SPP[6]); + nextP[0][5] = P[0][5] + P[1][5]*SF[7] + P[2][5]*SF[9] + P[3][5]*SF[8] + P[10][5]*SF[11] + P[11][5]*SPP[7] + P[12][5]*SPP[6] + SF[2]*(P[0][0] + P[1][0]*SF[7] + P[2][0]*SF[9] + P[3][0]*SF[8] + P[10][0]*SF[11] + P[11][0]*SPP[7] + P[12][0]*SPP[6]) + SF[1]*(P[0][2] + P[1][2]*SF[7] + P[2][2]*SF[9] + P[3][2]*SF[8] + P[10][2]*SF[11] + P[11][2]*SPP[7] + P[12][2]*SPP[6]) + SF[3]*(P[0][3] + P[1][3]*SF[7] + P[2][3]*SF[9] + P[3][3]*SF[8] + P[10][3]*SF[11] + P[11][3]*SPP[7] + P[12][3]*SPP[6]) - SPP[0]*(P[0][1] + P[1][1]*SF[7] + P[2][1]*SF[9] + P[3][1]*SF[8] + P[10][1]*SF[11] + P[11][1]*SPP[7] + P[12][1]*SPP[6]) + SPP[3]*(P[0][13] + P[1][13]*SF[7] + P[2][13]*SF[9] + P[3][13]*SF[8] + P[10][13]*SF[11] + P[11][13]*SPP[7] + P[12][13]*SPP[6]); + nextP[0][6] = P[0][6] + P[1][6]*SF[7] + P[2][6]*SF[9] + P[3][6]*SF[8] + P[10][6]*SF[11] + P[11][6]*SPP[7] + P[12][6]*SPP[6] + SF[2]*(P[0][1] + P[1][1]*SF[7] + P[2][1]*SF[9] + P[3][1]*SF[8] + P[10][1]*SF[11] + P[11][1]*SPP[7] + P[12][1]*SPP[6]) + SF[1]*(P[0][3] + P[1][3]*SF[7] + P[2][3]*SF[9] + P[3][3]*SF[8] + P[10][3]*SF[11] + P[11][3]*SPP[7] + P[12][3]*SPP[6]) + SPP[0]*(P[0][0] + P[1][0]*SF[7] + P[2][0]*SF[9] + P[3][0]*SF[8] + P[10][0]*SF[11] + P[11][0]*SPP[7] + P[12][0]*SPP[6]) - SPP[1]*(P[0][2] + P[1][2]*SF[7] + P[2][2]*SF[9] + P[3][2]*SF[8] + P[10][2]*SF[11] + P[11][2]*SPP[7] + P[12][2]*SPP[6]) - (sq(q0) - sq(q1) - sq(q2) + sq(q3))*(P[0][13] + P[1][13]*SF[7] + P[2][13]*SF[9] + P[3][13]*SF[8] + P[10][13]*SF[11] + P[11][13]*SPP[7] + P[12][13]*SPP[6]); + nextP[0][7] = P[0][7] + P[1][7]*SF[7] + P[2][7]*SF[9] + P[3][7]*SF[8] + P[10][7]*SF[11] + P[11][7]*SPP[7] + P[12][7]*SPP[6] + dt*(P[0][4] + P[1][4]*SF[7] + P[2][4]*SF[9] + P[3][4]*SF[8] + P[10][4]*SF[11] + P[11][4]*SPP[7] + P[12][4]*SPP[6]); + nextP[0][8] = P[0][8] + P[1][8]*SF[7] + P[2][8]*SF[9] + P[3][8]*SF[8] + P[10][8]*SF[11] + P[11][8]*SPP[7] + P[12][8]*SPP[6] + dt*(P[0][5] + P[1][5]*SF[7] + P[2][5]*SF[9] + P[3][5]*SF[8] + P[10][5]*SF[11] + P[11][5]*SPP[7] + P[12][5]*SPP[6]); + nextP[0][9] = P[0][9] + P[1][9]*SF[7] + P[2][9]*SF[9] + P[3][9]*SF[8] + P[10][9]*SF[11] + P[11][9]*SPP[7] + P[12][9]*SPP[6] + dt*(P[0][6] + P[1][6]*SF[7] + P[2][6]*SF[9] + P[3][6]*SF[8] + P[10][6]*SF[11] + P[11][6]*SPP[7] + P[12][6]*SPP[6]); + nextP[0][10] = P[0][10] + P[1][10]*SF[7] + P[2][10]*SF[9] + P[3][10]*SF[8] + P[10][10]*SF[11] + P[11][10]*SPP[7] + P[12][10]*SPP[6]; + nextP[0][11] = P[0][11] + P[1][11]*SF[7] + P[2][11]*SF[9] + P[3][11]*SF[8] + P[10][11]*SF[11] + P[11][11]*SPP[7] + P[12][11]*SPP[6]; + nextP[0][12] = P[0][12] + P[1][12]*SF[7] + P[2][12]*SF[9] + P[3][12]*SF[8] + P[10][12]*SF[11] + P[11][12]*SPP[7] + P[12][12]*SPP[6]; + nextP[0][13] = P[0][13] + P[1][13]*SF[7] + P[2][13]*SF[9] + P[3][13]*SF[8] + P[10][13]*SF[11] + P[11][13]*SPP[7] + P[12][13]*SPP[6]; + nextP[0][14] = P[0][14] + P[1][14]*SF[7] + P[2][14]*SF[9] + P[3][14]*SF[8] + P[10][14]*SF[11] + P[11][14]*SPP[7] + P[12][14]*SPP[6]; + nextP[0][15] = P[0][15] + P[1][15]*SF[7] + P[2][15]*SF[9] + P[3][15]*SF[8] + P[10][15]*SF[11] + P[11][15]*SPP[7] + P[12][15]*SPP[6]; + nextP[0][16] = P[0][16] + P[1][16]*SF[7] + P[2][16]*SF[9] + P[3][16]*SF[8] + P[10][16]*SF[11] + P[11][16]*SPP[7] + P[12][16]*SPP[6]; + nextP[0][17] = P[0][17] + P[1][17]*SF[7] + P[2][17]*SF[9] + P[3][17]*SF[8] + P[10][17]*SF[11] + P[11][17]*SPP[7] + P[12][17]*SPP[6]; + nextP[0][18] = P[0][18] + P[1][18]*SF[7] + P[2][18]*SF[9] + P[3][18]*SF[8] + P[10][18]*SF[11] + P[11][18]*SPP[7] + P[12][18]*SPP[6]; + nextP[0][19] = P[0][19] + P[1][19]*SF[7] + P[2][19]*SF[9] + P[3][19]*SF[8] + P[10][19]*SF[11] + P[11][19]*SPP[7] + P[12][19]*SPP[6]; + nextP[0][20] = P[0][20] + P[1][20]*SF[7] + P[2][20]*SF[9] + P[3][20]*SF[8] + P[10][20]*SF[11] + P[11][20]*SPP[7] + P[12][20]*SPP[6]; + nextP[0][21] = P[0][21] + P[1][21]*SF[7] + P[2][21]*SF[9] + P[3][21]*SF[8] + P[10][21]*SF[11] + P[11][21]*SPP[7] + P[12][21]*SPP[6]; + nextP[0][22] = P[0][22] + P[1][22]*SF[7] + P[2][22]*SF[9] + P[3][22]*SF[8] + P[10][22]*SF[11] + P[11][22]*SPP[7] + P[12][22]*SPP[6]; + nextP[1][0] = P[1][0] + SQ[8] + P[0][0]*SF[6] + P[2][0]*SF[5] + P[3][0]*SF[9] + P[11][0]*SPP[6] - P[12][0]*SPP[7] - (P[10][0]*q0)/2 + SF[7]*(P[1][1] + P[0][1]*SF[6] + P[2][1]*SF[5] + P[3][1]*SF[9] + P[11][1]*SPP[6] - P[12][1]*SPP[7] - (P[10][1]*q0)/2) + SF[9]*(P[1][2] + P[0][2]*SF[6] + P[2][2]*SF[5] + P[3][2]*SF[9] + P[11][2]*SPP[6] - P[12][2]*SPP[7] - (P[10][2]*q0)/2) + SF[8]*(P[1][3] + P[0][3]*SF[6] + P[2][3]*SF[5] + P[3][3]*SF[9] + P[11][3]*SPP[6] - P[12][3]*SPP[7] - (P[10][3]*q0)/2) + SF[11]*(P[1][10] + P[0][10]*SF[6] + P[2][10]*SF[5] + P[3][10]*SF[9] + P[11][10]*SPP[6] - P[12][10]*SPP[7] - (P[10][10]*q0)/2) + SPP[7]*(P[1][11] + P[0][11]*SF[6] + P[2][11]*SF[5] + P[3][11]*SF[9] + P[11][11]*SPP[6] - P[12][11]*SPP[7] - (P[10][11]*q0)/2) + SPP[6]*(P[1][12] + P[0][12]*SF[6] + P[2][12]*SF[5] + P[3][12]*SF[9] + P[11][12]*SPP[6] - P[12][12]*SPP[7] - (P[10][12]*q0)/2); + nextP[1][1] = P[1][1] + P[0][1]*SF[6] + P[2][1]*SF[5] + P[3][1]*SF[9] + P[11][1]*SPP[6] - P[12][1]*SPP[7] + daxCov*SQ[9] - (P[10][1]*q0)/2 + SF[6]*(P[1][0] + P[0][0]*SF[6] + P[2][0]*SF[5] + P[3][0]*SF[9] + P[11][0]*SPP[6] - P[12][0]*SPP[7] - (P[10][0]*q0)/2) + SF[5]*(P[1][2] + P[0][2]*SF[6] + P[2][2]*SF[5] + P[3][2]*SF[9] + P[11][2]*SPP[6] - P[12][2]*SPP[7] - (P[10][2]*q0)/2) + SF[9]*(P[1][3] + P[0][3]*SF[6] + P[2][3]*SF[5] + P[3][3]*SF[9] + P[11][3]*SPP[6] - P[12][3]*SPP[7] - (P[10][3]*q0)/2) + SPP[6]*(P[1][11] + P[0][11]*SF[6] + P[2][11]*SF[5] + P[3][11]*SF[9] + P[11][11]*SPP[6] - P[12][11]*SPP[7] - (P[10][11]*q0)/2) - SPP[7]*(P[1][12] + P[0][12]*SF[6] + P[2][12]*SF[5] + P[3][12]*SF[9] + P[11][12]*SPP[6] - P[12][12]*SPP[7] - (P[10][12]*q0)/2) + (dayCov*sq(q3))/4 + (dazCov*sq(q2))/4 - (q0*(P[1][10] + P[0][10]*SF[6] + P[2][10]*SF[5] + P[3][10]*SF[9] + P[11][10]*SPP[6] - P[12][10]*SPP[7] - (P[10][10]*q0)/2))/2; + nextP[1][2] = P[1][2] + SQ[5] + P[0][2]*SF[6] + P[2][2]*SF[5] + P[3][2]*SF[9] + P[11][2]*SPP[6] - P[12][2]*SPP[7] - (P[10][2]*q0)/2 + SF[4]*(P[1][0] + P[0][0]*SF[6] + P[2][0]*SF[5] + P[3][0]*SF[9] + P[11][0]*SPP[6] - P[12][0]*SPP[7] - (P[10][0]*q0)/2) + SF[8]*(P[1][1] + P[0][1]*SF[6] + P[2][1]*SF[5] + P[3][1]*SF[9] + P[11][1]*SPP[6] - P[12][1]*SPP[7] - (P[10][1]*q0)/2) + SF[6]*(P[1][3] + P[0][3]*SF[6] + P[2][3]*SF[5] + P[3][3]*SF[9] + P[11][3]*SPP[6] - P[12][3]*SPP[7] - (P[10][3]*q0)/2) + SF[11]*(P[1][12] + P[0][12]*SF[6] + P[2][12]*SF[5] + P[3][12]*SF[9] + P[11][12]*SPP[6] - P[12][12]*SPP[7] - (P[10][12]*q0)/2) - SPP[6]*(P[1][10] + P[0][10]*SF[6] + P[2][10]*SF[5] + P[3][10]*SF[9] + P[11][10]*SPP[6] - P[12][10]*SPP[7] - (P[10][10]*q0)/2) - (q0*(P[1][11] + P[0][11]*SF[6] + P[2][11]*SF[5] + P[3][11]*SF[9] + P[11][11]*SPP[6] - P[12][11]*SPP[7] - (P[10][11]*q0)/2))/2; + nextP[1][3] = P[1][3] + SQ[4] + P[0][3]*SF[6] + P[2][3]*SF[5] + P[3][3]*SF[9] + P[11][3]*SPP[6] - P[12][3]*SPP[7] - (P[10][3]*q0)/2 + SF[5]*(P[1][0] + P[0][0]*SF[6] + P[2][0]*SF[5] + P[3][0]*SF[9] + P[11][0]*SPP[6] - P[12][0]*SPP[7] - (P[10][0]*q0)/2) + SF[4]*(P[1][1] + P[0][1]*SF[6] + P[2][1]*SF[5] + P[3][1]*SF[9] + P[11][1]*SPP[6] - P[12][1]*SPP[7] - (P[10][1]*q0)/2) + SF[7]*(P[1][2] + P[0][2]*SF[6] + P[2][2]*SF[5] + P[3][2]*SF[9] + P[11][2]*SPP[6] - P[12][2]*SPP[7] - (P[10][2]*q0)/2) - SF[11]*(P[1][11] + P[0][11]*SF[6] + P[2][11]*SF[5] + P[3][11]*SF[9] + P[11][11]*SPP[6] - P[12][11]*SPP[7] - (P[10][11]*q0)/2) + SPP[7]*(P[1][10] + P[0][10]*SF[6] + P[2][10]*SF[5] + P[3][10]*SF[9] + P[11][10]*SPP[6] - P[12][10]*SPP[7] - (P[10][10]*q0)/2) - (q0*(P[1][12] + P[0][12]*SF[6] + P[2][12]*SF[5] + P[3][12]*SF[9] + P[11][12]*SPP[6] - P[12][12]*SPP[7] - (P[10][12]*q0)/2))/2; + nextP[1][4] = P[1][4] + P[0][4]*SF[6] + P[2][4]*SF[5] + P[3][4]*SF[9] + P[11][4]*SPP[6] - P[12][4]*SPP[7] - (P[10][4]*q0)/2 + SF[3]*(P[1][0] + P[0][0]*SF[6] + P[2][0]*SF[5] + P[3][0]*SF[9] + P[11][0]*SPP[6] - P[12][0]*SPP[7] - (P[10][0]*q0)/2) + SF[1]*(P[1][1] + P[0][1]*SF[6] + P[2][1]*SF[5] + P[3][1]*SF[9] + P[11][1]*SPP[6] - P[12][1]*SPP[7] - (P[10][1]*q0)/2) + SPP[0]*(P[1][2] + P[0][2]*SF[6] + P[2][2]*SF[5] + P[3][2]*SF[9] + P[11][2]*SPP[6] - P[12][2]*SPP[7] - (P[10][2]*q0)/2) - SPP[2]*(P[1][3] + P[0][3]*SF[6] + P[2][3]*SF[5] + P[3][3]*SF[9] + P[11][3]*SPP[6] - P[12][3]*SPP[7] - (P[10][3]*q0)/2) - SPP[4]*(P[1][13] + P[0][13]*SF[6] + P[2][13]*SF[5] + P[3][13]*SF[9] + P[11][13]*SPP[6] - P[12][13]*SPP[7] - (P[10][13]*q0)/2); + nextP[1][5] = P[1][5] + P[0][5]*SF[6] + P[2][5]*SF[5] + P[3][5]*SF[9] + P[11][5]*SPP[6] - P[12][5]*SPP[7] - (P[10][5]*q0)/2 + SF[2]*(P[1][0] + P[0][0]*SF[6] + P[2][0]*SF[5] + P[3][0]*SF[9] + P[11][0]*SPP[6] - P[12][0]*SPP[7] - (P[10][0]*q0)/2) + SF[1]*(P[1][2] + P[0][2]*SF[6] + P[2][2]*SF[5] + P[3][2]*SF[9] + P[11][2]*SPP[6] - P[12][2]*SPP[7] - (P[10][2]*q0)/2) + SF[3]*(P[1][3] + P[0][3]*SF[6] + P[2][3]*SF[5] + P[3][3]*SF[9] + P[11][3]*SPP[6] - P[12][3]*SPP[7] - (P[10][3]*q0)/2) - SPP[0]*(P[1][1] + P[0][1]*SF[6] + P[2][1]*SF[5] + P[3][1]*SF[9] + P[11][1]*SPP[6] - P[12][1]*SPP[7] - (P[10][1]*q0)/2) + SPP[3]*(P[1][13] + P[0][13]*SF[6] + P[2][13]*SF[5] + P[3][13]*SF[9] + P[11][13]*SPP[6] - P[12][13]*SPP[7] - (P[10][13]*q0)/2); + nextP[1][6] = P[1][6] + P[0][6]*SF[6] + P[2][6]*SF[5] + P[3][6]*SF[9] + P[11][6]*SPP[6] - P[12][6]*SPP[7] - (P[10][6]*q0)/2 + SF[2]*(P[1][1] + P[0][1]*SF[6] + P[2][1]*SF[5] + P[3][1]*SF[9] + P[11][1]*SPP[6] - P[12][1]*SPP[7] - (P[10][1]*q0)/2) + SF[1]*(P[1][3] + P[0][3]*SF[6] + P[2][3]*SF[5] + P[3][3]*SF[9] + P[11][3]*SPP[6] - P[12][3]*SPP[7] - (P[10][3]*q0)/2) + SPP[0]*(P[1][0] + P[0][0]*SF[6] + P[2][0]*SF[5] + P[3][0]*SF[9] + P[11][0]*SPP[6] - P[12][0]*SPP[7] - (P[10][0]*q0)/2) - SPP[1]*(P[1][2] + P[0][2]*SF[6] + P[2][2]*SF[5] + P[3][2]*SF[9] + P[11][2]*SPP[6] - P[12][2]*SPP[7] - (P[10][2]*q0)/2) - (sq(q0) - sq(q1) - sq(q2) + sq(q3))*(P[1][13] + P[0][13]*SF[6] + P[2][13]*SF[5] + P[3][13]*SF[9] + P[11][13]*SPP[6] - P[12][13]*SPP[7] - (P[10][13]*q0)/2); + nextP[1][7] = P[1][7] + P[0][7]*SF[6] + P[2][7]*SF[5] + P[3][7]*SF[9] + P[11][7]*SPP[6] - P[12][7]*SPP[7] - (P[10][7]*q0)/2 + dt*(P[1][4] + P[0][4]*SF[6] + P[2][4]*SF[5] + P[3][4]*SF[9] + P[11][4]*SPP[6] - P[12][4]*SPP[7] - (P[10][4]*q0)/2); + nextP[1][8] = P[1][8] + P[0][8]*SF[6] + P[2][8]*SF[5] + P[3][8]*SF[9] + P[11][8]*SPP[6] - P[12][8]*SPP[7] - (P[10][8]*q0)/2 + dt*(P[1][5] + P[0][5]*SF[6] + P[2][5]*SF[5] + P[3][5]*SF[9] + P[11][5]*SPP[6] - P[12][5]*SPP[7] - (P[10][5]*q0)/2); + nextP[1][9] = P[1][9] + P[0][9]*SF[6] + P[2][9]*SF[5] + P[3][9]*SF[9] + P[11][9]*SPP[6] - P[12][9]*SPP[7] - (P[10][9]*q0)/2 + dt*(P[1][6] + P[0][6]*SF[6] + P[2][6]*SF[5] + P[3][6]*SF[9] + P[11][6]*SPP[6] - P[12][6]*SPP[7] - (P[10][6]*q0)/2); + nextP[1][10] = P[1][10] + P[0][10]*SF[6] + P[2][10]*SF[5] + P[3][10]*SF[9] + P[11][10]*SPP[6] - P[12][10]*SPP[7] - (P[10][10]*q0)/2; + nextP[1][11] = P[1][11] + P[0][11]*SF[6] + P[2][11]*SF[5] + P[3][11]*SF[9] + P[11][11]*SPP[6] - P[12][11]*SPP[7] - (P[10][11]*q0)/2; + nextP[1][12] = P[1][12] + P[0][12]*SF[6] + P[2][12]*SF[5] + P[3][12]*SF[9] + P[11][12]*SPP[6] - P[12][12]*SPP[7] - (P[10][12]*q0)/2; + nextP[1][13] = P[1][13] + P[0][13]*SF[6] + P[2][13]*SF[5] + P[3][13]*SF[9] + P[11][13]*SPP[6] - P[12][13]*SPP[7] - (P[10][13]*q0)/2; + nextP[1][14] = P[1][14] + P[0][14]*SF[6] + P[2][14]*SF[5] + P[3][14]*SF[9] + P[11][14]*SPP[6] - P[12][14]*SPP[7] - (P[10][14]*q0)/2; + nextP[1][15] = P[1][15] + P[0][15]*SF[6] + P[2][15]*SF[5] + P[3][15]*SF[9] + P[11][15]*SPP[6] - P[12][15]*SPP[7] - (P[10][15]*q0)/2; + nextP[1][16] = P[1][16] + P[0][16]*SF[6] + P[2][16]*SF[5] + P[3][16]*SF[9] + P[11][16]*SPP[6] - P[12][16]*SPP[7] - (P[10][16]*q0)/2; + nextP[1][17] = P[1][17] + P[0][17]*SF[6] + P[2][17]*SF[5] + P[3][17]*SF[9] + P[11][17]*SPP[6] - P[12][17]*SPP[7] - (P[10][17]*q0)/2; + nextP[1][18] = P[1][18] + P[0][18]*SF[6] + P[2][18]*SF[5] + P[3][18]*SF[9] + P[11][18]*SPP[6] - P[12][18]*SPP[7] - (P[10][18]*q0)/2; + nextP[1][19] = P[1][19] + P[0][19]*SF[6] + P[2][19]*SF[5] + P[3][19]*SF[9] + P[11][19]*SPP[6] - P[12][19]*SPP[7] - (P[10][19]*q0)/2; + nextP[1][20] = P[1][20] + P[0][20]*SF[6] + P[2][20]*SF[5] + P[3][20]*SF[9] + P[11][20]*SPP[6] - P[12][20]*SPP[7] - (P[10][20]*q0)/2; + nextP[1][21] = P[1][21] + P[0][21]*SF[6] + P[2][21]*SF[5] + P[3][21]*SF[9] + P[11][21]*SPP[6] - P[12][21]*SPP[7] - (P[10][21]*q0)/2; + nextP[1][22] = P[1][22] + P[0][22]*SF[6] + P[2][22]*SF[5] + P[3][22]*SF[9] + P[11][22]*SPP[6] - P[12][22]*SPP[7] - (P[10][22]*q0)/2; + nextP[2][0] = P[2][0] + SQ[7] + P[0][0]*SF[4] + P[1][0]*SF[8] + P[3][0]*SF[6] + P[12][0]*SF[11] - P[10][0]*SPP[6] - (P[11][0]*q0)/2 + SF[7]*(P[2][1] + P[0][1]*SF[4] + P[1][1]*SF[8] + P[3][1]*SF[6] + P[12][1]*SF[11] - P[10][1]*SPP[6] - (P[11][1]*q0)/2) + SF[9]*(P[2][2] + P[0][2]*SF[4] + P[1][2]*SF[8] + P[3][2]*SF[6] + P[12][2]*SF[11] - P[10][2]*SPP[6] - (P[11][2]*q0)/2) + SF[8]*(P[2][3] + P[0][3]*SF[4] + P[1][3]*SF[8] + P[3][3]*SF[6] + P[12][3]*SF[11] - P[10][3]*SPP[6] - (P[11][3]*q0)/2) + SF[11]*(P[2][10] + P[0][10]*SF[4] + P[1][10]*SF[8] + P[3][10]*SF[6] + P[12][10]*SF[11] - P[10][10]*SPP[6] - (P[11][10]*q0)/2) + SPP[7]*(P[2][11] + P[0][11]*SF[4] + P[1][11]*SF[8] + P[3][11]*SF[6] + P[12][11]*SF[11] - P[10][11]*SPP[6] - (P[11][11]*q0)/2) + SPP[6]*(P[2][12] + P[0][12]*SF[4] + P[1][12]*SF[8] + P[3][12]*SF[6] + P[12][12]*SF[11] - P[10][12]*SPP[6] - (P[11][12]*q0)/2); + nextP[2][1] = P[2][1] + SQ[5] + P[0][1]*SF[4] + P[1][1]*SF[8] + P[3][1]*SF[6] + P[12][1]*SF[11] - P[10][1]*SPP[6] - (P[11][1]*q0)/2 + SF[6]*(P[2][0] + P[0][0]*SF[4] + P[1][0]*SF[8] + P[3][0]*SF[6] + P[12][0]*SF[11] - P[10][0]*SPP[6] - (P[11][0]*q0)/2) + SF[5]*(P[2][2] + P[0][2]*SF[4] + P[1][2]*SF[8] + P[3][2]*SF[6] + P[12][2]*SF[11] - P[10][2]*SPP[6] - (P[11][2]*q0)/2) + SF[9]*(P[2][3] + P[0][3]*SF[4] + P[1][3]*SF[8] + P[3][3]*SF[6] + P[12][3]*SF[11] - P[10][3]*SPP[6] - (P[11][3]*q0)/2) + SPP[6]*(P[2][11] + P[0][11]*SF[4] + P[1][11]*SF[8] + P[3][11]*SF[6] + P[12][11]*SF[11] - P[10][11]*SPP[6] - (P[11][11]*q0)/2) - SPP[7]*(P[2][12] + P[0][12]*SF[4] + P[1][12]*SF[8] + P[3][12]*SF[6] + P[12][12]*SF[11] - P[10][12]*SPP[6] - (P[11][12]*q0)/2) - (q0*(P[2][10] + P[0][10]*SF[4] + P[1][10]*SF[8] + P[3][10]*SF[6] + P[12][10]*SF[11] - P[10][10]*SPP[6] - (P[11][10]*q0)/2))/2; + nextP[2][2] = P[2][2] + P[0][2]*SF[4] + P[1][2]*SF[8] + P[3][2]*SF[6] + P[12][2]*SF[11] - P[10][2]*SPP[6] + dayCov*SQ[9] + (dazCov*SQ[10])/4 - (P[11][2]*q0)/2 + SF[4]*(P[2][0] + P[0][0]*SF[4] + P[1][0]*SF[8] + P[3][0]*SF[6] + P[12][0]*SF[11] - P[10][0]*SPP[6] - (P[11][0]*q0)/2) + SF[8]*(P[2][1] + P[0][1]*SF[4] + P[1][1]*SF[8] + P[3][1]*SF[6] + P[12][1]*SF[11] - P[10][1]*SPP[6] - (P[11][1]*q0)/2) + SF[6]*(P[2][3] + P[0][3]*SF[4] + P[1][3]*SF[8] + P[3][3]*SF[6] + P[12][3]*SF[11] - P[10][3]*SPP[6] - (P[11][3]*q0)/2) + SF[11]*(P[2][12] + P[0][12]*SF[4] + P[1][12]*SF[8] + P[3][12]*SF[6] + P[12][12]*SF[11] - P[10][12]*SPP[6] - (P[11][12]*q0)/2) - SPP[6]*(P[2][10] + P[0][10]*SF[4] + P[1][10]*SF[8] + P[3][10]*SF[6] + P[12][10]*SF[11] - P[10][10]*SPP[6] - (P[11][10]*q0)/2) + (daxCov*sq(q3))/4 - (q0*(P[2][11] + P[0][11]*SF[4] + P[1][11]*SF[8] + P[3][11]*SF[6] + P[12][11]*SF[11] - P[10][11]*SPP[6] - (P[11][11]*q0)/2))/2; + nextP[2][3] = P[2][3] + SQ[3] + P[0][3]*SF[4] + P[1][3]*SF[8] + P[3][3]*SF[6] + P[12][3]*SF[11] - P[10][3]*SPP[6] - (P[11][3]*q0)/2 + SF[5]*(P[2][0] + P[0][0]*SF[4] + P[1][0]*SF[8] + P[3][0]*SF[6] + P[12][0]*SF[11] - P[10][0]*SPP[6] - (P[11][0]*q0)/2) + SF[4]*(P[2][1] + P[0][1]*SF[4] + P[1][1]*SF[8] + P[3][1]*SF[6] + P[12][1]*SF[11] - P[10][1]*SPP[6] - (P[11][1]*q0)/2) + SF[7]*(P[2][2] + P[0][2]*SF[4] + P[1][2]*SF[8] + P[3][2]*SF[6] + P[12][2]*SF[11] - P[10][2]*SPP[6] - (P[11][2]*q0)/2) - SF[11]*(P[2][11] + P[0][11]*SF[4] + P[1][11]*SF[8] + P[3][11]*SF[6] + P[12][11]*SF[11] - P[10][11]*SPP[6] - (P[11][11]*q0)/2) + SPP[7]*(P[2][10] + P[0][10]*SF[4] + P[1][10]*SF[8] + P[3][10]*SF[6] + P[12][10]*SF[11] - P[10][10]*SPP[6] - (P[11][10]*q0)/2) - (q0*(P[2][12] + P[0][12]*SF[4] + P[1][12]*SF[8] + P[3][12]*SF[6] + P[12][12]*SF[11] - P[10][12]*SPP[6] - (P[11][12]*q0)/2))/2; + nextP[2][4] = P[2][4] + P[0][4]*SF[4] + P[1][4]*SF[8] + P[3][4]*SF[6] + P[12][4]*SF[11] - P[10][4]*SPP[6] - (P[11][4]*q0)/2 + SF[3]*(P[2][0] + P[0][0]*SF[4] + P[1][0]*SF[8] + P[3][0]*SF[6] + P[12][0]*SF[11] - P[10][0]*SPP[6] - (P[11][0]*q0)/2) + SF[1]*(P[2][1] + P[0][1]*SF[4] + P[1][1]*SF[8] + P[3][1]*SF[6] + P[12][1]*SF[11] - P[10][1]*SPP[6] - (P[11][1]*q0)/2) + SPP[0]*(P[2][2] + P[0][2]*SF[4] + P[1][2]*SF[8] + P[3][2]*SF[6] + P[12][2]*SF[11] - P[10][2]*SPP[6] - (P[11][2]*q0)/2) - SPP[2]*(P[2][3] + P[0][3]*SF[4] + P[1][3]*SF[8] + P[3][3]*SF[6] + P[12][3]*SF[11] - P[10][3]*SPP[6] - (P[11][3]*q0)/2) - SPP[4]*(P[2][13] + P[0][13]*SF[4] + P[1][13]*SF[8] + P[3][13]*SF[6] + P[12][13]*SF[11] - P[10][13]*SPP[6] - (P[11][13]*q0)/2); + nextP[2][5] = P[2][5] + P[0][5]*SF[4] + P[1][5]*SF[8] + P[3][5]*SF[6] + P[12][5]*SF[11] - P[10][5]*SPP[6] - (P[11][5]*q0)/2 + SF[2]*(P[2][0] + P[0][0]*SF[4] + P[1][0]*SF[8] + P[3][0]*SF[6] + P[12][0]*SF[11] - P[10][0]*SPP[6] - (P[11][0]*q0)/2) + SF[1]*(P[2][2] + P[0][2]*SF[4] + P[1][2]*SF[8] + P[3][2]*SF[6] + P[12][2]*SF[11] - P[10][2]*SPP[6] - (P[11][2]*q0)/2) + SF[3]*(P[2][3] + P[0][3]*SF[4] + P[1][3]*SF[8] + P[3][3]*SF[6] + P[12][3]*SF[11] - P[10][3]*SPP[6] - (P[11][3]*q0)/2) - SPP[0]*(P[2][1] + P[0][1]*SF[4] + P[1][1]*SF[8] + P[3][1]*SF[6] + P[12][1]*SF[11] - P[10][1]*SPP[6] - (P[11][1]*q0)/2) + SPP[3]*(P[2][13] + P[0][13]*SF[4] + P[1][13]*SF[8] + P[3][13]*SF[6] + P[12][13]*SF[11] - P[10][13]*SPP[6] - (P[11][13]*q0)/2); + nextP[2][6] = P[2][6] + P[0][6]*SF[4] + P[1][6]*SF[8] + P[3][6]*SF[6] + P[12][6]*SF[11] - P[10][6]*SPP[6] - (P[11][6]*q0)/2 + SF[2]*(P[2][1] + P[0][1]*SF[4] + P[1][1]*SF[8] + P[3][1]*SF[6] + P[12][1]*SF[11] - P[10][1]*SPP[6] - (P[11][1]*q0)/2) + SF[1]*(P[2][3] + P[0][3]*SF[4] + P[1][3]*SF[8] + P[3][3]*SF[6] + P[12][3]*SF[11] - P[10][3]*SPP[6] - (P[11][3]*q0)/2) + SPP[0]*(P[2][0] + P[0][0]*SF[4] + P[1][0]*SF[8] + P[3][0]*SF[6] + P[12][0]*SF[11] - P[10][0]*SPP[6] - (P[11][0]*q0)/2) - SPP[1]*(P[2][2] + P[0][2]*SF[4] + P[1][2]*SF[8] + P[3][2]*SF[6] + P[12][2]*SF[11] - P[10][2]*SPP[6] - (P[11][2]*q0)/2) - (sq(q0) - sq(q1) - sq(q2) + sq(q3))*(P[2][13] + P[0][13]*SF[4] + P[1][13]*SF[8] + P[3][13]*SF[6] + P[12][13]*SF[11] - P[10][13]*SPP[6] - (P[11][13]*q0)/2); + nextP[2][7] = P[2][7] + P[0][7]*SF[4] + P[1][7]*SF[8] + P[3][7]*SF[6] + P[12][7]*SF[11] - P[10][7]*SPP[6] - (P[11][7]*q0)/2 + dt*(P[2][4] + P[0][4]*SF[4] + P[1][4]*SF[8] + P[3][4]*SF[6] + P[12][4]*SF[11] - P[10][4]*SPP[6] - (P[11][4]*q0)/2); + nextP[2][8] = P[2][8] + P[0][8]*SF[4] + P[1][8]*SF[8] + P[3][8]*SF[6] + P[12][8]*SF[11] - P[10][8]*SPP[6] - (P[11][8]*q0)/2 + dt*(P[2][5] + P[0][5]*SF[4] + P[1][5]*SF[8] + P[3][5]*SF[6] + P[12][5]*SF[11] - P[10][5]*SPP[6] - (P[11][5]*q0)/2); + nextP[2][9] = P[2][9] + P[0][9]*SF[4] + P[1][9]*SF[8] + P[3][9]*SF[6] + P[12][9]*SF[11] - P[10][9]*SPP[6] - (P[11][9]*q0)/2 + dt*(P[2][6] + P[0][6]*SF[4] + P[1][6]*SF[8] + P[3][6]*SF[6] + P[12][6]*SF[11] - P[10][6]*SPP[6] - (P[11][6]*q0)/2); + nextP[2][10] = P[2][10] + P[0][10]*SF[4] + P[1][10]*SF[8] + P[3][10]*SF[6] + P[12][10]*SF[11] - P[10][10]*SPP[6] - (P[11][10]*q0)/2; + nextP[2][11] = P[2][11] + P[0][11]*SF[4] + P[1][11]*SF[8] + P[3][11]*SF[6] + P[12][11]*SF[11] - P[10][11]*SPP[6] - (P[11][11]*q0)/2; + nextP[2][12] = P[2][12] + P[0][12]*SF[4] + P[1][12]*SF[8] + P[3][12]*SF[6] + P[12][12]*SF[11] - P[10][12]*SPP[6] - (P[11][12]*q0)/2; + nextP[2][13] = P[2][13] + P[0][13]*SF[4] + P[1][13]*SF[8] + P[3][13]*SF[6] + P[12][13]*SF[11] - P[10][13]*SPP[6] - (P[11][13]*q0)/2; + nextP[2][14] = P[2][14] + P[0][14]*SF[4] + P[1][14]*SF[8] + P[3][14]*SF[6] + P[12][14]*SF[11] - P[10][14]*SPP[6] - (P[11][14]*q0)/2; + nextP[2][15] = P[2][15] + P[0][15]*SF[4] + P[1][15]*SF[8] + P[3][15]*SF[6] + P[12][15]*SF[11] - P[10][15]*SPP[6] - (P[11][15]*q0)/2; + nextP[2][16] = P[2][16] + P[0][16]*SF[4] + P[1][16]*SF[8] + P[3][16]*SF[6] + P[12][16]*SF[11] - P[10][16]*SPP[6] - (P[11][16]*q0)/2; + nextP[2][17] = P[2][17] + P[0][17]*SF[4] + P[1][17]*SF[8] + P[3][17]*SF[6] + P[12][17]*SF[11] - P[10][17]*SPP[6] - (P[11][17]*q0)/2; + nextP[2][18] = P[2][18] + P[0][18]*SF[4] + P[1][18]*SF[8] + P[3][18]*SF[6] + P[12][18]*SF[11] - P[10][18]*SPP[6] - (P[11][18]*q0)/2; + nextP[2][19] = P[2][19] + P[0][19]*SF[4] + P[1][19]*SF[8] + P[3][19]*SF[6] + P[12][19]*SF[11] - P[10][19]*SPP[6] - (P[11][19]*q0)/2; + nextP[2][20] = P[2][20] + P[0][20]*SF[4] + P[1][20]*SF[8] + P[3][20]*SF[6] + P[12][20]*SF[11] - P[10][20]*SPP[6] - (P[11][20]*q0)/2; + nextP[2][21] = P[2][21] + P[0][21]*SF[4] + P[1][21]*SF[8] + P[3][21]*SF[6] + P[12][21]*SF[11] - P[10][21]*SPP[6] - (P[11][21]*q0)/2; + nextP[2][22] = P[2][22] + P[0][22]*SF[4] + P[1][22]*SF[8] + P[3][22]*SF[6] + P[12][22]*SF[11] - P[10][22]*SPP[6] - (P[11][22]*q0)/2; + nextP[3][0] = P[3][0] + SQ[6] + P[0][0]*SF[5] + P[1][0]*SF[4] + P[2][0]*SF[7] - P[11][0]*SF[11] + P[10][0]*SPP[7] - (P[12][0]*q0)/2 + SF[7]*(P[3][1] + P[0][1]*SF[5] + P[1][1]*SF[4] + P[2][1]*SF[7] - P[11][1]*SF[11] + P[10][1]*SPP[7] - (P[12][1]*q0)/2) + SF[9]*(P[3][2] + P[0][2]*SF[5] + P[1][2]*SF[4] + P[2][2]*SF[7] - P[11][2]*SF[11] + P[10][2]*SPP[7] - (P[12][2]*q0)/2) + SF[8]*(P[3][3] + P[0][3]*SF[5] + P[1][3]*SF[4] + P[2][3]*SF[7] - P[11][3]*SF[11] + P[10][3]*SPP[7] - (P[12][3]*q0)/2) + SF[11]*(P[3][10] + P[0][10]*SF[5] + P[1][10]*SF[4] + P[2][10]*SF[7] - P[11][10]*SF[11] + P[10][10]*SPP[7] - (P[12][10]*q0)/2) + SPP[7]*(P[3][11] + P[0][11]*SF[5] + P[1][11]*SF[4] + P[2][11]*SF[7] - P[11][11]*SF[11] + P[10][11]*SPP[7] - (P[12][11]*q0)/2) + SPP[6]*(P[3][12] + P[0][12]*SF[5] + P[1][12]*SF[4] + P[2][12]*SF[7] - P[11][12]*SF[11] + P[10][12]*SPP[7] - (P[12][12]*q0)/2); + nextP[3][1] = P[3][1] + SQ[4] + P[0][1]*SF[5] + P[1][1]*SF[4] + P[2][1]*SF[7] - P[11][1]*SF[11] + P[10][1]*SPP[7] - (P[12][1]*q0)/2 + SF[6]*(P[3][0] + P[0][0]*SF[5] + P[1][0]*SF[4] + P[2][0]*SF[7] - P[11][0]*SF[11] + P[10][0]*SPP[7] - (P[12][0]*q0)/2) + SF[5]*(P[3][2] + P[0][2]*SF[5] + P[1][2]*SF[4] + P[2][2]*SF[7] - P[11][2]*SF[11] + P[10][2]*SPP[7] - (P[12][2]*q0)/2) + SF[9]*(P[3][3] + P[0][3]*SF[5] + P[1][3]*SF[4] + P[2][3]*SF[7] - P[11][3]*SF[11] + P[10][3]*SPP[7] - (P[12][3]*q0)/2) + SPP[6]*(P[3][11] + P[0][11]*SF[5] + P[1][11]*SF[4] + P[2][11]*SF[7] - P[11][11]*SF[11] + P[10][11]*SPP[7] - (P[12][11]*q0)/2) - SPP[7]*(P[3][12] + P[0][12]*SF[5] + P[1][12]*SF[4] + P[2][12]*SF[7] - P[11][12]*SF[11] + P[10][12]*SPP[7] - (P[12][12]*q0)/2) - (q0*(P[3][10] + P[0][10]*SF[5] + P[1][10]*SF[4] + P[2][10]*SF[7] - P[11][10]*SF[11] + P[10][10]*SPP[7] - (P[12][10]*q0)/2))/2; + nextP[3][2] = P[3][2] + SQ[3] + P[0][2]*SF[5] + P[1][2]*SF[4] + P[2][2]*SF[7] - P[11][2]*SF[11] + P[10][2]*SPP[7] - (P[12][2]*q0)/2 + SF[4]*(P[3][0] + P[0][0]*SF[5] + P[1][0]*SF[4] + P[2][0]*SF[7] - P[11][0]*SF[11] + P[10][0]*SPP[7] - (P[12][0]*q0)/2) + SF[8]*(P[3][1] + P[0][1]*SF[5] + P[1][1]*SF[4] + P[2][1]*SF[7] - P[11][1]*SF[11] + P[10][1]*SPP[7] - (P[12][1]*q0)/2) + SF[6]*(P[3][3] + P[0][3]*SF[5] + P[1][3]*SF[4] + P[2][3]*SF[7] - P[11][3]*SF[11] + P[10][3]*SPP[7] - (P[12][3]*q0)/2) + SF[11]*(P[3][12] + P[0][12]*SF[5] + P[1][12]*SF[4] + P[2][12]*SF[7] - P[11][12]*SF[11] + P[10][12]*SPP[7] - (P[12][12]*q0)/2) - SPP[6]*(P[3][10] + P[0][10]*SF[5] + P[1][10]*SF[4] + P[2][10]*SF[7] - P[11][10]*SF[11] + P[10][10]*SPP[7] - (P[12][10]*q0)/2) - (q0*(P[3][11] + P[0][11]*SF[5] + P[1][11]*SF[4] + P[2][11]*SF[7] - P[11][11]*SF[11] + P[10][11]*SPP[7] - (P[12][11]*q0)/2))/2; + nextP[3][3] = P[3][3] + P[0][3]*SF[5] + P[1][3]*SF[4] + P[2][3]*SF[7] - P[11][3]*SF[11] + P[10][3]*SPP[7] + (dayCov*SQ[10])/4 + dazCov*SQ[9] - (P[12][3]*q0)/2 + SF[5]*(P[3][0] + P[0][0]*SF[5] + P[1][0]*SF[4] + P[2][0]*SF[7] - P[11][0]*SF[11] + P[10][0]*SPP[7] - (P[12][0]*q0)/2) + SF[4]*(P[3][1] + P[0][1]*SF[5] + P[1][1]*SF[4] + P[2][1]*SF[7] - P[11][1]*SF[11] + P[10][1]*SPP[7] - (P[12][1]*q0)/2) + SF[7]*(P[3][2] + P[0][2]*SF[5] + P[1][2]*SF[4] + P[2][2]*SF[7] - P[11][2]*SF[11] + P[10][2]*SPP[7] - (P[12][2]*q0)/2) - SF[11]*(P[3][11] + P[0][11]*SF[5] + P[1][11]*SF[4] + P[2][11]*SF[7] - P[11][11]*SF[11] + P[10][11]*SPP[7] - (P[12][11]*q0)/2) + SPP[7]*(P[3][10] + P[0][10]*SF[5] + P[1][10]*SF[4] + P[2][10]*SF[7] - P[11][10]*SF[11] + P[10][10]*SPP[7] - (P[12][10]*q0)/2) + (daxCov*sq(q2))/4 - (q0*(P[3][12] + P[0][12]*SF[5] + P[1][12]*SF[4] + P[2][12]*SF[7] - P[11][12]*SF[11] + P[10][12]*SPP[7] - (P[12][12]*q0)/2))/2; + nextP[3][4] = P[3][4] + P[0][4]*SF[5] + P[1][4]*SF[4] + P[2][4]*SF[7] - P[11][4]*SF[11] + P[10][4]*SPP[7] - (P[12][4]*q0)/2 + SF[3]*(P[3][0] + P[0][0]*SF[5] + P[1][0]*SF[4] + P[2][0]*SF[7] - P[11][0]*SF[11] + P[10][0]*SPP[7] - (P[12][0]*q0)/2) + SF[1]*(P[3][1] + P[0][1]*SF[5] + P[1][1]*SF[4] + P[2][1]*SF[7] - P[11][1]*SF[11] + P[10][1]*SPP[7] - (P[12][1]*q0)/2) + SPP[0]*(P[3][2] + P[0][2]*SF[5] + P[1][2]*SF[4] + P[2][2]*SF[7] - P[11][2]*SF[11] + P[10][2]*SPP[7] - (P[12][2]*q0)/2) - SPP[2]*(P[3][3] + P[0][3]*SF[5] + P[1][3]*SF[4] + P[2][3]*SF[7] - P[11][3]*SF[11] + P[10][3]*SPP[7] - (P[12][3]*q0)/2) - SPP[4]*(P[3][13] + P[0][13]*SF[5] + P[1][13]*SF[4] + P[2][13]*SF[7] - P[11][13]*SF[11] + P[10][13]*SPP[7] - (P[12][13]*q0)/2); + nextP[3][5] = P[3][5] + P[0][5]*SF[5] + P[1][5]*SF[4] + P[2][5]*SF[7] - P[11][5]*SF[11] + P[10][5]*SPP[7] - (P[12][5]*q0)/2 + SF[2]*(P[3][0] + P[0][0]*SF[5] + P[1][0]*SF[4] + P[2][0]*SF[7] - P[11][0]*SF[11] + P[10][0]*SPP[7] - (P[12][0]*q0)/2) + SF[1]*(P[3][2] + P[0][2]*SF[5] + P[1][2]*SF[4] + P[2][2]*SF[7] - P[11][2]*SF[11] + P[10][2]*SPP[7] - (P[12][2]*q0)/2) + SF[3]*(P[3][3] + P[0][3]*SF[5] + P[1][3]*SF[4] + P[2][3]*SF[7] - P[11][3]*SF[11] + P[10][3]*SPP[7] - (P[12][3]*q0)/2) - SPP[0]*(P[3][1] + P[0][1]*SF[5] + P[1][1]*SF[4] + P[2][1]*SF[7] - P[11][1]*SF[11] + P[10][1]*SPP[7] - (P[12][1]*q0)/2) + SPP[3]*(P[3][13] + P[0][13]*SF[5] + P[1][13]*SF[4] + P[2][13]*SF[7] - P[11][13]*SF[11] + P[10][13]*SPP[7] - (P[12][13]*q0)/2); + nextP[3][6] = P[3][6] + P[0][6]*SF[5] + P[1][6]*SF[4] + P[2][6]*SF[7] - P[11][6]*SF[11] + P[10][6]*SPP[7] - (P[12][6]*q0)/2 + SF[2]*(P[3][1] + P[0][1]*SF[5] + P[1][1]*SF[4] + P[2][1]*SF[7] - P[11][1]*SF[11] + P[10][1]*SPP[7] - (P[12][1]*q0)/2) + SF[1]*(P[3][3] + P[0][3]*SF[5] + P[1][3]*SF[4] + P[2][3]*SF[7] - P[11][3]*SF[11] + P[10][3]*SPP[7] - (P[12][3]*q0)/2) + SPP[0]*(P[3][0] + P[0][0]*SF[5] + P[1][0]*SF[4] + P[2][0]*SF[7] - P[11][0]*SF[11] + P[10][0]*SPP[7] - (P[12][0]*q0)/2) - SPP[1]*(P[3][2] + P[0][2]*SF[5] + P[1][2]*SF[4] + P[2][2]*SF[7] - P[11][2]*SF[11] + P[10][2]*SPP[7] - (P[12][2]*q0)/2) - (sq(q0) - sq(q1) - sq(q2) + sq(q3))*(P[3][13] + P[0][13]*SF[5] + P[1][13]*SF[4] + P[2][13]*SF[7] - P[11][13]*SF[11] + P[10][13]*SPP[7] - (P[12][13]*q0)/2); + nextP[3][7] = P[3][7] + P[0][7]*SF[5] + P[1][7]*SF[4] + P[2][7]*SF[7] - P[11][7]*SF[11] + P[10][7]*SPP[7] - (P[12][7]*q0)/2 + dt*(P[3][4] + P[0][4]*SF[5] + P[1][4]*SF[4] + P[2][4]*SF[7] - P[11][4]*SF[11] + P[10][4]*SPP[7] - (P[12][4]*q0)/2); + nextP[3][8] = P[3][8] + P[0][8]*SF[5] + P[1][8]*SF[4] + P[2][8]*SF[7] - P[11][8]*SF[11] + P[10][8]*SPP[7] - (P[12][8]*q0)/2 + dt*(P[3][5] + P[0][5]*SF[5] + P[1][5]*SF[4] + P[2][5]*SF[7] - P[11][5]*SF[11] + P[10][5]*SPP[7] - (P[12][5]*q0)/2); + nextP[3][9] = P[3][9] + P[0][9]*SF[5] + P[1][9]*SF[4] + P[2][9]*SF[7] - P[11][9]*SF[11] + P[10][9]*SPP[7] - (P[12][9]*q0)/2 + dt*(P[3][6] + P[0][6]*SF[5] + P[1][6]*SF[4] + P[2][6]*SF[7] - P[11][6]*SF[11] + P[10][6]*SPP[7] - (P[12][6]*q0)/2); + nextP[3][10] = P[3][10] + P[0][10]*SF[5] + P[1][10]*SF[4] + P[2][10]*SF[7] - P[11][10]*SF[11] + P[10][10]*SPP[7] - (P[12][10]*q0)/2; + nextP[3][11] = P[3][11] + P[0][11]*SF[5] + P[1][11]*SF[4] + P[2][11]*SF[7] - P[11][11]*SF[11] + P[10][11]*SPP[7] - (P[12][11]*q0)/2; + nextP[3][12] = P[3][12] + P[0][12]*SF[5] + P[1][12]*SF[4] + P[2][12]*SF[7] - P[11][12]*SF[11] + P[10][12]*SPP[7] - (P[12][12]*q0)/2; + nextP[3][13] = P[3][13] + P[0][13]*SF[5] + P[1][13]*SF[4] + P[2][13]*SF[7] - P[11][13]*SF[11] + P[10][13]*SPP[7] - (P[12][13]*q0)/2; + nextP[3][14] = P[3][14] + P[0][14]*SF[5] + P[1][14]*SF[4] + P[2][14]*SF[7] - P[11][14]*SF[11] + P[10][14]*SPP[7] - (P[12][14]*q0)/2; + nextP[3][15] = P[3][15] + P[0][15]*SF[5] + P[1][15]*SF[4] + P[2][15]*SF[7] - P[11][15]*SF[11] + P[10][15]*SPP[7] - (P[12][15]*q0)/2; + nextP[3][16] = P[3][16] + P[0][16]*SF[5] + P[1][16]*SF[4] + P[2][16]*SF[7] - P[11][16]*SF[11] + P[10][16]*SPP[7] - (P[12][16]*q0)/2; + nextP[3][17] = P[3][17] + P[0][17]*SF[5] + P[1][17]*SF[4] + P[2][17]*SF[7] - P[11][17]*SF[11] + P[10][17]*SPP[7] - (P[12][17]*q0)/2; + nextP[3][18] = P[3][18] + P[0][18]*SF[5] + P[1][18]*SF[4] + P[2][18]*SF[7] - P[11][18]*SF[11] + P[10][18]*SPP[7] - (P[12][18]*q0)/2; + nextP[3][19] = P[3][19] + P[0][19]*SF[5] + P[1][19]*SF[4] + P[2][19]*SF[7] - P[11][19]*SF[11] + P[10][19]*SPP[7] - (P[12][19]*q0)/2; + nextP[3][20] = P[3][20] + P[0][20]*SF[5] + P[1][20]*SF[4] + P[2][20]*SF[7] - P[11][20]*SF[11] + P[10][20]*SPP[7] - (P[12][20]*q0)/2; + nextP[3][21] = P[3][21] + P[0][21]*SF[5] + P[1][21]*SF[4] + P[2][21]*SF[7] - P[11][21]*SF[11] + P[10][21]*SPP[7] - (P[12][21]*q0)/2; + nextP[3][22] = P[3][22] + P[0][22]*SF[5] + P[1][22]*SF[4] + P[2][22]*SF[7] - P[11][22]*SF[11] + P[10][22]*SPP[7] - (P[12][22]*q0)/2; + nextP[4][0] = P[4][0] + P[0][0]*SF[3] + P[1][0]*SF[1] + P[2][0]*SPP[0] - P[3][0]*SPP[2] - P[13][0]*SPP[4] + SF[7]*(P[4][1] + P[0][1]*SF[3] + P[1][1]*SF[1] + P[2][1]*SPP[0] - P[3][1]*SPP[2] - P[13][1]*SPP[4]) + SF[9]*(P[4][2] + P[0][2]*SF[3] + P[1][2]*SF[1] + P[2][2]*SPP[0] - P[3][2]*SPP[2] - P[13][2]*SPP[4]) + SF[8]*(P[4][3] + P[0][3]*SF[3] + P[1][3]*SF[1] + P[2][3]*SPP[0] - P[3][3]*SPP[2] - P[13][3]*SPP[4]) + SF[11]*(P[4][10] + P[0][10]*SF[3] + P[1][10]*SF[1] + P[2][10]*SPP[0] - P[3][10]*SPP[2] - P[13][10]*SPP[4]) + SPP[7]*(P[4][11] + P[0][11]*SF[3] + P[1][11]*SF[1] + P[2][11]*SPP[0] - P[3][11]*SPP[2] - P[13][11]*SPP[4]) + SPP[6]*(P[4][12] + P[0][12]*SF[3] + P[1][12]*SF[1] + P[2][12]*SPP[0] - P[3][12]*SPP[2] - P[13][12]*SPP[4]); + nextP[4][1] = P[4][1] + P[0][1]*SF[3] + P[1][1]*SF[1] + P[2][1]*SPP[0] - P[3][1]*SPP[2] - P[13][1]*SPP[4] + SF[6]*(P[4][0] + P[0][0]*SF[3] + P[1][0]*SF[1] + P[2][0]*SPP[0] - P[3][0]*SPP[2] - P[13][0]*SPP[4]) + SF[5]*(P[4][2] + P[0][2]*SF[3] + P[1][2]*SF[1] + P[2][2]*SPP[0] - P[3][2]*SPP[2] - P[13][2]*SPP[4]) + SF[9]*(P[4][3] + P[0][3]*SF[3] + P[1][3]*SF[1] + P[2][3]*SPP[0] - P[3][3]*SPP[2] - P[13][3]*SPP[4]) + SPP[6]*(P[4][11] + P[0][11]*SF[3] + P[1][11]*SF[1] + P[2][11]*SPP[0] - P[3][11]*SPP[2] - P[13][11]*SPP[4]) - SPP[7]*(P[4][12] + P[0][12]*SF[3] + P[1][12]*SF[1] + P[2][12]*SPP[0] - P[3][12]*SPP[2] - P[13][12]*SPP[4]) - (q0*(P[4][10] + P[0][10]*SF[3] + P[1][10]*SF[1] + P[2][10]*SPP[0] - P[3][10]*SPP[2] - P[13][10]*SPP[4]))/2; + nextP[4][2] = P[4][2] + P[0][2]*SF[3] + P[1][2]*SF[1] + P[2][2]*SPP[0] - P[3][2]*SPP[2] - P[13][2]*SPP[4] + SF[4]*(P[4][0] + P[0][0]*SF[3] + P[1][0]*SF[1] + P[2][0]*SPP[0] - P[3][0]*SPP[2] - P[13][0]*SPP[4]) + SF[8]*(P[4][1] + P[0][1]*SF[3] + P[1][1]*SF[1] + P[2][1]*SPP[0] - P[3][1]*SPP[2] - P[13][1]*SPP[4]) + SF[6]*(P[4][3] + P[0][3]*SF[3] + P[1][3]*SF[1] + P[2][3]*SPP[0] - P[3][3]*SPP[2] - P[13][3]*SPP[4]) + SF[11]*(P[4][12] + P[0][12]*SF[3] + P[1][12]*SF[1] + P[2][12]*SPP[0] - P[3][12]*SPP[2] - P[13][12]*SPP[4]) - SPP[6]*(P[4][10] + P[0][10]*SF[3] + P[1][10]*SF[1] + P[2][10]*SPP[0] - P[3][10]*SPP[2] - P[13][10]*SPP[4]) - (q0*(P[4][11] + P[0][11]*SF[3] + P[1][11]*SF[1] + P[2][11]*SPP[0] - P[3][11]*SPP[2] - P[13][11]*SPP[4]))/2; + nextP[4][3] = P[4][3] + P[0][3]*SF[3] + P[1][3]*SF[1] + P[2][3]*SPP[0] - P[3][3]*SPP[2] - P[13][3]*SPP[4] + SF[5]*(P[4][0] + P[0][0]*SF[3] + P[1][0]*SF[1] + P[2][0]*SPP[0] - P[3][0]*SPP[2] - P[13][0]*SPP[4]) + SF[4]*(P[4][1] + P[0][1]*SF[3] + P[1][1]*SF[1] + P[2][1]*SPP[0] - P[3][1]*SPP[2] - P[13][1]*SPP[4]) + SF[7]*(P[4][2] + P[0][2]*SF[3] + P[1][2]*SF[1] + P[2][2]*SPP[0] - P[3][2]*SPP[2] - P[13][2]*SPP[4]) - SF[11]*(P[4][11] + P[0][11]*SF[3] + P[1][11]*SF[1] + P[2][11]*SPP[0] - P[3][11]*SPP[2] - P[13][11]*SPP[4]) + SPP[7]*(P[4][10] + P[0][10]*SF[3] + P[1][10]*SF[1] + P[2][10]*SPP[0] - P[3][10]*SPP[2] - P[13][10]*SPP[4]) - (q0*(P[4][12] + P[0][12]*SF[3] + P[1][12]*SF[1] + P[2][12]*SPP[0] - P[3][12]*SPP[2] - P[13][12]*SPP[4]))/2; + nextP[4][4] = P[4][4] + P[0][4]*SF[3] + P[1][4]*SF[1] + P[2][4]*SPP[0] - P[3][4]*SPP[2] - P[13][4]*SPP[4] + dvyCov*sq(SG[7] - 2*q0*q3) + dvzCov*sq(SG[6] + 2*q0*q2) + SF[3]*(P[4][0] + P[0][0]*SF[3] + P[1][0]*SF[1] + P[2][0]*SPP[0] - P[3][0]*SPP[2] - P[13][0]*SPP[4]) + SF[1]*(P[4][1] + P[0][1]*SF[3] + P[1][1]*SF[1] + P[2][1]*SPP[0] - P[3][1]*SPP[2] - P[13][1]*SPP[4]) + SPP[0]*(P[4][2] + P[0][2]*SF[3] + P[1][2]*SF[1] + P[2][2]*SPP[0] - P[3][2]*SPP[2] - P[13][2]*SPP[4]) - SPP[2]*(P[4][3] + P[0][3]*SF[3] + P[1][3]*SF[1] + P[2][3]*SPP[0] - P[3][3]*SPP[2] - P[13][3]*SPP[4]) - SPP[4]*(P[4][13] + P[0][13]*SF[3] + P[1][13]*SF[1] + P[2][13]*SPP[0] - P[3][13]*SPP[2] - P[13][13]*SPP[4]) + dvxCov*sq(SG[1] + SG[2] - SG[3] - SG[4]); + nextP[4][5] = P[4][5] + SQ[2] + P[0][5]*SF[3] + P[1][5]*SF[1] + P[2][5]*SPP[0] - P[3][5]*SPP[2] - P[13][5]*SPP[4] + SF[2]*(P[4][0] + P[0][0]*SF[3] + P[1][0]*SF[1] + P[2][0]*SPP[0] - P[3][0]*SPP[2] - P[13][0]*SPP[4]) + SF[1]*(P[4][2] + P[0][2]*SF[3] + P[1][2]*SF[1] + P[2][2]*SPP[0] - P[3][2]*SPP[2] - P[13][2]*SPP[4]) + SF[3]*(P[4][3] + P[0][3]*SF[3] + P[1][3]*SF[1] + P[2][3]*SPP[0] - P[3][3]*SPP[2] - P[13][3]*SPP[4]) - SPP[0]*(P[4][1] + P[0][1]*SF[3] + P[1][1]*SF[1] + P[2][1]*SPP[0] - P[3][1]*SPP[2] - P[13][1]*SPP[4]) + SPP[3]*(P[4][13] + P[0][13]*SF[3] + P[1][13]*SF[1] + P[2][13]*SPP[0] - P[3][13]*SPP[2] - P[13][13]*SPP[4]); + nextP[4][6] = P[4][6] + SQ[1] + P[0][6]*SF[3] + P[1][6]*SF[1] + P[2][6]*SPP[0] - P[3][6]*SPP[2] - P[13][6]*SPP[4] + SF[2]*(P[4][1] + P[0][1]*SF[3] + P[1][1]*SF[1] + P[2][1]*SPP[0] - P[3][1]*SPP[2] - P[13][1]*SPP[4]) + SF[1]*(P[4][3] + P[0][3]*SF[3] + P[1][3]*SF[1] + P[2][3]*SPP[0] - P[3][3]*SPP[2] - P[13][3]*SPP[4]) + SPP[0]*(P[4][0] + P[0][0]*SF[3] + P[1][0]*SF[1] + P[2][0]*SPP[0] - P[3][0]*SPP[2] - P[13][0]*SPP[4]) - SPP[1]*(P[4][2] + P[0][2]*SF[3] + P[1][2]*SF[1] + P[2][2]*SPP[0] - P[3][2]*SPP[2] - P[13][2]*SPP[4]) - (sq(q0) - sq(q1) - sq(q2) + sq(q3))*(P[4][13] + P[0][13]*SF[3] + P[1][13]*SF[1] + P[2][13]*SPP[0] - P[3][13]*SPP[2] - P[13][13]*SPP[4]); + nextP[4][7] = P[4][7] + P[0][7]*SF[3] + P[1][7]*SF[1] + P[2][7]*SPP[0] - P[3][7]*SPP[2] - P[13][7]*SPP[4] + dt*(P[4][4] + P[0][4]*SF[3] + P[1][4]*SF[1] + P[2][4]*SPP[0] - P[3][4]*SPP[2] - P[13][4]*SPP[4]); + nextP[4][8] = P[4][8] + P[0][8]*SF[3] + P[1][8]*SF[1] + P[2][8]*SPP[0] - P[3][8]*SPP[2] - P[13][8]*SPP[4] + dt*(P[4][5] + P[0][5]*SF[3] + P[1][5]*SF[1] + P[2][5]*SPP[0] - P[3][5]*SPP[2] - P[13][5]*SPP[4]); + nextP[4][9] = P[4][9] + P[0][9]*SF[3] + P[1][9]*SF[1] + P[2][9]*SPP[0] - P[3][9]*SPP[2] - P[13][9]*SPP[4] + dt*(P[4][6] + P[0][6]*SF[3] + P[1][6]*SF[1] + P[2][6]*SPP[0] - P[3][6]*SPP[2] - P[13][6]*SPP[4]); + nextP[4][10] = P[4][10] + P[0][10]*SF[3] + P[1][10]*SF[1] + P[2][10]*SPP[0] - P[3][10]*SPP[2] - P[13][10]*SPP[4]; + nextP[4][11] = P[4][11] + P[0][11]*SF[3] + P[1][11]*SF[1] + P[2][11]*SPP[0] - P[3][11]*SPP[2] - P[13][11]*SPP[4]; + nextP[4][12] = P[4][12] + P[0][12]*SF[3] + P[1][12]*SF[1] + P[2][12]*SPP[0] - P[3][12]*SPP[2] - P[13][12]*SPP[4]; + nextP[4][13] = P[4][13] + P[0][13]*SF[3] + P[1][13]*SF[1] + P[2][13]*SPP[0] - P[3][13]*SPP[2] - P[13][13]*SPP[4]; + nextP[4][14] = P[4][14] + P[0][14]*SF[3] + P[1][14]*SF[1] + P[2][14]*SPP[0] - P[3][14]*SPP[2] - P[13][14]*SPP[4]; + nextP[4][15] = P[4][15] + P[0][15]*SF[3] + P[1][15]*SF[1] + P[2][15]*SPP[0] - P[3][15]*SPP[2] - P[13][15]*SPP[4]; + nextP[4][16] = P[4][16] + P[0][16]*SF[3] + P[1][16]*SF[1] + P[2][16]*SPP[0] - P[3][16]*SPP[2] - P[13][16]*SPP[4]; + nextP[4][17] = P[4][17] + P[0][17]*SF[3] + P[1][17]*SF[1] + P[2][17]*SPP[0] - P[3][17]*SPP[2] - P[13][17]*SPP[4]; + nextP[4][18] = P[4][18] + P[0][18]*SF[3] + P[1][18]*SF[1] + P[2][18]*SPP[0] - P[3][18]*SPP[2] - P[13][18]*SPP[4]; + nextP[4][19] = P[4][19] + P[0][19]*SF[3] + P[1][19]*SF[1] + P[2][19]*SPP[0] - P[3][19]*SPP[2] - P[13][19]*SPP[4]; + nextP[4][20] = P[4][20] + P[0][20]*SF[3] + P[1][20]*SF[1] + P[2][20]*SPP[0] - P[3][20]*SPP[2] - P[13][20]*SPP[4]; + nextP[4][21] = P[4][21] + P[0][21]*SF[3] + P[1][21]*SF[1] + P[2][21]*SPP[0] - P[3][21]*SPP[2] - P[13][21]*SPP[4]; + nextP[4][22] = P[4][22] + P[0][22]*SF[3] + P[1][22]*SF[1] + P[2][22]*SPP[0] - P[3][22]*SPP[2] - P[13][22]*SPP[4]; + nextP[5][0] = P[5][0] + P[0][0]*SF[2] + P[2][0]*SF[1] + P[3][0]*SF[3] - P[1][0]*SPP[0] + P[13][0]*SPP[3] + SF[7]*(P[5][1] + P[0][1]*SF[2] + P[2][1]*SF[1] + P[3][1]*SF[3] - P[1][1]*SPP[0] + P[13][1]*SPP[3]) + SF[9]*(P[5][2] + P[0][2]*SF[2] + P[2][2]*SF[1] + P[3][2]*SF[3] - P[1][2]*SPP[0] + P[13][2]*SPP[3]) + SF[8]*(P[5][3] + P[0][3]*SF[2] + P[2][3]*SF[1] + P[3][3]*SF[3] - P[1][3]*SPP[0] + P[13][3]*SPP[3]) + SF[11]*(P[5][10] + P[0][10]*SF[2] + P[2][10]*SF[1] + P[3][10]*SF[3] - P[1][10]*SPP[0] + P[13][10]*SPP[3]) + SPP[7]*(P[5][11] + P[0][11]*SF[2] + P[2][11]*SF[1] + P[3][11]*SF[3] - P[1][11]*SPP[0] + P[13][11]*SPP[3]) + SPP[6]*(P[5][12] + P[0][12]*SF[2] + P[2][12]*SF[1] + P[3][12]*SF[3] - P[1][12]*SPP[0] + P[13][12]*SPP[3]); + nextP[5][1] = P[5][1] + P[0][1]*SF[2] + P[2][1]*SF[1] + P[3][1]*SF[3] - P[1][1]*SPP[0] + P[13][1]*SPP[3] + SF[6]*(P[5][0] + P[0][0]*SF[2] + P[2][0]*SF[1] + P[3][0]*SF[3] - P[1][0]*SPP[0] + P[13][0]*SPP[3]) + SF[5]*(P[5][2] + P[0][2]*SF[2] + P[2][2]*SF[1] + P[3][2]*SF[3] - P[1][2]*SPP[0] + P[13][2]*SPP[3]) + SF[9]*(P[5][3] + P[0][3]*SF[2] + P[2][3]*SF[1] + P[3][3]*SF[3] - P[1][3]*SPP[0] + P[13][3]*SPP[3]) + SPP[6]*(P[5][11] + P[0][11]*SF[2] + P[2][11]*SF[1] + P[3][11]*SF[3] - P[1][11]*SPP[0] + P[13][11]*SPP[3]) - SPP[7]*(P[5][12] + P[0][12]*SF[2] + P[2][12]*SF[1] + P[3][12]*SF[3] - P[1][12]*SPP[0] + P[13][12]*SPP[3]) - (q0*(P[5][10] + P[0][10]*SF[2] + P[2][10]*SF[1] + P[3][10]*SF[3] - P[1][10]*SPP[0] + P[13][10]*SPP[3]))/2; + nextP[5][2] = P[5][2] + P[0][2]*SF[2] + P[2][2]*SF[1] + P[3][2]*SF[3] - P[1][2]*SPP[0] + P[13][2]*SPP[3] + SF[4]*(P[5][0] + P[0][0]*SF[2] + P[2][0]*SF[1] + P[3][0]*SF[3] - P[1][0]*SPP[0] + P[13][0]*SPP[3]) + SF[8]*(P[5][1] + P[0][1]*SF[2] + P[2][1]*SF[1] + P[3][1]*SF[3] - P[1][1]*SPP[0] + P[13][1]*SPP[3]) + SF[6]*(P[5][3] + P[0][3]*SF[2] + P[2][3]*SF[1] + P[3][3]*SF[3] - P[1][3]*SPP[0] + P[13][3]*SPP[3]) + SF[11]*(P[5][12] + P[0][12]*SF[2] + P[2][12]*SF[1] + P[3][12]*SF[3] - P[1][12]*SPP[0] + P[13][12]*SPP[3]) - SPP[6]*(P[5][10] + P[0][10]*SF[2] + P[2][10]*SF[1] + P[3][10]*SF[3] - P[1][10]*SPP[0] + P[13][10]*SPP[3]) - (q0*(P[5][11] + P[0][11]*SF[2] + P[2][11]*SF[1] + P[3][11]*SF[3] - P[1][11]*SPP[0] + P[13][11]*SPP[3]))/2; + nextP[5][3] = P[5][3] + P[0][3]*SF[2] + P[2][3]*SF[1] + P[3][3]*SF[3] - P[1][3]*SPP[0] + P[13][3]*SPP[3] + SF[5]*(P[5][0] + P[0][0]*SF[2] + P[2][0]*SF[1] + P[3][0]*SF[3] - P[1][0]*SPP[0] + P[13][0]*SPP[3]) + SF[4]*(P[5][1] + P[0][1]*SF[2] + P[2][1]*SF[1] + P[3][1]*SF[3] - P[1][1]*SPP[0] + P[13][1]*SPP[3]) + SF[7]*(P[5][2] + P[0][2]*SF[2] + P[2][2]*SF[1] + P[3][2]*SF[3] - P[1][2]*SPP[0] + P[13][2]*SPP[3]) - SF[11]*(P[5][11] + P[0][11]*SF[2] + P[2][11]*SF[1] + P[3][11]*SF[3] - P[1][11]*SPP[0] + P[13][11]*SPP[3]) + SPP[7]*(P[5][10] + P[0][10]*SF[2] + P[2][10]*SF[1] + P[3][10]*SF[3] - P[1][10]*SPP[0] + P[13][10]*SPP[3]) - (q0*(P[5][12] + P[0][12]*SF[2] + P[2][12]*SF[1] + P[3][12]*SF[3] - P[1][12]*SPP[0] + P[13][12]*SPP[3]))/2; + nextP[5][4] = P[5][4] + SQ[2] + P[0][4]*SF[2] + P[2][4]*SF[1] + P[3][4]*SF[3] - P[1][4]*SPP[0] + P[13][4]*SPP[3] + SF[3]*(P[5][0] + P[0][0]*SF[2] + P[2][0]*SF[1] + P[3][0]*SF[3] - P[1][0]*SPP[0] + P[13][0]*SPP[3]) + SF[1]*(P[5][1] + P[0][1]*SF[2] + P[2][1]*SF[1] + P[3][1]*SF[3] - P[1][1]*SPP[0] + P[13][1]*SPP[3]) + SPP[0]*(P[5][2] + P[0][2]*SF[2] + P[2][2]*SF[1] + P[3][2]*SF[3] - P[1][2]*SPP[0] + P[13][2]*SPP[3]) - SPP[2]*(P[5][3] + P[0][3]*SF[2] + P[2][3]*SF[1] + P[3][3]*SF[3] - P[1][3]*SPP[0] + P[13][3]*SPP[3]) - SPP[4]*(P[5][13] + P[0][13]*SF[2] + P[2][13]*SF[1] + P[3][13]*SF[3] - P[1][13]*SPP[0] + P[13][13]*SPP[3]); + nextP[5][5] = P[5][5] + P[0][5]*SF[2] + P[2][5]*SF[1] + P[3][5]*SF[3] - P[1][5]*SPP[0] + P[13][5]*SPP[3] + dvxCov*sq(SG[7] + 2*q0*q3) + dvzCov*sq(SG[5] - 2*q0*q1) + SF[2]*(P[5][0] + P[0][0]*SF[2] + P[2][0]*SF[1] + P[3][0]*SF[3] - P[1][0]*SPP[0] + P[13][0]*SPP[3]) + SF[1]*(P[5][2] + P[0][2]*SF[2] + P[2][2]*SF[1] + P[3][2]*SF[3] - P[1][2]*SPP[0] + P[13][2]*SPP[3]) + SF[3]*(P[5][3] + P[0][3]*SF[2] + P[2][3]*SF[1] + P[3][3]*SF[3] - P[1][3]*SPP[0] + P[13][3]*SPP[3]) - SPP[0]*(P[5][1] + P[0][1]*SF[2] + P[2][1]*SF[1] + P[3][1]*SF[3] - P[1][1]*SPP[0] + P[13][1]*SPP[3]) + SPP[3]*(P[5][13] + P[0][13]*SF[2] + P[2][13]*SF[1] + P[3][13]*SF[3] - P[1][13]*SPP[0] + P[13][13]*SPP[3]) + dvyCov*sq(SG[1] - SG[2] + SG[3] - SG[4]); + nextP[5][6] = P[5][6] + SQ[0] + P[0][6]*SF[2] + P[2][6]*SF[1] + P[3][6]*SF[3] - P[1][6]*SPP[0] + P[13][6]*SPP[3] + SF[2]*(P[5][1] + P[0][1]*SF[2] + P[2][1]*SF[1] + P[3][1]*SF[3] - P[1][1]*SPP[0] + P[13][1]*SPP[3]) + SF[1]*(P[5][3] + P[0][3]*SF[2] + P[2][3]*SF[1] + P[3][3]*SF[3] - P[1][3]*SPP[0] + P[13][3]*SPP[3]) + SPP[0]*(P[5][0] + P[0][0]*SF[2] + P[2][0]*SF[1] + P[3][0]*SF[3] - P[1][0]*SPP[0] + P[13][0]*SPP[3]) - SPP[1]*(P[5][2] + P[0][2]*SF[2] + P[2][2]*SF[1] + P[3][2]*SF[3] - P[1][2]*SPP[0] + P[13][2]*SPP[3]) - (sq(q0) - sq(q1) - sq(q2) + sq(q3))*(P[5][13] + P[0][13]*SF[2] + P[2][13]*SF[1] + P[3][13]*SF[3] - P[1][13]*SPP[0] + P[13][13]*SPP[3]); + nextP[5][7] = P[5][7] + P[0][7]*SF[2] + P[2][7]*SF[1] + P[3][7]*SF[3] - P[1][7]*SPP[0] + P[13][7]*SPP[3] + dt*(P[5][4] + P[0][4]*SF[2] + P[2][4]*SF[1] + P[3][4]*SF[3] - P[1][4]*SPP[0] + P[13][4]*SPP[3]); + nextP[5][8] = P[5][8] + P[0][8]*SF[2] + P[2][8]*SF[1] + P[3][8]*SF[3] - P[1][8]*SPP[0] + P[13][8]*SPP[3] + dt*(P[5][5] + P[0][5]*SF[2] + P[2][5]*SF[1] + P[3][5]*SF[3] - P[1][5]*SPP[0] + P[13][5]*SPP[3]); + nextP[5][9] = P[5][9] + P[0][9]*SF[2] + P[2][9]*SF[1] + P[3][9]*SF[3] - P[1][9]*SPP[0] + P[13][9]*SPP[3] + dt*(P[5][6] + P[0][6]*SF[2] + P[2][6]*SF[1] + P[3][6]*SF[3] - P[1][6]*SPP[0] + P[13][6]*SPP[3]); + nextP[5][10] = P[5][10] + P[0][10]*SF[2] + P[2][10]*SF[1] + P[3][10]*SF[3] - P[1][10]*SPP[0] + P[13][10]*SPP[3]; + nextP[5][11] = P[5][11] + P[0][11]*SF[2] + P[2][11]*SF[1] + P[3][11]*SF[3] - P[1][11]*SPP[0] + P[13][11]*SPP[3]; + nextP[5][12] = P[5][12] + P[0][12]*SF[2] + P[2][12]*SF[1] + P[3][12]*SF[3] - P[1][12]*SPP[0] + P[13][12]*SPP[3]; + nextP[5][13] = P[5][13] + P[0][13]*SF[2] + P[2][13]*SF[1] + P[3][13]*SF[3] - P[1][13]*SPP[0] + P[13][13]*SPP[3]; + nextP[5][14] = P[5][14] + P[0][14]*SF[2] + P[2][14]*SF[1] + P[3][14]*SF[3] - P[1][14]*SPP[0] + P[13][14]*SPP[3]; + nextP[5][15] = P[5][15] + P[0][15]*SF[2] + P[2][15]*SF[1] + P[3][15]*SF[3] - P[1][15]*SPP[0] + P[13][15]*SPP[3]; + nextP[5][16] = P[5][16] + P[0][16]*SF[2] + P[2][16]*SF[1] + P[3][16]*SF[3] - P[1][16]*SPP[0] + P[13][16]*SPP[3]; + nextP[5][17] = P[5][17] + P[0][17]*SF[2] + P[2][17]*SF[1] + P[3][17]*SF[3] - P[1][17]*SPP[0] + P[13][17]*SPP[3]; + nextP[5][18] = P[5][18] + P[0][18]*SF[2] + P[2][18]*SF[1] + P[3][18]*SF[3] - P[1][18]*SPP[0] + P[13][18]*SPP[3]; + nextP[5][19] = P[5][19] + P[0][19]*SF[2] + P[2][19]*SF[1] + P[3][19]*SF[3] - P[1][19]*SPP[0] + P[13][19]*SPP[3]; + nextP[5][20] = P[5][20] + P[0][20]*SF[2] + P[2][20]*SF[1] + P[3][20]*SF[3] - P[1][20]*SPP[0] + P[13][20]*SPP[3]; + nextP[5][21] = P[5][21] + P[0][21]*SF[2] + P[2][21]*SF[1] + P[3][21]*SF[3] - P[1][21]*SPP[0] + P[13][21]*SPP[3]; + nextP[5][22] = P[5][22] + P[0][22]*SF[2] + P[2][22]*SF[1] + P[3][22]*SF[3] - P[1][22]*SPP[0] + P[13][22]*SPP[3]; + nextP[6][0] = P[6][0] + P[1][0]*SF[2] + P[3][0]*SF[1] + P[0][0]*SPP[0] - P[2][0]*SPP[1] - P[13][0]*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + SF[7]*(P[6][1] + P[1][1]*SF[2] + P[3][1]*SF[1] + P[0][1]*SPP[0] - P[2][1]*SPP[1] - P[13][1]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[9]*(P[6][2] + P[1][2]*SF[2] + P[3][2]*SF[1] + P[0][2]*SPP[0] - P[2][2]*SPP[1] - P[13][2]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[8]*(P[6][3] + P[1][3]*SF[2] + P[3][3]*SF[1] + P[0][3]*SPP[0] - P[2][3]*SPP[1] - P[13][3]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[11]*(P[6][10] + P[1][10]*SF[2] + P[3][10]*SF[1] + P[0][10]*SPP[0] - P[2][10]*SPP[1] - P[13][10]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SPP[7]*(P[6][11] + P[1][11]*SF[2] + P[3][11]*SF[1] + P[0][11]*SPP[0] - P[2][11]*SPP[1] - P[13][11]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SPP[6]*(P[6][12] + P[1][12]*SF[2] + P[3][12]*SF[1] + P[0][12]*SPP[0] - P[2][12]*SPP[1] - P[13][12]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))); + nextP[6][1] = P[6][1] + P[1][1]*SF[2] + P[3][1]*SF[1] + P[0][1]*SPP[0] - P[2][1]*SPP[1] - P[13][1]*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + SF[6]*(P[6][0] + P[1][0]*SF[2] + P[3][0]*SF[1] + P[0][0]*SPP[0] - P[2][0]*SPP[1] - P[13][0]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[5]*(P[6][2] + P[1][2]*SF[2] + P[3][2]*SF[1] + P[0][2]*SPP[0] - P[2][2]*SPP[1] - P[13][2]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[9]*(P[6][3] + P[1][3]*SF[2] + P[3][3]*SF[1] + P[0][3]*SPP[0] - P[2][3]*SPP[1] - P[13][3]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SPP[6]*(P[6][11] + P[1][11]*SF[2] + P[3][11]*SF[1] + P[0][11]*SPP[0] - P[2][11]*SPP[1] - P[13][11]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) - SPP[7]*(P[6][12] + P[1][12]*SF[2] + P[3][12]*SF[1] + P[0][12]*SPP[0] - P[2][12]*SPP[1] - P[13][12]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) - (q0*(P[6][10] + P[1][10]*SF[2] + P[3][10]*SF[1] + P[0][10]*SPP[0] - P[2][10]*SPP[1] - P[13][10]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))))/2; + nextP[6][2] = P[6][2] + P[1][2]*SF[2] + P[3][2]*SF[1] + P[0][2]*SPP[0] - P[2][2]*SPP[1] - P[13][2]*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + SF[4]*(P[6][0] + P[1][0]*SF[2] + P[3][0]*SF[1] + P[0][0]*SPP[0] - P[2][0]*SPP[1] - P[13][0]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[8]*(P[6][1] + P[1][1]*SF[2] + P[3][1]*SF[1] + P[0][1]*SPP[0] - P[2][1]*SPP[1] - P[13][1]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[6]*(P[6][3] + P[1][3]*SF[2] + P[3][3]*SF[1] + P[0][3]*SPP[0] - P[2][3]*SPP[1] - P[13][3]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[11]*(P[6][12] + P[1][12]*SF[2] + P[3][12]*SF[1] + P[0][12]*SPP[0] - P[2][12]*SPP[1] - P[13][12]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) - SPP[6]*(P[6][10] + P[1][10]*SF[2] + P[3][10]*SF[1] + P[0][10]*SPP[0] - P[2][10]*SPP[1] - P[13][10]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) - (q0*(P[6][11] + P[1][11]*SF[2] + P[3][11]*SF[1] + P[0][11]*SPP[0] - P[2][11]*SPP[1] - P[13][11]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))))/2; + nextP[6][3] = P[6][3] + P[1][3]*SF[2] + P[3][3]*SF[1] + P[0][3]*SPP[0] - P[2][3]*SPP[1] - P[13][3]*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + SF[5]*(P[6][0] + P[1][0]*SF[2] + P[3][0]*SF[1] + P[0][0]*SPP[0] - P[2][0]*SPP[1] - P[13][0]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[4]*(P[6][1] + P[1][1]*SF[2] + P[3][1]*SF[1] + P[0][1]*SPP[0] - P[2][1]*SPP[1] - P[13][1]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[7]*(P[6][2] + P[1][2]*SF[2] + P[3][2]*SF[1] + P[0][2]*SPP[0] - P[2][2]*SPP[1] - P[13][2]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) - SF[11]*(P[6][11] + P[1][11]*SF[2] + P[3][11]*SF[1] + P[0][11]*SPP[0] - P[2][11]*SPP[1] - P[13][11]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SPP[7]*(P[6][10] + P[1][10]*SF[2] + P[3][10]*SF[1] + P[0][10]*SPP[0] - P[2][10]*SPP[1] - P[13][10]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) - (q0*(P[6][12] + P[1][12]*SF[2] + P[3][12]*SF[1] + P[0][12]*SPP[0] - P[2][12]*SPP[1] - P[13][12]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))))/2; + nextP[6][4] = P[6][4] + SQ[1] + P[1][4]*SF[2] + P[3][4]*SF[1] + P[0][4]*SPP[0] - P[2][4]*SPP[1] - P[13][4]*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + SF[3]*(P[6][0] + P[1][0]*SF[2] + P[3][0]*SF[1] + P[0][0]*SPP[0] - P[2][0]*SPP[1] - P[13][0]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[1]*(P[6][1] + P[1][1]*SF[2] + P[3][1]*SF[1] + P[0][1]*SPP[0] - P[2][1]*SPP[1] - P[13][1]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SPP[0]*(P[6][2] + P[1][2]*SF[2] + P[3][2]*SF[1] + P[0][2]*SPP[0] - P[2][2]*SPP[1] - P[13][2]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) - SPP[2]*(P[6][3] + P[1][3]*SF[2] + P[3][3]*SF[1] + P[0][3]*SPP[0] - P[2][3]*SPP[1] - P[13][3]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) - SPP[4]*(P[6][13] + P[1][13]*SF[2] + P[3][13]*SF[1] + P[0][13]*SPP[0] - P[2][13]*SPP[1] - P[13][13]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))); + nextP[6][5] = P[6][5] + SQ[0] + P[1][5]*SF[2] + P[3][5]*SF[1] + P[0][5]*SPP[0] - P[2][5]*SPP[1] - P[13][5]*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + SF[2]*(P[6][0] + P[1][0]*SF[2] + P[3][0]*SF[1] + P[0][0]*SPP[0] - P[2][0]*SPP[1] - P[13][0]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[1]*(P[6][2] + P[1][2]*SF[2] + P[3][2]*SF[1] + P[0][2]*SPP[0] - P[2][2]*SPP[1] - P[13][2]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[3]*(P[6][3] + P[1][3]*SF[2] + P[3][3]*SF[1] + P[0][3]*SPP[0] - P[2][3]*SPP[1] - P[13][3]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) - SPP[0]*(P[6][1] + P[1][1]*SF[2] + P[3][1]*SF[1] + P[0][1]*SPP[0] - P[2][1]*SPP[1] - P[13][1]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SPP[3]*(P[6][13] + P[1][13]*SF[2] + P[3][13]*SF[1] + P[0][13]*SPP[0] - P[2][13]*SPP[1] - P[13][13]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))); + nextP[6][6] = P[6][6] + P[1][6]*SF[2] + P[3][6]*SF[1] + P[0][6]*SPP[0] - P[2][6]*SPP[1] - P[13][6]*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + dvxCov*sq(SG[6] - 2*q0*q2) + dvyCov*sq(SG[5] + 2*q0*q1) - SPP[5]*(P[6][13] + P[1][13]*SF[2] + P[3][13]*SF[1] + P[0][13]*SPP[0] - P[2][13]*SPP[1] - P[13][13]*SPP[5]) + SF[2]*(P[6][1] + P[1][1]*SF[2] + P[3][1]*SF[1] + P[0][1]*SPP[0] - P[2][1]*SPP[1] - P[13][1]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SF[1]*(P[6][3] + P[1][3]*SF[2] + P[3][3]*SF[1] + P[0][3]*SPP[0] - P[2][3]*SPP[1] - P[13][3]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + SPP[0]*(P[6][0] + P[1][0]*SF[2] + P[3][0]*SF[1] + P[0][0]*SPP[0] - P[2][0]*SPP[1] - P[13][0]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) - SPP[1]*(P[6][2] + P[1][2]*SF[2] + P[3][2]*SF[1] + P[0][2]*SPP[0] - P[2][2]*SPP[1] - P[13][2]*(sq(q0) - sq(q1) - sq(q2) + sq(q3))) + dvzCov*sq(SG[1] - SG[2] - SG[3] + SG[4]); + nextP[6][7] = P[6][7] + P[1][7]*SF[2] + P[3][7]*SF[1] + P[0][7]*SPP[0] - P[2][7]*SPP[1] - P[13][7]*SPP[5] + dt*(P[6][4] + P[1][4]*SF[2] + P[3][4]*SF[1] + P[0][4]*SPP[0] - P[2][4]*SPP[1] - P[13][4]*SPP[5]); + nextP[6][8] = P[6][8] + P[1][8]*SF[2] + P[3][8]*SF[1] + P[0][8]*SPP[0] - P[2][8]*SPP[1] - P[13][8]*SPP[5] + dt*(P[6][5] + P[1][5]*SF[2] + P[3][5]*SF[1] + P[0][5]*SPP[0] - P[2][5]*SPP[1] - P[13][5]*SPP[5]); + nextP[6][9] = P[6][9] + P[1][9]*SF[2] + P[3][9]*SF[1] + P[0][9]*SPP[0] - P[2][9]*SPP[1] - P[13][9]*SPP[5] + dt*(P[6][6] + P[1][6]*SF[2] + P[3][6]*SF[1] + P[0][6]*SPP[0] - P[2][6]*SPP[1] - P[13][6]*SPP[5]); + nextP[6][10] = P[6][10] + P[1][10]*SF[2] + P[3][10]*SF[1] + P[0][10]*SPP[0] - P[2][10]*SPP[1] - P[13][10]*SPP[5]; + nextP[6][11] = P[6][11] + P[1][11]*SF[2] + P[3][11]*SF[1] + P[0][11]*SPP[0] - P[2][11]*SPP[1] - P[13][11]*SPP[5]; + nextP[6][12] = P[6][12] + P[1][12]*SF[2] + P[3][12]*SF[1] + P[0][12]*SPP[0] - P[2][12]*SPP[1] - P[13][12]*SPP[5]; + nextP[6][13] = P[6][13] + P[1][13]*SF[2] + P[3][13]*SF[1] + P[0][13]*SPP[0] - P[2][13]*SPP[1] - P[13][13]*SPP[5]; + nextP[6][14] = P[6][14] + P[1][14]*SF[2] + P[3][14]*SF[1] + P[0][14]*SPP[0] - P[2][14]*SPP[1] - P[13][14]*SPP[5]; + nextP[6][15] = P[6][15] + P[1][15]*SF[2] + P[3][15]*SF[1] + P[0][15]*SPP[0] - P[2][15]*SPP[1] - P[13][15]*SPP[5]; + nextP[6][16] = P[6][16] + P[1][16]*SF[2] + P[3][16]*SF[1] + P[0][16]*SPP[0] - P[2][16]*SPP[1] - P[13][16]*SPP[5]; + nextP[6][17] = P[6][17] + P[1][17]*SF[2] + P[3][17]*SF[1] + P[0][17]*SPP[0] - P[2][17]*SPP[1] - P[13][17]*SPP[5]; + nextP[6][18] = P[6][18] + P[1][18]*SF[2] + P[3][18]*SF[1] + P[0][18]*SPP[0] - P[2][18]*SPP[1] - P[13][18]*SPP[5]; + nextP[6][19] = P[6][19] + P[1][19]*SF[2] + P[3][19]*SF[1] + P[0][19]*SPP[0] - P[2][19]*SPP[1] - P[13][19]*SPP[5]; + nextP[6][20] = P[6][20] + P[1][20]*SF[2] + P[3][20]*SF[1] + P[0][20]*SPP[0] - P[2][20]*SPP[1] - P[13][20]*SPP[5]; + nextP[6][21] = P[6][21] + P[1][21]*SF[2] + P[3][21]*SF[1] + P[0][21]*SPP[0] - P[2][21]*SPP[1] - P[13][21]*SPP[5]; + nextP[6][22] = P[6][22] + P[1][22]*SF[2] + P[3][22]*SF[1] + P[0][22]*SPP[0] - P[2][22]*SPP[1] - P[13][22]*SPP[5]; + nextP[7][0] = P[7][0] + P[4][0]*dt + SF[7]*(P[7][1] + P[4][1]*dt) + SF[9]*(P[7][2] + P[4][2]*dt) + SF[8]*(P[7][3] + P[4][3]*dt) + SF[11]*(P[7][10] + P[4][10]*dt) + SPP[7]*(P[7][11] + P[4][11]*dt) + SPP[6]*(P[7][12] + P[4][12]*dt); + nextP[7][1] = P[7][1] + P[4][1]*dt + SF[6]*(P[7][0] + P[4][0]*dt) + SF[5]*(P[7][2] + P[4][2]*dt) + SF[9]*(P[7][3] + P[4][3]*dt) + SPP[6]*(P[7][11] + P[4][11]*dt) - SPP[7]*(P[7][12] + P[4][12]*dt) - (q0*(P[7][10] + P[4][10]*dt))/2; + nextP[7][2] = P[7][2] + P[4][2]*dt + SF[4]*(P[7][0] + P[4][0]*dt) + SF[8]*(P[7][1] + P[4][1]*dt) + SF[6]*(P[7][3] + P[4][3]*dt) + SF[11]*(P[7][12] + P[4][12]*dt) - SPP[6]*(P[7][10] + P[4][10]*dt) - (q0*(P[7][11] + P[4][11]*dt))/2; + nextP[7][3] = P[7][3] + P[4][3]*dt + SF[5]*(P[7][0] + P[4][0]*dt) + SF[4]*(P[7][1] + P[4][1]*dt) + SF[7]*(P[7][2] + P[4][2]*dt) - SF[11]*(P[7][11] + P[4][11]*dt) + SPP[7]*(P[7][10] + P[4][10]*dt) - (q0*(P[7][12] + P[4][12]*dt))/2; + nextP[7][4] = P[7][4] + P[4][4]*dt + SF[1]*(P[7][1] + P[4][1]*dt) + SF[3]*(P[7][0] + P[4][0]*dt) + SPP[0]*(P[7][2] + P[4][2]*dt) - SPP[2]*(P[7][3] + P[4][3]*dt) - SPP[4]*(P[7][13] + P[4][13]*dt); + nextP[7][5] = P[7][5] + P[4][5]*dt + SF[2]*(P[7][0] + P[4][0]*dt) + SF[1]*(P[7][2] + P[4][2]*dt) + SF[3]*(P[7][3] + P[4][3]*dt) - SPP[0]*(P[7][1] + P[4][1]*dt) + SPP[3]*(P[7][13] + P[4][13]*dt); + nextP[7][6] = P[7][6] + P[4][6]*dt + SF[2]*(P[7][1] + P[4][1]*dt) + SF[1]*(P[7][3] + P[4][3]*dt) + SPP[0]*(P[7][0] + P[4][0]*dt) - SPP[1]*(P[7][2] + P[4][2]*dt) - SPP[5]*(P[7][13] + P[4][13]*dt); + nextP[7][7] = P[7][7] + P[4][7]*dt + dt*(P[7][4] + P[4][4]*dt); + nextP[7][8] = P[7][8] + P[4][8]*dt + dt*(P[7][5] + P[4][5]*dt); + nextP[7][9] = P[7][9] + P[4][9]*dt + dt*(P[7][6] + P[4][6]*dt); + nextP[7][10] = P[7][10] + P[4][10]*dt; + nextP[7][11] = P[7][11] + P[4][11]*dt; + nextP[7][12] = P[7][12] + P[4][12]*dt; + nextP[7][13] = P[7][13] + P[4][13]*dt; + nextP[7][14] = P[7][14] + P[4][14]*dt; + nextP[7][15] = P[7][15] + P[4][15]*dt; + nextP[7][16] = P[7][16] + P[4][16]*dt; + nextP[7][17] = P[7][17] + P[4][17]*dt; + nextP[7][18] = P[7][18] + P[4][18]*dt; + nextP[7][19] = P[7][19] + P[4][19]*dt; + nextP[7][20] = P[7][20] + P[4][20]*dt; + nextP[7][21] = P[7][21] + P[4][21]*dt; + nextP[7][22] = P[7][22] + P[4][22]*dt; + nextP[8][0] = P[8][0] + P[5][0]*dt + SF[7]*(P[8][1] + P[5][1]*dt) + SF[9]*(P[8][2] + P[5][2]*dt) + SF[8]*(P[8][3] + P[5][3]*dt) + SF[11]*(P[8][10] + P[5][10]*dt) + SPP[7]*(P[8][11] + P[5][11]*dt) + SPP[6]*(P[8][12] + P[5][12]*dt); + nextP[8][1] = P[8][1] + P[5][1]*dt + SF[6]*(P[8][0] + P[5][0]*dt) + SF[5]*(P[8][2] + P[5][2]*dt) + SF[9]*(P[8][3] + P[5][3]*dt) + SPP[6]*(P[8][11] + P[5][11]*dt) - SPP[7]*(P[8][12] + P[5][12]*dt) - (q0*(P[8][10] + P[5][10]*dt))/2; + nextP[8][2] = P[8][2] + P[5][2]*dt + SF[4]*(P[8][0] + P[5][0]*dt) + SF[8]*(P[8][1] + P[5][1]*dt) + SF[6]*(P[8][3] + P[5][3]*dt) + SF[11]*(P[8][12] + P[5][12]*dt) - SPP[6]*(P[8][10] + P[5][10]*dt) - (q0*(P[8][11] + P[5][11]*dt))/2; + nextP[8][3] = P[8][3] + P[5][3]*dt + SF[5]*(P[8][0] + P[5][0]*dt) + SF[4]*(P[8][1] + P[5][1]*dt) + SF[7]*(P[8][2] + P[5][2]*dt) - SF[11]*(P[8][11] + P[5][11]*dt) + SPP[7]*(P[8][10] + P[5][10]*dt) - (q0*(P[8][12] + P[5][12]*dt))/2; + nextP[8][4] = P[8][4] + P[5][4]*dt + SF[1]*(P[8][1] + P[5][1]*dt) + SF[3]*(P[8][0] + P[5][0]*dt) + SPP[0]*(P[8][2] + P[5][2]*dt) - SPP[2]*(P[8][3] + P[5][3]*dt) - SPP[4]*(P[8][13] + P[5][13]*dt); + nextP[8][5] = P[8][5] + P[5][5]*dt + SF[2]*(P[8][0] + P[5][0]*dt) + SF[1]*(P[8][2] + P[5][2]*dt) + SF[3]*(P[8][3] + P[5][3]*dt) - SPP[0]*(P[8][1] + P[5][1]*dt) + SPP[3]*(P[8][13] + P[5][13]*dt); + nextP[8][6] = P[8][6] + P[5][6]*dt + SF[2]*(P[8][1] + P[5][1]*dt) + SF[1]*(P[8][3] + P[5][3]*dt) + SPP[0]*(P[8][0] + P[5][0]*dt) - SPP[1]*(P[8][2] + P[5][2]*dt) - SPP[5]*(P[8][13] + P[5][13]*dt); + nextP[8][7] = P[8][7] + P[5][7]*dt + dt*(P[8][4] + P[5][4]*dt); + nextP[8][8] = P[8][8] + P[5][8]*dt + dt*(P[8][5] + P[5][5]*dt); + nextP[8][9] = P[8][9] + P[5][9]*dt + dt*(P[8][6] + P[5][6]*dt); + nextP[8][10] = P[8][10] + P[5][10]*dt; + nextP[8][11] = P[8][11] + P[5][11]*dt; + nextP[8][12] = P[8][12] + P[5][12]*dt; + nextP[8][13] = P[8][13] + P[5][13]*dt; + nextP[8][14] = P[8][14] + P[5][14]*dt; + nextP[8][15] = P[8][15] + P[5][15]*dt; + nextP[8][16] = P[8][16] + P[5][16]*dt; + nextP[8][17] = P[8][17] + P[5][17]*dt; + nextP[8][18] = P[8][18] + P[5][18]*dt; + nextP[8][19] = P[8][19] + P[5][19]*dt; + nextP[8][20] = P[8][20] + P[5][20]*dt; + nextP[8][21] = P[8][21] + P[5][21]*dt; + nextP[8][22] = P[8][22] + P[5][22]*dt; + nextP[9][0] = P[9][0] + P[6][0]*dt + SF[7]*(P[9][1] + P[6][1]*dt) + SF[9]*(P[9][2] + P[6][2]*dt) + SF[8]*(P[9][3] + P[6][3]*dt) + SF[11]*(P[9][10] + P[6][10]*dt) + SPP[7]*(P[9][11] + P[6][11]*dt) + SPP[6]*(P[9][12] + P[6][12]*dt); + nextP[9][1] = P[9][1] + P[6][1]*dt + SF[6]*(P[9][0] + P[6][0]*dt) + SF[5]*(P[9][2] + P[6][2]*dt) + SF[9]*(P[9][3] + P[6][3]*dt) + SPP[6]*(P[9][11] + P[6][11]*dt) - SPP[7]*(P[9][12] + P[6][12]*dt) - (q0*(P[9][10] + P[6][10]*dt))/2; + nextP[9][2] = P[9][2] + P[6][2]*dt + SF[4]*(P[9][0] + P[6][0]*dt) + SF[8]*(P[9][1] + P[6][1]*dt) + SF[6]*(P[9][3] + P[6][3]*dt) + SF[11]*(P[9][12] + P[6][12]*dt) - SPP[6]*(P[9][10] + P[6][10]*dt) - (q0*(P[9][11] + P[6][11]*dt))/2; + nextP[9][3] = P[9][3] + P[6][3]*dt + SF[5]*(P[9][0] + P[6][0]*dt) + SF[4]*(P[9][1] + P[6][1]*dt) + SF[7]*(P[9][2] + P[6][2]*dt) - SF[11]*(P[9][11] + P[6][11]*dt) + SPP[7]*(P[9][10] + P[6][10]*dt) - (q0*(P[9][12] + P[6][12]*dt))/2; + nextP[9][4] = P[9][4] + P[6][4]*dt + SF[1]*(P[9][1] + P[6][1]*dt) + SF[3]*(P[9][0] + P[6][0]*dt) + SPP[0]*(P[9][2] + P[6][2]*dt) - SPP[2]*(P[9][3] + P[6][3]*dt) - SPP[4]*(P[9][13] + P[6][13]*dt); + nextP[9][5] = P[9][5] + P[6][5]*dt + SF[2]*(P[9][0] + P[6][0]*dt) + SF[1]*(P[9][2] + P[6][2]*dt) + SF[3]*(P[9][3] + P[6][3]*dt) - SPP[0]*(P[9][1] + P[6][1]*dt) + SPP[3]*(P[9][13] + P[6][13]*dt); + nextP[9][6] = P[9][6] + P[6][6]*dt + SF[2]*(P[9][1] + P[6][1]*dt) + SF[1]*(P[9][3] + P[6][3]*dt) + SPP[0]*(P[9][0] + P[6][0]*dt) - SPP[1]*(P[9][2] + P[6][2]*dt) - SPP[5]*(P[9][13] + P[6][13]*dt); + nextP[9][7] = P[9][7] + P[6][7]*dt + dt*(P[9][4] + P[6][4]*dt); + nextP[9][8] = P[9][8] + P[6][8]*dt + dt*(P[9][5] + P[6][5]*dt); + nextP[9][9] = P[9][9] + P[6][9]*dt + dt*(P[9][6] + P[6][6]*dt); + nextP[9][10] = P[9][10] + P[6][10]*dt; + nextP[9][11] = P[9][11] + P[6][11]*dt; + nextP[9][12] = P[9][12] + P[6][12]*dt; + nextP[9][13] = P[9][13] + P[6][13]*dt; + nextP[9][14] = P[9][14] + P[6][14]*dt; + nextP[9][15] = P[9][15] + P[6][15]*dt; + nextP[9][16] = P[9][16] + P[6][16]*dt; + nextP[9][17] = P[9][17] + P[6][17]*dt; + nextP[9][18] = P[9][18] + P[6][18]*dt; + nextP[9][19] = P[9][19] + P[6][19]*dt; + nextP[9][20] = P[9][20] + P[6][20]*dt; + nextP[9][21] = P[9][21] + P[6][21]*dt; + nextP[9][22] = P[9][22] + P[6][22]*dt; + nextP[10][0] = P[10][0] + P[10][1]*SF[7] + P[10][2]*SF[9] + P[10][3]*SF[8] + P[10][10]*SF[11] + P[10][11]*SPP[7] + P[10][12]*SPP[6]; + nextP[10][1] = P[10][1] + P[10][0]*SF[6] + P[10][2]*SF[5] + P[10][3]*SF[9] + P[10][11]*SPP[6] - P[10][12]*SPP[7] - (P[10][10]*q0)/2; + nextP[10][2] = P[10][2] + P[10][0]*SF[4] + P[10][1]*SF[8] + P[10][3]*SF[6] + P[10][12]*SF[11] - P[10][10]*SPP[6] - (P[10][11]*q0)/2; + nextP[10][3] = P[10][3] + P[10][0]*SF[5] + P[10][1]*SF[4] + P[10][2]*SF[7] - P[10][11]*SF[11] + P[10][10]*SPP[7] - (P[10][12]*q0)/2; + nextP[10][4] = P[10][4] + P[10][1]*SF[1] + P[10][0]*SF[3] + P[10][2]*SPP[0] - P[10][3]*SPP[2] - P[10][13]*SPP[4]; + nextP[10][5] = P[10][5] + P[10][0]*SF[2] + P[10][2]*SF[1] + P[10][3]*SF[3] - P[10][1]*SPP[0] + P[10][13]*SPP[3]; + nextP[10][6] = P[10][6] + P[10][1]*SF[2] + P[10][3]*SF[1] + P[10][0]*SPP[0] - P[10][2]*SPP[1] - P[10][13]*SPP[5]; + nextP[10][7] = P[10][7] + P[10][4]*dt; + nextP[10][8] = P[10][8] + P[10][5]*dt; + nextP[10][9] = P[10][9] + P[10][6]*dt; + nextP[10][10] = P[10][10]; + nextP[10][11] = P[10][11]; + nextP[10][12] = P[10][12]; + nextP[10][13] = P[10][13]; + nextP[10][14] = P[10][14]; + nextP[10][15] = P[10][15]; + nextP[10][16] = P[10][16]; + nextP[10][17] = P[10][17]; + nextP[10][18] = P[10][18]; + nextP[10][19] = P[10][19]; + nextP[10][20] = P[10][20]; + nextP[10][21] = P[10][21]; + nextP[10][22] = P[10][22]; + nextP[11][0] = P[11][0] + P[11][1]*SF[7] + P[11][2]*SF[9] + P[11][3]*SF[8] + P[11][10]*SF[11] + P[11][11]*SPP[7] + P[11][12]*SPP[6]; + nextP[11][1] = P[11][1] + P[11][0]*SF[6] + P[11][2]*SF[5] + P[11][3]*SF[9] + P[11][11]*SPP[6] - P[11][12]*SPP[7] - (P[11][10]*q0)/2; + nextP[11][2] = P[11][2] + P[11][0]*SF[4] + P[11][1]*SF[8] + P[11][3]*SF[6] + P[11][12]*SF[11] - P[11][10]*SPP[6] - (P[11][11]*q0)/2; + nextP[11][3] = P[11][3] + P[11][0]*SF[5] + P[11][1]*SF[4] + P[11][2]*SF[7] - P[11][11]*SF[11] + P[11][10]*SPP[7] - (P[11][12]*q0)/2; + nextP[11][4] = P[11][4] + P[11][1]*SF[1] + P[11][0]*SF[3] + P[11][2]*SPP[0] - P[11][3]*SPP[2] - P[11][13]*SPP[4]; + nextP[11][5] = P[11][5] + P[11][0]*SF[2] + P[11][2]*SF[1] + P[11][3]*SF[3] - P[11][1]*SPP[0] + P[11][13]*SPP[3]; + nextP[11][6] = P[11][6] + P[11][1]*SF[2] + P[11][3]*SF[1] + P[11][0]*SPP[0] - P[11][2]*SPP[1] - P[11][13]*SPP[5]; + nextP[11][7] = P[11][7] + P[11][4]*dt; + nextP[11][8] = P[11][8] + P[11][5]*dt; + nextP[11][9] = P[11][9] + P[11][6]*dt; + nextP[11][10] = P[11][10]; + nextP[11][11] = P[11][11]; + nextP[11][12] = P[11][12]; + nextP[11][13] = P[11][13]; + nextP[11][14] = P[11][14]; + nextP[11][15] = P[11][15]; + nextP[11][16] = P[11][16]; + nextP[11][17] = P[11][17]; + nextP[11][18] = P[11][18]; + nextP[11][19] = P[11][19]; + nextP[11][20] = P[11][20]; + nextP[11][21] = P[11][21]; + nextP[11][22] = P[11][22]; + nextP[12][0] = P[12][0] + P[12][1]*SF[7] + P[12][2]*SF[9] + P[12][3]*SF[8] + P[12][10]*SF[11] + P[12][11]*SPP[7] + P[12][12]*SPP[6]; + nextP[12][1] = P[12][1] + P[12][0]*SF[6] + P[12][2]*SF[5] + P[12][3]*SF[9] + P[12][11]*SPP[6] - P[12][12]*SPP[7] - (P[12][10]*q0)/2; + nextP[12][2] = P[12][2] + P[12][0]*SF[4] + P[12][1]*SF[8] + P[12][3]*SF[6] + P[12][12]*SF[11] - P[12][10]*SPP[6] - (P[12][11]*q0)/2; + nextP[12][3] = P[12][3] + P[12][0]*SF[5] + P[12][1]*SF[4] + P[12][2]*SF[7] - P[12][11]*SF[11] + P[12][10]*SPP[7] - (P[12][12]*q0)/2; + nextP[12][4] = P[12][4] + P[12][1]*SF[1] + P[12][0]*SF[3] + P[12][2]*SPP[0] - P[12][3]*SPP[2] - P[12][13]*SPP[4]; + nextP[12][5] = P[12][5] + P[12][0]*SF[2] + P[12][2]*SF[1] + P[12][3]*SF[3] - P[12][1]*SPP[0] + P[12][13]*SPP[3]; + nextP[12][6] = P[12][6] + P[12][1]*SF[2] + P[12][3]*SF[1] + P[12][0]*SPP[0] - P[12][2]*SPP[1] - P[12][13]*SPP[5]; + nextP[12][7] = P[12][7] + P[12][4]*dt; + nextP[12][8] = P[12][8] + P[12][5]*dt; + nextP[12][9] = P[12][9] + P[12][6]*dt; + nextP[12][10] = P[12][10]; + nextP[12][11] = P[12][11]; + nextP[12][12] = P[12][12]; + nextP[12][13] = P[12][13]; + nextP[12][14] = P[12][14]; + nextP[12][15] = P[12][15]; + nextP[12][16] = P[12][16]; + nextP[12][17] = P[12][17]; + nextP[12][18] = P[12][18]; + nextP[12][19] = P[12][19]; + nextP[12][20] = P[12][20]; + nextP[12][21] = P[12][21]; + nextP[12][22] = P[12][22]; + nextP[13][0] = P[13][0] + P[13][1]*SF[7] + P[13][2]*SF[9] + P[13][3]*SF[8] + P[13][10]*SF[11] + P[13][11]*SPP[7] + P[13][12]*SPP[6]; + nextP[13][1] = P[13][1] + P[13][0]*SF[6] + P[13][2]*SF[5] + P[13][3]*SF[9] + P[13][11]*SPP[6] - P[13][12]*SPP[7] - (P[13][10]*q0)/2; + nextP[13][2] = P[13][2] + P[13][0]*SF[4] + P[13][1]*SF[8] + P[13][3]*SF[6] + P[13][12]*SF[11] - P[13][10]*SPP[6] - (P[13][11]*q0)/2; + nextP[13][3] = P[13][3] + P[13][0]*SF[5] + P[13][1]*SF[4] + P[13][2]*SF[7] - P[13][11]*SF[11] + P[13][10]*SPP[7] - (P[13][12]*q0)/2; + nextP[13][4] = P[13][4] + P[13][1]*SF[1] + P[13][0]*SF[3] + P[13][2]*SPP[0] - P[13][3]*SPP[2] - P[13][13]*SPP[4]; + nextP[13][5] = P[13][5] + P[13][0]*SF[2] + P[13][2]*SF[1] + P[13][3]*SF[3] - P[13][1]*SPP[0] + P[13][13]*SPP[3]; + nextP[13][6] = P[13][6] + P[13][1]*SF[2] + P[13][3]*SF[1] + P[13][0]*SPP[0] - P[13][2]*SPP[1] - P[13][13]*SPP[5]; + nextP[13][7] = P[13][7] + P[13][4]*dt; + nextP[13][8] = P[13][8] + P[13][5]*dt; + nextP[13][9] = P[13][9] + P[13][6]*dt; + nextP[13][10] = P[13][10]; + nextP[13][11] = P[13][11]; + nextP[13][12] = P[13][12]; + nextP[13][13] = P[13][13]; + nextP[13][14] = P[13][14]; + nextP[13][15] = P[13][15]; + nextP[13][16] = P[13][16]; + nextP[13][17] = P[13][17]; + nextP[13][18] = P[13][18]; + nextP[13][19] = P[13][19]; + nextP[13][20] = P[13][20]; + nextP[13][21] = P[13][21]; + nextP[13][22] = P[13][22]; + nextP[14][0] = P[14][0] + P[14][1]*SF[7] + P[14][2]*SF[9] + P[14][3]*SF[8] + P[14][10]*SF[11] + P[14][11]*SPP[7] + P[14][12]*SPP[6]; + nextP[14][1] = P[14][1] + P[14][0]*SF[6] + P[14][2]*SF[5] + P[14][3]*SF[9] + P[14][11]*SPP[6] - P[14][12]*SPP[7] - (P[14][10]*q0)/2; + nextP[14][2] = P[14][2] + P[14][0]*SF[4] + P[14][1]*SF[8] + P[14][3]*SF[6] + P[14][12]*SF[11] - P[14][10]*SPP[6] - (P[14][11]*q0)/2; + nextP[14][3] = P[14][3] + P[14][0]*SF[5] + P[14][1]*SF[4] + P[14][2]*SF[7] - P[14][11]*SF[11] + P[14][10]*SPP[7] - (P[14][12]*q0)/2; + nextP[14][4] = P[14][4] + P[14][1]*SF[1] + P[14][0]*SF[3] + P[14][2]*SPP[0] - P[14][3]*SPP[2] - P[14][13]*SPP[4]; + nextP[14][5] = P[14][5] + P[14][0]*SF[2] + P[14][2]*SF[1] + P[14][3]*SF[3] - P[14][1]*SPP[0] + P[14][13]*SPP[3]; + nextP[14][6] = P[14][6] + P[14][1]*SF[2] + P[14][3]*SF[1] + P[14][0]*SPP[0] - P[14][2]*SPP[1] - P[14][13]*SPP[5]; + nextP[14][7] = P[14][7] + P[14][4]*dt; + nextP[14][8] = P[14][8] + P[14][5]*dt; + nextP[14][9] = P[14][9] + P[14][6]*dt; + nextP[14][10] = P[14][10]; + nextP[14][11] = P[14][11]; + nextP[14][12] = P[14][12]; + nextP[14][13] = P[14][13]; + nextP[14][14] = P[14][14]; + nextP[14][15] = P[14][15]; + nextP[14][16] = P[14][16]; + nextP[14][17] = P[14][17]; + nextP[14][18] = P[14][18]; + nextP[14][19] = P[14][19]; + nextP[14][20] = P[14][20]; + nextP[14][21] = P[14][21]; + nextP[14][22] = P[14][22]; + nextP[15][0] = P[15][0] + P[15][1]*SF[7] + P[15][2]*SF[9] + P[15][3]*SF[8] + P[15][10]*SF[11] + P[15][11]*SPP[7] + P[15][12]*SPP[6]; + nextP[15][1] = P[15][1] + P[15][0]*SF[6] + P[15][2]*SF[5] + P[15][3]*SF[9] + P[15][11]*SPP[6] - P[15][12]*SPP[7] - (P[15][10]*q0)/2; + nextP[15][2] = P[15][2] + P[15][0]*SF[4] + P[15][1]*SF[8] + P[15][3]*SF[6] + P[15][12]*SF[11] - P[15][10]*SPP[6] - (P[15][11]*q0)/2; + nextP[15][3] = P[15][3] + P[15][0]*SF[5] + P[15][1]*SF[4] + P[15][2]*SF[7] - P[15][11]*SF[11] + P[15][10]*SPP[7] - (P[15][12]*q0)/2; + nextP[15][4] = P[15][4] + P[15][1]*SF[1] + P[15][0]*SF[3] + P[15][2]*SPP[0] - P[15][3]*SPP[2] - P[15][13]*SPP[4]; + nextP[15][5] = P[15][5] + P[15][0]*SF[2] + P[15][2]*SF[1] + P[15][3]*SF[3] - P[15][1]*SPP[0] + P[15][13]*SPP[3]; + nextP[15][6] = P[15][6] + P[15][1]*SF[2] + P[15][3]*SF[1] + P[15][0]*SPP[0] - P[15][2]*SPP[1] - P[15][13]*SPP[5]; + nextP[15][7] = P[15][7] + P[15][4]*dt; + nextP[15][8] = P[15][8] + P[15][5]*dt; + nextP[15][9] = P[15][9] + P[15][6]*dt; + nextP[15][10] = P[15][10]; + nextP[15][11] = P[15][11]; + nextP[15][12] = P[15][12]; + nextP[15][13] = P[15][13]; + nextP[15][14] = P[15][14]; + nextP[15][15] = P[15][15]; + nextP[15][16] = P[15][16]; + nextP[15][17] = P[15][17]; + nextP[15][18] = P[15][18]; + nextP[15][19] = P[15][19]; + nextP[15][20] = P[15][20]; + nextP[15][21] = P[15][21]; + nextP[15][22] = P[15][22]; + nextP[16][0] = P[16][0] + P[16][1]*SF[7] + P[16][2]*SF[9] + P[16][3]*SF[8] + P[16][10]*SF[11] + P[16][11]*SPP[7] + P[16][12]*SPP[6]; + nextP[16][1] = P[16][1] + P[16][0]*SF[6] + P[16][2]*SF[5] + P[16][3]*SF[9] + P[16][11]*SPP[6] - P[16][12]*SPP[7] - (P[16][10]*q0)/2; + nextP[16][2] = P[16][2] + P[16][0]*SF[4] + P[16][1]*SF[8] + P[16][3]*SF[6] + P[16][12]*SF[11] - P[16][10]*SPP[6] - (P[16][11]*q0)/2; + nextP[16][3] = P[16][3] + P[16][0]*SF[5] + P[16][1]*SF[4] + P[16][2]*SF[7] - P[16][11]*SF[11] + P[16][10]*SPP[7] - (P[16][12]*q0)/2; + nextP[16][4] = P[16][4] + P[16][1]*SF[1] + P[16][0]*SF[3] + P[16][2]*SPP[0] - P[16][3]*SPP[2] - P[16][13]*SPP[4]; + nextP[16][5] = P[16][5] + P[16][0]*SF[2] + P[16][2]*SF[1] + P[16][3]*SF[3] - P[16][1]*SPP[0] + P[16][13]*SPP[3]; + nextP[16][6] = P[16][6] + P[16][1]*SF[2] + P[16][3]*SF[1] + P[16][0]*SPP[0] - P[16][2]*SPP[1] - P[16][13]*SPP[5]; + nextP[16][7] = P[16][7] + P[16][4]*dt; + nextP[16][8] = P[16][8] + P[16][5]*dt; + nextP[16][9] = P[16][9] + P[16][6]*dt; + nextP[16][10] = P[16][10]; + nextP[16][11] = P[16][11]; + nextP[16][12] = P[16][12]; + nextP[16][13] = P[16][13]; + nextP[16][14] = P[16][14]; + nextP[16][15] = P[16][15]; + nextP[16][16] = P[16][16]; + nextP[16][17] = P[16][17]; + nextP[16][18] = P[16][18]; + nextP[16][19] = P[16][19]; + nextP[16][20] = P[16][20]; + nextP[16][21] = P[16][21]; + nextP[16][22] = P[16][22]; + nextP[17][0] = P[17][0] + P[17][1]*SF[7] + P[17][2]*SF[9] + P[17][3]*SF[8] + P[17][10]*SF[11] + P[17][11]*SPP[7] + P[17][12]*SPP[6]; + nextP[17][1] = P[17][1] + P[17][0]*SF[6] + P[17][2]*SF[5] + P[17][3]*SF[9] + P[17][11]*SPP[6] - P[17][12]*SPP[7] - (P[17][10]*q0)/2; + nextP[17][2] = P[17][2] + P[17][0]*SF[4] + P[17][1]*SF[8] + P[17][3]*SF[6] + P[17][12]*SF[11] - P[17][10]*SPP[6] - (P[17][11]*q0)/2; + nextP[17][3] = P[17][3] + P[17][0]*SF[5] + P[17][1]*SF[4] + P[17][2]*SF[7] - P[17][11]*SF[11] + P[17][10]*SPP[7] - (P[17][12]*q0)/2; + nextP[17][4] = P[17][4] + P[17][1]*SF[1] + P[17][0]*SF[3] + P[17][2]*SPP[0] - P[17][3]*SPP[2] - P[17][13]*SPP[4]; + nextP[17][5] = P[17][5] + P[17][0]*SF[2] + P[17][2]*SF[1] + P[17][3]*SF[3] - P[17][1]*SPP[0] + P[17][13]*SPP[3]; + nextP[17][6] = P[17][6] + P[17][1]*SF[2] + P[17][3]*SF[1] + P[17][0]*SPP[0] - P[17][2]*SPP[1] - P[17][13]*SPP[5]; + nextP[17][7] = P[17][7] + P[17][4]*dt; + nextP[17][8] = P[17][8] + P[17][5]*dt; + nextP[17][9] = P[17][9] + P[17][6]*dt; + nextP[17][10] = P[17][10]; + nextP[17][11] = P[17][11]; + nextP[17][12] = P[17][12]; + nextP[17][13] = P[17][13]; + nextP[17][14] = P[17][14]; + nextP[17][15] = P[17][15]; + nextP[17][16] = P[17][16]; + nextP[17][17] = P[17][17]; + nextP[17][18] = P[17][18]; + nextP[17][19] = P[17][19]; + nextP[17][20] = P[17][20]; + nextP[17][21] = P[17][21]; + nextP[17][22] = P[17][22]; + nextP[18][0] = P[18][0] + P[18][1]*SF[7] + P[18][2]*SF[9] + P[18][3]*SF[8] + P[18][10]*SF[11] + P[18][11]*SPP[7] + P[18][12]*SPP[6]; + nextP[18][1] = P[18][1] + P[18][0]*SF[6] + P[18][2]*SF[5] + P[18][3]*SF[9] + P[18][11]*SPP[6] - P[18][12]*SPP[7] - (P[18][10]*q0)/2; + nextP[18][2] = P[18][2] + P[18][0]*SF[4] + P[18][1]*SF[8] + P[18][3]*SF[6] + P[18][12]*SF[11] - P[18][10]*SPP[6] - (P[18][11]*q0)/2; + nextP[18][3] = P[18][3] + P[18][0]*SF[5] + P[18][1]*SF[4] + P[18][2]*SF[7] - P[18][11]*SF[11] + P[18][10]*SPP[7] - (P[18][12]*q0)/2; + nextP[18][4] = P[18][4] + P[18][1]*SF[1] + P[18][0]*SF[3] + P[18][2]*SPP[0] - P[18][3]*SPP[2] - P[18][13]*SPP[4]; + nextP[18][5] = P[18][5] + P[18][0]*SF[2] + P[18][2]*SF[1] + P[18][3]*SF[3] - P[18][1]*SPP[0] + P[18][13]*SPP[3]; + nextP[18][6] = P[18][6] + P[18][1]*SF[2] + P[18][3]*SF[1] + P[18][0]*SPP[0] - P[18][2]*SPP[1] - P[18][13]*SPP[5]; + nextP[18][7] = P[18][7] + P[18][4]*dt; + nextP[18][8] = P[18][8] + P[18][5]*dt; + nextP[18][9] = P[18][9] + P[18][6]*dt; + nextP[18][10] = P[18][10]; + nextP[18][11] = P[18][11]; + nextP[18][12] = P[18][12]; + nextP[18][13] = P[18][13]; + nextP[18][14] = P[18][14]; + nextP[18][15] = P[18][15]; + nextP[18][16] = P[18][16]; + nextP[18][17] = P[18][17]; + nextP[18][18] = P[18][18]; + nextP[18][19] = P[18][19]; + nextP[18][20] = P[18][20]; + nextP[18][21] = P[18][21]; + nextP[18][22] = P[18][22]; + nextP[19][0] = P[19][0] + P[19][1]*SF[7] + P[19][2]*SF[9] + P[19][3]*SF[8] + P[19][10]*SF[11] + P[19][11]*SPP[7] + P[19][12]*SPP[6]; + nextP[19][1] = P[19][1] + P[19][0]*SF[6] + P[19][2]*SF[5] + P[19][3]*SF[9] + P[19][11]*SPP[6] - P[19][12]*SPP[7] - (P[19][10]*q0)/2; + nextP[19][2] = P[19][2] + P[19][0]*SF[4] + P[19][1]*SF[8] + P[19][3]*SF[6] + P[19][12]*SF[11] - P[19][10]*SPP[6] - (P[19][11]*q0)/2; + nextP[19][3] = P[19][3] + P[19][0]*SF[5] + P[19][1]*SF[4] + P[19][2]*SF[7] - P[19][11]*SF[11] + P[19][10]*SPP[7] - (P[19][12]*q0)/2; + nextP[19][4] = P[19][4] + P[19][1]*SF[1] + P[19][0]*SF[3] + P[19][2]*SPP[0] - P[19][3]*SPP[2] - P[19][13]*SPP[4]; + nextP[19][5] = P[19][5] + P[19][0]*SF[2] + P[19][2]*SF[1] + P[19][3]*SF[3] - P[19][1]*SPP[0] + P[19][13]*SPP[3]; + nextP[19][6] = P[19][6] + P[19][1]*SF[2] + P[19][3]*SF[1] + P[19][0]*SPP[0] - P[19][2]*SPP[1] - P[19][13]*SPP[5]; + nextP[19][7] = P[19][7] + P[19][4]*dt; + nextP[19][8] = P[19][8] + P[19][5]*dt; + nextP[19][9] = P[19][9] + P[19][6]*dt; + nextP[19][10] = P[19][10]; + nextP[19][11] = P[19][11]; + nextP[19][12] = P[19][12]; + nextP[19][13] = P[19][13]; + nextP[19][14] = P[19][14]; + nextP[19][15] = P[19][15]; + nextP[19][16] = P[19][16]; + nextP[19][17] = P[19][17]; + nextP[19][18] = P[19][18]; + nextP[19][19] = P[19][19]; + nextP[19][20] = P[19][20]; + nextP[19][21] = P[19][21]; + nextP[19][22] = P[19][22]; + nextP[20][0] = P[20][0] + P[20][1]*SF[7] + P[20][2]*SF[9] + P[20][3]*SF[8] + P[20][10]*SF[11] + P[20][11]*SPP[7] + P[20][12]*SPP[6]; + nextP[20][1] = P[20][1] + P[20][0]*SF[6] + P[20][2]*SF[5] + P[20][3]*SF[9] + P[20][11]*SPP[6] - P[20][12]*SPP[7] - (P[20][10]*q0)/2; + nextP[20][2] = P[20][2] + P[20][0]*SF[4] + P[20][1]*SF[8] + P[20][3]*SF[6] + P[20][12]*SF[11] - P[20][10]*SPP[6] - (P[20][11]*q0)/2; + nextP[20][3] = P[20][3] + P[20][0]*SF[5] + P[20][1]*SF[4] + P[20][2]*SF[7] - P[20][11]*SF[11] + P[20][10]*SPP[7] - (P[20][12]*q0)/2; + nextP[20][4] = P[20][4] + P[20][1]*SF[1] + P[20][0]*SF[3] + P[20][2]*SPP[0] - P[20][3]*SPP[2] - P[20][13]*SPP[4]; + nextP[20][5] = P[20][5] + P[20][0]*SF[2] + P[20][2]*SF[1] + P[20][3]*SF[3] - P[20][1]*SPP[0] + P[20][13]*SPP[3]; + nextP[20][6] = P[20][6] + P[20][1]*SF[2] + P[20][3]*SF[1] + P[20][0]*SPP[0] - P[20][2]*SPP[1] - P[20][13]*SPP[5]; + nextP[20][7] = P[20][7] + P[20][4]*dt; + nextP[20][8] = P[20][8] + P[20][5]*dt; + nextP[20][9] = P[20][9] + P[20][6]*dt; + nextP[20][10] = P[20][10]; + nextP[20][11] = P[20][11]; + nextP[20][12] = P[20][12]; + nextP[20][13] = P[20][13]; + nextP[20][14] = P[20][14]; + nextP[20][15] = P[20][15]; + nextP[20][16] = P[20][16]; + nextP[20][17] = P[20][17]; + nextP[20][18] = P[20][18]; + nextP[20][19] = P[20][19]; + nextP[20][20] = P[20][20]; + nextP[20][21] = P[20][21]; + nextP[20][22] = P[20][22]; + nextP[21][0] = P[21][0] + P[21][1]*SF[7] + P[21][2]*SF[9] + P[21][3]*SF[8] + P[21][10]*SF[11] + P[21][11]*SPP[7] + P[21][12]*SPP[6]; + nextP[21][1] = P[21][1] + P[21][0]*SF[6] + P[21][2]*SF[5] + P[21][3]*SF[9] + P[21][11]*SPP[6] - P[21][12]*SPP[7] - (P[21][10]*q0)/2; + nextP[21][2] = P[21][2] + P[21][0]*SF[4] + P[21][1]*SF[8] + P[21][3]*SF[6] + P[21][12]*SF[11] - P[21][10]*SPP[6] - (P[21][11]*q0)/2; + nextP[21][3] = P[21][3] + P[21][0]*SF[5] + P[21][1]*SF[4] + P[21][2]*SF[7] - P[21][11]*SF[11] + P[21][10]*SPP[7] - (P[21][12]*q0)/2; + nextP[21][4] = P[21][4] + P[21][1]*SF[1] + P[21][0]*SF[3] + P[21][2]*SPP[0] - P[21][3]*SPP[2] - P[21][13]*SPP[4]; + nextP[21][5] = P[21][5] + P[21][0]*SF[2] + P[21][2]*SF[1] + P[21][3]*SF[3] - P[21][1]*SPP[0] + P[21][13]*SPP[3]; + nextP[21][6] = P[21][6] + P[21][1]*SF[2] + P[21][3]*SF[1] + P[21][0]*SPP[0] - P[21][2]*SPP[1] - P[21][13]*SPP[5]; + nextP[21][7] = P[21][7] + P[21][4]*dt; + nextP[21][8] = P[21][8] + P[21][5]*dt; + nextP[21][9] = P[21][9] + P[21][6]*dt; + nextP[21][10] = P[21][10]; + nextP[21][11] = P[21][11]; + nextP[21][12] = P[21][12]; + nextP[21][13] = P[21][13]; + nextP[21][14] = P[21][14]; + nextP[21][15] = P[21][15]; + nextP[21][16] = P[21][16]; + nextP[21][17] = P[21][17]; + nextP[21][18] = P[21][18]; + nextP[21][19] = P[21][19]; + nextP[21][20] = P[21][20]; + nextP[21][21] = P[21][21]; + nextP[21][22] = P[21][22]; + nextP[22][0] = P[22][0] + P[22][1]*SF[7] + P[22][2]*SF[9] + P[22][3]*SF[8] + P[22][10]*SF[11] + P[22][11]*SPP[7] + P[22][12]*SPP[6]; + nextP[22][1] = P[22][1] + P[22][0]*SF[6] + P[22][2]*SF[5] + P[22][3]*SF[9] + P[22][11]*SPP[6] - P[22][12]*SPP[7] - (P[22][10]*q0)/2; + nextP[22][2] = P[22][2] + P[22][0]*SF[4] + P[22][1]*SF[8] + P[22][3]*SF[6] + P[22][12]*SF[11] - P[22][10]*SPP[6] - (P[22][11]*q0)/2; + nextP[22][3] = P[22][3] + P[22][0]*SF[5] + P[22][1]*SF[4] + P[22][2]*SF[7] - P[22][11]*SF[11] + P[22][10]*SPP[7] - (P[22][12]*q0)/2; + nextP[22][4] = P[22][4] + P[22][1]*SF[1] + P[22][0]*SF[3] + P[22][2]*SPP[0] - P[22][3]*SPP[2] - P[22][13]*SPP[4]; + nextP[22][5] = P[22][5] + P[22][0]*SF[2] + P[22][2]*SF[1] + P[22][3]*SF[3] - P[22][1]*SPP[0] + P[22][13]*SPP[3]; + nextP[22][6] = P[22][6] + P[22][1]*SF[2] + P[22][3]*SF[1] + P[22][0]*SPP[0] - P[22][2]*SPP[1] - P[22][13]*SPP[5]; + nextP[22][7] = P[22][7] + P[22][4]*dt; + nextP[22][8] = P[22][8] + P[22][5]*dt; + nextP[22][9] = P[22][9] + P[22][6]*dt; + nextP[22][10] = P[22][10]; + nextP[22][11] = P[22][11]; + nextP[22][12] = P[22][12]; + nextP[22][13] = P[22][13]; + nextP[22][14] = P[22][14]; + nextP[22][15] = P[22][15]; + nextP[22][16] = P[22][16]; + nextP[22][17] = P[22][17]; + nextP[22][18] = P[22][18]; + nextP[22][19] = P[22][19]; + nextP[22][20] = P[22][20]; + nextP[22][21] = P[22][21]; + nextP[22][22] = P[22][22]; + + for (unsigned i = 0; i < n_states; i++) + { + nextP[i][i] = nextP[i][i] + processNoise[i]; + } + + // If on ground or no magnetometer fitted, inhibit magnetometer bias updates by + // setting the coresponding covariance terms to zero. + if (onGround || !useCompass) + { + zeroRows(nextP,16,21); + zeroCols(nextP,16,21); + } + + // If on ground or not using airspeed sensing, inhibit wind velocity + // covariance growth. + if (onGround || !useAirspeed) + { + zeroRows(nextP,14,15); + zeroCols(nextP,14,15); + } + + // If on ground, inhibit terrain offset updates by + // setting the coresponding covariance terms to zero. + if (onGround) + { + zeroRows(nextP,22,22); + zeroCols(nextP,22,22); + } + + // If the total position variance exceds 1E6 (1000m), then stop covariance + // growth by setting the predicted to the previous values + // This prevent an ill conditioned matrix from occurring for long periods + // without GPS + if ((P[7][7] + P[8][8]) > 1E6f) + { + for (uint8_t i=7; i<=8; i++) + { + for (unsigned j = 0; j < n_states; j++) + { + nextP[i][j] = P[i][j]; + nextP[j][i] = P[j][i]; + } + } + } + + if (onGround || staticMode) { + // copy the portion of the variances we want to + // propagate + for (unsigned i = 0; i <= 13; i++) { + P[i][i] = nextP[i][i]; + + // force symmetry for observable states + // force zero for non-observable states + for (unsigned i = 1; i < n_states; i++) + { + for (uint8_t j = 0; j < i; j++) + { + if ((i > 13) || (j > 13)) { + P[i][j] = 0.0f; + } else { + P[i][j] = 0.5f * (nextP[i][j] + nextP[j][i]); + } + P[j][i] = P[i][j]; + } + } + } + + } else { + + // Copy covariance + for (unsigned i = 0; i < n_states; i++) { + P[i][i] = nextP[i][i]; + } + + // force symmetry for observable states + for (unsigned i = 1; i < n_states; i++) + { + for (uint8_t j = 0; j < i; j++) + { + P[i][j] = 0.5f * (nextP[i][j] + nextP[j][i]); + P[j][i] = P[i][j]; + } + } + + } + + ConstrainVariances(); +} + +void AttPosEKF::FuseVelposNED() +{ + +// declare variables used by fault isolation logic + uint32_t gpsRetryTime = 30000; // time in msec before GPS fusion will be retried following innovation consistency failure + uint32_t gpsRetryTimeNoTAS = 5000; // retry time if no TAS measurement available + uint32_t hgtRetryTime = 5000; // height measurement retry time + uint32_t horizRetryTime; + +// declare variables used to check measurement errors + float velInnov[3] = {0.0f,0.0f,0.0f}; + float posInnov[2] = {0.0f,0.0f}; + float hgtInnov = 0.0f; + +// declare variables used to control access to arrays + bool fuseData[6] = {false,false,false,false,false,false}; + uint8_t stateIndex; + uint8_t obsIndex; + uint8_t indexLimit; + +// declare variables used by state and covariance update calculations + float velErr; + float posErr; + float R_OBS[6]; + float observation[6]; + float SK; + float quatMag; + +// Perform sequential fusion of GPS measurements. This assumes that the +// errors in the different velocity and position components are +// uncorrelated which is not true, however in the absence of covariance +// data from the GPS receiver it is the only assumption we can make +// so we might as well take advantage of the computational efficiencies +// associated with sequential fusion + if (fuseVelData || fusePosData || fuseHgtData) + { + // set the GPS data timeout depending on whether airspeed data is present + if (useAirspeed) horizRetryTime = gpsRetryTime; + else horizRetryTime = gpsRetryTimeNoTAS; + + // Form the observation vector + for (uint8_t i=0; i<=2; i++) observation[i] = velNED[i]; + for (uint8_t i=3; i<=4; i++) observation[i] = posNE[i-3]; + observation[5] = -(hgtMea); + + // Estimate the GPS Velocity, GPS horiz position and height measurement variances. + velErr = 0.2f*accNavMag; // additional error in GPS velocities caused by manoeuvring + posErr = 0.2f*accNavMag; // additional error in GPS position caused by manoeuvring + R_OBS[0] = sq(vneSigma) + sq(velErr); + R_OBS[1] = R_OBS[0]; + R_OBS[2] = sq(vdSigma) + sq(velErr); + R_OBS[3] = sq(posNeSigma) + sq(posErr); + R_OBS[4] = R_OBS[3]; + R_OBS[5] = sq(posDSigma) + sq(posErr); + + // Set innovation variances to zero default + for (uint8_t i = 0; i<=5; i++) + { + varInnovVelPos[i] = 0.0f; + } + // calculate innovations and check GPS data validity using an innovation consistency check + if (fuseVelData) + { + // test velocity measurements + uint8_t imax = 2; + if (fusionModeGPS == 1) imax = 1; + for (uint8_t i = 0; i<=imax; i++) + { + velInnov[i] = statesAtVelTime[i+4] - velNED[i]; + stateIndex = 4 + i; + varInnovVelPos[i] = P[stateIndex][stateIndex] + R_OBS[i]; + } + // apply a 5-sigma threshold + current_ekf_state.velHealth = (sq(velInnov[0]) + sq(velInnov[1]) + sq(velInnov[2])) < 25.0f * (varInnovVelPos[0] + varInnovVelPos[1] + varInnovVelPos[2]); + current_ekf_state.velTimeout = (millis() - current_ekf_state.velFailTime) > horizRetryTime; + if (current_ekf_state.velHealth || current_ekf_state.velTimeout) + { + current_ekf_state.velHealth = true; + current_ekf_state.velFailTime = millis(); + } + else + { + current_ekf_state.velHealth = false; + } + } + if (fusePosData) + { + // test horizontal position measurements + posInnov[0] = statesAtPosTime[7] - posNE[0]; + posInnov[1] = statesAtPosTime[8] - posNE[1]; + varInnovVelPos[3] = P[7][7] + R_OBS[3]; + varInnovVelPos[4] = P[8][8] + R_OBS[4]; + // apply a 10-sigma threshold + current_ekf_state.posHealth = (sq(posInnov[0]) + sq(posInnov[1])) < 100.0f*(varInnovVelPos[3] + varInnovVelPos[4]); + current_ekf_state.posTimeout = (millis() - current_ekf_state.posFailTime) > horizRetryTime; + if (current_ekf_state.posHealth || current_ekf_state.posTimeout) + { + current_ekf_state.posHealth = true; + current_ekf_state.posFailTime = millis(); + } + else + { + current_ekf_state.posHealth = false; + } + } + // test height measurements + if (fuseHgtData) + { + hgtInnov = statesAtHgtTime[9] + hgtMea; + varInnovVelPos[5] = P[9][9] + R_OBS[5]; + // apply a 10-sigma threshold + current_ekf_state.hgtHealth = sq(hgtInnov) < 100.0f*varInnovVelPos[5]; + current_ekf_state.hgtTimeout = (millis() - current_ekf_state.hgtFailTime) > hgtRetryTime; + if (current_ekf_state.hgtHealth || current_ekf_state.hgtTimeout) + { + current_ekf_state.hgtHealth = true; + current_ekf_state.hgtFailTime = millis(); + } + else + { + current_ekf_state.hgtHealth = false; + } + } + // Set range for sequential fusion of velocity and position measurements depending + // on which data is available and its health + if (fuseVelData && fusionModeGPS == 0 && current_ekf_state.velHealth) + { + fuseData[0] = true; + fuseData[1] = true; + fuseData[2] = true; + } + if (fuseVelData && fusionModeGPS == 1 && current_ekf_state.velHealth) + { + fuseData[0] = true; + fuseData[1] = true; + } + if (fusePosData && fusionModeGPS <= 2 && current_ekf_state.posHealth) + { + fuseData[3] = true; + fuseData[4] = true; + } + if (fuseHgtData && current_ekf_state.hgtHealth) + { + fuseData[5] = true; + } + // Limit range of states modified when on ground + if(!onGround) + { + indexLimit = 22; + } + else + { + indexLimit = 13; + } + // Fuse measurements sequentially + for (obsIndex=0; obsIndex<=5; obsIndex++) + { + if (fuseData[obsIndex]) + { + stateIndex = 4 + obsIndex; + // Calculate the measurement innovation, using states from a + // different time coordinate if fusing height data + if (obsIndex >= 0 && obsIndex <= 2) + { + innovVelPos[obsIndex] = statesAtVelTime[stateIndex] - observation[obsIndex]; + } + else if (obsIndex == 3 || obsIndex == 4) + { + innovVelPos[obsIndex] = statesAtPosTime[stateIndex] - observation[obsIndex]; + } + else if (obsIndex == 5) + { + innovVelPos[obsIndex] = statesAtHgtTime[stateIndex] - observation[obsIndex]; + } + // Calculate the Kalman Gain + // Calculate innovation variances - also used for data logging + varInnovVelPos[obsIndex] = P[stateIndex][stateIndex] + R_OBS[obsIndex]; + SK = 1.0/varInnovVelPos[obsIndex]; + for (uint8_t i= 0; i<=indexLimit; i++) + { + Kfusion[i] = P[i][stateIndex]*SK; + } + + // Don't update Z accel bias state unless using a height observation (GPS velocities can be biased) + if (obsIndex != 5) { + Kfusion[13] = 0; + } + + // Calculate state corrections and re-normalise the quaternions + for (uint8_t i = 0; i<=indexLimit; i++) + { + states[i] = states[i] - Kfusion[i] * innovVelPos[obsIndex]; + } + quatMag = sqrt(states[0]*states[0] + states[1]*states[1] + states[2]*states[2] + states[3]*states[3]); + if (quatMag > 1e-12f) // divide by 0 protection + { + for (uint8_t i = 0; i<=3; i++) + { + states[i] = states[i] / quatMag; + } + } + // Update the covariance - take advantage of direct observation of a + // single state at index = stateIndex to reduce computations + // Optimised implementation of standard equation P = (I - K*H)*P; + for (uint8_t i= 0; i<=indexLimit; i++) + { + for (uint8_t j= 0; j<=indexLimit; j++) + { + KHP[i][j] = Kfusion[i] * P[stateIndex][j]; + } + } + for (uint8_t i= 0; i<=indexLimit; i++) + { + for (uint8_t j= 0; j<=indexLimit; j++) + { + P[i][j] = P[i][j] - KHP[i][j]; + } + } + } + } + } + + ForceSymmetry(); + ConstrainVariances(); + +} + +void AttPosEKF::FuseMagnetometer() +{ + + float &q0 = magstate.q0; + float &q1 = magstate.q1; + float &q2 = magstate.q2; + float &q3 = magstate.q3; + float &magN = magstate.magN; + float &magE = magstate.magE; + float &magD = magstate.magD; + float &magXbias = magstate.magXbias; + float &magYbias = magstate.magYbias; + float &magZbias = magstate.magZbias; + unsigned &obsIndex = magstate.obsIndex; + Mat3f &DCM = magstate.DCM; + float *MagPred = &magstate.MagPred[0]; + float &R_MAG = magstate.R_MAG; + float *SH_MAG = &magstate.SH_MAG[0]; + + float SK_MX[6]; + float SK_MY[5]; + float SK_MZ[6]; + float H_MAG[n_states]; + for (uint8_t i = 0; i < n_states; i++) { + H_MAG[i] = 0.0f; + } + unsigned indexLimit; + +// Perform sequential fusion of Magnetometer measurements. +// This assumes that the errors in the different components are +// uncorrelated which is not true, however in the absence of covariance +// data fit is the only assumption we can make +// so we might as well take advantage of the computational efficiencies +// associated with sequential fusion + if (useCompass && (fuseMagData || obsIndex == 1 || obsIndex == 2)) + { + // Limit range of states modified when on ground + if(!onGround) + { + indexLimit = n_states; + } + else + { + indexLimit = 13 + 1; + } + + // Sequential fusion of XYZ components to spread processing load across + // three prediction time steps. + + // Calculate observation jacobians and Kalman gains + if (fuseMagData) + { + // Copy required states to local variable names + q0 = statesAtMagMeasTime[0]; + q1 = statesAtMagMeasTime[1]; + q2 = statesAtMagMeasTime[2]; + q3 = statesAtMagMeasTime[3]; + magN = statesAtMagMeasTime[16]; + magE = statesAtMagMeasTime[17]; + magD = statesAtMagMeasTime[18]; + magXbias = statesAtMagMeasTime[19]; + magYbias = statesAtMagMeasTime[20]; + magZbias = statesAtMagMeasTime[21]; + + // rotate predicted earth components into body axes and calculate + // predicted measurments + DCM.x.x = q0*q0 + q1*q1 - q2*q2 - q3*q3; + DCM.x.y = 2*(q1*q2 + q0*q3); + DCM.x.z = 2*(q1*q3-q0*q2); + DCM.y.x = 2*(q1*q2 - q0*q3); + DCM.y.y = q0*q0 - q1*q1 + q2*q2 - q3*q3; + DCM.y.z = 2*(q2*q3 + q0*q1); + DCM.z.x = 2*(q1*q3 + q0*q2); + DCM.z.y = 2*(q2*q3 - q0*q1); + DCM.z.z = q0*q0 - q1*q1 - q2*q2 + q3*q3; + MagPred[0] = DCM.x.x*magN + DCM.x.y*magE + DCM.x.z*magD + magXbias; + MagPred[1] = DCM.y.x*magN + DCM.y.y*magE + DCM.y.z*magD + magYbias; + MagPred[2] = DCM.z.x*magN + DCM.z.y*magE + DCM.z.z*magD + magZbias; + + // scale magnetometer observation error with total angular rate + R_MAG = sq(magMeasurementSigma) + sq(0.05f*dAngIMU.length()/dtIMU); + + // Calculate observation jacobians + SH_MAG[0] = 2*magD*q3 + 2*magE*q2 + 2*magN*q1; + SH_MAG[1] = 2*magD*q0 - 2*magE*q1 + 2*magN*q2; + SH_MAG[2] = 2*magD*q1 + 2*magE*q0 - 2*magN*q3; + SH_MAG[3] = sq(q3); + SH_MAG[4] = sq(q2); + SH_MAG[5] = sq(q1); + SH_MAG[6] = sq(q0); + SH_MAG[7] = 2*magN*q0; + SH_MAG[8] = 2*magE*q3; + + for (uint8_t i = 0; i < n_states; i++) H_MAG[i] = 0; + H_MAG[0] = SH_MAG[7] + SH_MAG[8] - 2*magD*q2; + H_MAG[1] = SH_MAG[0]; + H_MAG[2] = 2*magE*q1 - 2*magD*q0 - 2*magN*q2; + H_MAG[3] = SH_MAG[2]; + H_MAG[16] = SH_MAG[5] - SH_MAG[4] - SH_MAG[3] + SH_MAG[6]; + H_MAG[17] = 2*q0*q3 + 2*q1*q2; + H_MAG[18] = 2*q1*q3 - 2*q0*q2; + H_MAG[19] = 1.0f; + + // Calculate Kalman gain + float temp = (P[19][19] + R_MAG + P[1][19]*SH_MAG[0] + P[3][19]*SH_MAG[2] - P[16][19]*(SH_MAG[3] + SH_MAG[4] - SH_MAG[5] - SH_MAG[6]) - (2*magD*q0 - 2*magE*q1 + 2*magN*q2)*(P[19][2] + P[1][2]*SH_MAG[0] + P[3][2]*SH_MAG[2] - P[16][2]*(SH_MAG[3] + SH_MAG[4] - SH_MAG[5] - SH_MAG[6]) + P[17][2]*(2*q0*q3 + 2*q1*q2) - P[18][2]*(2*q0*q2 - 2*q1*q3) - P[2][2]*(2*magD*q0 - 2*magE*q1 + 2*magN*q2) + P[0][2]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + (SH_MAG[7] + SH_MAG[8] - 2*magD*q2)*(P[19][0] + P[1][0]*SH_MAG[0] + P[3][0]*SH_MAG[2] - P[16][0]*(SH_MAG[3] + SH_MAG[4] - SH_MAG[5] - SH_MAG[6]) + P[17][0]*(2*q0*q3 + 2*q1*q2) - P[18][0]*(2*q0*q2 - 2*q1*q3) - P[2][0]*(2*magD*q0 - 2*magE*q1 + 2*magN*q2) + P[0][0]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + SH_MAG[0]*(P[19][1] + P[1][1]*SH_MAG[0] + P[3][1]*SH_MAG[2] - P[16][1]*(SH_MAG[3] + SH_MAG[4] - SH_MAG[5] - SH_MAG[6]) + P[17][1]*(2*q0*q3 + 2*q1*q2) - P[18][1]*(2*q0*q2 - 2*q1*q3) - P[2][1]*(2*magD*q0 - 2*magE*q1 + 2*magN*q2) + P[0][1]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + SH_MAG[2]*(P[19][3] + P[1][3]*SH_MAG[0] + P[3][3]*SH_MAG[2] - P[16][3]*(SH_MAG[3] + SH_MAG[4] - SH_MAG[5] - SH_MAG[6]) + P[17][3]*(2*q0*q3 + 2*q1*q2) - P[18][3]*(2*q0*q2 - 2*q1*q3) - P[2][3]*(2*magD*q0 - 2*magE*q1 + 2*magN*q2) + P[0][3]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) - (SH_MAG[3] + SH_MAG[4] - SH_MAG[5] - SH_MAG[6])*(P[19][16] + P[1][16]*SH_MAG[0] + P[3][16]*SH_MAG[2] - P[16][16]*(SH_MAG[3] + SH_MAG[4] - SH_MAG[5] - SH_MAG[6]) + P[17][16]*(2*q0*q3 + 2*q1*q2) - P[18][16]*(2*q0*q2 - 2*q1*q3) - P[2][16]*(2*magD*q0 - 2*magE*q1 + 2*magN*q2) + P[0][16]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + P[17][19]*(2*q0*q3 + 2*q1*q2) - P[18][19]*(2*q0*q2 - 2*q1*q3) - P[2][19]*(2*magD*q0 - 2*magE*q1 + 2*magN*q2) + (2*q0*q3 + 2*q1*q2)*(P[19][17] + P[1][17]*SH_MAG[0] + P[3][17]*SH_MAG[2] - P[16][17]*(SH_MAG[3] + SH_MAG[4] - SH_MAG[5] - SH_MAG[6]) + P[17][17]*(2*q0*q3 + 2*q1*q2) - P[18][17]*(2*q0*q2 - 2*q1*q3) - P[2][17]*(2*magD*q0 - 2*magE*q1 + 2*magN*q2) + P[0][17]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) - (2*q0*q2 - 2*q1*q3)*(P[19][18] + P[1][18]*SH_MAG[0] + P[3][18]*SH_MAG[2] - P[16][18]*(SH_MAG[3] + SH_MAG[4] - SH_MAG[5] - SH_MAG[6]) + P[17][18]*(2*q0*q3 + 2*q1*q2) - P[18][18]*(2*q0*q2 - 2*q1*q3) - P[2][18]*(2*magD*q0 - 2*magE*q1 + 2*magN*q2) + P[0][18]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + P[0][19]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)); + if (temp >= R_MAG) { + SK_MX[0] = 1.0f / temp; + } else { + // the calculation is badly conditioned, so we cannot perform fusion on this step + // we increase the state variances and try again next time + P[19][19] += 0.1f*R_MAG; + obsIndex = 1; + return; + } + SK_MX[1] = SH_MAG[3] + SH_MAG[4] - SH_MAG[5] - SH_MAG[6]; + SK_MX[2] = 2*magD*q0 - 2*magE*q1 + 2*magN*q2; + SK_MX[3] = SH_MAG[7] + SH_MAG[8] - 2*magD*q2; + SK_MX[4] = 2*q0*q2 - 2*q1*q3; + SK_MX[5] = 2*q0*q3 + 2*q1*q2; + Kfusion[0] = SK_MX[0]*(P[0][19] + P[0][1]*SH_MAG[0] + P[0][3]*SH_MAG[2] + P[0][0]*SK_MX[3] - P[0][2]*SK_MX[2] - P[0][16]*SK_MX[1] + P[0][17]*SK_MX[5] - P[0][18]*SK_MX[4]); + Kfusion[1] = SK_MX[0]*(P[1][19] + P[1][1]*SH_MAG[0] + P[1][3]*SH_MAG[2] + P[1][0]*SK_MX[3] - P[1][2]*SK_MX[2] - P[1][16]*SK_MX[1] + P[1][17]*SK_MX[5] - P[1][18]*SK_MX[4]); + Kfusion[2] = SK_MX[0]*(P[2][19] + P[2][1]*SH_MAG[0] + P[2][3]*SH_MAG[2] + P[2][0]*SK_MX[3] - P[2][2]*SK_MX[2] - P[2][16]*SK_MX[1] + P[2][17]*SK_MX[5] - P[2][18]*SK_MX[4]); + Kfusion[3] = SK_MX[0]*(P[3][19] + P[3][1]*SH_MAG[0] + P[3][3]*SH_MAG[2] + P[3][0]*SK_MX[3] - P[3][2]*SK_MX[2] - P[3][16]*SK_MX[1] + P[3][17]*SK_MX[5] - P[3][18]*SK_MX[4]); + Kfusion[4] = SK_MX[0]*(P[4][19] + P[4][1]*SH_MAG[0] + P[4][3]*SH_MAG[2] + P[4][0]*SK_MX[3] - P[4][2]*SK_MX[2] - P[4][16]*SK_MX[1] + P[4][17]*SK_MX[5] - P[4][18]*SK_MX[4]); + Kfusion[5] = SK_MX[0]*(P[5][19] + P[5][1]*SH_MAG[0] + P[5][3]*SH_MAG[2] + P[5][0]*SK_MX[3] - P[5][2]*SK_MX[2] - P[5][16]*SK_MX[1] + P[5][17]*SK_MX[5] - P[5][18]*SK_MX[4]); + Kfusion[6] = SK_MX[0]*(P[6][19] + P[6][1]*SH_MAG[0] + P[6][3]*SH_MAG[2] + P[6][0]*SK_MX[3] - P[6][2]*SK_MX[2] - P[6][16]*SK_MX[1] + P[6][17]*SK_MX[5] - P[6][18]*SK_MX[4]); + Kfusion[7] = SK_MX[0]*(P[7][19] + P[7][1]*SH_MAG[0] + P[7][3]*SH_MAG[2] + P[7][0]*SK_MX[3] - P[7][2]*SK_MX[2] - P[7][16]*SK_MX[1] + P[7][17]*SK_MX[5] - P[7][18]*SK_MX[4]); + Kfusion[8] = SK_MX[0]*(P[8][19] + P[8][1]*SH_MAG[0] + P[8][3]*SH_MAG[2] + P[8][0]*SK_MX[3] - P[8][2]*SK_MX[2] - P[8][16]*SK_MX[1] + P[8][17]*SK_MX[5] - P[8][18]*SK_MX[4]); + Kfusion[9] = SK_MX[0]*(P[9][19] + P[9][1]*SH_MAG[0] + P[9][3]*SH_MAG[2] + P[9][0]*SK_MX[3] - P[9][2]*SK_MX[2] - P[9][16]*SK_MX[1] + P[9][17]*SK_MX[5] - P[9][18]*SK_MX[4]); + Kfusion[10] = SK_MX[0]*(P[10][19] + P[10][1]*SH_MAG[0] + P[10][3]*SH_MAG[2] + P[10][0]*SK_MX[3] - P[10][2]*SK_MX[2] - P[10][16]*SK_MX[1] + P[10][17]*SK_MX[5] - P[10][18]*SK_MX[4]); + Kfusion[11] = SK_MX[0]*(P[11][19] + P[11][1]*SH_MAG[0] + P[11][3]*SH_MAG[2] + P[11][0]*SK_MX[3] - P[11][2]*SK_MX[2] - P[11][16]*SK_MX[1] + P[11][17]*SK_MX[5] - P[11][18]*SK_MX[4]); + Kfusion[12] = SK_MX[0]*(P[12][19] + P[12][1]*SH_MAG[0] + P[12][3]*SH_MAG[2] + P[12][0]*SK_MX[3] - P[12][2]*SK_MX[2] - P[12][16]*SK_MX[1] + P[12][17]*SK_MX[5] - P[12][18]*SK_MX[4]); + // Only height measurements are allowed to modify the Z delta velocity bias state. This improves the stability of the estimate + Kfusion[13] = 0.0f;//SK_MX[0]*(P[13][19] + P[13][1]*SH_MAG[0] + P[13][3]*SH_MAG[2] + P[13][0]*SK_MX[3] - P[13][2]*SK_MX[2] - P[13][16]*SK_MX[1] + P[13][17]*SK_MX[5] - P[13][18]*SK_MX[4]); + Kfusion[14] = SK_MX[0]*(P[14][19] + P[14][1]*SH_MAG[0] + P[14][3]*SH_MAG[2] + P[14][0]*SK_MX[3] - P[14][2]*SK_MX[2] - P[14][16]*SK_MX[1] + P[14][17]*SK_MX[5] - P[14][18]*SK_MX[4]); + Kfusion[15] = SK_MX[0]*(P[15][19] + P[15][1]*SH_MAG[0] + P[15][3]*SH_MAG[2] + P[15][0]*SK_MX[3] - P[15][2]*SK_MX[2] - P[15][16]*SK_MX[1] + P[15][17]*SK_MX[5] - P[15][18]*SK_MX[4]); + Kfusion[16] = SK_MX[0]*(P[16][19] + P[16][1]*SH_MAG[0] + P[16][3]*SH_MAG[2] + P[16][0]*SK_MX[3] - P[16][2]*SK_MX[2] - P[16][16]*SK_MX[1] + P[16][17]*SK_MX[5] - P[16][18]*SK_MX[4]); + Kfusion[17] = SK_MX[0]*(P[17][19] + P[17][1]*SH_MAG[0] + P[17][3]*SH_MAG[2] + P[17][0]*SK_MX[3] - P[17][2]*SK_MX[2] - P[17][16]*SK_MX[1] + P[17][17]*SK_MX[5] - P[17][18]*SK_MX[4]); + Kfusion[18] = SK_MX[0]*(P[18][19] + P[18][1]*SH_MAG[0] + P[18][3]*SH_MAG[2] + P[18][0]*SK_MX[3] - P[18][2]*SK_MX[2] - P[18][16]*SK_MX[1] + P[18][17]*SK_MX[5] - P[18][18]*SK_MX[4]); + Kfusion[19] = SK_MX[0]*(P[19][19] + P[19][1]*SH_MAG[0] + P[19][3]*SH_MAG[2] + P[19][0]*SK_MX[3] - P[19][2]*SK_MX[2] - P[19][16]*SK_MX[1] + P[19][17]*SK_MX[5] - P[19][18]*SK_MX[4]); + Kfusion[20] = SK_MX[0]*(P[20][19] + P[20][1]*SH_MAG[0] + P[20][3]*SH_MAG[2] + P[20][0]*SK_MX[3] - P[20][2]*SK_MX[2] - P[20][16]*SK_MX[1] + P[20][17]*SK_MX[5] - P[20][18]*SK_MX[4]); + Kfusion[21] = SK_MX[0]*(P[21][19] + P[21][1]*SH_MAG[0] + P[21][3]*SH_MAG[2] + P[21][0]*SK_MX[3] - P[21][2]*SK_MX[2] - P[21][16]*SK_MX[1] + P[21][17]*SK_MX[5] - P[21][18]*SK_MX[4]); + Kfusion[22] = SK_MX[0]*(P[22][19] + P[22][1]*SH_MAG[0] + P[22][3]*SH_MAG[2] + P[22][0]*SK_MX[3] - P[22][2]*SK_MX[2] - P[22][16]*SK_MX[1] + P[22][17]*SK_MX[5] - P[22][18]*SK_MX[4]); + varInnovMag[0] = 1.0f/SK_MX[0]; + innovMag[0] = MagPred[0] - magData.x; + + // reset the observation index to 0 (we start by fusing the X + // measurement) + obsIndex = 0; + fuseMagData = false; + } + else if (obsIndex == 1) // we are now fusing the Y measurement + { + // Calculate observation jacobians + for (unsigned int i = 0; i < n_states; i++) H_MAG[i] = 0; + H_MAG[0] = SH_MAG[2]; + H_MAG[1] = SH_MAG[1]; + H_MAG[2] = SH_MAG[0]; + H_MAG[3] = 2*magD*q2 - SH_MAG[8] - SH_MAG[7]; + H_MAG[16] = 2*q1*q2 - 2*q0*q3; + H_MAG[17] = SH_MAG[4] - SH_MAG[3] - SH_MAG[5] + SH_MAG[6]; + H_MAG[18] = 2*q0*q1 + 2*q2*q3; + H_MAG[20] = 1; + + // Calculate Kalman gain + float temp = (P[20][20] + R_MAG + P[0][20]*SH_MAG[2] + P[1][20]*SH_MAG[1] + P[2][20]*SH_MAG[0] - P[17][20]*(SH_MAG[3] - SH_MAG[4] + SH_MAG[5] - SH_MAG[6]) - (2*q0*q3 - 2*q1*q2)*(P[20][16] + P[0][16]*SH_MAG[2] + P[1][16]*SH_MAG[1] + P[2][16]*SH_MAG[0] - P[17][16]*(SH_MAG[3] - SH_MAG[4] + SH_MAG[5] - SH_MAG[6]) - P[16][16]*(2*q0*q3 - 2*q1*q2) + P[18][16]*(2*q0*q1 + 2*q2*q3) - P[3][16]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + (2*q0*q1 + 2*q2*q3)*(P[20][18] + P[0][18]*SH_MAG[2] + P[1][18]*SH_MAG[1] + P[2][18]*SH_MAG[0] - P[17][18]*(SH_MAG[3] - SH_MAG[4] + SH_MAG[5] - SH_MAG[6]) - P[16][18]*(2*q0*q3 - 2*q1*q2) + P[18][18]*(2*q0*q1 + 2*q2*q3) - P[3][18]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) - (SH_MAG[7] + SH_MAG[8] - 2*magD*q2)*(P[20][3] + P[0][3]*SH_MAG[2] + P[1][3]*SH_MAG[1] + P[2][3]*SH_MAG[0] - P[17][3]*(SH_MAG[3] - SH_MAG[4] + SH_MAG[5] - SH_MAG[6]) - P[16][3]*(2*q0*q3 - 2*q1*q2) + P[18][3]*(2*q0*q1 + 2*q2*q3) - P[3][3]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) - P[16][20]*(2*q0*q3 - 2*q1*q2) + P[18][20]*(2*q0*q1 + 2*q2*q3) + SH_MAG[2]*(P[20][0] + P[0][0]*SH_MAG[2] + P[1][0]*SH_MAG[1] + P[2][0]*SH_MAG[0] - P[17][0]*(SH_MAG[3] - SH_MAG[4] + SH_MAG[5] - SH_MAG[6]) - P[16][0]*(2*q0*q3 - 2*q1*q2) + P[18][0]*(2*q0*q1 + 2*q2*q3) - P[3][0]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + SH_MAG[1]*(P[20][1] + P[0][1]*SH_MAG[2] + P[1][1]*SH_MAG[1] + P[2][1]*SH_MAG[0] - P[17][1]*(SH_MAG[3] - SH_MAG[4] + SH_MAG[5] - SH_MAG[6]) - P[16][1]*(2*q0*q3 - 2*q1*q2) + P[18][1]*(2*q0*q1 + 2*q2*q3) - P[3][1]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + SH_MAG[0]*(P[20][2] + P[0][2]*SH_MAG[2] + P[1][2]*SH_MAG[1] + P[2][2]*SH_MAG[0] - P[17][2]*(SH_MAG[3] - SH_MAG[4] + SH_MAG[5] - SH_MAG[6]) - P[16][2]*(2*q0*q3 - 2*q1*q2) + P[18][2]*(2*q0*q1 + 2*q2*q3) - P[3][2]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) - (SH_MAG[3] - SH_MAG[4] + SH_MAG[5] - SH_MAG[6])*(P[20][17] + P[0][17]*SH_MAG[2] + P[1][17]*SH_MAG[1] + P[2][17]*SH_MAG[0] - P[17][17]*(SH_MAG[3] - SH_MAG[4] + SH_MAG[5] - SH_MAG[6]) - P[16][17]*(2*q0*q3 - 2*q1*q2) + P[18][17]*(2*q0*q1 + 2*q2*q3) - P[3][17]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) - P[3][20]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)); + if (temp >= R_MAG) { + SK_MY[0] = 1.0f / temp; + } else { + // the calculation is badly conditioned, so we cannot perform fusion on this step + // we increase the state variances and try again next time + P[20][20] += 0.1f*R_MAG; + obsIndex = 2; + return; + } + SK_MY[1] = SH_MAG[3] - SH_MAG[4] + SH_MAG[5] - SH_MAG[6]; + SK_MY[2] = SH_MAG[7] + SH_MAG[8] - 2*magD*q2; + SK_MY[3] = 2*q0*q3 - 2*q1*q2; + SK_MY[4] = 2*q0*q1 + 2*q2*q3; + Kfusion[0] = SK_MY[0]*(P[0][20] + P[0][0]*SH_MAG[2] + P[0][1]*SH_MAG[1] + P[0][2]*SH_MAG[0] - P[0][3]*SK_MY[2] - P[0][17]*SK_MY[1] - P[0][16]*SK_MY[3] + P[0][18]*SK_MY[4]); + Kfusion[1] = SK_MY[0]*(P[1][20] + P[1][0]*SH_MAG[2] + P[1][1]*SH_MAG[1] + P[1][2]*SH_MAG[0] - P[1][3]*SK_MY[2] - P[1][17]*SK_MY[1] - P[1][16]*SK_MY[3] + P[1][18]*SK_MY[4]); + Kfusion[2] = SK_MY[0]*(P[2][20] + P[2][0]*SH_MAG[2] + P[2][1]*SH_MAG[1] + P[2][2]*SH_MAG[0] - P[2][3]*SK_MY[2] - P[2][17]*SK_MY[1] - P[2][16]*SK_MY[3] + P[2][18]*SK_MY[4]); + Kfusion[3] = SK_MY[0]*(P[3][20] + P[3][0]*SH_MAG[2] + P[3][1]*SH_MAG[1] + P[3][2]*SH_MAG[0] - P[3][3]*SK_MY[2] - P[3][17]*SK_MY[1] - P[3][16]*SK_MY[3] + P[3][18]*SK_MY[4]); + Kfusion[4] = SK_MY[0]*(P[4][20] + P[4][0]*SH_MAG[2] + P[4][1]*SH_MAG[1] + P[4][2]*SH_MAG[0] - P[4][3]*SK_MY[2] - P[4][17]*SK_MY[1] - P[4][16]*SK_MY[3] + P[4][18]*SK_MY[4]); + Kfusion[5] = SK_MY[0]*(P[5][20] + P[5][0]*SH_MAG[2] + P[5][1]*SH_MAG[1] + P[5][2]*SH_MAG[0] - P[5][3]*SK_MY[2] - P[5][17]*SK_MY[1] - P[5][16]*SK_MY[3] + P[5][18]*SK_MY[4]); + Kfusion[6] = SK_MY[0]*(P[6][20] + P[6][0]*SH_MAG[2] + P[6][1]*SH_MAG[1] + P[6][2]*SH_MAG[0] - P[6][3]*SK_MY[2] - P[6][17]*SK_MY[1] - P[6][16]*SK_MY[3] + P[6][18]*SK_MY[4]); + Kfusion[7] = SK_MY[0]*(P[7][20] + P[7][0]*SH_MAG[2] + P[7][1]*SH_MAG[1] + P[7][2]*SH_MAG[0] - P[7][3]*SK_MY[2] - P[7][17]*SK_MY[1] - P[7][16]*SK_MY[3] + P[7][18]*SK_MY[4]); + Kfusion[8] = SK_MY[0]*(P[8][20] + P[8][0]*SH_MAG[2] + P[8][1]*SH_MAG[1] + P[8][2]*SH_MAG[0] - P[8][3]*SK_MY[2] - P[8][17]*SK_MY[1] - P[8][16]*SK_MY[3] + P[8][18]*SK_MY[4]); + Kfusion[9] = SK_MY[0]*(P[9][20] + P[9][0]*SH_MAG[2] + P[9][1]*SH_MAG[1] + P[9][2]*SH_MAG[0] - P[9][3]*SK_MY[2] - P[9][17]*SK_MY[1] - P[9][16]*SK_MY[3] + P[9][18]*SK_MY[4]); + Kfusion[10] = SK_MY[0]*(P[10][20] + P[10][0]*SH_MAG[2] + P[10][1]*SH_MAG[1] + P[10][2]*SH_MAG[0] - P[10][3]*SK_MY[2] - P[10][17]*SK_MY[1] - P[10][16]*SK_MY[3] + P[10][18]*SK_MY[4]); + Kfusion[11] = SK_MY[0]*(P[11][20] + P[11][0]*SH_MAG[2] + P[11][1]*SH_MAG[1] + P[11][2]*SH_MAG[0] - P[11][3]*SK_MY[2] - P[11][17]*SK_MY[1] - P[11][16]*SK_MY[3] + P[11][18]*SK_MY[4]); + Kfusion[12] = SK_MY[0]*(P[12][20] + P[12][0]*SH_MAG[2] + P[12][1]*SH_MAG[1] + P[12][2]*SH_MAG[0] - P[12][3]*SK_MY[2] - P[12][17]*SK_MY[1] - P[12][16]*SK_MY[3] + P[12][18]*SK_MY[4]); + // Only height measurements are allowed to modify the Z delta velocity bias state. This improves the stability of the estimate + Kfusion[13] = 0.0f;//SK_MY[0]*(P[13][20] + P[13][0]*SH_MAG[2] + P[13][1]*SH_MAG[1] + P[13][2]*SH_MAG[0] - P[13][3]*SK_MY[2] - P[13][17]*SK_MY[1] - P[13][16]*SK_MY[3] + P[13][18]*SK_MY[4]); + Kfusion[14] = SK_MY[0]*(P[14][20] + P[14][0]*SH_MAG[2] + P[14][1]*SH_MAG[1] + P[14][2]*SH_MAG[0] - P[14][3]*SK_MY[2] - P[14][17]*SK_MY[1] - P[14][16]*SK_MY[3] + P[14][18]*SK_MY[4]); + Kfusion[15] = SK_MY[0]*(P[15][20] + P[15][0]*SH_MAG[2] + P[15][1]*SH_MAG[1] + P[15][2]*SH_MAG[0] - P[15][3]*SK_MY[2] - P[15][17]*SK_MY[1] - P[15][16]*SK_MY[3] + P[15][18]*SK_MY[4]); + Kfusion[16] = SK_MY[0]*(P[16][20] + P[16][0]*SH_MAG[2] + P[16][1]*SH_MAG[1] + P[16][2]*SH_MAG[0] - P[16][3]*SK_MY[2] - P[16][17]*SK_MY[1] - P[16][16]*SK_MY[3] + P[16][18]*SK_MY[4]); + Kfusion[17] = SK_MY[0]*(P[17][20] + P[17][0]*SH_MAG[2] + P[17][1]*SH_MAG[1] + P[17][2]*SH_MAG[0] - P[17][3]*SK_MY[2] - P[17][17]*SK_MY[1] - P[17][16]*SK_MY[3] + P[17][18]*SK_MY[4]); + Kfusion[18] = SK_MY[0]*(P[18][20] + P[18][0]*SH_MAG[2] + P[18][1]*SH_MAG[1] + P[18][2]*SH_MAG[0] - P[18][3]*SK_MY[2] - P[18][17]*SK_MY[1] - P[18][16]*SK_MY[3] + P[18][18]*SK_MY[4]); + Kfusion[19] = SK_MY[0]*(P[19][20] + P[19][0]*SH_MAG[2] + P[19][1]*SH_MAG[1] + P[19][2]*SH_MAG[0] - P[19][3]*SK_MY[2] - P[19][17]*SK_MY[1] - P[19][16]*SK_MY[3] + P[19][18]*SK_MY[4]); + Kfusion[20] = SK_MY[0]*(P[20][20] + P[20][0]*SH_MAG[2] + P[20][1]*SH_MAG[1] + P[20][2]*SH_MAG[0] - P[20][3]*SK_MY[2] - P[20][17]*SK_MY[1] - P[20][16]*SK_MY[3] + P[20][18]*SK_MY[4]); + Kfusion[21] = SK_MY[0]*(P[21][20] + P[21][0]*SH_MAG[2] + P[21][1]*SH_MAG[1] + P[21][2]*SH_MAG[0] - P[21][3]*SK_MY[2] - P[21][17]*SK_MY[1] - P[21][16]*SK_MY[3] + P[21][18]*SK_MY[4]); + Kfusion[22] = SK_MY[0]*(P[22][20] + P[22][0]*SH_MAG[2] + P[22][1]*SH_MAG[1] + P[22][2]*SH_MAG[0] - P[22][3]*SK_MY[2] - P[22][17]*SK_MY[1] - P[22][16]*SK_MY[3] + P[22][18]*SK_MY[4]); + varInnovMag[1] = 1.0f/SK_MY[0]; + innovMag[1] = MagPred[1] - magData.y; + } + else if (obsIndex == 2) // we are now fusing the Z measurement + { + // Calculate observation jacobians + for (uint8_t i = 0; i < n_states; i++) H_MAG[i] = 0; + H_MAG[0] = SH_MAG[1]; + H_MAG[1] = 2*magN*q3 - 2*magE*q0 - 2*magD*q1; + H_MAG[2] = SH_MAG[7] + SH_MAG[8] - 2*magD*q2; + H_MAG[3] = SH_MAG[0]; + H_MAG[16] = 2*q0*q2 + 2*q1*q3; + H_MAG[17] = 2*q2*q3 - 2*q0*q1; + H_MAG[18] = SH_MAG[3] - SH_MAG[4] - SH_MAG[5] + SH_MAG[6]; + H_MAG[21] = 1; + + // Calculate Kalman gain + float temp = (P[21][21] + R_MAG + P[0][21]*SH_MAG[1] + P[3][21]*SH_MAG[0] + P[18][21]*(SH_MAG[3] - SH_MAG[4] - SH_MAG[5] + SH_MAG[6]) - (2*magD*q1 + 2*magE*q0 - 2*magN*q3)*(P[21][1] + P[0][1]*SH_MAG[1] + P[3][1]*SH_MAG[0] + P[18][1]*(SH_MAG[3] - SH_MAG[4] - SH_MAG[5] + SH_MAG[6]) + P[16][1]*(2*q0*q2 + 2*q1*q3) - P[17][1]*(2*q0*q1 - 2*q2*q3) - P[1][1]*(2*magD*q1 + 2*magE*q0 - 2*magN*q3) + P[2][1]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + (SH_MAG[7] + SH_MAG[8] - 2*magD*q2)*(P[21][2] + P[0][2]*SH_MAG[1] + P[3][2]*SH_MAG[0] + P[18][2]*(SH_MAG[3] - SH_MAG[4] - SH_MAG[5] + SH_MAG[6]) + P[16][2]*(2*q0*q2 + 2*q1*q3) - P[17][2]*(2*q0*q1 - 2*q2*q3) - P[1][2]*(2*magD*q1 + 2*magE*q0 - 2*magN*q3) + P[2][2]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + SH_MAG[1]*(P[21][0] + P[0][0]*SH_MAG[1] + P[3][0]*SH_MAG[0] + P[18][0]*(SH_MAG[3] - SH_MAG[4] - SH_MAG[5] + SH_MAG[6]) + P[16][0]*(2*q0*q2 + 2*q1*q3) - P[17][0]*(2*q0*q1 - 2*q2*q3) - P[1][0]*(2*magD*q1 + 2*magE*q0 - 2*magN*q3) + P[2][0]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + SH_MAG[0]*(P[21][3] + P[0][3]*SH_MAG[1] + P[3][3]*SH_MAG[0] + P[18][3]*(SH_MAG[3] - SH_MAG[4] - SH_MAG[5] + SH_MAG[6]) + P[16][3]*(2*q0*q2 + 2*q1*q3) - P[17][3]*(2*q0*q1 - 2*q2*q3) - P[1][3]*(2*magD*q1 + 2*magE*q0 - 2*magN*q3) + P[2][3]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + (SH_MAG[3] - SH_MAG[4] - SH_MAG[5] + SH_MAG[6])*(P[21][18] + P[0][18]*SH_MAG[1] + P[3][18]*SH_MAG[0] + P[18][18]*(SH_MAG[3] - SH_MAG[4] - SH_MAG[5] + SH_MAG[6]) + P[16][18]*(2*q0*q2 + 2*q1*q3) - P[17][18]*(2*q0*q1 - 2*q2*q3) - P[1][18]*(2*magD*q1 + 2*magE*q0 - 2*magN*q3) + P[2][18]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + P[16][21]*(2*q0*q2 + 2*q1*q3) - P[17][21]*(2*q0*q1 - 2*q2*q3) - P[1][21]*(2*magD*q1 + 2*magE*q0 - 2*magN*q3) + (2*q0*q2 + 2*q1*q3)*(P[21][16] + P[0][16]*SH_MAG[1] + P[3][16]*SH_MAG[0] + P[18][16]*(SH_MAG[3] - SH_MAG[4] - SH_MAG[5] + SH_MAG[6]) + P[16][16]*(2*q0*q2 + 2*q1*q3) - P[17][16]*(2*q0*q1 - 2*q2*q3) - P[1][16]*(2*magD*q1 + 2*magE*q0 - 2*magN*q3) + P[2][16]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) - (2*q0*q1 - 2*q2*q3)*(P[21][17] + P[0][17]*SH_MAG[1] + P[3][17]*SH_MAG[0] + P[18][17]*(SH_MAG[3] - SH_MAG[4] - SH_MAG[5] + SH_MAG[6]) + P[16][17]*(2*q0*q2 + 2*q1*q3) - P[17][17]*(2*q0*q1 - 2*q2*q3) - P[1][17]*(2*magD*q1 + 2*magE*q0 - 2*magN*q3) + P[2][17]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)) + P[2][21]*(SH_MAG[7] + SH_MAG[8] - 2*magD*q2)); + if (temp >= R_MAG) { + SK_MZ[0] = 1.0f / temp; + } else { + // the calculation is badly conditioned, so we cannot perform fusion on this step + // we increase the state variances and try again next time + P[21][21] += 0.1f*R_MAG; + obsIndex = 3; + return; + } + SK_MZ[1] = SH_MAG[3] - SH_MAG[4] - SH_MAG[5] + SH_MAG[6]; + SK_MZ[2] = 2*magD*q1 + 2*magE*q0 - 2*magN*q3; + SK_MZ[3] = SH_MAG[7] + SH_MAG[8] - 2*magD*q2; + SK_MZ[4] = 2*q0*q1 - 2*q2*q3; + SK_MZ[5] = 2*q0*q2 + 2*q1*q3; + Kfusion[0] = SK_MZ[0]*(P[0][21] + P[0][0]*SH_MAG[1] + P[0][3]*SH_MAG[0] - P[0][1]*SK_MZ[2] + P[0][2]*SK_MZ[3] + P[0][18]*SK_MZ[1] + P[0][16]*SK_MZ[5] - P[0][17]*SK_MZ[4]); + Kfusion[1] = SK_MZ[0]*(P[1][21] + P[1][0]*SH_MAG[1] + P[1][3]*SH_MAG[0] - P[1][1]*SK_MZ[2] + P[1][2]*SK_MZ[3] + P[1][18]*SK_MZ[1] + P[1][16]*SK_MZ[5] - P[1][17]*SK_MZ[4]); + Kfusion[2] = SK_MZ[0]*(P[2][21] + P[2][0]*SH_MAG[1] + P[2][3]*SH_MAG[0] - P[2][1]*SK_MZ[2] + P[2][2]*SK_MZ[3] + P[2][18]*SK_MZ[1] + P[2][16]*SK_MZ[5] - P[2][17]*SK_MZ[4]); + Kfusion[3] = SK_MZ[0]*(P[3][21] + P[3][0]*SH_MAG[1] + P[3][3]*SH_MAG[0] - P[3][1]*SK_MZ[2] + P[3][2]*SK_MZ[3] + P[3][18]*SK_MZ[1] + P[3][16]*SK_MZ[5] - P[3][17]*SK_MZ[4]); + Kfusion[4] = SK_MZ[0]*(P[4][21] + P[4][0]*SH_MAG[1] + P[4][3]*SH_MAG[0] - P[4][1]*SK_MZ[2] + P[4][2]*SK_MZ[3] + P[4][18]*SK_MZ[1] + P[4][16]*SK_MZ[5] - P[4][17]*SK_MZ[4]); + Kfusion[5] = SK_MZ[0]*(P[5][21] + P[5][0]*SH_MAG[1] + P[5][3]*SH_MAG[0] - P[5][1]*SK_MZ[2] + P[5][2]*SK_MZ[3] + P[5][18]*SK_MZ[1] + P[5][16]*SK_MZ[5] - P[5][17]*SK_MZ[4]); + Kfusion[6] = SK_MZ[0]*(P[6][21] + P[6][0]*SH_MAG[1] + P[6][3]*SH_MAG[0] - P[6][1]*SK_MZ[2] + P[6][2]*SK_MZ[3] + P[6][18]*SK_MZ[1] + P[6][16]*SK_MZ[5] - P[6][17]*SK_MZ[4]); + Kfusion[7] = SK_MZ[0]*(P[7][21] + P[7][0]*SH_MAG[1] + P[7][3]*SH_MAG[0] - P[7][1]*SK_MZ[2] + P[7][2]*SK_MZ[3] + P[7][18]*SK_MZ[1] + P[7][16]*SK_MZ[5] - P[7][17]*SK_MZ[4]); + Kfusion[8] = SK_MZ[0]*(P[8][21] + P[8][0]*SH_MAG[1] + P[8][3]*SH_MAG[0] - P[8][1]*SK_MZ[2] + P[8][2]*SK_MZ[3] + P[8][18]*SK_MZ[1] + P[8][16]*SK_MZ[5] - P[8][17]*SK_MZ[4]); + Kfusion[9] = SK_MZ[0]*(P[9][21] + P[9][0]*SH_MAG[1] + P[9][3]*SH_MAG[0] - P[9][1]*SK_MZ[2] + P[9][2]*SK_MZ[3] + P[9][18]*SK_MZ[1] + P[9][16]*SK_MZ[5] - P[9][17]*SK_MZ[4]); + Kfusion[10] = SK_MZ[0]*(P[10][21] + P[10][0]*SH_MAG[1] + P[10][3]*SH_MAG[0] - P[10][1]*SK_MZ[2] + P[10][2]*SK_MZ[3] + P[10][18]*SK_MZ[1] + P[10][16]*SK_MZ[5] - P[10][17]*SK_MZ[4]); + Kfusion[11] = SK_MZ[0]*(P[11][21] + P[11][0]*SH_MAG[1] + P[11][3]*SH_MAG[0] - P[11][1]*SK_MZ[2] + P[11][2]*SK_MZ[3] + P[11][18]*SK_MZ[1] + P[11][16]*SK_MZ[5] - P[11][17]*SK_MZ[4]); + Kfusion[12] = SK_MZ[0]*(P[12][21] + P[12][0]*SH_MAG[1] + P[12][3]*SH_MAG[0] - P[12][1]*SK_MZ[2] + P[12][2]*SK_MZ[3] + P[12][18]*SK_MZ[1] + P[12][16]*SK_MZ[5] - P[12][17]*SK_MZ[4]); + // Only height measurements are allowed to modify the Z delta velocity bias state. This improves the stability of the estimate + Kfusion[13] = 0.0f;//SK_MZ[0]*(P[13][21] + P[13][0]*SH_MAG[1] + P[13][3]*SH_MAG[0] - P[13][1]*SK_MZ[2] + P[13][2]*SK_MZ[3] + P[13][18]*SK_MZ[1] + P[13][16]*SK_MZ[5] - P[13][17]*SK_MZ[4]); + Kfusion[14] = SK_MZ[0]*(P[14][21] + P[14][0]*SH_MAG[1] + P[14][3]*SH_MAG[0] - P[14][1]*SK_MZ[2] + P[14][2]*SK_MZ[3] + P[14][18]*SK_MZ[1] + P[14][16]*SK_MZ[5] - P[14][17]*SK_MZ[4]); + Kfusion[15] = SK_MZ[0]*(P[15][21] + P[15][0]*SH_MAG[1] + P[15][3]*SH_MAG[0] - P[15][1]*SK_MZ[2] + P[15][2]*SK_MZ[3] + P[15][18]*SK_MZ[1] + P[15][16]*SK_MZ[5] - P[15][17]*SK_MZ[4]); + Kfusion[16] = SK_MZ[0]*(P[16][21] + P[16][0]*SH_MAG[1] + P[16][3]*SH_MAG[0] - P[16][1]*SK_MZ[2] + P[16][2]*SK_MZ[3] + P[16][18]*SK_MZ[1] + P[16][16]*SK_MZ[5] - P[16][17]*SK_MZ[4]); + Kfusion[17] = SK_MZ[0]*(P[17][21] + P[17][0]*SH_MAG[1] + P[17][3]*SH_MAG[0] - P[17][1]*SK_MZ[2] + P[17][2]*SK_MZ[3] + P[17][18]*SK_MZ[1] + P[17][16]*SK_MZ[5] - P[17][17]*SK_MZ[4]); + Kfusion[18] = SK_MZ[0]*(P[18][21] + P[18][0]*SH_MAG[1] + P[18][3]*SH_MAG[0] - P[18][1]*SK_MZ[2] + P[18][2]*SK_MZ[3] + P[18][18]*SK_MZ[1] + P[18][16]*SK_MZ[5] - P[18][17]*SK_MZ[4]); + Kfusion[19] = SK_MZ[0]*(P[19][21] + P[19][0]*SH_MAG[1] + P[19][3]*SH_MAG[0] - P[19][1]*SK_MZ[2] + P[19][2]*SK_MZ[3] + P[19][18]*SK_MZ[1] + P[19][16]*SK_MZ[5] - P[19][17]*SK_MZ[4]); + Kfusion[20] = SK_MZ[0]*(P[20][21] + P[20][0]*SH_MAG[1] + P[20][3]*SH_MAG[0] - P[20][1]*SK_MZ[2] + P[20][2]*SK_MZ[3] + P[20][18]*SK_MZ[1] + P[20][16]*SK_MZ[5] - P[20][17]*SK_MZ[4]); + Kfusion[21] = SK_MZ[0]*(P[21][21] + P[21][0]*SH_MAG[1] + P[21][3]*SH_MAG[0] - P[21][1]*SK_MZ[2] + P[21][2]*SK_MZ[3] + P[21][18]*SK_MZ[1] + P[21][16]*SK_MZ[5] - P[21][17]*SK_MZ[4]); + Kfusion[22] = SK_MZ[0]*(P[22][21] + P[22][0]*SH_MAG[1] + P[22][3]*SH_MAG[0] - P[22][1]*SK_MZ[2] + P[22][2]*SK_MZ[3] + P[22][18]*SK_MZ[1] + P[22][16]*SK_MZ[5] - P[22][17]*SK_MZ[4]); + varInnovMag[2] = 1.0f/SK_MZ[0]; + innovMag[2] = MagPred[2] - magData.z; + + } + + // Check the innovation for consistency and don't fuse if > 5Sigma + if ((innovMag[obsIndex]*innovMag[obsIndex]/varInnovMag[obsIndex]) < 25.0) + { + // correct the state vector + for (uint8_t j= 0; j < indexLimit; j++) + { + states[j] = states[j] - Kfusion[j] * innovMag[obsIndex]; + } + // normalise the quaternion states + float quatMag = sqrt(states[0]*states[0] + states[1]*states[1] + states[2]*states[2] + states[3]*states[3]); + if (quatMag > 1e-12) + { + for (uint8_t j= 0; j<=3; j++) + { + float quatMagInv = 1.0f/quatMag; + states[j] = states[j] * quatMagInv; + } + } + // correct the covariance P = (I - K*H)*P + // take advantage of the empty columns in KH to reduce the + // number of operations + for (uint8_t i = 0; i < indexLimit; i++) + { + for (uint8_t j = 0; j <= 3; j++) + { + KH[i][j] = Kfusion[i] * H_MAG[j]; + } + for (uint8_t j = 4; j <= 15; j++) KH[i][j] = 0.0f; + if (!onGround) + { + for (uint8_t j = 16; j <= 21; j++) + { + KH[i][j] = Kfusion[i] * H_MAG[j]; + } + } + else + { + for (uint8_t j = 16; j <= 21; j++) + { + KH[i][j] = 0.0f; + } + } + } + for (uint8_t i = 0; i < indexLimit; i++) + { + for (uint8_t j = 0; j < indexLimit; j++) + { + KHP[i][j] = 0.0f; + for (uint8_t k = 0; k <= 3; k++) + { + KHP[i][j] = KHP[i][j] + KH[i][k] * P[k][j]; + } + if (!onGround) + { + for (uint8_t k = 16; k<=21; k++) + { + KHP[i][j] = KHP[i][j] + KH[i][k] * P[k][j]; + } + } + } + } + } + for (uint8_t i = 0; i < indexLimit; i++) + { + for (uint8_t j = 0; j < indexLimit; j++) + { + P[i][j] = P[i][j] - KHP[i][j]; + } + } + } + obsIndex = obsIndex + 1; + + ForceSymmetry(); + ConstrainVariances(); +} + +void AttPosEKF::FuseAirspeed() +{ + float vn; + float ve; + float vd; + float vwn; + float vwe; + float R_TAS = sq(airspeedMeasurementSigma); + float SH_TAS[3]; + float SK_TAS; + float VtasPred; + + // Copy required states to local variable names + vn = statesAtVtasMeasTime[4]; + ve = statesAtVtasMeasTime[5]; + vd = statesAtVtasMeasTime[6]; + vwn = statesAtVtasMeasTime[14]; + vwe = statesAtVtasMeasTime[15]; + + // Need to check that it is flying before fusing airspeed data + // Calculate the predicted airspeed + VtasPred = sqrtf((ve - vwe)*(ve - vwe) + (vn - vwn)*(vn - vwn) + vd*vd); + // Perform fusion of True Airspeed measurement + if (useAirspeed && fuseVtasData && (VtasPred > 1.0f) && (VtasMeas > 8.0f)) + { + // Calculate observation jacobians + SH_TAS[0] = 1/(sqrt(sq(ve - vwe) + sq(vn - vwn) + sq(vd))); + SH_TAS[1] = (SH_TAS[0]*(2.0f*ve - 2*vwe))/2.0f; + SH_TAS[2] = (SH_TAS[0]*(2.0f*vn - 2*vwn))/2.0f; + + float H_TAS[n_states]; + for (uint8_t i = 0; i < n_states; i++) H_TAS[i] = 0.0f; + H_TAS[4] = SH_TAS[2]; + H_TAS[5] = SH_TAS[1]; + H_TAS[6] = vd*SH_TAS[0]; + H_TAS[14] = -SH_TAS[2]; + H_TAS[15] = -SH_TAS[1]; + + // Calculate Kalman gains + float temp = (R_TAS + SH_TAS[2]*(P[4][4]*SH_TAS[2] + P[5][4]*SH_TAS[1] - P[14][4]*SH_TAS[2] - P[15][4]*SH_TAS[1] + P[6][4]*vd*SH_TAS[0]) + SH_TAS[1]*(P[4][5]*SH_TAS[2] + P[5][5]*SH_TAS[1] - P[14][5]*SH_TAS[2] - P[15][5]*SH_TAS[1] + P[6][5]*vd*SH_TAS[0]) - SH_TAS[2]*(P[4][14]*SH_TAS[2] + P[5][14]*SH_TAS[1] - P[14][14]*SH_TAS[2] - P[15][14]*SH_TAS[1] + P[6][14]*vd*SH_TAS[0]) - SH_TAS[1]*(P[4][15]*SH_TAS[2] + P[5][15]*SH_TAS[1] - P[14][15]*SH_TAS[2] - P[15][15]*SH_TAS[1] + P[6][15]*vd*SH_TAS[0]) + vd*SH_TAS[0]*(P[4][6]*SH_TAS[2] + P[5][6]*SH_TAS[1] - P[14][6]*SH_TAS[2] - P[15][6]*SH_TAS[1] + P[6][6]*vd*SH_TAS[0])); + if (temp >= R_TAS) { + SK_TAS = 1.0f / temp; + } else { + // the calculation is badly conditioned, so we cannot perform fusion on this step + // we increase the wind state variances and try again next time + P[14][14] += 0.05f*R_TAS; + P[15][15] += 0.05f*R_TAS; + return; + } + Kfusion[0] = SK_TAS*(P[0][4]*SH_TAS[2] - P[0][14]*SH_TAS[2] + P[0][5]*SH_TAS[1] - P[0][15]*SH_TAS[1] + P[0][6]*vd*SH_TAS[0]); + Kfusion[1] = SK_TAS*(P[1][4]*SH_TAS[2] - P[1][14]*SH_TAS[2] + P[1][5]*SH_TAS[1] - P[1][15]*SH_TAS[1] + P[1][6]*vd*SH_TAS[0]); + Kfusion[2] = SK_TAS*(P[2][4]*SH_TAS[2] - P[2][14]*SH_TAS[2] + P[2][5]*SH_TAS[1] - P[2][15]*SH_TAS[1] + P[2][6]*vd*SH_TAS[0]); + Kfusion[3] = SK_TAS*(P[3][4]*SH_TAS[2] - P[3][14]*SH_TAS[2] + P[3][5]*SH_TAS[1] - P[3][15]*SH_TAS[1] + P[3][6]*vd*SH_TAS[0]); + Kfusion[4] = SK_TAS*(P[4][4]*SH_TAS[2] - P[4][14]*SH_TAS[2] + P[4][5]*SH_TAS[1] - P[4][15]*SH_TAS[1] + P[4][6]*vd*SH_TAS[0]); + Kfusion[5] = SK_TAS*(P[5][4]*SH_TAS[2] - P[5][14]*SH_TAS[2] + P[5][5]*SH_TAS[1] - P[5][15]*SH_TAS[1] + P[5][6]*vd*SH_TAS[0]); + Kfusion[6] = SK_TAS*(P[6][4]*SH_TAS[2] - P[6][14]*SH_TAS[2] + P[6][5]*SH_TAS[1] - P[6][15]*SH_TAS[1] + P[6][6]*vd*SH_TAS[0]); + Kfusion[7] = SK_TAS*(P[7][4]*SH_TAS[2] - P[7][14]*SH_TAS[2] + P[7][5]*SH_TAS[1] - P[7][15]*SH_TAS[1] + P[7][6]*vd*SH_TAS[0]); + Kfusion[8] = SK_TAS*(P[8][4]*SH_TAS[2] - P[8][14]*SH_TAS[2] + P[8][5]*SH_TAS[1] - P[8][15]*SH_TAS[1] + P[8][6]*vd*SH_TAS[0]); + Kfusion[9] = SK_TAS*(P[9][4]*SH_TAS[2] - P[9][14]*SH_TAS[2] + P[9][5]*SH_TAS[1] - P[9][15]*SH_TAS[1] + P[9][6]*vd*SH_TAS[0]); + Kfusion[10] = SK_TAS*(P[10][4]*SH_TAS[2] - P[10][14]*SH_TAS[2] + P[10][5]*SH_TAS[1] - P[10][15]*SH_TAS[1] + P[10][6]*vd*SH_TAS[0]); + Kfusion[11] = SK_TAS*(P[11][4]*SH_TAS[2] - P[11][14]*SH_TAS[2] + P[11][5]*SH_TAS[1] - P[11][15]*SH_TAS[1] + P[11][6]*vd*SH_TAS[0]); + Kfusion[12] = SK_TAS*(P[12][4]*SH_TAS[2] - P[12][14]*SH_TAS[2] + P[12][5]*SH_TAS[1] - P[12][15]*SH_TAS[1] + P[12][6]*vd*SH_TAS[0]); + // Only height measurements are allowed to modify the Z delta velocity bias state. This improves the stability of the estimate + Kfusion[13] = 0.0f;//SK_TAS*(P[13][4]*SH_TAS[2] - P[13][14]*SH_TAS[2] + P[13][5]*SH_TAS[1] - P[13][15]*SH_TAS[1] + P[13][6]*vd*SH_TAS[0]); + Kfusion[14] = SK_TAS*(P[14][4]*SH_TAS[2] - P[14][14]*SH_TAS[2] + P[14][5]*SH_TAS[1] - P[14][15]*SH_TAS[1] + P[14][6]*vd*SH_TAS[0]); + Kfusion[15] = SK_TAS*(P[15][4]*SH_TAS[2] - P[15][14]*SH_TAS[2] + P[15][5]*SH_TAS[1] - P[15][15]*SH_TAS[1] + P[15][6]*vd*SH_TAS[0]); + Kfusion[16] = SK_TAS*(P[16][4]*SH_TAS[2] - P[16][14]*SH_TAS[2] + P[16][5]*SH_TAS[1] - P[16][15]*SH_TAS[1] + P[16][6]*vd*SH_TAS[0]); + Kfusion[17] = SK_TAS*(P[17][4]*SH_TAS[2] - P[17][14]*SH_TAS[2] + P[17][5]*SH_TAS[1] - P[17][15]*SH_TAS[1] + P[17][6]*vd*SH_TAS[0]); + Kfusion[18] = SK_TAS*(P[18][4]*SH_TAS[2] - P[18][14]*SH_TAS[2] + P[18][5]*SH_TAS[1] - P[18][15]*SH_TAS[1] + P[18][6]*vd*SH_TAS[0]); + Kfusion[19] = SK_TAS*(P[19][4]*SH_TAS[2] - P[19][14]*SH_TAS[2] + P[19][5]*SH_TAS[1] - P[19][15]*SH_TAS[1] + P[19][6]*vd*SH_TAS[0]); + Kfusion[20] = SK_TAS*(P[20][4]*SH_TAS[2] - P[20][14]*SH_TAS[2] + P[20][5]*SH_TAS[1] - P[20][15]*SH_TAS[1] + P[20][6]*vd*SH_TAS[0]); + Kfusion[21] = SK_TAS*(P[21][4]*SH_TAS[2] - P[21][14]*SH_TAS[2] + P[21][5]*SH_TAS[1] - P[21][15]*SH_TAS[1] + P[21][6]*vd*SH_TAS[0]); + Kfusion[22] = SK_TAS*(P[22][4]*SH_TAS[2] - P[22][14]*SH_TAS[2] + P[22][5]*SH_TAS[1] - P[22][15]*SH_TAS[1] + P[22][6]*vd*SH_TAS[0]); + varInnovVtas = 1.0f/SK_TAS; + + // Calculate the measurement innovation + innovVtas = VtasPred - VtasMeas; + // Check the innovation for consistency and don't fuse if > 5Sigma + if ((innovVtas*innovVtas*SK_TAS) < 25.0) + { + // correct the state vector + for (uint8_t j=0; j <= 22; j++) + { + states[j] = states[j] - Kfusion[j] * innovVtas; + } + // normalise the quaternion states + float quatMag = sqrt(states[0]*states[0] + states[1]*states[1] + states[2]*states[2] + states[3]*states[3]); + if (quatMag > 1e-12f) + { + for (uint8_t j= 0; j <= 3; j++) + { + float quatMagInv = 1.0f/quatMag; + states[j] = states[j] * quatMagInv; + } + } + // correct the covariance P = (I - K*H)*P + // take advantage of the empty columns in H to reduce the + // number of operations + for (uint8_t i = 0; i <= 22; i++) + { + for (uint8_t j = 0; j <= 3; j++) KH[i][j] = 0.0; + for (uint8_t j = 4; j <= 6; j++) + { + KH[i][j] = Kfusion[i] * H_TAS[j]; + } + for (uint8_t j = 7; j <= 13; j++) KH[i][j] = 0.0; + for (uint8_t j = 14; j <= 15; j++) + { + KH[i][j] = Kfusion[i] * H_TAS[j]; + } + for (uint8_t j = 16; j <= 22; j++) KH[i][j] = 0.0; + } + for (uint8_t i = 0; i <= 22; i++) + { + for (uint8_t j = 0; j <= 22; j++) + { + KHP[i][j] = 0.0; + for (uint8_t k = 4; k <= 6; k++) + { + KHP[i][j] = KHP[i][j] + KH[i][k] * P[k][j]; + } + for (uint8_t k = 14; k <= 15; k++) + { + KHP[i][j] = KHP[i][j] + KH[i][k] * P[k][j]; + } + } + } + for (uint8_t i = 0; i <= 22; i++) + { + for (uint8_t j = 0; j <= 22; j++) + { + P[i][j] = P[i][j] - KHP[i][j]; + } + } + } + } + + ForceSymmetry(); + ConstrainVariances(); +} + +void AttPosEKF::zeroRows(float (&covMat)[n_states][n_states], uint8_t first, uint8_t last) +{ + uint8_t row; + uint8_t col; + for (row=first; row<=last; row++) + { + for (col=0; col<n_states; col++) + { + covMat[row][col] = 0.0; + } + } +} + +void AttPosEKF::FuseRangeFinder() +{ + + // Local variables + float rngPred; + float SH_RNG[5]; + float H_RNG[23]; + float SK_RNG[6]; + float cosRngTilt; + const float R_RNG = 0.25f; // 0.5 m2 rangefinder measurement variance + + // Copy required states to local variable names + float q0 = statesAtRngTime[0]; + float q1 = statesAtRngTime[1]; + float q2 = statesAtRngTime[2]; + float q3 = statesAtRngTime[3]; + float pd = statesAtRngTime[9]; + float ptd = statesAtRngTime[22]; + + // Need to check that our range finder tilt angle is less than 30 degrees and we are using range finder data + SH_RNG[4] = sin(rngFinderPitch); + cosRngTilt = - Tbn.z.x * SH_RNG[4] + Tbn.z.z * cos(rngFinderPitch); + if (useRangeFinder && cosRngTilt > 0.87f) + { + // Calculate observation jacobian and Kalman gain ignoring all states other than the terrain offset + // This prevents the range finder measurement modifying any of the other filter states and significantly reduces computations + SH_RNG[0] = SH_RNG[4]*(2*q0*q2 - 2*q1*q3) - sq(q0) + sq(q1) + sq(q2) - sq(q3); + SH_RNG[1] = pd - ptd; + SH_RNG[2] = 1/sq(SH_RNG[0]); + SH_RNG[3] = 1/SH_RNG[0]; + for (uint8_t i = 0; i < n_states; i++) { + H_RNG[i] = 0.0f; + Kfusion[i] = 0.0f; + } + H_RNG[22] = -SH_RNG[3]; + SK_RNG[0] = 1/(R_RNG + SH_RNG[3]*(P[9][9]*SH_RNG[3] - P[22][9]*SH_RNG[3] + P[0][9]*SH_RNG[1]*SH_RNG[2]*(2*q0 - 2*q2*SH_RNG[4]) - P[1][9]*SH_RNG[1]*SH_RNG[2]*(2*q1 - 2*q3*SH_RNG[4]) - P[2][9]*SH_RNG[1]*SH_RNG[2]*(2*q2 + 2*q0*SH_RNG[4]) + P[3][9]*SH_RNG[1]*SH_RNG[2]*(2*q3 + 2*q1*SH_RNG[4])) - SH_RNG[3]*(P[9][22]*SH_RNG[3] - P[22][22]*SH_RNG[3] + P[0][22]*SH_RNG[1]*SH_RNG[2]*(2*q0 - 2*q2*SH_RNG[4]) - P[1][22]*SH_RNG[1]*SH_RNG[2]*(2*q1 - 2*q3*SH_RNG[4]) - P[2][22]*SH_RNG[1]*SH_RNG[2]*(2*q2 + 2*q0*SH_RNG[4]) + P[3][22]*SH_RNG[1]*SH_RNG[2]*(2*q3 + 2*q1*SH_RNG[4])) + SH_RNG[1]*SH_RNG[2]*(2*q0 - 2*q2*SH_RNG[4])*(P[9][0]*SH_RNG[3] - P[22][0]*SH_RNG[3] + P[0][0]*SH_RNG[1]*SH_RNG[2]*(2*q0 - 2*q2*SH_RNG[4]) - P[1][0]*SH_RNG[1]*SH_RNG[2]*(2*q1 - 2*q3*SH_RNG[4]) - P[2][0]*SH_RNG[1]*SH_RNG[2]*(2*q2 + 2*q0*SH_RNG[4]) + P[3][0]*SH_RNG[1]*SH_RNG[2]*(2*q3 + 2*q1*SH_RNG[4])) - SH_RNG[1]*SH_RNG[2]*(2*q1 - 2*q3*SH_RNG[4])*(P[9][1]*SH_RNG[3] - P[22][1]*SH_RNG[3] + P[0][1]*SH_RNG[1]*SH_RNG[2]*(2*q0 - 2*q2*SH_RNG[4]) - P[1][1]*SH_RNG[1]*SH_RNG[2]*(2*q1 - 2*q3*SH_RNG[4]) - P[2][1]*SH_RNG[1]*SH_RNG[2]*(2*q2 + 2*q0*SH_RNG[4]) + P[3][1]*SH_RNG[1]*SH_RNG[2]*(2*q3 + 2*q1*SH_RNG[4])) - SH_RNG[1]*SH_RNG[2]*(2*q2 + 2*q0*SH_RNG[4])*(P[9][2]*SH_RNG[3] - P[22][2]*SH_RNG[3] + P[0][2]*SH_RNG[1]*SH_RNG[2]*(2*q0 - 2*q2*SH_RNG[4]) - P[1][2]*SH_RNG[1]*SH_RNG[2]*(2*q1 - 2*q3*SH_RNG[4]) - P[2][2]*SH_RNG[1]*SH_RNG[2]*(2*q2 + 2*q0*SH_RNG[4]) + P[3][2]*SH_RNG[1]*SH_RNG[2]*(2*q3 + 2*q1*SH_RNG[4])) + SH_RNG[1]*SH_RNG[2]*(2*q3 + 2*q1*SH_RNG[4])*(P[9][3]*SH_RNG[3] - P[22][3]*SH_RNG[3] + P[0][3]*SH_RNG[1]*SH_RNG[2]*(2*q0 - 2*q2*SH_RNG[4]) - P[1][3]*SH_RNG[1]*SH_RNG[2]*(2*q1 - 2*q3*SH_RNG[4]) - P[2][3]*SH_RNG[1]*SH_RNG[2]*(2*q2 + 2*q0*SH_RNG[4]) + P[3][3]*SH_RNG[1]*SH_RNG[2]*(2*q3 + 2*q1*SH_RNG[4]))); + SK_RNG[1] = 2*q1 - 2*q3*SH_RNG[4]; + SK_RNG[2] = 2*q0 - 2*q2*SH_RNG[4]; + SK_RNG[3] = 2*q3 + 2*q1*SH_RNG[4]; + SK_RNG[4] = 2*q2 + 2*q0*SH_RNG[4]; + SK_RNG[5] = SH_RNG[2]; + Kfusion[22] = SK_RNG[0]*(P[22][9]*SH_RNG[3] - P[22][22]*SH_RNG[3] + P[22][0]*SH_RNG[1]*SK_RNG[2]*SK_RNG[5] - P[22][1]*SH_RNG[1]*SK_RNG[1]*SK_RNG[5] - P[22][2]*SH_RNG[1]*SK_RNG[4]*SK_RNG[5] + P[22][3]*SH_RNG[1]*SK_RNG[3]*SK_RNG[5]); + + // Calculate the measurement innovation + rngPred = (ptd - pd)/cosRngTilt; + innovRng = rngPred - rngMea; + //printf("mea=%5.1f, pred=%5.1f, pd=%5.1f, ptd=%5.2f\n", rngMea, rngPred, pd, ptd); + + // Check the innovation for consistency and don't fuse if > 5Sigma + if ((innovRng*innovRng*SK_RNG[0]) < 25) + { + // correct the state vector + states[22] = states[22] - Kfusion[22] * innovRng; + + // correct the covariance P = (I - K*H)*P + P[22][22] = P[22][22] - Kfusion[22] * H_RNG[22] * P[22][22]; + P[22][22] = ConstrainFloat(P[22][22], 0.0f, 10000.0f); + } + } + +} + +void AttPosEKF::zeroCols(float (&covMat)[n_states][n_states], uint8_t first, uint8_t last) +{ + uint8_t row; + uint8_t col; + for (col=first; col<=last; col++) + { + for (row=0; row < n_states; row++) + { + covMat[row][col] = 0.0; + } + } +} + +float AttPosEKF::sq(float valIn) +{ + return valIn*valIn; +} + +// Store states in a history array along with time stamp +void AttPosEKF::StoreStates(uint64_t timestamp_ms) +{ + for (unsigned i=0; i<n_states; i++) + storedStates[i][storeIndex] = states[i]; + statetimeStamp[storeIndex] = timestamp_ms; + storeIndex++; + if (storeIndex == data_buffer_size) + storeIndex = 0; +} + +void AttPosEKF::ResetStoredStates() +{ + // reset all stored states + memset(&storedStates[0][0], 0, sizeof(storedStates)); + memset(&statetimeStamp[0], 0, sizeof(statetimeStamp)); + + // reset store index to first + storeIndex = 0; + + // overwrite all existing states + for (unsigned i = 0; i < n_states; i++) { + storedStates[i][storeIndex] = states[i]; + } + + statetimeStamp[storeIndex] = millis(); + + // increment to next storage index + storeIndex++; +} + +// Output the state vector stored at the time that best matches that specified by msec +int AttPosEKF::RecallStates(float* statesForFusion, uint64_t msec) +{ + int ret = 0; + + int64_t bestTimeDelta = 200; + unsigned bestStoreIndex = 0; + for (unsigned storeIndex = 0; storeIndex < data_buffer_size; storeIndex++) + { + // Work around a GCC compiler bug - we know 64bit support on ARM is + // sketchy in GCC. + uint64_t timeDelta; + + if (msec > statetimeStamp[storeIndex]) { + timeDelta = msec - statetimeStamp[storeIndex]; + } else { + timeDelta = statetimeStamp[storeIndex] - msec; + } + + if (timeDelta < bestTimeDelta) + { + bestStoreIndex = storeIndex; + bestTimeDelta = timeDelta; + } + } + if (bestTimeDelta < 200) // only output stored state if < 200 msec retrieval error + { + for (unsigned i=0; i < n_states; i++) { + if (isfinite(storedStates[i][bestStoreIndex])) { + statesForFusion[i] = storedStates[i][bestStoreIndex]; + } else if (isfinite(states[i])) { + statesForFusion[i] = states[i]; + } else { + // There is not much we can do here, except reporting the error we just + // found. + ret++; + } + } + } + else // otherwise output current state + { + for (unsigned i = 0; i < n_states; i++) { + if (isfinite(states[i])) { + statesForFusion[i] = states[i]; + } else { + ret++; + } + } + } + + return ret; +} + +void AttPosEKF::quat2Tnb(Mat3f &Tnb, const float (&quat)[4]) +{ + // Calculate the nav to body cosine matrix + float q00 = sq(quat[0]); + float q11 = sq(quat[1]); + float q22 = sq(quat[2]); + float q33 = sq(quat[3]); + float q01 = quat[0]*quat[1]; + float q02 = quat[0]*quat[2]; + float q03 = quat[0]*quat[3]; + float q12 = quat[1]*quat[2]; + float q13 = quat[1]*quat[3]; + float q23 = quat[2]*quat[3]; + + Tnb.x.x = q00 + q11 - q22 - q33; + Tnb.y.y = q00 - q11 + q22 - q33; + Tnb.z.z = q00 - q11 - q22 + q33; + Tnb.y.x = 2*(q12 - q03); + Tnb.z.x = 2*(q13 + q02); + Tnb.x.y = 2*(q12 + q03); + Tnb.z.y = 2*(q23 - q01); + Tnb.x.z = 2*(q13 - q02); + Tnb.y.z = 2*(q23 + q01); +} + +void AttPosEKF::quat2Tbn(Mat3f &Tbn, const float (&quat)[4]) +{ + // Calculate the body to nav cosine matrix + float q00 = sq(quat[0]); + float q11 = sq(quat[1]); + float q22 = sq(quat[2]); + float q33 = sq(quat[3]); + float q01 = quat[0]*quat[1]; + float q02 = quat[0]*quat[2]; + float q03 = quat[0]*quat[3]; + float q12 = quat[1]*quat[2]; + float q13 = quat[1]*quat[3]; + float q23 = quat[2]*quat[3]; + + Tbn.x.x = q00 + q11 - q22 - q33; + Tbn.y.y = q00 - q11 + q22 - q33; + Tbn.z.z = q00 - q11 - q22 + q33; + Tbn.x.y = 2*(q12 - q03); + Tbn.x.z = 2*(q13 + q02); + Tbn.y.x = 2*(q12 + q03); + Tbn.y.z = 2*(q23 - q01); + Tbn.z.x = 2*(q13 - q02); + Tbn.z.y = 2*(q23 + q01); +} + +void AttPosEKF::eul2quat(float (&quat)[4], const float (&eul)[3]) +{ + float u1 = cos(0.5f*eul[0]); + float u2 = cos(0.5f*eul[1]); + float u3 = cos(0.5f*eul[2]); + float u4 = sin(0.5f*eul[0]); + float u5 = sin(0.5f*eul[1]); + float u6 = sin(0.5f*eul[2]); + quat[0] = u1*u2*u3+u4*u5*u6; + quat[1] = u4*u2*u3-u1*u5*u6; + quat[2] = u1*u5*u3+u4*u2*u6; + quat[3] = u1*u2*u6-u4*u5*u3; +} + +void AttPosEKF::quat2eul(float (&y)[3], const float (&u)[4]) +{ + y[0] = atan2f((2.0f*(u[2]*u[3]+u[0]*u[1])) , (u[0]*u[0]-u[1]*u[1]-u[2]*u[2]+u[3]*u[3])); + y[1] = -asinf(2.0f*(u[1]*u[3]-u[0]*u[2])); + y[2] = atan2f((2.0f*(u[1]*u[2]+u[0]*u[3])) , (u[0]*u[0]+u[1]*u[1]-u[2]*u[2]-u[3]*u[3])); +} + +void AttPosEKF::calcvelNED(float (&velNED)[3], float gpsCourse, float gpsGndSpd, float gpsVelD) +{ + velNED[0] = gpsGndSpd*cosf(gpsCourse); + velNED[1] = gpsGndSpd*sinf(gpsCourse); + velNED[2] = gpsVelD; +} + +void AttPosEKF::calcposNED(float (&posNED)[3], double lat, double lon, float hgt, double latRef, double lonRef, float hgtRef) +{ + posNED[0] = earthRadius * (lat - latRef); + posNED[1] = earthRadius * cos(latRef) * (lon - lonRef); + posNED[2] = -(hgt - hgtRef); +} + +void AttPosEKF::calcLLH(float (&posNED)[3], float lat, float lon, float hgt, float latRef, float lonRef, float hgtRef) +{ + lat = latRef + posNED[0] * earthRadiusInv; + lon = lonRef + posNED[1] * earthRadiusInv / cos(latRef); + hgt = hgtRef - posNED[2]; +} + +void AttPosEKF::OnGroundCheck() +{ + onGround = (((sq(velNED[0]) + sq(velNED[1]) + sq(velNED[2])) < 4.0f) && (VtasMeas < 6.0f)); + if (staticMode) { + staticMode = (!refSet || (GPSstatus < GPS_FIX_3D)); + } +} + +void AttPosEKF::calcEarthRateNED(Vector3f &omega, float latitude) +{ + //Define Earth rotation vector in the NED navigation frame + omega.x = earthRate*cosf(latitude); + omega.y = 0.0f; + omega.z = -earthRate*sinf(latitude); +} + +void AttPosEKF::CovarianceInit() +{ + // Calculate the initial covariance matrix P + P[0][0] = 0.25f * sq(1.0f*deg2rad); + P[1][1] = 0.25f * sq(1.0f*deg2rad); + P[2][2] = 0.25f * sq(1.0f*deg2rad); + P[3][3] = 0.25f * sq(10.0f*deg2rad); + P[4][4] = sq(0.7f); + P[5][5] = P[4][4]; + P[6][6] = sq(0.7f); + P[7][7] = sq(15.0f); + P[8][8] = P[7][7]; + P[9][9] = sq(5.0f); + P[10][10] = sq(0.1f*deg2rad*dtIMU); + P[11][11] = P[10][10]; + P[12][12] = P[10][10]; + P[13][13] = sq(0.2f*dtIMU); + P[14][14] = sq(8.0f); + P[15][14] = P[14][14]; + P[16][16] = sq(0.02f); + P[17][17] = P[16][16]; + P[18][18] = P[16][16]; + P[19][19] = sq(0.02f); + P[20][20] = P[19][19]; + P[21][21] = P[19][19]; + P[22][22] = sq(0.5f); +} + +float AttPosEKF::ConstrainFloat(float val, float min, float max) +{ + float ret; + if (val > max) { + ret = max; + ekf_debug("> max: %8.4f, val: %8.4f", max, val); + } else if (val < min) { + ret = min; + ekf_debug("< min: %8.4f, val: %8.4f", min, val); + } else { + ret = val; + } + + if (!isfinite(val)) { + ekf_debug("constrain: non-finite!"); + } + + return ret; +} + +void AttPosEKF::ConstrainVariances() +{ + if (!numericalProtection) { + return; + } + + // State vector: + // 0-3: quaternions (q0, q1, q2, q3) + // 4-6: Velocity - m/sec (North, East, Down) + // 7-9: Position - m (North, East, Down) + // 10-12: Delta Angle bias - rad (X,Y,Z) + // 13: Delta Velocity bias - m/s (Z) + // 14-15: Wind Vector - m/sec (North,East) + // 16-18: Earth Magnetic Field Vector - gauss (North, East, Down) + // 19-21: Body Magnetic Field Vector - gauss (X,Y,Z) + // 22: Terrain offset - m + + // Constrain quaternion variances + for (unsigned i = 0; i <= 3; i++) { + P[i][i] = ConstrainFloat(P[i][i], 0.0f, 1.0f); + } + + // Constrain velocity variances + for (unsigned i = 4; i <= 6; i++) { + P[i][i] = ConstrainFloat(P[i][i], 0.0f, 1.0e3f); + } + + // Constrain position variances + for (unsigned i = 7; i <= 9; i++) { + P[i][i] = ConstrainFloat(P[i][i], 0.0f, 1.0e6f); + } + + // Constrain delta angle bias variances + for (unsigned i = 10; i <= 12; i++) { + P[i][i] = ConstrainFloat(P[i][i], 0.0f, sq(0.12f * dtIMU)); + } + + // Constrain delta velocity bias variance + P[13][13] = ConstrainFloat(P[13][13], 0.0f, sq(1.0f * dtIMU)); + + // Wind velocity variances + for (unsigned i = 14; i <= 15; i++) { + P[i][i] = ConstrainFloat(P[i][i], 0.0f, 1.0e3f); + } + + // Earth magnetic field variances + for (unsigned i = 16; i <= 18; i++) { + P[i][i] = ConstrainFloat(P[i][i], 0.0f, 1.0f); + } + + // Body magnetic field variances + for (unsigned i = 19; i <= 21; i++) { + P[i][i] = ConstrainFloat(P[i][i], 0.0f, 1.0f); + } + + // Constrain terrain offset variance + P[22][22] = ConstrainFloat(P[22][22], 0.0f, 10000.0f); +} + +void AttPosEKF::ConstrainStates() +{ + if (!numericalProtection) { + return; + } + + // State vector: + // 0-3: quaternions (q0, q1, q2, q3) + // 4-6: Velocity - m/sec (North, East, Down) + // 7-9: Position - m (North, East, Down) + // 10-12: Delta Angle bias - rad (X,Y,Z) + // 13: Delta Velocity bias - m/s (Z) + // 14-15: Wind Vector - m/sec (North,East) + // 16-18: Earth Magnetic Field Vector - gauss (North, East, Down) + // 19-21: Body Magnetic Field Vector - gauss (X,Y,Z) + // 22: Terrain offset - m + + // Constrain quaternion + for (unsigned i = 0; i <= 3; i++) { + states[i] = ConstrainFloat(states[i], -1.0f, 1.0f); + } + + // Constrain velocities to what GPS can do for us + for (unsigned i = 4; i <= 6; i++) { + states[i] = ConstrainFloat(states[i], -5.0e2f, 5.0e2f); + } + + // Constrain position to a reasonable vehicle range (in meters) + for (unsigned i = 7; i <= 8; i++) { + states[i] = ConstrainFloat(states[i], -1.0e6f, 1.0e6f); + } + + // Constrain altitude + states[9] = ConstrainFloat(states[9], -4.0e4f, 1.0e4f); + + // Angle bias limit - set to 8 degrees / sec + for (unsigned i = 10; i <= 12; i++) { + states[i] = ConstrainFloat(states[i], -0.12f * dtIMU, 0.12f * dtIMU); + } + + // Constrain delta velocity bias + states[13] = ConstrainFloat(states[13], -1.0f * dtIMU, 1.0f * dtIMU); + + // Wind velocity limits - assume 120 m/s max velocity + for (unsigned i = 14; i <= 15; i++) { + states[i] = ConstrainFloat(states[i], -120.0f, 120.0f); + } + + // Earth magnetic field limits (in Gauss) + for (unsigned i = 16; i <= 18; i++) { + states[i] = ConstrainFloat(states[i], -1.0f, 1.0f); + } + + // Body magnetic field variances (in Gauss). + // the max offset should be in this range. + for (unsigned i = 19; i <= 21; i++) { + states[i] = ConstrainFloat(states[i], -0.5f, 0.5f); + } + + // Constrain terrain offset + states[22] = ConstrainFloat(states[22], -1000.0f, 1000.0f); + +} + +void AttPosEKF::ForceSymmetry() +{ + if (!numericalProtection) { + return; + } + + // Force symmetry on the covariance matrix to prevent ill-conditioning + // of the matrix which would cause the filter to blow-up + for (unsigned i = 1; i < n_states; i++) + { + for (uint8_t j = 0; j < i; j++) + { + P[i][j] = 0.5f * (P[i][j] + P[j][i]); + P[j][i] = P[i][j]; + } + } +} + +bool AttPosEKF::FilterHealthy() +{ + if (!statesInitialised) { + return false; + } + + // XXX Check state vector for NaNs and ill-conditioning + + // Check if any of the major inputs timed out + if (current_ekf_state.posTimeout || current_ekf_state.velTimeout || current_ekf_state.hgtTimeout) { + return false; + } + + // Nothing fired, return ok. + return true; +} + +/** + * Reset the filter position states + * + * This resets the position to the last GPS measurement + * or to zero in case of static position. + */ +void AttPosEKF::ResetPosition(void) +{ + if (staticMode) { + states[7] = 0; + states[8] = 0; + } else if (GPSstatus >= GPS_FIX_3D) { + + // reset the states from the GPS measurements + states[7] = posNE[0]; + states[8] = posNE[1]; + } +} + +/** + * Reset the height state. + * + * This resets the height state with the last altitude measurements + */ +void AttPosEKF::ResetHeight(void) +{ + // write to the state vector + states[9] = -hgtMea; +} + +/** + * Reset the velocity state. + */ +void AttPosEKF::ResetVelocity(void) +{ + if (staticMode) { + states[4] = 0.0f; + states[5] = 0.0f; + states[6] = 0.0f; + } else if (GPSstatus >= GPS_FIX_3D) { + + states[4] = velNED[0]; // north velocity from last reading + states[5] = velNED[1]; // east velocity from last reading + states[6] = velNED[2]; // down velocity from last reading + } +} + + +void AttPosEKF::FillErrorReport(struct ekf_status_report *err) +{ + for (unsigned i = 0; i < n_states; i++) + { + err->states[i] = states[i]; + } + + err->velHealth = current_ekf_state.velHealth; + err->posHealth = current_ekf_state.posHealth; + err->hgtHealth = current_ekf_state.hgtHealth; + err->velTimeout = current_ekf_state.velTimeout; + err->posTimeout = current_ekf_state.posTimeout; + err->hgtTimeout = current_ekf_state.hgtTimeout; +} + +bool AttPosEKF::StatesNaN(struct ekf_status_report *err_report) { + bool err = false; + + // check all integrators + if (!isfinite(summedDelAng.x) || !isfinite(summedDelAng.y) || !isfinite(summedDelAng.z)) { + err_report->statesNaN = true; + ekf_debug("summedDelAng NaN: x: %f y: %f z: %f", (double)summedDelAng.x, (double)summedDelAng.y, (double)summedDelAng.z); + err = true; + goto out; + } // delta angles + + if (!isfinite(correctedDelAng.x) || !isfinite(correctedDelAng.y) || !isfinite(correctedDelAng.z)) { + err_report->statesNaN = true; + ekf_debug("correctedDelAng NaN: x: %f y: %f z: %f", (double)correctedDelAng.x, (double)correctedDelAng.y, (double)correctedDelAng.z); + err = true; + goto out; + } // delta angles + + if (!isfinite(summedDelVel.x) || !isfinite(summedDelVel.y) || !isfinite(summedDelVel.z)) { + err_report->statesNaN = true; + ekf_debug("summedDelVel NaN: x: %f y: %f z: %f", (double)summedDelVel.x, (double)summedDelVel.y, (double)summedDelVel.z); + err = true; + goto out; + } // delta velocities + + // check all states and covariance matrices + for (unsigned i = 0; i < n_states; i++) { + for (unsigned j = 0; j < n_states; j++) { + if (!isfinite(KH[i][j])) { + + err_report->covarianceNaN = true; + err = true; + ekf_debug("KH NaN"); + goto out; + } // intermediate result used for covariance updates + + if (!isfinite(KHP[i][j])) { + + err_report->covarianceNaN = true; + err = true; + ekf_debug("KHP NaN"); + goto out; + } // intermediate result used for covariance updates + + if (!isfinite(P[i][j])) { + + err_report->covarianceNaN = true; + err = true; + ekf_debug("P NaN"); + } // covariance matrix + } + + if (!isfinite(Kfusion[i])) { + + err_report->kalmanGainsNaN = true; + ekf_debug("Kfusion NaN"); + err = true; + goto out; + } // Kalman gains + + if (!isfinite(states[i])) { + + err_report->statesNaN = true; + ekf_debug("states NaN: i: %u val: %f", i, (double)states[i]); + err = true; + goto out; + } // state matrix + } + +out: + if (err) { + FillErrorReport(err_report); + } + + return err; + +} + +/** + * Check the filter inputs and bound its operational state + * + * This check will reset the filter states if required + * due to a failure of consistency or timeout checks. + * it should be run after the measurement data has been + * updated, but before any of the fusion steps are + * executed. + */ +int AttPosEKF::CheckAndBound() +{ + + // Store the old filter state + bool currStaticMode = staticMode; + + // Reset the filter if the states went NaN + if (StatesNaN(&last_ekf_error)) { + ekf_debug("re-initializing dynamic"); + + InitializeDynamic(velNED, magDeclination); + + return 1; + } + + // Reset the filter if the IMU data is too old + if (dtIMU > 0.3f) { + + ResetVelocity(); + ResetPosition(); + ResetHeight(); + ResetStoredStates(); + + // that's all we can do here, return + return 2; + } + + // Check if we're on ground - this also sets static mode. + OnGroundCheck(); + + // Check if we switched between states + if (currStaticMode != staticMode) { + ResetVelocity(); + ResetPosition(); + ResetHeight(); + ResetStoredStates(); + + return 3; + } + + return 0; +} + +void AttPosEKF::AttitudeInit(float ax, float ay, float az, float mx, float my, float mz, float declination, float *initQuat) +{ + float initialRoll, initialPitch; + float cosRoll, sinRoll, cosPitch, sinPitch; + float magX, magY; + float initialHdg, cosHeading, sinHeading; + + initialRoll = atan2f(-ay, -az); + initialPitch = atan2f(ax, -az); + + cosRoll = cosf(initialRoll); + sinRoll = sinf(initialRoll); + cosPitch = cosf(initialPitch); + sinPitch = sinf(initialPitch); + + magX = mx * cosPitch + my * sinRoll * sinPitch + mz * cosRoll * sinPitch; + + magY = my * cosRoll - mz * sinRoll; + + initialHdg = atan2f(-magY, magX); + /* true heading is the mag heading minus declination */ + initialHdg += declination; + + cosRoll = cosf(initialRoll * 0.5f); + sinRoll = sinf(initialRoll * 0.5f); + + cosPitch = cosf(initialPitch * 0.5f); + sinPitch = sinf(initialPitch * 0.5f); + + cosHeading = cosf(initialHdg * 0.5f); + sinHeading = sinf(initialHdg * 0.5f); + + initQuat[0] = cosRoll * cosPitch * cosHeading + sinRoll * sinPitch * sinHeading; + initQuat[1] = sinRoll * cosPitch * cosHeading - cosRoll * sinPitch * sinHeading; + initQuat[2] = cosRoll * sinPitch * cosHeading + sinRoll * cosPitch * sinHeading; + initQuat[3] = cosRoll * cosPitch * sinHeading - sinRoll * sinPitch * cosHeading; + + /* normalize */ + float norm = sqrtf(initQuat[0]*initQuat[0] + initQuat[1]*initQuat[1] + initQuat[2]*initQuat[2] + initQuat[3]*initQuat[3]); + + initQuat[0] /= norm; + initQuat[1] /= norm; + initQuat[2] /= norm; + initQuat[3] /= norm; +} + +void AttPosEKF::InitializeDynamic(float (&initvelNED)[3], float declination) +{ + + // Fill variables with valid data + velNED[0] = initvelNED[0]; + velNED[1] = initvelNED[1]; + velNED[2] = initvelNED[2]; + magDeclination = declination; + + // Calculate initial filter quaternion states from raw measurements + float initQuat[4]; + Vector3f initMagXYZ; + initMagXYZ = magData - magBias; + AttitudeInit(accel.x, accel.y, accel.z, initMagXYZ.x, initMagXYZ.y, initMagXYZ.z, declination, initQuat); + + // Calculate initial Tbn matrix and rotate Mag measurements into NED + // to set initial NED magnetic field states + Mat3f DCM; + quat2Tbn(DCM, initQuat); + Vector3f initMagNED; + initMagNED.x = DCM.x.x*initMagXYZ.x + DCM.x.y*initMagXYZ.y + DCM.x.z*initMagXYZ.z; + initMagNED.y = DCM.y.x*initMagXYZ.x + DCM.y.y*initMagXYZ.y + DCM.y.z*initMagXYZ.z; + initMagNED.z = DCM.z.x*initMagXYZ.x + DCM.z.y*initMagXYZ.y + DCM.z.z*initMagXYZ.z; + + magstate.q0 = initQuat[0]; + magstate.q1 = initQuat[1]; + magstate.q2 = initQuat[2]; + magstate.q3 = initQuat[3]; + magstate.magN = initMagNED.x; + magstate.magE = initMagNED.y; + magstate.magD = initMagNED.z; + magstate.magXbias = magBias.x; + magstate.magYbias = magBias.y; + magstate.magZbias = magBias.z; + magstate.R_MAG = sq(magMeasurementSigma); + magstate.DCM = DCM; + + // write to state vector + for (uint8_t j=0; j<=3; j++) states[j] = initQuat[j]; // quaternions + for (uint8_t j=4; j<=6; j++) states[j] = initvelNED[j-4]; // velocities + for (uint8_t j=7; j<=15; j++) states[j] = 0.0f; // positions, dAngBias, dVelBias, windVel + states[16] = initMagNED.x; // Magnetic Field North + states[17] = initMagNED.y; // Magnetic Field East + states[18] = initMagNED.z; // Magnetic Field Down + states[19] = magBias.x; // Magnetic Field Bias X + states[20] = magBias.y; // Magnetic Field Bias Y + states[21] = magBias.z; // Magnetic Field Bias Z + states[22] = 0.0f; // terrain height + + ResetVelocity(); + ResetPosition(); + ResetHeight(); + + statesInitialised = true; + + // initialise the covariance matrix + CovarianceInit(); + + //Define Earth rotation vector in the NED navigation frame + calcEarthRateNED(earthRateNED, latRef); + +} + +void AttPosEKF::InitialiseFilter(float (&initvelNED)[3], double referenceLat, double referenceLon, float referenceHgt, float declination) +{ + // store initial lat,long and height + latRef = referenceLat; + lonRef = referenceLon; + hgtRef = referenceHgt; + refSet = true; + + // we are at reference altitude, so measurement must be zero + hgtMea = 0.0f; + + // the baro offset must be this difference now + baroHgtOffset = baroHgt - referenceHgt; + + memset(&last_ekf_error, 0, sizeof(last_ekf_error)); + + InitializeDynamic(initvelNED, declination); +} + +void AttPosEKF::ZeroVariables() +{ + + // Initialize on-init initialized variables + fusionModeGPS = 0; + covSkipCount = 0; + statesInitialised = false; + fuseVelData = false; + fusePosData = false; + fuseHgtData = false; + fuseMagData = false; + fuseVtasData = false; + onGround = true; + staticMode = true; + useAirspeed = true; + useCompass = true; + useRangeFinder = true; + numericalProtection = true; + refSet = false; + storeIndex = 0; + gpsHgt = 0.0f; + baroHgt = 0.0f; + GPSstatus = 0; + VtasMeas = 0.0f; + magDeclination = 0.0f; + + // Do the data structure init + for (unsigned i = 0; i < n_states; i++) { + for (unsigned j = 0; j < n_states; j++) { + KH[i][j] = 0.0f; // intermediate result used for covariance updates + KHP[i][j] = 0.0f; // intermediate result used for covariance updates + P[i][j] = 0.0f; // covariance matrix + } + + Kfusion[i] = 0.0f; // Kalman gains + states[i] = 0.0f; // state matrix + } + + correctedDelAng.zero(); + summedDelAng.zero(); + summedDelVel.zero(); + + dAngIMU.zero(); + dVelIMU.zero(); + + for (unsigned i = 0; i < data_buffer_size; i++) { + + for (unsigned j = 0; j < n_states; j++) { + storedStates[j][i] = 0.0f; + } + + statetimeStamp[i] = 0; + } + + memset(&magstate, 0, sizeof(magstate)); + magstate.q0 = 1.0f; + magstate.DCM.identity(); + + memset(¤t_ekf_state, 0, sizeof(current_ekf_state)); + +} + +void AttPosEKF::GetFilterState(struct ekf_status_report *state) +{ + memcpy(state, ¤t_ekf_state, sizeof(*state)); +} + +void AttPosEKF::GetLastErrorState(struct ekf_status_report *last_error) +{ + memcpy(last_error, &last_ekf_error, sizeof(*last_error)); +} diff --git a/src/modules/ekf_att_pos_estimator/estimator.h b/src/modules/ekf_att_pos_estimator/estimator.h new file mode 100644 index 000000000..e821089f2 --- /dev/null +++ b/src/modules/ekf_att_pos_estimator/estimator.h @@ -0,0 +1,352 @@ +#include <math.h> +#include <stdint.h> + +#pragma once + +#define GRAVITY_MSS 9.80665f +#define deg2rad 0.017453292f +#define rad2deg 57.295780f +#define pi 3.141592657f +#define earthRate 0.000072921f +#define earthRadius 6378145.0f +#define earthRadiusInv 1.5678540e-7f + +class Vector3f +{ +private: +public: + float x; + float y; + float z; + + float length(void) const; + void zero(void); +}; + +class Mat3f +{ +private: +public: + Vector3f x; + Vector3f y; + Vector3f z; + + Mat3f(); + + void identity(); + Mat3f transpose(void) const; +}; + +Vector3f operator*(float sclIn1, Vector3f vecIn1); +Vector3f operator+( Vector3f vecIn1, Vector3f vecIn2); +Vector3f operator-( Vector3f vecIn1, Vector3f vecIn2); +Vector3f operator*( Mat3f matIn, Vector3f vecIn); +Vector3f operator%( Vector3f vecIn1, Vector3f vecIn2); +Vector3f operator*(Vector3f vecIn1, float sclIn1); + +void swap_var(float &d1, float &d2); + +const unsigned int n_states = 23; +const unsigned int data_buffer_size = 50; + +enum GPS_FIX { + GPS_FIX_NOFIX = 0, + GPS_FIX_2D = 2, + GPS_FIX_3D = 3 +}; + +struct ekf_status_report { + bool velHealth; + bool posHealth; + bool hgtHealth; + bool velTimeout; + bool posTimeout; + bool hgtTimeout; + uint32_t velFailTime; + uint32_t posFailTime; + uint32_t hgtFailTime; + float states[n_states]; + bool statesNaN; + bool covarianceNaN; + bool kalmanGainsNaN; +}; + +class AttPosEKF { + +public: + + AttPosEKF(); + ~AttPosEKF(); + + + + /* ############################################## + * + * M A I N F I L T E R P A R A M E T E R S + * + * ########################################### */ + + /* + * parameters are defined here and initialised in + * the InitialiseParameters() (which is just 20 lines down) + */ + + float covTimeStepMax; // maximum time allowed between covariance predictions + float covDelAngMax; // maximum delta angle between covariance predictions + float rngFinderPitch; // pitch angle of laser range finder in radians. Zero is aligned with the Z body axis. Positive is RH rotation about Y body axis. + + float yawVarScale; + float windVelSigma; + float dAngBiasSigma; + float dVelBiasSigma; + float magEarthSigma; + float magBodySigma; + float gndHgtSigma; + + float vneSigma; + float vdSigma; + float posNeSigma; + float posDSigma; + float magMeasurementSigma; + float airspeedMeasurementSigma; + + float gyroProcessNoise; + float accelProcessNoise; + + float EAS2TAS; // ratio f true to equivalent airspeed + + void InitialiseParameters() + { + covTimeStepMax = 0.07f; // maximum time allowed between covariance predictions + covDelAngMax = 0.02f; // maximum delta angle between covariance predictions + rngFinderPitch = 0.0f; // pitch angle of laser range finder in radians. Zero is aligned with the Z body axis. Positive is RH rotation about Y body axis. + EAS2TAS = 1.0f; + + yawVarScale = 1.0f; + windVelSigma = 0.1f; + dAngBiasSigma = 5.0e-7f; + dVelBiasSigma = 1e-4f; + magEarthSigma = 3.0e-4f; + magBodySigma = 3.0e-4f; + gndHgtSigma = 0.02f; // assume 2% terrain gradient 1-sigma + + vneSigma = 0.2f; + vdSigma = 0.3f; + posNeSigma = 2.0f; + posDSigma = 2.0f; + + magMeasurementSigma = 0.05; + airspeedMeasurementSigma = 1.4f; + gyroProcessNoise = 1.4544411e-2f; + accelProcessNoise = 0.5f; + } + + struct { + unsigned obsIndex; + float MagPred[3]; + float SH_MAG[9]; + float q0; + float q1; + float q2; + float q3; + float magN; + float magE; + float magD; + float magXbias; + float magYbias; + float magZbias; + float R_MAG; + Mat3f DCM; + } magstate; + + + // Global variables + float KH[n_states][n_states]; // intermediate result used for covariance updates + float KHP[n_states][n_states]; // intermediate result used for covariance updates + float P[n_states][n_states]; // covariance matrix + float Kfusion[n_states]; // Kalman gains + float states[n_states]; // state matrix + float storedStates[n_states][data_buffer_size]; // state vectors stored for the last 50 time steps + uint32_t statetimeStamp[data_buffer_size]; // time stamp for each state vector stored + + float statesAtVelTime[n_states]; // States at the effective measurement time for posNE and velNED measurements + float statesAtPosTime[n_states]; // States at the effective measurement time for posNE and velNED measurements + float statesAtHgtTime[n_states]; // States at the effective measurement time for the hgtMea measurement + float statesAtMagMeasTime[n_states]; // filter satates at the effective measurement time + float statesAtVtasMeasTime[n_states]; // filter states at the effective measurement time + float statesAtRngTime[n_states]; // filter states at the effective measurement time + + Vector3f correctedDelAng; // delta angles about the xyz body axes corrected for errors (rad) + Vector3f correctedDelVel; // delta velocities along the XYZ body axes corrected for errors (m/s) + Vector3f summedDelAng; // summed delta angles about the xyz body axes corrected for errors (rad) + Vector3f summedDelVel; // summed delta velocities along the XYZ body axes corrected for errors (m/s) + float accNavMag; // magnitude of navigation accel (- used to adjust GPS obs variance (m/s^2) + Vector3f earthRateNED; // earths angular rate vector in NED (rad/s) + Vector3f angRate; // angular rate vector in XYZ body axes measured by the IMU (rad/s) + + Mat3f Tbn; // transformation matrix from body to NED coordinates + Mat3f Tnb; // transformation amtrix from NED to body coordinates + + Vector3f accel; // acceleration vector in XYZ body axes measured by the IMU (m/s^2) + Vector3f dVelIMU; + Vector3f dAngIMU; + float dtIMU; // time lapsed since the last IMU measurement or covariance update (sec) + uint8_t fusionModeGPS; // 0 = GPS outputs 3D velocity, 1 = GPS outputs 2D velocity, 2 = GPS outputs no velocity + float innovVelPos[6]; // innovation output + float varInnovVelPos[6]; // innovation variance output + + float velNED[3]; // North, East, Down velocity obs (m/s) + float posNE[2]; // North, East position obs (m) + float hgtMea; // measured height (m) + float baroHgtOffset; ///< the baro (weather) offset from normalized altitude + float rngMea; // Ground distance + float posNED[3]; // North, East Down position (m) + + float innovMag[3]; // innovation output + float varInnovMag[3]; // innovation variance output + Vector3f magData; // magnetometer flux radings in X,Y,Z body axes + float innovVtas; // innovation output + float innovRng; ///< Range finder innovation + float varInnovVtas; // innovation variance output + float VtasMeas; // true airspeed measurement (m/s) + float magDeclination; ///< magnetic declination + double latRef; // WGS-84 latitude of reference point (rad) + double lonRef; // WGS-84 longitude of reference point (rad) + float hgtRef; // WGS-84 height of reference point (m) + bool refSet; ///< flag to indicate if the reference position has been set + Vector3f magBias; // states representing magnetometer bias vector in XYZ body axes + unsigned covSkipCount; // Number of state prediction frames (IMU daya updates to skip before doing the covariance prediction + + // GPS input data variables + float gpsCourse; + float gpsVelD; + double gpsLat; + double gpsLon; + float gpsHgt; + uint8_t GPSstatus; + + // Baro input + float baroHgt; + + bool statesInitialised; + + bool fuseVelData; // this boolean causes the posNE and velNED obs to be fused + bool fusePosData; // this boolean causes the posNE and velNED obs to be fused + bool fuseHgtData; // this boolean causes the hgtMea obs to be fused + bool fuseMagData; // boolean true when magnetometer data is to be fused + bool fuseVtasData; // boolean true when airspeed data is to be fused + bool fuseRngData; ///< true when range data is fused + + bool onGround; ///< boolean true when the flight vehicle is on the ground (not flying) + bool staticMode; ///< boolean true if no position feedback is fused + bool useAirspeed; ///< boolean true if airspeed data is being used + bool useCompass; ///< boolean true if magnetometer data is being used + bool useRangeFinder; ///< true when rangefinder is being used + + struct ekf_status_report current_ekf_state; + struct ekf_status_report last_ekf_error; + + bool numericalProtection; + + unsigned storeIndex; + + +void UpdateStrapdownEquationsNED(); + +void CovariancePrediction(float dt); + +void FuseVelposNED(); + +void FuseMagnetometer(); + +void FuseAirspeed(); + +void FuseRangeFinder(); + +void FuseOpticalFlow(); + +void zeroRows(float (&covMat)[n_states][n_states], uint8_t first, uint8_t last); + +void zeroCols(float (&covMat)[n_states][n_states], uint8_t first, uint8_t last); + +void quatNorm(float (&quatOut)[4], const float quatIn[4]); + +// store staes along with system time stamp in msces +void StoreStates(uint64_t timestamp_ms); + +/** + * Recall the state vector. + * + * Recalls the vector stored at closest time to the one specified by msec + * + * @return zero on success, integer indicating the number of invalid states on failure. + * Does only copy valid states, if the statesForFusion vector was initialized + * correctly by the caller, the result can be safely used, but is a mixture + * time-wise where valid states were updated and invalid remained at the old + * value. + */ +int RecallStates(float *statesForFusion, uint64_t msec); + +void ResetStoredStates(); + +void quat2Tbn(Mat3f &Tbn, const float (&quat)[4]); + +void calcEarthRateNED(Vector3f &omega, float latitude); + +static void eul2quat(float (&quat)[4], const float (&eul)[3]); + +static void quat2eul(float (&eul)[3], const float (&quat)[4]); + +static void calcvelNED(float (&velNED)[3], float gpsCourse, float gpsGndSpd, float gpsVelD); + +static void calcposNED(float (&posNED)[3], double lat, double lon, float hgt, double latRef, double lonRef, float hgtRef); + +static void calcLLH(float (&posNED)[3], float lat, float lon, float hgt, float latRef, float lonRef, float hgtRef); + +static void quat2Tnb(Mat3f &Tnb, const float (&quat)[4]); + +static float sq(float valIn); + +void OnGroundCheck(); + +void CovarianceInit(); + +void InitialiseFilter(float (&initvelNED)[3], double referenceLat, double referenceLon, float referenceHgt, float declination); + +float ConstrainFloat(float val, float min, float max); + +void ConstrainVariances(); + +void ConstrainStates(); + +void ForceSymmetry(); + +int CheckAndBound(); + +void ResetPosition(); + +void ResetVelocity(); + +void ZeroVariables(); + +void GetFilterState(struct ekf_status_report *state); + +void GetLastErrorState(struct ekf_status_report *last_error); + +bool StatesNaN(struct ekf_status_report *err_report); +void FillErrorReport(struct ekf_status_report *err); + +void InitializeDynamic(float (&initvelNED)[3], float declination); + +protected: + +bool FilterHealthy(); + +void ResetHeight(void); + +void AttitudeInit(float ax, float ay, float az, float mx, float my, float mz, float declination, float *initQuat); + +}; + +uint32_t millis(); + diff --git a/src/modules/att_pos_estimator_ekf/module.mk b/src/modules/ekf_att_pos_estimator/module.mk index 8d4a40d95..6fefec2c2 100644 --- a/src/modules/att_pos_estimator_ekf/module.mk +++ b/src/modules/ekf_att_pos_estimator/module.mk @@ -1,6 +1,6 @@ ############################################################################ # -# Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved. +# Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. # # Redistribution and use in source and binary forms, with or without # modification, are permitted provided that the following conditions @@ -32,11 +32,11 @@ ############################################################################ # -# Full attitude / position Extended Kalman Filter +# Main EKF Attitude and Position Estimator # -MODULE_COMMAND = att_pos_estimator_ekf +MODULE_COMMAND = ekf_att_pos_estimator -SRCS = kalman_main.cpp \ - KalmanNav.cpp \ - params.c +SRCS = ekf_att_pos_estimator_main.cpp \ + ekf_att_pos_estimator_params.c \ + estimator.cpp diff --git a/src/modules/fixedwing_att_control/fixedwing_att_control_att.c b/src/modules/fixedwing_att_control/fixedwing_att_control_att.c deleted file mode 100644 index 2aeca3a98..000000000 --- a/src/modules/fixedwing_att_control/fixedwing_att_control_att.c +++ /dev/null @@ -1,169 +0,0 @@ -/**************************************************************************** - * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: @author Thomas Gubler <thomasgubler@student.ethz.ch> - * - * Redistribution and use in source and binary forms, with or without - * modification, are permitted provided that the following conditions - * are met: - * - * 1. Redistributions of source code must retain the above copyright - * notice, this list of conditions and the following disclaimer. - * 2. Redistributions in binary form must reproduce the above copyright - * notice, this list of conditions and the following disclaimer in - * the documentation and/or other materials provided with the - * distribution. - * 3. Neither the name PX4 nor the names of its contributors may be - * used to endorse or promote products derived from this software - * without specific prior written permission. - * - * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS - * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT - * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS - * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE - * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, - * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, - * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS - * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED - * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT - * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN - * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE - * POSSIBILITY OF SUCH DAMAGE. - * - ****************************************************************************/ -/** - * @file fixedwing_att_control_rate.c - * Implementation of a fixed wing attitude controller. - */ - -#include <nuttx/config.h> -#include <stdio.h> -#include <stdlib.h> -#include <string.h> -#include <unistd.h> -#include <fcntl.h> -#include <errno.h> -#include <math.h> -#include <poll.h> -#include <time.h> -#include <drivers/drv_hrt.h> -#include <arch/board/board.h> -#include <uORB/uORB.h> - -#include <uORB/topics/vehicle_attitude.h> -#include <uORB/topics/vehicle_attitude_setpoint.h> -#include <uORB/topics/manual_control_setpoint.h> -#include <systemlib/param/param.h> -#include <systemlib/pid/pid.h> -#include <systemlib/geo/geo.h> -#include <systemlib/systemlib.h> - -#include "fixedwing_att_control_att.h" - - -struct fw_att_control_params { - float roll_p; - float rollrate_lim; - float pitch_p; - float pitchrate_lim; - float yawrate_lim; - float pitch_roll_compensation_p; -}; - -struct fw_pos_control_param_handles { - param_t roll_p; - param_t rollrate_lim; - param_t pitch_p; - param_t pitchrate_lim; - param_t yawrate_lim; - param_t pitch_roll_compensation_p; -}; - - - -/* Internal Prototypes */ -static int parameters_init(struct fw_pos_control_param_handles *h); -static int parameters_update(const struct fw_pos_control_param_handles *h, struct fw_att_control_params *p); - -static int parameters_init(struct fw_pos_control_param_handles *h) -{ - /* PID parameters */ - h->roll_p = param_find("FW_ROLL_P"); - h->rollrate_lim = param_find("FW_ROLLR_LIM"); - h->pitch_p = param_find("FW_PITCH_P"); - h->pitchrate_lim = param_find("FW_PITCHR_LIM"); - h->yawrate_lim = param_find("FW_YAWR_LIM"); - h->pitch_roll_compensation_p = param_find("FW_PITCH_RCOMP"); - - return OK; -} - -static int parameters_update(const struct fw_pos_control_param_handles *h, struct fw_att_control_params *p) -{ - param_get(h->roll_p, &(p->roll_p)); - param_get(h->rollrate_lim, &(p->rollrate_lim)); - param_get(h->pitch_p, &(p->pitch_p)); - param_get(h->pitchrate_lim, &(p->pitchrate_lim)); - param_get(h->yawrate_lim, &(p->yawrate_lim)); - param_get(h->pitch_roll_compensation_p, &(p->pitch_roll_compensation_p)); - - return OK; -} - -int fixedwing_att_control_attitude(const struct vehicle_attitude_setpoint_s *att_sp, - const struct vehicle_attitude_s *att, - const float speed_body[], - struct vehicle_rates_setpoint_s *rates_sp) -{ - static int counter = 0; - static bool initialized = false; - - static struct fw_att_control_params p; - static struct fw_pos_control_param_handles h; - - static PID_t roll_controller; - static PID_t pitch_controller; - - - if (!initialized) { - parameters_init(&h); - parameters_update(&h, &p); - pid_init(&roll_controller, p.roll_p, 0, 0, 0, p.rollrate_lim, PID_MODE_DERIVATIV_NONE, 0.0f); //P Controller - pid_init(&pitch_controller, p.pitch_p, 0, 0, 0, p.pitchrate_lim, PID_MODE_DERIVATIV_NONE, 0.0f); //P Controller - initialized = true; - } - - /* load new parameters with lower rate */ - if (counter % 100 == 0) { - /* update parameters from storage */ - parameters_update(&h, &p); - pid_set_parameters(&roll_controller, p.roll_p, 0, 0, 0, p.rollrate_lim); - pid_set_parameters(&pitch_controller, p.pitch_p, 0, 0, 0, p.pitchrate_lim); - } - - /* Roll (P) */ - rates_sp->roll = pid_calculate(&roll_controller, att_sp->roll_body, att->roll, 0, 0); - - - /* Pitch (P) */ - - /* compensate feedforward for loss of lift due to non-horizontal angle of wing */ - float pitch_sp_rollcompensation = p.pitch_roll_compensation_p * fabsf(sinf(att_sp->roll_body)); - /* set pitch plus feedforward roll compensation */ - rates_sp->pitch = pid_calculate(&pitch_controller, - att_sp->pitch_body + pitch_sp_rollcompensation, - att->pitch, 0, 0); - - /* Yaw (from coordinated turn constraint or lateral force) */ - rates_sp->yaw = (att->rollspeed * rates_sp->roll + 9.81f * sinf(att->roll) * cosf(att->pitch) + speed_body[0] * rates_sp->pitch * sinf(att->roll)) - / (speed_body[0] * cosf(att->roll) * cosf(att->pitch) + speed_body[2] * sinf(att->pitch)); - -// printf("rates_sp->yaw %.4f \n", (double)rates_sp->yaw); - - counter++; - - return 0; -} - - - diff --git a/src/modules/fixedwing_att_control/fixedwing_att_control_main.c b/src/modules/fixedwing_att_control/fixedwing_att_control_main.c deleted file mode 100644 index b6b4546c2..000000000 --- a/src/modules/fixedwing_att_control/fixedwing_att_control_main.c +++ /dev/null @@ -1,367 +0,0 @@ -/**************************************************************************** - * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: @author Thomas Gubler <thomasgubler@student.ethz.ch> - * @author Doug Weibel <douglas.weibel@colorado.edu> - * - * Redistribution and use in source and binary forms, with or without - * modification, are permitted provided that the following conditions - * are met: - * - * 1. Redistributions of source code must retain the above copyright - * notice, this list of conditions and the following disclaimer. - * 2. Redistributions in binary form must reproduce the above copyright - * notice, this list of conditions and the following disclaimer in - * the documentation and/or other materials provided with the - * distribution. - * 3. Neither the name PX4 nor the names of its contributors may be - * used to endorse or promote products derived from this software - * without specific prior written permission. - * - * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS - * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT - * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS - * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE - * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, - * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, - * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS - * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED - * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT - * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN - * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE - * POSSIBILITY OF SUCH DAMAGE. - * - ****************************************************************************/ -/** - * @file fixedwing_att_control.c - * Implementation of a fixed wing attitude controller. - */ - -#include <nuttx/config.h> -#include <stdio.h> -#include <stdlib.h> -#include <string.h> -#include <unistd.h> -#include <fcntl.h> -#include <errno.h> -#include <math.h> -#include <poll.h> -#include <time.h> -#include <drivers/drv_hrt.h> -#include <arch/board/board.h> -#include <uORB/uORB.h> -#include <uORB/topics/vehicle_global_position.h> -#include <uORB/topics/vehicle_global_position_setpoint.h> -#include <uORB/topics/vehicle_attitude.h> -#include <uORB/topics/vehicle_control_mode.h> -#include <uORB/topics/vehicle_status.h> -#include <uORB/topics/vehicle_attitude_setpoint.h> -#include <uORB/topics/manual_control_setpoint.h> -#include <uORB/topics/actuator_controls.h> -#include <uORB/topics/vehicle_rates_setpoint.h> -#include <uORB/topics/vehicle_global_position.h> -#include <uORB/topics/debug_key_value.h> -#include <systemlib/param/param.h> -#include <systemlib/pid/pid.h> -#include <systemlib/geo/geo.h> -#include <systemlib/perf_counter.h> -#include <systemlib/systemlib.h> - -#include "fixedwing_att_control_rate.h" -#include "fixedwing_att_control_att.h" - -/* Prototypes */ -/** - * Deamon management function. - */ -__EXPORT int fixedwing_att_control_main(int argc, char *argv[]); - -/** - * Mainloop of deamon. - */ -int fixedwing_att_control_thread_main(int argc, char *argv[]); - -/** - * Print the correct usage. - */ -static void usage(const char *reason); - -/* Variables */ -static bool thread_should_exit = false; /**< Deamon exit flag */ -static bool thread_running = false; /**< Deamon status flag */ -static int deamon_task; /**< Handle of deamon task / thread */ - -/* Main Thread */ -int fixedwing_att_control_thread_main(int argc, char *argv[]) -{ - /* read arguments */ - bool verbose = false; - - for (int i = 1; i < argc; i++) { - if (strcmp(argv[i], "-v") == 0 || strcmp(argv[i], "--verbose") == 0) { - verbose = true; - } - } - - /* welcome user */ - printf("[fixedwing att control] started\n"); - - /* declare and safely initialize all structs */ - struct vehicle_attitude_s att; - memset(&att, 0, sizeof(att)); - struct vehicle_attitude_setpoint_s att_sp; - memset(&att_sp, 0, sizeof(att_sp)); - struct vehicle_rates_setpoint_s rates_sp; - memset(&rates_sp, 0, sizeof(rates_sp)); - struct vehicle_global_position_s global_pos; - memset(&global_pos, 0, sizeof(global_pos)); - struct manual_control_setpoint_s manual_sp; - memset(&manual_sp, 0, sizeof(manual_sp)); - struct vehicle_control_mode_s control_mode; - memset(&control_mode, 0, sizeof(control_mode)); - struct vehicle_status_s vstatus; - memset(&vstatus, 0, sizeof(vstatus)); - - /* output structs */ - struct actuator_controls_s actuators; - memset(&actuators, 0, sizeof(actuators)); - - - /* publish actuator controls */ - for (unsigned i = 0; i < NUM_ACTUATOR_CONTROLS; i++) { - actuators.control[i] = 0.0f; - } - - orb_advert_t actuator_pub = orb_advertise(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, &actuators); - orb_advert_t rates_pub = orb_advertise(ORB_ID(vehicle_rates_setpoint), &rates_sp); - - /* subscribe */ - int att_sub = orb_subscribe(ORB_ID(vehicle_attitude)); - int att_sp_sub = orb_subscribe(ORB_ID(vehicle_attitude_setpoint)); - int global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position)); - int manual_sp_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); - int control_mode_sub = orb_subscribe(ORB_ID(vehicle_control_mode)); - int vehicle_status_sub = orb_subscribe(ORB_ID(vehicle_status)); - - /* Setup of loop */ - float gyro[3] = {0.0f, 0.0f, 0.0f}; - float speed_body[3] = {0.0f, 0.0f, 0.0f}; - struct pollfd fds = { .fd = att_sub, .events = POLLIN }; - - while (!thread_should_exit) { - /* wait for a sensor update, check for exit condition every 500 ms */ - poll(&fds, 1, 500); - - /* Check if there is a new position measurement or attitude setpoint */ - bool pos_updated; - orb_check(global_pos_sub, &pos_updated); - bool att_sp_updated; - orb_check(att_sp_sub, &att_sp_updated); - - /* get a local copy of attitude */ - orb_copy(ORB_ID(vehicle_attitude), att_sub, &att); - - if (att_sp_updated) - orb_copy(ORB_ID(vehicle_attitude_setpoint), att_sp_sub, &att_sp); - - if (pos_updated) { - orb_copy(ORB_ID(vehicle_global_position), global_pos_sub, &global_pos); - - if (att.R_valid) { - speed_body[0] = att.R[0][0] * global_pos.vx + att.R[0][1] * global_pos.vy + att.R[0][2] * global_pos.vz; - speed_body[1] = att.R[1][0] * global_pos.vx + att.R[1][1] * global_pos.vy + att.R[1][2] * global_pos.vz; - speed_body[2] = att.R[2][0] * global_pos.vx + att.R[2][1] * global_pos.vy + att.R[2][2] * global_pos.vz; - - } else { - speed_body[0] = 0; - speed_body[1] = 0; - speed_body[2] = 0; - - printf("FW ATT CONTROL: Did not get a valid R\n"); - } - } - - orb_copy(ORB_ID(manual_control_setpoint), manual_sp_sub, &manual_sp); - orb_copy(ORB_ID(vehicle_control_mode), control_mode_sub, &control_mode); - orb_copy(ORB_ID(vehicle_status), vehicle_status_sub, &vstatus); - - gyro[0] = att.rollspeed; - gyro[1] = att.pitchspeed; - gyro[2] = att.yawspeed; - - /* set manual setpoints if required */ - if (control_mode.flag_control_manual_enabled) { - if (control_mode.flag_control_attitude_enabled) { - - /* if the RC signal is lost, try to stay level and go slowly back down to ground */ - if (vstatus.rc_signal_lost) { - - /* put plane into loiter */ - att_sp.roll_body = 0.3f; - att_sp.pitch_body = 0.0f; - - /* limit throttle to 60 % of last value if sane */ - if (isfinite(manual_sp.throttle) && - (manual_sp.throttle >= 0.0f) && - (manual_sp.throttle <= 1.0f)) { - att_sp.thrust = 0.6f * manual_sp.throttle; - - } else { - att_sp.thrust = 0.0f; - } - - att_sp.yaw_body = 0; - - // XXX disable yaw control, loiter - - } else { - - att_sp.roll_body = manual_sp.roll; - att_sp.pitch_body = manual_sp.pitch; - att_sp.yaw_body = 0; - att_sp.thrust = manual_sp.throttle; - } - - att_sp.timestamp = hrt_absolute_time(); - - /* pass through flaps */ - if (isfinite(manual_sp.flaps)) { - actuators.control[4] = manual_sp.flaps; - - } else { - actuators.control[4] = 0.0f; - } - - } else { - /* directly pass through values */ - actuators.control[0] = manual_sp.roll; - /* positive pitch means negative actuator -> pull up */ - actuators.control[1] = manual_sp.pitch; - actuators.control[2] = manual_sp.yaw; - actuators.control[3] = manual_sp.throttle; - - if (isfinite(manual_sp.flaps)) { - actuators.control[4] = manual_sp.flaps; - - } else { - actuators.control[4] = 0.0f; - } - } - } - - /* execute attitude control if requested */ - if (control_mode.flag_control_attitude_enabled) { - /* attitude control */ - fixedwing_att_control_attitude(&att_sp, &att, speed_body, &rates_sp); - - /* angular rate control */ - fixedwing_att_control_rates(&rates_sp, gyro, &actuators); - - /* pass through throttle */ - actuators.control[3] = att_sp.thrust; - - /* set flaps to zero */ - actuators.control[4] = 0.0f; - - } - - /* publish rates */ - orb_publish(ORB_ID(vehicle_rates_setpoint), rates_pub, &rates_sp); - - /* sanity check and publish actuator outputs */ - if (isfinite(actuators.control[0]) && - isfinite(actuators.control[1]) && - isfinite(actuators.control[2]) && - isfinite(actuators.control[3])) { - orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators); - } - } - - printf("[fixedwing_att_control] exiting, stopping all motors.\n"); - thread_running = false; - - /* kill all outputs */ - for (unsigned i = 0; i < NUM_ACTUATOR_CONTROLS; i++) - actuators.control[i] = 0.0f; - - orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators); - - - - close(att_sub); - close(actuator_pub); - close(rates_pub); - - fflush(stdout); - exit(0); - - return 0; - -} - -/* Startup Functions */ - -static void -usage(const char *reason) -{ - if (reason) - fprintf(stderr, "%s\n", reason); - - fprintf(stderr, "usage: fixedwing_att_control {start|stop|status}\n\n"); - exit(1); -} - -/** - * The deamon app only briefly exists to start - * the background job. The stack size assigned in the - * Makefile does only apply to this management task. - * - * The actual stack size should be set in the call - * to task_create(). - */ -int fixedwing_att_control_main(int argc, char *argv[]) -{ - if (argc < 1) - usage("missing command"); - - if (!strcmp(argv[1], "start")) { - - if (thread_running) { - printf("fixedwing_att_control already running\n"); - /* this is not an error */ - exit(0); - } - - thread_should_exit = false; - deamon_task = task_spawn_cmd("fixedwing_att_control", - SCHED_DEFAULT, - SCHED_PRIORITY_MAX - 20, - 2048, - fixedwing_att_control_thread_main, - (argv) ? (const char **)&argv[2] : (const char **)NULL); - thread_running = true; - exit(0); - } - - if (!strcmp(argv[1], "stop")) { - thread_should_exit = true; - exit(0); - } - - if (!strcmp(argv[1], "status")) { - if (thread_running) { - printf("\tfixedwing_att_control is running\n"); - - } else { - printf("\tfixedwing_att_control not started\n"); - } - - exit(0); - } - - usage("unrecognized command"); - exit(1); -} - - - diff --git a/src/modules/fixedwing_att_control/fixedwing_att_control_rate.c b/src/modules/fixedwing_att_control/fixedwing_att_control_rate.c deleted file mode 100644 index cdab39edc..000000000 --- a/src/modules/fixedwing_att_control/fixedwing_att_control_rate.c +++ /dev/null @@ -1,211 +0,0 @@ -/**************************************************************************** - * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: Thomas Gubler <thomasgubler@student.ethz.ch> - * - * Redistribution and use in source and binary forms, with or without - * modification, are permitted provided that the following conditions - * are met: - * - * 1. Redistributions of source code must retain the above copyright - * notice, this list of conditions and the following disclaimer. - * 2. Redistributions in binary form must reproduce the above copyright - * notice, this list of conditions and the following disclaimer in - * the documentation and/or other materials provided with the - * distribution. - * 3. Neither the name PX4 nor the names of its contributors may be - * used to endorse or promote products derived from this software - * without specific prior written permission. - * - * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS - * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT - * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS - * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE - * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, - * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, - * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS - * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED - * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT - * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN - * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE - * POSSIBILITY OF SUCH DAMAGE. - * - ****************************************************************************/ -/** - * @file fixedwing_att_control_rate.c - * @author Thomas Gubler <thomasgubler@student.ethz.ch> - * - * Implementation of a fixed wing attitude controller. - * - */ - -#include <nuttx/config.h> -#include <stdio.h> -#include <stdlib.h> -#include <string.h> -#include <unistd.h> -#include <fcntl.h> -#include <errno.h> -#include <math.h> -#include <poll.h> -#include <time.h> -#include <drivers/drv_hrt.h> -#include <arch/board/board.h> -#include <uORB/uORB.h> - -#include <uORB/topics/vehicle_attitude.h> -#include <uORB/topics/vehicle_attitude_setpoint.h> -#include <uORB/topics/manual_control_setpoint.h> -#include <systemlib/param/param.h> -#include <systemlib/pid/pid.h> -#include <systemlib/geo/geo.h> -#include <systemlib/systemlib.h> - -#include "fixedwing_att_control_rate.h" - -/* - * Controller parameters, accessible via MAVLink - * - */ -// Roll control parameters -PARAM_DEFINE_FLOAT(FW_ROLLR_P, 0.9f); -PARAM_DEFINE_FLOAT(FW_ROLLR_I, 0.2f); -PARAM_DEFINE_FLOAT(FW_ROLLR_AWU, 0.9f); -PARAM_DEFINE_FLOAT(FW_ROLLR_LIM, 0.7f); // Roll rate limit in radians/sec, applies to the roll controller -PARAM_DEFINE_FLOAT(FW_ROLL_P, 4.0f); -PARAM_DEFINE_FLOAT(FW_PITCH_RCOMP, 0.1f); - -//Pitch control parameters -PARAM_DEFINE_FLOAT(FW_PITCHR_P, 0.8f); -PARAM_DEFINE_FLOAT(FW_PITCHR_I, 0.2f); -PARAM_DEFINE_FLOAT(FW_PITCHR_AWU, 0.8f); -PARAM_DEFINE_FLOAT(FW_PITCHR_LIM, 0.35f); // Pitch rate limit in radians/sec, applies to the pitch controller -PARAM_DEFINE_FLOAT(FW_PITCH_P, 8.0f); - -//Yaw control parameters //XXX TODO this is copy paste, asign correct values -PARAM_DEFINE_FLOAT(FW_YAWR_P, 0.3f); -PARAM_DEFINE_FLOAT(FW_YAWR_I, 0.0f); -PARAM_DEFINE_FLOAT(FW_YAWR_AWU, 0.0f); -PARAM_DEFINE_FLOAT(FW_YAWR_LIM, 0.35f); // Yaw rate limit in radians/sec - -/* feedforward compensation */ -PARAM_DEFINE_FLOAT(FW_PITCH_THR_P, 0.1f); /**< throttle to pitch coupling feedforward */ - -struct fw_rate_control_params { - float rollrate_p; - float rollrate_i; - float rollrate_awu; - float pitchrate_p; - float pitchrate_i; - float pitchrate_awu; - float yawrate_p; - float yawrate_i; - float yawrate_awu; - float pitch_thr_ff; -}; - -struct fw_rate_control_param_handles { - param_t rollrate_p; - param_t rollrate_i; - param_t rollrate_awu; - param_t pitchrate_p; - param_t pitchrate_i; - param_t pitchrate_awu; - param_t yawrate_p; - param_t yawrate_i; - param_t yawrate_awu; - param_t pitch_thr_ff; -}; - - - -/* Internal Prototypes */ -static int parameters_init(struct fw_rate_control_param_handles *h); -static int parameters_update(const struct fw_rate_control_param_handles *h, struct fw_rate_control_params *p); - -static int parameters_init(struct fw_rate_control_param_handles *h) -{ - /* PID parameters */ - h->rollrate_p = param_find("FW_ROLLR_P"); //TODO define rate params for fixed wing - h->rollrate_i = param_find("FW_ROLLR_I"); - h->rollrate_awu = param_find("FW_ROLLR_AWU"); - - h->pitchrate_p = param_find("FW_PITCHR_P"); - h->pitchrate_i = param_find("FW_PITCHR_I"); - h->pitchrate_awu = param_find("FW_PITCHR_AWU"); - - h->yawrate_p = param_find("FW_YAWR_P"); - h->yawrate_i = param_find("FW_YAWR_I"); - h->yawrate_awu = param_find("FW_YAWR_AWU"); - h->pitch_thr_ff = param_find("FW_PITCH_THR_P"); - - return OK; -} - -static int parameters_update(const struct fw_rate_control_param_handles *h, struct fw_rate_control_params *p) -{ - param_get(h->rollrate_p, &(p->rollrate_p)); - param_get(h->rollrate_i, &(p->rollrate_i)); - param_get(h->rollrate_awu, &(p->rollrate_awu)); - param_get(h->pitchrate_p, &(p->pitchrate_p)); - param_get(h->pitchrate_i, &(p->pitchrate_i)); - param_get(h->pitchrate_awu, &(p->pitchrate_awu)); - param_get(h->yawrate_p, &(p->yawrate_p)); - param_get(h->yawrate_i, &(p->yawrate_i)); - param_get(h->yawrate_awu, &(p->yawrate_awu)); - param_get(h->pitch_thr_ff, &(p->pitch_thr_ff)); - - return OK; -} - -int fixedwing_att_control_rates(const struct vehicle_rates_setpoint_s *rate_sp, - const float rates[], - struct actuator_controls_s *actuators) -{ - static int counter = 0; - static bool initialized = false; - - static struct fw_rate_control_params p; - static struct fw_rate_control_param_handles h; - - static PID_t roll_rate_controller; - static PID_t pitch_rate_controller; - static PID_t yaw_rate_controller; - - static uint64_t last_run = 0; - const float deltaT = (hrt_absolute_time() - last_run) / 1000000.0f; - last_run = hrt_absolute_time(); - - if (!initialized) { - parameters_init(&h); - parameters_update(&h, &p); - pid_init(&roll_rate_controller, p.rollrate_p, p.rollrate_i, 0, p.rollrate_awu, 1, PID_MODE_DERIVATIV_NONE, 0.0f); // set D part to 0 because the controller layout is with a PI rate controller - pid_init(&pitch_rate_controller, p.pitchrate_p, p.pitchrate_i, 0, p.pitchrate_awu, 1, PID_MODE_DERIVATIV_NONE, 0.0f); // set D part to 0 because the contpitcher layout is with a PI rate contpitcher - pid_init(&yaw_rate_controller, p.yawrate_p, p.yawrate_i, 0, p.yawrate_awu, 1, PID_MODE_DERIVATIV_NONE, 0.0f); // set D part to 0 because the contpitcher layout is with a PI rate contpitcher - initialized = true; - } - - /* load new parameters with lower rate */ - if (counter % 100 == 0) { - /* update parameters from storage */ - parameters_update(&h, &p); - pid_set_parameters(&roll_rate_controller, p.rollrate_p, p.rollrate_i, 0, p.rollrate_awu, 1); - pid_set_parameters(&pitch_rate_controller, p.pitchrate_p, p.pitchrate_i, 0, p.pitchrate_awu, 1); - pid_set_parameters(&yaw_rate_controller, p.yawrate_p, p.yawrate_i, 0, p.yawrate_awu, 1); - } - - - /* roll rate (PI) */ - actuators->control[0] = pid_calculate(&roll_rate_controller, rate_sp->roll, rates[0], 0.0f, deltaT); - /* pitch rate (PI) */ - actuators->control[1] = -pid_calculate(&pitch_rate_controller, rate_sp->pitch, rates[1], 0.0f, deltaT); - /* yaw rate (PI) */ - actuators->control[2] = pid_calculate(&yaw_rate_controller, rate_sp->yaw, rates[2], 0.0f, deltaT); - - counter++; - - return 0; -} - - - diff --git a/src/modules/fixedwing_att_control/module.mk b/src/modules/fixedwing_att_control/module.mk deleted file mode 100644 index fd1a8724a..000000000 --- a/src/modules/fixedwing_att_control/module.mk +++ /dev/null @@ -1,42 +0,0 @@ -############################################################################ -# -# Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved. -# -# Redistribution and use in source and binary forms, with or without -# modification, are permitted provided that the following conditions -# are met: -# -# 1. Redistributions of source code must retain the above copyright -# notice, this list of conditions and the following disclaimer. -# 2. Redistributions in binary form must reproduce the above copyright -# notice, this list of conditions and the following disclaimer in -# the documentation and/or other materials provided with the -# distribution. -# 3. Neither the name PX4 nor the names of its contributors may be -# used to endorse or promote products derived from this software -# without specific prior written permission. -# -# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS -# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT -# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS -# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE -# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, -# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, -# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS -# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED -# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT -# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN -# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE -# POSSIBILITY OF SUCH DAMAGE. -# -############################################################################ - -# -# Fixedwing Attitude Control application -# - -MODULE_COMMAND = fixedwing_att_control - -SRCS = fixedwing_att_control_main.c \ - fixedwing_att_control_att.c \ - fixedwing_att_control_rate.c diff --git a/src/modules/fixedwing_backside/fixedwing.cpp b/src/modules/fixedwing_backside/fixedwing.cpp index cfae07275..bbb39f20f 100644 --- a/src/modules/fixedwing_backside/fixedwing.cpp +++ b/src/modules/fixedwing_backside/fixedwing.cpp @@ -229,8 +229,8 @@ void BlockMultiModeBacksideAutopilot::update() _actuators.control[CH_RDR] = _manual.yaw; _actuators.control[CH_THR] = _manual.throttle; - } else if (_status.main_state == MAIN_STATE_SEATBELT || - _status.main_state == MAIN_STATE_EASY /* TODO, implement easy */) { + } else if (_status.main_state == MAIN_STATE_ALTCTL || + _status.main_state == MAIN_STATE_POSCTL /* TODO, implement pos control */) { // calculate velocity, XXX should be airspeed, but using ground speed for now // for the purpose of control we will limit the velocity feedback between diff --git a/src/modules/fixedwing_pos_control/fixedwing_pos_control_main.c b/src/modules/fixedwing_pos_control/fixedwing_pos_control_main.c deleted file mode 100644 index 888dd0942..000000000 --- a/src/modules/fixedwing_pos_control/fixedwing_pos_control_main.c +++ /dev/null @@ -1,479 +0,0 @@ -/**************************************************************************** - * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: @author Thomas Gubler <thomasgubler@student.ethz.ch> - * @author Doug Weibel <douglas.weibel@colorado.edu> - * - * Redistribution and use in source and binary forms, with or without - * modification, are permitted provided that the following conditions - * are met: - * - * 1. Redistributions of source code must retain the above copyright - * notice, this list of conditions and the following disclaimer. - * 2. Redistributions in binary form must reproduce the above copyright - * notice, this list of conditions and the following disclaimer in - * the documentation and/or other materials provided with the - * distribution. - * 3. Neither the name PX4 nor the names of its contributors may be - * used to endorse or promote products derived from this software - * without specific prior written permission. - * - * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS - * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT - * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS - * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE - * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, - * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, - * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS - * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED - * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT - * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN - * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE - * POSSIBILITY OF SUCH DAMAGE. - * - ****************************************************************************/ -/** - * @file fixedwing_pos_control.c - * Implementation of a fixed wing attitude controller. - */ - -#include <nuttx/config.h> -#include <stdio.h> -#include <stdlib.h> -#include <string.h> -#include <unistd.h> -#include <fcntl.h> -#include <errno.h> -#include <math.h> -#include <poll.h> -#include <time.h> -#include <drivers/drv_hrt.h> -#include <arch/board/board.h> -#include <uORB/uORB.h> -#include <uORB/topics/vehicle_global_position.h> -#include <uORB/topics/vehicle_global_position_setpoint.h> -#include <uORB/topics/vehicle_attitude_setpoint.h> -#include <uORB/topics/manual_control_setpoint.h> -#include <uORB/topics/actuator_controls.h> -#include <uORB/topics/vehicle_rates_setpoint.h> -#include <uORB/topics/vehicle_attitude.h> -#include <uORB/topics/parameter_update.h> -#include <systemlib/param/param.h> -#include <systemlib/pid/pid.h> -#include <systemlib/geo/geo.h> -#include <systemlib/perf_counter.h> -#include <systemlib/systemlib.h> - -/* - * Controller parameters, accessible via MAVLink - * - */ -PARAM_DEFINE_FLOAT(FW_HEAD_P, 0.1f); -PARAM_DEFINE_FLOAT(FW_HEADR_I, 0.1f); -PARAM_DEFINE_FLOAT(FW_HEADR_LIM, 1.5f); //TODO: think about reasonable value -PARAM_DEFINE_FLOAT(FW_XTRACK_P, 0.01745f); // Radians per meter off track -PARAM_DEFINE_FLOAT(FW_ALT_P, 0.1f); -PARAM_DEFINE_FLOAT(FW_ROLL_LIM, 0.7f); // Roll angle limit in radians -PARAM_DEFINE_FLOAT(FW_HEADR_P, 0.1f); -PARAM_DEFINE_FLOAT(FW_PITCH_LIM, 0.35f); /**< Pitch angle limit in radians per second */ - -struct fw_pos_control_params { - float heading_p; - float headingr_p; - float headingr_i; - float headingr_lim; - float xtrack_p; - float altitude_p; - float roll_lim; - float pitch_lim; -}; - -struct fw_pos_control_param_handles { - param_t heading_p; - param_t headingr_p; - param_t headingr_i; - param_t headingr_lim; - param_t xtrack_p; - param_t altitude_p; - param_t roll_lim; - param_t pitch_lim; -}; - - -struct planned_path_segments_s { - bool segment_type; - double start_lat; // Start of line or center of arc - double start_lon; - double end_lat; - double end_lon; - float radius; // Radius of arc - float arc_start_bearing; // Bearing from center to start of arc - float arc_sweep; // Angle (radians) swept out by arc around center. - // Positive for clockwise, negative for counter-clockwise -}; - - -/* Prototypes */ -/* Internal Prototypes */ -static int parameters_init(struct fw_pos_control_param_handles *h); -static int parameters_update(const struct fw_pos_control_param_handles *h, struct fw_pos_control_params *p); - -/** - * Deamon management function. - */ -__EXPORT int fixedwing_pos_control_main(int argc, char *argv[]); - -/** - * Mainloop of deamon. - */ -int fixedwing_pos_control_thread_main(int argc, char *argv[]); - -/** - * Print the correct usage. - */ -static void usage(const char *reason); - -/* Variables */ -static bool thread_should_exit = false; /**< Deamon exit flag */ -static bool thread_running = false; /**< Deamon status flag */ -static int deamon_task; /**< Handle of deamon task / thread */ - - -/** - * Parameter management - */ -static int parameters_init(struct fw_pos_control_param_handles *h) -{ - /* PID parameters */ - h->heading_p = param_find("FW_HEAD_P"); - h->headingr_p = param_find("FW_HEADR_P"); - h->headingr_i = param_find("FW_HEADR_I"); - h->headingr_lim = param_find("FW_HEADR_LIM"); - h->xtrack_p = param_find("FW_XTRACK_P"); - h->altitude_p = param_find("FW_ALT_P"); - h->roll_lim = param_find("FW_ROLL_LIM"); - h->pitch_lim = param_find("FW_PITCH_LIM"); - - return OK; -} - -static int parameters_update(const struct fw_pos_control_param_handles *h, struct fw_pos_control_params *p) -{ - param_get(h->heading_p, &(p->heading_p)); - param_get(h->headingr_p, &(p->headingr_p)); - param_get(h->headingr_i, &(p->headingr_i)); - param_get(h->headingr_lim, &(p->headingr_lim)); - param_get(h->xtrack_p, &(p->xtrack_p)); - param_get(h->altitude_p, &(p->altitude_p)); - param_get(h->roll_lim, &(p->roll_lim)); - param_get(h->pitch_lim, &(p->pitch_lim)); - - return OK; -} - - -/* Main Thread */ -int fixedwing_pos_control_thread_main(int argc, char *argv[]) -{ - /* read arguments */ - bool verbose = false; - - for (int i = 1; i < argc; i++) { - if (strcmp(argv[i], "-v") == 0 || strcmp(argv[i], "--verbose") == 0) { - verbose = true; - } - } - - /* welcome user */ - printf("[fixedwing pos control] started\n"); - - /* declare and safely initialize all structs */ - struct vehicle_global_position_s global_pos; - memset(&global_pos, 0, sizeof(global_pos)); - struct vehicle_global_position_s start_pos; // Temporary variable, replace with - memset(&start_pos, 0, sizeof(start_pos)); // previous waypoint when available - struct vehicle_global_position_setpoint_s global_setpoint; - memset(&global_setpoint, 0, sizeof(global_setpoint)); - struct vehicle_attitude_s att; - memset(&att, 0, sizeof(att)); - struct crosstrack_error_s xtrack_err; - memset(&xtrack_err, 0, sizeof(xtrack_err)); - struct parameter_update_s param_update; - memset(¶m_update, 0, sizeof(param_update)); - - /* output structs */ - struct vehicle_attitude_setpoint_s attitude_setpoint; - memset(&attitude_setpoint, 0, sizeof(attitude_setpoint)); - - /* publish attitude setpoint */ - attitude_setpoint.roll_body = 0.0f; - attitude_setpoint.pitch_body = 0.0f; - attitude_setpoint.yaw_body = 0.0f; - attitude_setpoint.thrust = 0.0f; - orb_advert_t attitude_setpoint_pub = orb_advertise(ORB_ID(vehicle_attitude_setpoint), &attitude_setpoint); - - /* subscribe */ - int global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position)); - int global_setpoint_sub = orb_subscribe(ORB_ID(vehicle_global_position_setpoint)); - int att_sub = orb_subscribe(ORB_ID(vehicle_attitude)); - int param_sub = orb_subscribe(ORB_ID(parameter_update)); - - /* Setup of loop */ - struct pollfd fds[2] = { - { .fd = param_sub, .events = POLLIN }, - { .fd = att_sub, .events = POLLIN } - }; - bool global_sp_updated_set_once = false; - - float psi_track = 0.0f; - - int counter = 0; - - struct fw_pos_control_params p; - struct fw_pos_control_param_handles h; - - PID_t heading_controller; - PID_t heading_rate_controller; - PID_t offtrack_controller; - PID_t altitude_controller; - - parameters_init(&h); - parameters_update(&h, &p); - pid_init(&heading_controller, p.heading_p, 0.0f, 0.0f, 0.0f, 10000.0f, PID_MODE_DERIVATIV_NONE, 0.0f); //arbitrary high limit - pid_init(&heading_rate_controller, p.headingr_p, p.headingr_i, 0.0f, 0.0f, p.roll_lim, PID_MODE_DERIVATIV_NONE, 0.0f); - pid_init(&altitude_controller, p.altitude_p, 0.0f, 0.0f, 0.0f, p.pitch_lim, PID_MODE_DERIVATIV_NONE, 0.0f); - pid_init(&offtrack_controller, p.xtrack_p, 0.0f, 0.0f, 0.0f , 60.0f * M_DEG_TO_RAD, PID_MODE_DERIVATIV_NONE, 0.0f); //TODO: remove hardcoded value - - /* error and performance monitoring */ - perf_counter_t fw_interval_perf = perf_alloc(PC_INTERVAL, "fixedwing_pos_control_interval"); - perf_counter_t fw_err_perf = perf_alloc(PC_COUNT, "fixedwing_pos_control_err"); - - while (!thread_should_exit) { - /* wait for a sensor update, check for exit condition every 500 ms */ - int ret = poll(fds, 2, 500); - - if (ret < 0) { - /* poll error, count it in perf */ - perf_count(fw_err_perf); - - } else if (ret == 0) { - /* no return value, ignore */ - } else { - - /* only update parameters if they changed */ - if (fds[0].revents & POLLIN) { - /* read from param to clear updated flag */ - struct parameter_update_s update; - orb_copy(ORB_ID(parameter_update), param_sub, &update); - - /* update parameters from storage */ - parameters_update(&h, &p); - pid_set_parameters(&heading_controller, p.heading_p, 0, 0, 0, 10000.0f); //arbitrary high limit - pid_set_parameters(&heading_rate_controller, p.headingr_p, p.headingr_i, 0, 0, p.roll_lim); - pid_set_parameters(&altitude_controller, p.altitude_p, 0, 0, 0, p.pitch_lim); - pid_set_parameters(&offtrack_controller, p.xtrack_p, 0, 0, 0, 60.0f * M_DEG_TO_RAD); //TODO: remove hardcoded value - } - - /* only run controller if attitude changed */ - if (fds[1].revents & POLLIN) { - - - static uint64_t last_run = 0; - const float deltaT = (hrt_absolute_time() - last_run) / 1000000.0f; - last_run = hrt_absolute_time(); - - /* check if there is a new position or setpoint */ - bool pos_updated; - orb_check(global_pos_sub, &pos_updated); - bool global_sp_updated; - orb_check(global_setpoint_sub, &global_sp_updated); - - /* load local copies */ - orb_copy(ORB_ID(vehicle_attitude), att_sub, &att); - - if (pos_updated) { - orb_copy(ORB_ID(vehicle_global_position), global_pos_sub, &global_pos); - } - - if (global_sp_updated) { - orb_copy(ORB_ID(vehicle_global_position_setpoint), global_setpoint_sub, &global_setpoint); - start_pos = global_pos; //for now using the current position as the startpoint (= approx. last waypoint because the setpoint switch occurs at the waypoint) - global_sp_updated_set_once = true; - psi_track = get_bearing_to_next_waypoint(global_pos.lat, global_pos.lon, - (double)global_setpoint.lat / (double)1e7d, (double)global_setpoint.lon / (double)1e7d); - - printf("next wp direction: %0.4f\n", (double)psi_track); - } - - /* Simple Horizontal Control */ - if (global_sp_updated_set_once) { - // if (counter % 100 == 0) - // printf("lat_sp %d, ln_sp %d, lat: %d, lon: %d\n", global_setpoint.lat, global_setpoint.lon, global_pos.lat, global_pos.lon); - - /* calculate crosstrack error */ - // Only the case of a straight line track following handled so far - int distance_res = get_distance_to_line(&xtrack_err, (double)global_pos.lat / (double)1e7d, (double)global_pos.lon / (double)1e7d, - (double)start_pos.lat / (double)1e7d, (double)start_pos.lon / (double)1e7d, - (double)global_setpoint.lat / (double)1e7d, (double)global_setpoint.lon / (double)1e7d); - - // XXX what is xtrack_err.past_end? - if (distance_res == OK /*&& !xtrack_err.past_end*/) { - - float delta_psi_c = pid_calculate(&offtrack_controller, 0, xtrack_err.distance, 0.0f, 0.0f); //p.xtrack_p * xtrack_err.distance - - float psi_c = psi_track + delta_psi_c; - float psi_e = psi_c - att.yaw; - - /* wrap difference back onto -pi..pi range */ - psi_e = _wrap_pi(psi_e); - - if (verbose) { - printf("xtrack_err.distance %.4f ", (double)xtrack_err.distance); - printf("delta_psi_c %.4f ", (double)delta_psi_c); - printf("psi_c %.4f ", (double)psi_c); - printf("att.yaw %.4f ", (double)att.yaw); - printf("psi_e %.4f ", (double)psi_e); - } - - /* calculate roll setpoint, do this artificially around zero */ - float delta_psi_rate_c = pid_calculate(&heading_controller, psi_e, 0.0f, 0.0f, 0.0f); - float psi_rate_track = 0; //=V_gr/r_track , this will be needed for implementation of arc following - float psi_rate_c = delta_psi_rate_c + psi_rate_track; - - /* limit turn rate */ - if (psi_rate_c > p.headingr_lim) { - psi_rate_c = p.headingr_lim; - - } else if (psi_rate_c < -p.headingr_lim) { - psi_rate_c = -p.headingr_lim; - } - - float psi_rate_e = psi_rate_c - att.yawspeed; - - // XXX sanity check: Assume 10 m/s stall speed and no stall condition - float ground_speed = sqrtf(global_pos.vx * global_pos.vx + global_pos.vy * global_pos.vy); - - if (ground_speed < 10.0f) { - ground_speed = 10.0f; - } - - float psi_rate_e_scaled = psi_rate_e * ground_speed / 9.81f; //* V_gr / g - - attitude_setpoint.roll_body = pid_calculate(&heading_rate_controller, psi_rate_e_scaled, 0.0f, 0.0f, deltaT); - - if (verbose) { - printf("psi_rate_c %.4f ", (double)psi_rate_c); - printf("psi_rate_e_scaled %.4f ", (double)psi_rate_e_scaled); - printf("rollbody %.4f\n", (double)attitude_setpoint.roll_body); - } - - if (verbose && counter % 100 == 0) - printf("xtrack_err.distance: %0.4f, delta_psi_c: %0.4f\n", xtrack_err.distance, delta_psi_c); - - } else { - if (verbose && counter % 100 == 0) - printf("distance_res: %d, past_end %d\n", distance_res, xtrack_err.past_end); - } - - /* Very simple Altitude Control */ - if (pos_updated) { - - //TODO: take care of relative vs. ab. altitude - attitude_setpoint.pitch_body = pid_calculate(&altitude_controller, global_setpoint.altitude, global_pos.alt, 0.0f, 0.0f); - - } - - // XXX need speed control - attitude_setpoint.thrust = 0.7f; - - /* publish the attitude setpoint */ - orb_publish(ORB_ID(vehicle_attitude_setpoint), attitude_setpoint_pub, &attitude_setpoint); - - /* measure in what intervals the controller runs */ - perf_count(fw_interval_perf); - - counter++; - - } else { - // XXX no setpoint, decent default needed (loiter?) - } - } - } - } - - printf("[fixedwing_pos_control] exiting.\n"); - thread_running = false; - - - close(attitude_setpoint_pub); - - fflush(stdout); - exit(0); - - return 0; - -} - -/* Startup Functions */ - -static void -usage(const char *reason) -{ - if (reason) - fprintf(stderr, "%s\n", reason); - - fprintf(stderr, "usage: fixedwing_pos_control {start|stop|status}\n\n"); - exit(1); -} - -/** - * The deamon app only briefly exists to start - * the background job. The stack size assigned in the - * Makefile does only apply to this management task. - * - * The actual stack size should be set in the call - * to task_create(). - */ -int fixedwing_pos_control_main(int argc, char *argv[]) -{ - if (argc < 1) - usage("missing command"); - - if (!strcmp(argv[1], "start")) { - - if (thread_running) { - printf("fixedwing_pos_control already running\n"); - /* this is not an error */ - exit(0); - } - - thread_should_exit = false; - deamon_task = task_spawn_cmd("fixedwing_pos_control", - SCHED_DEFAULT, - SCHED_PRIORITY_MAX - 20, - 2048, - fixedwing_pos_control_thread_main, - (argv) ? (const char **)&argv[2] : (const char **)NULL); - thread_running = true; - exit(0); - } - - if (!strcmp(argv[1], "stop")) { - thread_should_exit = true; - exit(0); - } - - if (!strcmp(argv[1], "status")) { - if (thread_running) { - printf("\tfixedwing_pos_control is running\n"); - - } else { - printf("\tfixedwing_pos_control not started\n"); - } - - exit(0); - } - - usage("unrecognized command"); - exit(1); -} diff --git a/src/modules/fw_att_control/fw_att_control_main.cpp b/src/modules/fw_att_control/fw_att_control_main.cpp index f139c25f4..1f3e9f098 100644 --- a/src/modules/fw_att_control/fw_att_control_main.cpp +++ b/src/modules/fw_att_control/fw_att_control_main.cpp @@ -173,6 +173,8 @@ private: float pitchsp_offset_deg; /**< Pitch Setpoint Offset in deg */ float rollsp_offset_rad; /**< Roll Setpoint Offset in rad */ float pitchsp_offset_rad; /**< Pitch Setpoint Offset in rad */ + float man_roll_max; /**< Max Roll in rad */ + float man_pitch_max; /**< Max Pitch in rad */ } _parameters; /**< local copies of interesting parameters */ @@ -211,6 +213,8 @@ private: param_t trim_yaw; param_t rollsp_offset_deg; param_t pitchsp_offset_deg; + param_t man_roll_max; + param_t man_pitch_max; } _parameter_handles; /**< handles for interesting parameters */ @@ -269,7 +273,7 @@ private: /** * Main sensor collection task. */ - void task_main() __attribute__((noreturn)); + void task_main(); }; namespace att_control @@ -354,6 +358,9 @@ FixedwingAttitudeControl::FixedwingAttitudeControl() : _parameter_handles.rollsp_offset_deg = param_find("FW_RSP_OFF"); _parameter_handles.pitchsp_offset_deg = param_find("FW_PSP_OFF"); + _parameter_handles.man_roll_max = param_find("FW_MAN_R_MAX"); + _parameter_handles.man_pitch_max = param_find("FW_MAN_P_MAX"); + /* fetch initial parameter values */ parameters_update(); } @@ -421,6 +428,10 @@ FixedwingAttitudeControl::parameters_update() param_get(_parameter_handles.pitchsp_offset_deg, &(_parameters.pitchsp_offset_deg)); _parameters.rollsp_offset_rad = math::radians(_parameters.rollsp_offset_deg); _parameters.pitchsp_offset_rad = math::radians(_parameters.pitchsp_offset_deg); + param_get(_parameter_handles.man_roll_max, &(_parameters.man_roll_max)); + param_get(_parameter_handles.man_pitch_max, &(_parameters.man_pitch_max)); + _parameters.man_roll_max = math::radians(_parameters.man_roll_max); + _parameters.man_pitch_max = math::radians(_parameters.man_pitch_max); /* pitch control parameters */ @@ -660,18 +671,24 @@ FixedwingAttitudeControl::task_main() float airspeed; - /* if airspeed is smaller than min, the sensor is not giving good readings */ - if ((_airspeed.indicated_airspeed_m_s < 0.5f * _parameters.airspeed_min) || - !isfinite(_airspeed.indicated_airspeed_m_s) || + /* if airspeed is not updating, we assume the normal average speed */ + if (!isfinite(_airspeed.true_airspeed_m_s) || hrt_elapsed_time(&_airspeed.timestamp) > 1e6) { airspeed = _parameters.airspeed_trim; } else { - airspeed = _airspeed.indicated_airspeed_m_s; + airspeed = _airspeed.true_airspeed_m_s; } - float airspeed_scaling = _parameters.airspeed_trim / airspeed; - //warnx("aspd scale: %6.2f act scale: %6.2f", airspeed_scaling, actuator_scaling); + /* + * For scaling our actuators using anything less than the min (close to stall) + * speed doesn't make any sense - its the strongest reasonable deflection we + * want to do in flight and its the baseline a human pilot would choose. + * + * Forcing the scaling to this value allows reasonable handheld tests. + */ + + float airspeed_scaling = _parameters.airspeed_trim / ((airspeed < _parameters.airspeed_min) ? _parameters.airspeed_min : airspeed); float roll_sp = _parameters.rollsp_offset_rad; float pitch_sp = _parameters.pitchsp_offset_rad; @@ -689,20 +706,21 @@ FixedwingAttitudeControl::task_main() } else { /* * Scale down roll and pitch as the setpoints are radians - * and a typical remote can only do 45 degrees, the mapping is - * -1..+1 to -45..+45 degrees or -0.75..+0.75 radians. + * and a typical remote can only do around 45 degrees, the mapping is + * -1..+1 to -man_roll_max rad..+man_roll_max rad (equivalent for pitch) * * With this mapping the stick angle is a 1:1 representation of - * the commanded attitude. If more than 45 degrees are desired, - * a scaling parameter can be applied to the remote. + * the commanded attitude. * * The trim gets subtracted here from the manual setpoint to get * the intended attitude setpoint. Later, after the rate control step the * trim is added again to the control signal. */ - roll_sp = (_manual.roll - _parameters.trim_roll) * 0.75f + _parameters.rollsp_offset_rad; - pitch_sp = (_manual.pitch - _parameters.trim_pitch) * 0.75f + _parameters.pitchsp_offset_rad; - throttle_sp = _manual.throttle; + roll_sp = (_manual.y * _parameters.man_roll_max - _parameters.trim_roll) + + _parameters.rollsp_offset_rad; + pitch_sp = -(_manual.x * _parameters.man_pitch_max - _parameters.trim_pitch) + + _parameters.pitchsp_offset_rad; + throttle_sp = _manual.z; _actuators.control[4] = _manual.flaps; /* @@ -765,7 +783,7 @@ FixedwingAttitudeControl::task_main() _actuators.control[1] = (isfinite(pitch_u)) ? pitch_u + _parameters.trim_pitch : _parameters.trim_pitch; if (!isfinite(pitch_u)) { warnx("pitch_u %.4f, _yaw_ctrl.get_desired_rate() %.4f, airspeed %.4f, airspeed_scaling %.4f, roll_sp %.4f, pitch_sp %.4f, _roll_ctrl.get_desired_rate() %.4f, _pitch_ctrl.get_desired_rate() %.4f att_sp.roll_body %.4f", - pitch_u, _yaw_ctrl.get_desired_rate(), airspeed, airspeed_scaling, roll_sp, pitch_sp, _roll_ctrl.get_desired_rate(), _pitch_ctrl.get_desired_rate(), _att_sp.roll_body); + (double)pitch_u, (double)_yaw_ctrl.get_desired_rate(), (double)airspeed, (double)airspeed_scaling, (double)roll_sp, (double)pitch_sp, (double)_roll_ctrl.get_desired_rate(), (double)_pitch_ctrl.get_desired_rate(), (double)_att_sp.roll_body); } float yaw_u = _yaw_ctrl.control_bodyrate(_att.roll, _att.pitch, @@ -774,16 +792,16 @@ FixedwingAttitudeControl::task_main() _parameters.airspeed_min, _parameters.airspeed_max, airspeed, airspeed_scaling, lock_integrator); _actuators.control[2] = (isfinite(yaw_u)) ? yaw_u + _parameters.trim_yaw : _parameters.trim_yaw; if (!isfinite(yaw_u)) { - warnx("yaw_u %.4f", yaw_u); + warnx("yaw_u %.4f", (double)yaw_u); } /* throttle passed through */ _actuators.control[3] = (isfinite(throttle_sp)) ? throttle_sp : 0.0f; if (!isfinite(throttle_sp)) { - warnx("throttle_sp %.4f", throttle_sp); + warnx("throttle_sp %.4f", (double)throttle_sp); } } else { - warnx("Non-finite setpoint roll_sp: %.4f, pitch_sp %.4f", roll_sp, pitch_sp); + warnx("Non-finite setpoint roll_sp: %.4f, pitch_sp %.4f", (double)roll_sp, (double)pitch_sp); } /* @@ -808,10 +826,10 @@ FixedwingAttitudeControl::task_main() } else { /* manual/direct control */ - _actuators.control[0] = _manual.roll; - _actuators.control[1] = _manual.pitch; - _actuators.control[2] = _manual.yaw; - _actuators.control[3] = _manual.throttle; + _actuators.control[0] = _manual.y; + _actuators.control[1] = -_manual.x; + _actuators.control[2] = _manual.r; + _actuators.control[3] = _manual.z; _actuators.control[4] = _manual.flaps; } diff --git a/src/modules/fw_att_control/fw_att_control_params.c b/src/modules/fw_att_control/fw_att_control_params.c index c80a44f2a..aa637e207 100644 --- a/src/modules/fw_att_control/fw_att_control_params.c +++ b/src/modules/fw_att_control/fw_att_control_params.c @@ -186,3 +186,13 @@ PARAM_DEFINE_FLOAT(FW_RSP_OFF, 0.0f); // @Description An airframe specific offset of the pitch setpoint in degrees, the value is added to the pitch setpoint and should correspond to the typical cruise speed of the airframe // @Range -90.0 to 90.0 PARAM_DEFINE_FLOAT(FW_PSP_OFF, 0.0f); + +// @DisplayName Max Manual Roll +// @Description Max roll for manual control in attitude stabilized mode +// @Range 0.0 to 90.0 +PARAM_DEFINE_FLOAT(FW_MAN_R_MAX, 45.0f); + +// @DisplayName Max Manual Pitch +// @Description Max pitch for manual control in attitude stabilized mode +// @Range 0.0 to 90.0 +PARAM_DEFINE_FLOAT(FW_MAN_P_MAX, 45.0f); diff --git a/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp b/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp index 7f13df785..9cbc26efe 100644 --- a/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp +++ b/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp @@ -89,6 +89,7 @@ #include <launchdetection/LaunchDetector.h> #include <ecl/l1/ecl_l1_pos_controller.h> #include <external_lgpl/tecs/tecs.h> +#include <drivers/drv_range_finder.h> #include "landingslope.h" @@ -134,6 +135,7 @@ private: int _params_sub; /**< notification of parameter updates */ int _manual_control_sub; /**< notification of manual control updates */ int _sensor_combined_sub; /**< for body frame accelerations */ + int _range_finder_sub; /**< range finder subscription */ orb_advert_t _attitude_sp_pub; /**< attitude setpoint */ orb_advert_t _nav_capabilities_pub; /**< navigation capabilities publication */ @@ -147,13 +149,14 @@ private: struct vehicle_global_position_s _global_pos; /**< global vehicle position */ struct position_setpoint_triplet_s _pos_sp_triplet; /**< triplet of mission items */ struct sensor_combined_s _sensor_combined; /**< for body frame accelerations */ + struct range_finder_report _range_finder; /**< range finder report */ perf_counter_t _loop_perf; /**< loop performance counter */ bool _setpoint_valid; /**< flag if the position control setpoint is valid */ /** manual control states */ - float _seatbelt_hold_heading; /**< heading the system should hold in seatbelt mode */ + float _altctrl_hold_heading; /**< heading the system should hold in altctrl mode */ double _loiter_hold_lat; double _loiter_hold_lon; float _loiter_hold_alt; @@ -181,7 +184,7 @@ private: /* Landingslope object */ Landingslope landingslope; - float flare_curve_alt_last; + float flare_curve_alt_rel_last; /* heading hold */ float target_bearing; @@ -239,6 +242,7 @@ private: float land_flare_alt_relative; float land_thrust_lim_alt_relative; float land_heading_hold_horizontal_distance; + float range_finder_rel_alt; } _parameters; /**< local copies of interesting parameters */ @@ -283,6 +287,7 @@ private: param_t land_flare_alt_relative; param_t land_thrust_lim_alt_relative; param_t land_heading_hold_horizontal_distance; + param_t range_finder_rel_alt; } _parameter_handles; /**< handles for interesting parameters */ @@ -309,6 +314,12 @@ private: bool vehicle_airspeed_poll(); /** + * Check for range finder updates. + */ + bool range_finder_poll(); + + + /** * Check for position updates. */ void vehicle_attitude_poll(); @@ -329,6 +340,11 @@ private: void navigation_capabilities_publish(); /** + * Get the relative alt either from the difference between estimate and waypoint or from the laser range finder + */ + float get_relative_landingalt(float land_setpoint_alt, float current_alt, const struct range_finder_report &range_finder, float range_finder_use_relative_alt); + + /** * Control position. */ bool control_position(const math::Vector<2> &global_pos, const math::Vector<2> &ground_speed, @@ -345,7 +361,7 @@ private: /** * Main sensor collection task. */ - void task_main() __attribute__((noreturn)); + void task_main(); /* * Reset takeoff state @@ -384,6 +400,7 @@ FixedwingPositionControl::FixedwingPositionControl() : _control_mode_sub(-1), _params_sub(-1), _manual_control_sub(-1), + _range_finder_sub(-1), /* publications */ _attitude_sp_pub(-1), @@ -403,7 +420,7 @@ FixedwingPositionControl::FixedwingPositionControl() : launch_detected(false), last_manual(false), usePreTakeoffThrust(false), - flare_curve_alt_last(0.0f), + flare_curve_alt_rel_last(0.0f), launchDetector(), _airspeed_error(0.0f), _airspeed_valid(false), @@ -417,7 +434,8 @@ FixedwingPositionControl::FixedwingPositionControl() : _control_mode(), _global_pos(), _pos_sp_triplet(), - _sensor_combined() + _sensor_combined(), + _range_finder() { _nav_capabilities.turn_distance = 0.0f; @@ -442,6 +460,7 @@ FixedwingPositionControl::FixedwingPositionControl() : _parameter_handles.land_flare_alt_relative = param_find("FW_LND_FLALT"); _parameter_handles.land_thrust_lim_alt_relative = param_find("FW_LND_TLALT"); _parameter_handles.land_heading_hold_horizontal_distance = param_find("FW_LND_HHDIST"); + _parameter_handles.range_finder_rel_alt = param_find("FW_LND_RFRALT"); _parameter_handles.time_const = param_find("FW_T_TIME_CONST"); _parameter_handles.min_sink_rate = param_find("FW_T_SINK_MIN"); @@ -531,6 +550,8 @@ FixedwingPositionControl::parameters_update() param_get(_parameter_handles.land_thrust_lim_alt_relative, &(_parameters.land_thrust_lim_alt_relative)); param_get(_parameter_handles.land_heading_hold_horizontal_distance, &(_parameters.land_heading_hold_horizontal_distance)); + param_get(_parameter_handles.range_finder_rel_alt, &(_parameters.range_finder_rel_alt)); + _l1_control.set_l1_damping(_parameters.l1_damping); _l1_control.set_l1_period(_parameters.l1_period); _l1_control.set_l1_roll_limit(math::radians(_parameters.roll_limit)); @@ -626,6 +647,20 @@ FixedwingPositionControl::vehicle_airspeed_poll() return airspeed_updated; } +bool +FixedwingPositionControl::range_finder_poll() +{ + /* check if there is a range finder measurement */ + bool range_finder_updated; + orb_check(_range_finder_sub, &range_finder_updated); + + if (range_finder_updated) { + orb_copy(ORB_ID(sensor_range_finder), _range_finder_sub, &_range_finder); + } + + return range_finder_updated; +} + void FixedwingPositionControl::vehicle_attitude_poll() { @@ -754,6 +789,23 @@ void FixedwingPositionControl::navigation_capabilities_publish() } } +float FixedwingPositionControl::get_relative_landingalt(float land_setpoint_alt, float current_alt, const struct range_finder_report &range_finder, float range_finder_use_relative_alt) +{ + float rel_alt_estimated = current_alt - land_setpoint_alt; + + /* only use range finder if: + * parameter (range_finder_use_relative_alt) > 0 + * the measurement is valid + * the estimated relative altitude (from global altitude estimate and landing waypoint) <= range_finder_use_relative_alt + */ + if (range_finder_use_relative_alt < 0 || !range_finder.valid || rel_alt_estimated > range_finder_use_relative_alt ) { + return rel_alt_estimated; + } + + return range_finder.distance; + +} + bool FixedwingPositionControl::control_position(const math::Vector<2> ¤t_position, const math::Vector<2> &ground_speed, const struct position_setpoint_triplet_s &pos_sp_triplet) @@ -896,12 +948,14 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi /* Calculate distance (to landing waypoint) and altitude of last ordinary waypoint L */ float L_wp_distance = get_distance_to_next_waypoint(prev_wp(0), prev_wp(1), curr_wp(0), curr_wp(1)); - float L_altitude = landingslope.getLandingSlopeAbsoluteAltitude(L_wp_distance, _pos_sp_triplet.current.alt); + float L_altitude_rel = landingslope.getLandingSlopeRelativeAltitude(L_wp_distance); float bearing_airplane_currwp = get_bearing_to_next_waypoint(current_position(0), current_position(1), curr_wp(0), curr_wp(1)); - float landing_slope_alt_desired = landingslope.getLandingSlopeAbsoluteAltitudeSave(wp_distance, bearing_lastwp_currwp, bearing_airplane_currwp, _pos_sp_triplet.current.alt); + float landing_slope_alt_rel_desired = landingslope.getLandingSlopeRelativeAltitudeSave(wp_distance, bearing_lastwp_currwp, bearing_airplane_currwp); + + float relative_alt = get_relative_landingalt(_pos_sp_triplet.current.alt, _global_pos.alt, _range_finder, _parameters.range_finder_rel_alt); - if ( (_global_pos.alt < _pos_sp_triplet.current.alt + landingslope.flare_relative_alt()) || land_noreturn_vertical) { //checking for land_noreturn to avoid unwanted climb out + if ( (relative_alt < landingslope.flare_relative_alt()) || land_noreturn_vertical) { //checking for land_noreturn to avoid unwanted climb out /* land with minimal speed */ @@ -911,7 +965,7 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi /* kill the throttle if param requests it */ throttle_max = _parameters.throttle_max; - if (_global_pos.alt < _pos_sp_triplet.current.alt + landingslope.motor_lim_relative_alt() || land_motor_lim) { + if (relative_alt < landingslope.motor_lim_relative_alt() || land_motor_lim) { throttle_max = math::min(throttle_max, _parameters.throttle_land_max); if (!land_motor_lim) { land_motor_lim = true; @@ -920,16 +974,16 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi } - float flare_curve_alt = landingslope.getFlareCurveAltitudeSave(wp_distance, bearing_lastwp_currwp, bearing_airplane_currwp, _pos_sp_triplet.current.alt); + float flare_curve_alt_rel = landingslope.getFlareCurveRelativeAltitudeSave(wp_distance, bearing_lastwp_currwp, bearing_airplane_currwp); /* avoid climbout */ - if ((flare_curve_alt_last < flare_curve_alt && land_noreturn_vertical) || land_stayonground) + if ((flare_curve_alt_rel_last < flare_curve_alt_rel && land_noreturn_vertical) || land_stayonground) { - flare_curve_alt = pos_sp_triplet.current.alt; + flare_curve_alt_rel = 0.0f; // stay on ground land_stayonground = true; } - _tecs.update_pitch_throttle(_R_nb, _att.pitch, _global_pos.alt, flare_curve_alt, calculate_target_airspeed(airspeed_land), + _tecs.update_pitch_throttle(_R_nb, _att.pitch, _pos_sp_triplet.current.alt + relative_alt, _pos_sp_triplet.current.alt + flare_curve_alt_rel, calculate_target_airspeed(airspeed_land), _airspeed.indicated_airspeed_m_s, eas2tas, false, flare_pitch_angle_rad, 0.0f, throttle_max, throttle_land, @@ -941,7 +995,7 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi } //warnx("Landing: flare, _global_pos.alt %.1f, flare_curve_alt %.1f, flare_curve_alt_last %.1f, flare_length %.1f, wp_distance %.1f", _global_pos.alt, flare_curve_alt, flare_curve_alt_last, flare_length, wp_distance); - flare_curve_alt_last = flare_curve_alt; + flare_curve_alt_rel_last = flare_curve_alt_rel; } else { /* intersect glide slope: @@ -949,20 +1003,20 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi * if current position is higher or within 10m of slope follow the glide slope * if current position is below slope -10m continue on maximum of previous wp altitude or L_altitude until the intersection with the slope * */ - float altitude_desired = _global_pos.alt; - if (_global_pos.alt > landing_slope_alt_desired - 10.0f) { + float altitude_desired_rel = relative_alt; + if (relative_alt > landing_slope_alt_rel_desired - 10.0f) { /* stay on slope */ - altitude_desired = landing_slope_alt_desired; + altitude_desired_rel = landing_slope_alt_rel_desired; if (!land_onslope) { mavlink_log_info(_mavlink_fd, "#audio: Landing, on slope"); land_onslope = true; } } else { /* continue horizontally */ - altitude_desired = math::max(_global_pos.alt, L_altitude); + altitude_desired_rel = math::max(relative_alt, L_altitude_rel); } - _tecs.update_pitch_throttle(_R_nb, _att.pitch, _global_pos.alt, altitude_desired, calculate_target_airspeed(airspeed_approach), + _tecs.update_pitch_throttle(_R_nb, _att.pitch, _pos_sp_triplet.current.alt + relative_alt, _pos_sp_triplet.current.alt + altitude_desired_rel, calculate_target_airspeed(airspeed_approach), _airspeed.indicated_airspeed_m_s, eas2tas, false, math::radians(_parameters.pitch_limit_min), _parameters.throttle_min, _parameters.throttle_max, _parameters.throttle_cruise, @@ -1051,16 +1105,16 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi _att_sp.roll_reset_integral = true; } - } else if (0/* easy mode enabled */) { + } else if (0/* posctrl mode enabled */) { - /** EASY FLIGHT **/ + /** POSCTRL FLIGHT **/ - if (0/* switched from another mode to easy */) { - _seatbelt_hold_heading = _att.yaw; + if (0/* switched from another mode to posctrl */) { + _altctrl_hold_heading = _att.yaw; } - if (0/* easy on and manual control yaw non-zero */) { - _seatbelt_hold_heading = _att.yaw + _manual.yaw; + if (0/* posctrl on and manual control yaw non-zero */) { + _altctrl_hold_heading = _att.yaw + _manual.r; } //XXX not used @@ -1073,44 +1127,44 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi // climb_out = true; // } - /* if in seatbelt mode, set airspeed based on manual control */ + /* if in altctrl mode, set airspeed based on manual control */ // XXX check if ground speed undershoot should be applied here - float seatbelt_airspeed = _parameters.airspeed_min + + float altctrl_airspeed = _parameters.airspeed_min + (_parameters.airspeed_max - _parameters.airspeed_min) * - _manual.throttle; + _manual.z; - _l1_control.navigate_heading(_seatbelt_hold_heading, _att.yaw, ground_speed); + _l1_control.navigate_heading(_altctrl_hold_heading, _att.yaw, ground_speed); _att_sp.roll_body = _l1_control.nav_roll(); _att_sp.yaw_body = _l1_control.nav_bearing(); - _tecs.update_pitch_throttle(_R_nb, _att.pitch, _global_pos.alt, _global_pos.alt + _manual.pitch * 2.0f, - seatbelt_airspeed, + _tecs.update_pitch_throttle(_R_nb, _att.pitch, _global_pos.alt, _global_pos.alt + _manual.x * 2.0f, + altctrl_airspeed, _airspeed.indicated_airspeed_m_s, eas2tas, false, _parameters.pitch_limit_min, _parameters.throttle_min, _parameters.throttle_max, _parameters.throttle_cruise, _parameters.pitch_limit_min, _parameters.pitch_limit_max); - } else if (0/* seatbelt mode enabled */) { + } else if (0/* altctrl mode enabled */) { - /** SEATBELT FLIGHT **/ + /** ALTCTRL FLIGHT **/ - if (0/* switched from another mode to seatbelt */) { - _seatbelt_hold_heading = _att.yaw; + if (0/* switched from another mode to altctrl */) { + _altctrl_hold_heading = _att.yaw; } - if (0/* seatbelt on and manual control yaw non-zero */) { - _seatbelt_hold_heading = _att.yaw + _manual.yaw; + if (0/* altctrl on and manual control yaw non-zero */) { + _altctrl_hold_heading = _att.yaw + _manual.r; } - /* if in seatbelt mode, set airspeed based on manual control */ + /* if in altctrl mode, set airspeed based on manual control */ // XXX check if ground speed undershoot should be applied here - float seatbelt_airspeed = _parameters.airspeed_min + + float altctrl_airspeed = _parameters.airspeed_min + (_parameters.airspeed_max - _parameters.airspeed_min) * - _manual.throttle; + _manual.z; /* user switched off throttle */ - if (_manual.throttle < 0.1f) { + if (_manual.z < 0.1f) { throttle_max = 0.0f; /* switch to pure pitch based altitude control, give up speed */ _tecs.set_speed_weight(0.0f); @@ -1120,15 +1174,15 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi bool climb_out = false; /* user wants to climb out */ - if (_manual.pitch > 0.3f && _manual.throttle > 0.8f) { + if (_manual.x > 0.3f && _manual.z > 0.8f) { climb_out = true; } - _l1_control.navigate_heading(_seatbelt_hold_heading, _att.yaw, ground_speed); - _att_sp.roll_body = _manual.roll; - _att_sp.yaw_body = _manual.yaw; - _tecs.update_pitch_throttle(_R_nb, _att.pitch, _global_pos.alt, _global_pos.alt + _manual.pitch * 2.0f, - seatbelt_airspeed, + _l1_control.navigate_heading(_altctrl_hold_heading, _att.yaw, ground_speed); + _att_sp.roll_body = _manual.y; + _att_sp.yaw_body = _manual.r; + _tecs.update_pitch_throttle(_R_nb, _att.pitch, _global_pos.alt, _global_pos.alt + _manual.x * 2.0f, + altctrl_airspeed, _airspeed.indicated_airspeed_m_s, eas2tas, climb_out, _parameters.pitch_limit_min, _parameters.throttle_min, _parameters.throttle_max, _parameters.throttle_cruise, @@ -1185,6 +1239,7 @@ FixedwingPositionControl::task_main() _airspeed_sub = orb_subscribe(ORB_ID(airspeed)); _params_sub = orb_subscribe(ORB_ID(parameter_update)); _manual_control_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); + _range_finder_sub = orb_subscribe(ORB_ID(sensor_range_finder)); /* rate limit vehicle status updates to 5Hz */ orb_set_interval(_control_mode_sub, 200); @@ -1264,6 +1319,7 @@ FixedwingPositionControl::task_main() vehicle_setpoint_poll(); vehicle_sensor_combined_poll(); vehicle_airspeed_poll(); + range_finder_poll(); // vehicle_baro_poll(); math::Vector<2> ground_speed(_global_pos.vel_n, _global_pos.vel_e); diff --git a/src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c b/src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c index 0909135e1..f258f77da 100644 --- a/src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c +++ b/src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c @@ -245,7 +245,7 @@ PARAM_DEFINE_FLOAT(FW_T_INTEG_GAIN, 0.1f); /** * Maximum vertical acceleration * - * This is the maximum vertical acceleration (in metres/second^2) + * This is the maximum vertical acceleration (in metres/second square) * either up or down that the controller will use to correct speed * or height errors. The default value of 7 m/s/s (equivalent to +- 0.7 g) * allows for reasonably aggressive pitch changes if required to recover @@ -375,3 +375,14 @@ PARAM_DEFINE_FLOAT(FW_LND_TLALT, 5.0f); * @group L1 Control */ PARAM_DEFINE_FLOAT(FW_LND_HHDIST, 15.0f); + +/** + * Relative altitude threshold for range finder measurements for use during landing + * + * range finder measurements will only be used if the estimated relative altitude (gobal_pos.alt - landing_waypoint.alt) is < FW_LND_RFRALT + * set to < 0 to disable + * the correct value of this parameter depends on your range measuring device as well as on the terrain at the landing location + * + * @group L1 Control + */ +PARAM_DEFINE_FLOAT(FW_LND_RFRALT, -1.0f); diff --git a/src/modules/fw_pos_control_l1/landingslope.cpp b/src/modules/fw_pos_control_l1/landingslope.cpp index e5f7023ae..8ce465fe8 100644 --- a/src/modules/fw_pos_control_l1/landingslope.cpp +++ b/src/modules/fw_pos_control_l1/landingslope.cpp @@ -69,26 +69,46 @@ void Landingslope::calculateSlopeValues() _horizontal_slope_displacement = (_flare_length - _d1); } -float Landingslope::getLandingSlopeAbsoluteAltitude(float wp_distance, float wp_altitude) +float Landingslope::getLandingSlopeRelativeAltitude(float wp_landing_distance) { - return Landingslope::getLandingSlopeAbsoluteAltitude(wp_distance, wp_altitude, _horizontal_slope_displacement, _landing_slope_angle_rad); + return Landingslope::getLandingSlopeRelativeAltitude(wp_landing_distance, _horizontal_slope_displacement, _landing_slope_angle_rad); } -float Landingslope::getLandingSlopeAbsoluteAltitudeSave(float wp_distance, float bearing_lastwp_currwp, float bearing_airplane_currwp, float wp_altitude) +float Landingslope::getLandingSlopeRelativeAltitudeSave(float wp_landing_distance, float bearing_lastwp_currwp, float bearing_airplane_currwp) { /* If airplane is in front of waypoint return slope altitude, else return waypoint altitude */ if (fabsf(bearing_airplane_currwp - bearing_lastwp_currwp) < math::radians(90.0f)) - return getLandingSlopeAbsoluteAltitude(wp_distance, wp_altitude); + return getLandingSlopeRelativeAltitude(wp_landing_distance); + else + return 0.0f; +} + +float Landingslope::getLandingSlopeAbsoluteAltitude(float wp_landing_distance, float wp_altitude) +{ + return Landingslope::getLandingSlopeAbsoluteAltitude(wp_landing_distance, wp_altitude, _horizontal_slope_displacement, _landing_slope_angle_rad); +} + +float Landingslope::getLandingSlopeAbsoluteAltitudeSave(float wp_landing_distance, float bearing_lastwp_currwp, float bearing_airplane_currwp, float wp_altitude) +{ + /* If airplane is in front of waypoint return slope altitude, else return waypoint altitude */ + if (fabsf(bearing_airplane_currwp - bearing_lastwp_currwp) < math::radians(90.0f)) + return getLandingSlopeAbsoluteAltitude(wp_landing_distance, wp_altitude); else return wp_altitude; } -float Landingslope::getFlareCurveAltitudeSave(float wp_landing_distance, float bearing_lastwp_currwp, float bearing_airplane_currwp, float wp_landing_altitude) +float Landingslope::getFlareCurveRelativeAltitudeSave(float wp_landing_distance, float bearing_lastwp_currwp, float bearing_airplane_currwp) { /* If airplane is in front of waypoint return flare curve altitude, else return waypoint altitude */ if (fabsf(bearing_airplane_currwp - bearing_lastwp_currwp) < math::radians(90.0f)) - return wp_landing_altitude + _H0 * expf(-math::max(0.0f, _flare_length - wp_landing_distance)/_flare_constant) - _H1_virt; + return _H0 * expf(-math::max(0.0f, _flare_length - wp_landing_distance)/_flare_constant) - _H1_virt; else - return wp_landing_altitude; + return 0.0f; +} + +float Landingslope::getFlareCurveAbsoluteAltitudeSave(float wp_landing_distance, float bearing_lastwp_currwp, float bearing_airplane_currwp, float wp_landing_altitude) +{ + + return wp_landing_altitude + getFlareCurveRelativeAltitudeSave(wp_landing_distance, bearing_lastwp_currwp, bearing_airplane_currwp); } diff --git a/src/modules/fw_pos_control_l1/landingslope.h b/src/modules/fw_pos_control_l1/landingslope.h index 76d65a55f..b54fd501c 100644 --- a/src/modules/fw_pos_control_l1/landingslope.h +++ b/src/modules/fw_pos_control_l1/landingslope.h @@ -63,11 +63,26 @@ public: Landingslope() {} ~Landingslope() {} + + /** + * + * @return relative altitude of point on landing slope at distance to landing waypoint=wp_landing_distance + */ + float getLandingSlopeRelativeAltitude(float wp_landing_distance); + + /** + * + * @return relative altitude of point on landing slope at distance to landing waypoint=wp_landing_distance + * Performs check if aircraft is in front of waypoint to avoid climbout + */ + float getLandingSlopeRelativeAltitudeSave(float wp_landing_distance, float bearing_lastwp_currwp, float bearing_airplane_currwp); + + /** * * @return Absolute altitude of point on landing slope at distance to landing waypoint=wp_landing_distance */ - float getLandingSlopeAbsoluteAltitude(float wp_distance, float wp_altitude); + float getLandingSlopeAbsoluteAltitude(float wp_landing_distance, float wp_altitude); /** * @@ -78,11 +93,20 @@ public: /** * + * @return Relative altitude of point on landing slope at distance to landing waypoint=wp_landing_distance + */ + __EXPORT static float getLandingSlopeRelativeAltitude(float wp_landing_distance, float horizontal_slope_displacement, float landing_slope_angle_rad) + { + return (wp_landing_distance - horizontal_slope_displacement) * tanf(landing_slope_angle_rad); //flare_relative_alt is negative + } + + /** + * * @return Absolute altitude of point on landing slope at distance to landing waypoint=wp_landing_distance */ __EXPORT static float getLandingSlopeAbsoluteAltitude(float wp_landing_distance, float wp_landing_altitude, float horizontal_slope_displacement, float landing_slope_angle_rad) { - return (wp_landing_distance - horizontal_slope_displacement) * tanf(landing_slope_angle_rad) + wp_landing_altitude; //flare_relative_alt is negative + return getLandingSlopeRelativeAltitude(wp_landing_distance, horizontal_slope_displacement, landing_slope_angle_rad) + wp_landing_altitude; } /** @@ -95,8 +119,9 @@ public: } + float getFlareCurveRelativeAltitudeSave(float wp_distance, float bearing_lastwp_currwp, float bearing_airplane_currwp); - float getFlareCurveAltitudeSave(float wp_distance, float bearing_lastwp_currwp, float bearing_airplane_currwp, float wp_altitude); + float getFlareCurveAbsoluteAltitudeSave(float wp_distance, float bearing_lastwp_currwp, float bearing_airplane_currwp, float wp_altitude); void update(float landing_slope_angle_rad, float flare_relative_alt, diff --git a/src/modules/mavlink/mavlink.c b/src/modules/mavlink/mavlink.c index ad435b251..e49288a74 100644 --- a/src/modules/mavlink/mavlink.c +++ b/src/modules/mavlink/mavlink.c @@ -62,6 +62,12 @@ PARAM_DEFINE_INT32(MAV_COMP_ID, 50); * @group MAVLink */ PARAM_DEFINE_INT32(MAV_TYPE, MAV_TYPE_FIXED_WING); +/** + * Use/Accept HIL GPS message (even if not in HIL mode) + * If set to 1 incomming HIL GPS messages are parsed. + * @group MAVLink + */ +PARAM_DEFINE_INT32(MAV_USEHILGPS, 0); mavlink_system_t mavlink_system = { 100, diff --git a/src/modules/position_estimator_mc/position_estimator_mc_params.c b/src/modules/mavlink/mavlink_commands.cpp index 72e5bc73b..1c1e097a4 100755..100644 --- a/src/modules/position_estimator_mc/position_estimator_mc_params.c +++ b/src/modules/mavlink/mavlink_commands.cpp @@ -1,9 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: Damian Aregger <daregger@student.ethz.ch> - * Tobias Naegeli <naegelit@student.ethz.ch> -* Lorenz Meier <lm@inf.ethz.ch> + * Copyright (c) 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -34,35 +31,43 @@ * ****************************************************************************/ -/* - * @file position_estimator_mc_params.c - * - * Parameters for position_estimator_mc +/** + * @file mavlink_commands.cpp + * Mavlink commands stream implementation. + * + * @author Anton Babushkin <anton.babushkin@me.com> */ -#include "position_estimator_mc_params.h" +#include "mavlink_commands.h" -/* Kalman Filter covariances */ -/* gps measurement noise standard deviation */ -PARAM_DEFINE_FLOAT(POS_EST_ADDN, 1.0f); -PARAM_DEFINE_FLOAT(POS_EST_SIGMA, 0.0f); -PARAM_DEFINE_FLOAT(POS_EST_R, 1.0f); -PARAM_DEFINE_INT32(POS_EST_BARO, 0.0f); +MavlinkCommandsStream::MavlinkCommandsStream(Mavlink *mavlink, mavlink_channel_t channel) : _channel(channel) +{ + _cmd_sub = mavlink->add_orb_subscription(ORB_ID(vehicle_command)); + _cmd = (struct vehicle_command_s *)_cmd_sub->get_data(); +} -int parameters_init(struct position_estimator_mc_param_handles *h) +MavlinkCommandsStream::~MavlinkCommandsStream() { - h->addNoise = param_find("POS_EST_ADDN"); - h->sigma = param_find("POS_EST_SIGMA"); - h->r = param_find("POS_EST_R"); - h->baro_param_handle = param_find("POS_EST_BARO"); - return OK; } -int parameters_update(const struct position_estimator_mc_param_handles *h, struct position_estimator_mc_params *p) +void +MavlinkCommandsStream::update(const hrt_abstime t) { - param_get(h->addNoise, &(p->addNoise)); - param_get(h->sigma, &(p->sigma)); - param_get(h->r, &(p->R)); - param_get(h->baro_param_handle, &(p->baro)); - return OK; + if (_cmd_sub->update(t)) { + /* only send commands for other systems/components */ + if (_cmd->target_system != mavlink_system.sysid || _cmd->target_component != mavlink_system.compid) { + mavlink_msg_command_long_send(_channel, + _cmd->target_system, + _cmd->target_component, + _cmd->command, + _cmd->confirmation, + _cmd->param1, + _cmd->param2, + _cmd->param3, + _cmd->param4, + _cmd->param5, + _cmd->param6, + _cmd->param7); + } + } } diff --git a/src/systemcmds/hw_ver/hw_ver.c b/src/modules/mavlink/mavlink_commands.h index 4b84523cc..6255d65df 100644 --- a/src/systemcmds/hw_ver/hw_ver.c +++ b/src/modules/mavlink/mavlink_commands.h @@ -32,42 +32,34 @@ ****************************************************************************/ /** - * @file hw_ver.c + * @file mavlink_commands.h + * Mavlink commands stream definition. * - * Show and test hardware version. + * @author Anton Babushkin <anton.babushkin@me.com> */ -#include <nuttx/config.h> +#ifndef MAVLINK_COMMANDS_H_ +#define MAVLINK_COMMANDS_H_ -#include <stdio.h> -#include <string.h> -#include <errno.h> -#include <version/version.h> +#include <uORB/uORB.h> +#include <uORB/topics/vehicle_command.h> -__EXPORT int hw_ver_main(int argc, char *argv[]); +class Mavlink; +class MavlinkCommansStream; -int -hw_ver_main(int argc, char *argv[]) -{ - if (argc >= 2) { - if (!strcmp(argv[1], "show")) { - printf(HW_ARCH "\n"); - exit(0); - } +#include "mavlink_main.h" - if (!strcmp(argv[1], "compare")) { - if (argc >= 3) { - int ret = strcmp(HW_ARCH, argv[2]) != 0; - if (ret == 0) { - printf("hw_ver match: %s\n", HW_ARCH); - } - exit(ret); +class MavlinkCommandsStream +{ +private: + MavlinkOrbSubscription *_cmd_sub; + struct vehicle_command_s *_cmd; + mavlink_channel_t _channel; - } else { - errx(1, "not enough arguments, try 'compare PX4FMU_1'"); - } - } - } +public: + MavlinkCommandsStream(Mavlink *mavlink, mavlink_channel_t channel); + ~MavlinkCommandsStream(); + void update(const hrt_abstime t); +}; - errx(1, "expected a command, try 'show' or 'compare'"); -} +#endif /* MAVLINK_COMMANDS_H_ */ diff --git a/src/modules/mavlink/mavlink_main.cpp b/src/modules/mavlink/mavlink_main.cpp index 18df577fe..6c97bfca7 100644 --- a/src/modules/mavlink/mavlink_main.cpp +++ b/src/modules/mavlink/mavlink_main.cpp @@ -81,6 +81,7 @@ #include "mavlink_messages.h" #include "mavlink_receiver.h" #include "mavlink_rate_limiter.h" +#include "mavlink_commands.h" /* oddly, ERROR is not defined for c++ */ #ifdef ERROR @@ -166,12 +167,12 @@ mavlink_send_uart_bytes(mavlink_channel_t channel, const uint8_t *ch, int length int buf_free = 0; if (instance->get_flow_control_enabled() - && ioctl(uart, FIONWRITE, (unsigned long)&buf_free) == 0) { + && ioctl(uart, FIONWRITE, (unsigned long)&buf_free) == 0) { if (buf_free == 0) { if (last_write_times[(unsigned)channel] != 0 && - hrt_elapsed_time(&last_write_times[(unsigned)channel]) > 500 * 1000UL) { + hrt_elapsed_time(&last_write_times[(unsigned)channel]) > 500 * 1000UL) { warnx("DISABLING HARDWARE FLOW CONTROL"); instance->enable_flow_control(false); @@ -185,12 +186,26 @@ mavlink_send_uart_bytes(mavlink_channel_t channel, const uint8_t *ch, int length } } - ssize_t ret = write(uart, ch, desired); + /* If the wait until transmit flag is on, only transmit after we've received messages. + Otherwise, transmit all the time. */ + if (instance->should_transmit()) { - if (ret != desired) { - // XXX do something here, but change to using FIONWRITE and OS buf size for detection + /* check if there is space in the buffer, let it overflow else */ + if (!ioctl(uart, FIONWRITE, (unsigned long)&buf_free)) { + + if (desired > buf_free) { + desired = buf_free; + } + } + + ssize_t ret = write(uart, ch, desired); + if (ret != desired) { + warnx("TX FAIL"); + } } + + } static void usage(void); @@ -202,15 +217,23 @@ Mavlink::Mavlink() : _mavlink_fd(-1), _task_running(false), _hil_enabled(false), + _use_hil_gps(false), _is_usb_uart(false), + _wait_to_transmit(false), + _received_messages(false), _main_loop_delay(1000), _subscriptions(nullptr), _streams(nullptr), _mission_pub(-1), + _verbose(false), + _forwarding_on(false), + _passing_on(false), + _uart_fd(-1), _mavlink_param_queue_index(0), _subscribe_to_stream(nullptr), _subscribe_to_stream_rate(0.0f), _flow_control_enabled(true), + _message_buffer({}), /* performance counters */ _loop_perf(perf_alloc(PC_ELAPSED, "mavlink")) @@ -261,7 +284,6 @@ Mavlink::Mavlink() : errx(1, "instance ID is out of range"); break; } - } Mavlink::~Mavlink() @@ -394,6 +416,18 @@ Mavlink::instance_exists(const char *device_name, Mavlink *self) return false; } +void +Mavlink::forward_message(mavlink_message_t *msg, Mavlink *self) +{ + + Mavlink *inst; + LL_FOREACH(_mavlink_instances, inst) { + if (inst != self) { + inst->pass_message(msg); + } + } +} + int Mavlink::get_uart_fd(unsigned index) { @@ -463,11 +497,13 @@ void Mavlink::mavlink_update_system(void) static param_t param_system_id; static param_t param_component_id; static param_t param_system_type; + static param_t param_use_hil_gps; if (!initialized) { param_system_id = param_find("MAV_SYS_ID"); param_component_id = param_find("MAV_COMP_ID"); param_system_type = param_find("MAV_TYPE"); + param_use_hil_gps = param_find("MAV_USEHILGPS"); initialized = true; } @@ -492,6 +528,11 @@ void Mavlink::mavlink_update_system(void) if (system_type >= 0 && system_type < MAV_TYPE_ENUM_END) { mavlink_system.type = system_type; } + + int32_t use_hil_gps; + param_get(param_use_hil_gps, &use_hil_gps); + + _use_hil_gps = (bool)use_hil_gps; } int Mavlink::mavlink_open_uart(int baud, const char *uart_name, struct termios *uart_config_original, bool *is_usb) @@ -550,6 +591,11 @@ int Mavlink::mavlink_open_uart(int baud, const char *uart_name, struct termios * /* open uart */ _uart_fd = open(uart_name, O_RDWR | O_NOCTTY); + if (_uart_fd < 0) { + return _uart_fd; + } + + /* Try to set baud rate */ struct termios uart_config; int termios_state; @@ -690,9 +736,9 @@ int Mavlink::mavlink_pm_send_param(param_t param) if (param == PARAM_INVALID) { return 1; } /* buffers for param transmission */ - static char name_buf[MAVLINK_MSG_PARAM_VALUE_FIELD_PARAM_ID_LEN]; + char name_buf[MAVLINK_MSG_PARAM_VALUE_FIELD_PARAM_ID_LEN]; float val_buf; - static mavlink_message_t tx_msg; + mavlink_message_t tx_msg; /* query parameter type */ param_type_t type = param_type(param); @@ -808,10 +854,10 @@ void Mavlink::publish_mission() { /* Initialize mission publication if necessary */ if (_mission_pub < 0) { - _mission_pub = orb_advertise(ORB_ID(mission), &mission); + _mission_pub = orb_advertise(ORB_ID(offboard_mission), &mission); } else { - orb_publish(ORB_ID(mission), _mission_pub, &mission); + orb_publish(ORB_ID(offboard_mission), _mission_pub, &mission); } } @@ -1486,6 +1532,8 @@ void Mavlink::mavlink_wpm_message_handler(const mavlink_message_t *msg) void Mavlink::mavlink_missionlib_send_message(mavlink_message_t *msg) { + uint8_t missionlib_msg_buf[MAVLINK_MAX_PACKET_LEN]; + uint16_t len = mavlink_msg_to_send_buffer(missionlib_msg_buf, msg); mavlink_send_uart_bytes(_channel, missionlib_msg_buf, len); @@ -1498,6 +1546,8 @@ Mavlink::mavlink_missionlib_send_gcs_string(const char *string) { const int len = MAVLINK_MSG_STATUSTEXT_FIELD_TEXT_LEN; mavlink_statustext_t statustext; + statustext.severity = MAV_SEVERITY_INFO; + int i = 0; while (i < len - 1) { @@ -1617,6 +1667,125 @@ Mavlink::configure_stream_threadsafe(const char *stream_name, const float rate) } int +Mavlink::message_buffer_init(int size) +{ + _message_buffer.size = size; + _message_buffer.write_ptr = 0; + _message_buffer.read_ptr = 0; + _message_buffer.data = (char*)malloc(_message_buffer.size); + return (_message_buffer.data == 0) ? ERROR : OK; +} + +void +Mavlink::message_buffer_destroy() +{ + _message_buffer.size = 0; + _message_buffer.write_ptr = 0; + _message_buffer.read_ptr = 0; + free(_message_buffer.data); +} + +int +Mavlink::message_buffer_count() +{ + int n = _message_buffer.write_ptr - _message_buffer.read_ptr; + + if (n < 0) { + n += _message_buffer.size; + } + + return n; +} + +int +Mavlink::message_buffer_is_empty() +{ + return _message_buffer.read_ptr == _message_buffer.write_ptr; +} + + +bool +Mavlink::message_buffer_write(void *ptr, int size) +{ + // bytes available to write + int available = _message_buffer.read_ptr - _message_buffer.write_ptr - 1; + + if (available < 0) { + available += _message_buffer.size; + } + + if (size > available) { + // buffer overflow + return false; + } + + char *c = (char *) ptr; + int n = _message_buffer.size - _message_buffer.write_ptr; // bytes to end of the buffer + + if (n < size) { + // message goes over end of the buffer + memcpy(&(_message_buffer.data[_message_buffer.write_ptr]), c, n); + _message_buffer.write_ptr = 0; + + } else { + n = 0; + } + + // now: n = bytes already written + int p = size - n; // number of bytes to write + memcpy(&(_message_buffer.data[_message_buffer.write_ptr]), &(c[n]), p); + _message_buffer.write_ptr = (_message_buffer.write_ptr + p) % _message_buffer.size; + return true; +} + +int +Mavlink::message_buffer_get_ptr(void **ptr, bool *is_part) +{ + // bytes available to read + int available = _message_buffer.write_ptr - _message_buffer.read_ptr; + + if (available == 0) { + return 0; // buffer is empty + } + + int n = 0; + + if (available > 0) { + // read pointer is before write pointer, all available bytes can be read + n = available; + *is_part = false; + + } else { + // read pointer is after write pointer, read bytes from read_ptr to end of the buffer + n = _message_buffer.size - _message_buffer.read_ptr; + *is_part = _message_buffer.write_ptr > 0; + } + + *ptr = &(_message_buffer.data[_message_buffer.read_ptr]); + return n; +} + +void +Mavlink::message_buffer_mark_read(int n) +{ + _message_buffer.read_ptr = (_message_buffer.read_ptr + n) % _message_buffer.size; +} + +void +Mavlink::pass_message(mavlink_message_t *msg) +{ + if (_passing_on) { + /* size is 8 bytes plus variable payload */ + int size = MAVLINK_NUM_NON_PAYLOAD_BYTES + msg->len; + pthread_mutex_lock(&_message_buffer_mutex); + message_buffer_write(msg, size); + pthread_mutex_unlock(&_message_buffer_mutex); + } +} + + + +int Mavlink::task_main(int argc, char *argv[]) { int ch; @@ -1632,7 +1801,7 @@ Mavlink::task_main(int argc, char *argv[]) * set error flag instead */ bool err_flag = false; - while ((ch = getopt(argc, argv, "b:r:d:m:v")) != EOF) { + while ((ch = getopt(argc, argv, "b:r:d:m:fpvw")) != EOF) { switch (ch) { case 'b': _baudrate = strtoul(optarg, NULL, 10); @@ -1672,10 +1841,22 @@ Mavlink::task_main(int argc, char *argv[]) break; + case 'f': + _forwarding_on = true; + break; + + case 'p': + _passing_on = true; + break; + case 'v': _verbose = true; break; + case 'w': + _wait_to_transmit = true; + break; + default: err_flag = true; break; @@ -1740,6 +1921,17 @@ Mavlink::task_main(int argc, char *argv[]) /* initialize mavlink text message buffering */ mavlink_logbuffer_init(&_logbuffer, 5); + /* if we are passing on mavlink messages, we need to prepare a buffer for this instance */ + if (_passing_on) { + /* initialize message buffer if multiplexing is on */ + if (OK != message_buffer_init(500)) { + errx(1, "can't allocate message buffer, exiting"); + } + + /* initialize message buffer mutex */ + pthread_mutex_init(&_message_buffer_mutex, NULL); + } + /* create the device node that's used for sending text log messages, etc. */ register_driver(MAVLINK_LOG_DEVICE, &fops, 0666, NULL); @@ -1766,6 +1958,8 @@ Mavlink::task_main(int argc, char *argv[]) struct vehicle_status_s *status = (struct vehicle_status_s *) status_sub->get_data(); + MavlinkCommandsStream commands_stream(this, _channel); + /* add default streams depending on mode and intervals depending on datarate */ float rate_mult = _datarate / 1000.0f; @@ -1783,6 +1977,9 @@ Mavlink::task_main(int argc, char *argv[]) configure_stream("LOCAL_POSITION_NED", 3.0f * rate_mult); configure_stream("RC_CHANNELS_RAW", 1.0f * rate_mult); configure_stream("NAMED_VALUE_FLOAT", 1.0f * rate_mult); + configure_stream("GLOBAL_POSITION_SETPOINT_INT", 3.0f * rate_mult); + configure_stream("ROLL_PITCH_YAW_THRUST_SETPOINT", 3.0f * rate_mult); + configure_stream("DISTANCE_SENSOR", 0.5f); break; case MAVLINK_MODE_CAMERA: @@ -1826,6 +2023,9 @@ Mavlink::task_main(int argc, char *argv[]) set_hil_enabled(status->hil_state == HIL_STATE_ON); } + /* update commands stream */ + commands_stream.update(t); + /* check for requested subscriptions */ if (_subscribe_to_stream != nullptr) { if (OK == configure_stream(_subscribe_to_stream, _subscribe_to_stream_rate)) { @@ -1884,6 +2084,37 @@ Mavlink::task_main(int argc, char *argv[]) } } + /* pass messages from other UARTs */ + if (_passing_on) { + + bool is_part; + void *read_ptr; + + /* guard get ptr by mutex */ + pthread_mutex_lock(&_message_buffer_mutex); + int available = message_buffer_get_ptr(&read_ptr, &is_part); + pthread_mutex_unlock(&_message_buffer_mutex); + + if (available > 0) { + /* write first part of buffer */ + _mavlink_resend_uart(_channel, (const mavlink_message_t*)read_ptr); + message_buffer_mark_read(available); + + /* write second part of buffer if there is some */ + if (is_part) { + /* guard get ptr by mutex */ + pthread_mutex_lock(&_message_buffer_mutex); + available = message_buffer_get_ptr(&read_ptr, &is_part); + pthread_mutex_unlock(&_message_buffer_mutex); + + _mavlink_resend_uart(_channel, (const mavlink_message_t*)read_ptr); + message_buffer_mark_read(available); + } + } + } + + + perf_end(_loop_perf); } @@ -1928,6 +2159,10 @@ Mavlink::task_main(int argc, char *argv[]) /* close mavlink logging device */ close(_mavlink_fd); + if (_passing_on) { + message_buffer_destroy(); + pthread_mutex_destroy(&_message_buffer_mutex); + } /* destroy log buffer */ mavlink_logbuffer_destroy(&_logbuffer); @@ -1969,7 +2204,7 @@ Mavlink::start(int argc, char *argv[]) task_spawn_cmd(buf, SCHED_DEFAULT, SCHED_PRIORITY_DEFAULT, - 2048, + 1950, (main_t)&Mavlink::start_helper, (const char **)argv); @@ -2067,7 +2302,7 @@ Mavlink::stream(int argc, char *argv[]) static void usage() { - warnx("usage: mavlink {start|stop-all|stream} [-d device] [-b baudrate] [-r rate] [-m mode] [-s stream] [-v]"); + warnx("usage: mavlink {start|stop-all|stream} [-d device] [-b baudrate] [-r rate] [-m mode] [-s stream] [-f] [-p] [-v] [-w]"); } int mavlink_main(int argc, char *argv[]) diff --git a/src/modules/mavlink/mavlink_main.h b/src/modules/mavlink/mavlink_main.h index 5a118a0ad..c7a7d32f8 100644 --- a/src/modules/mavlink/mavlink_main.h +++ b/src/modules/mavlink/mavlink_main.h @@ -138,6 +138,8 @@ public: static bool instance_exists(const char *device_name, Mavlink *self); + static void forward_message(mavlink_message_t *msg, Mavlink *self); + static int get_uart_fd(unsigned index); int get_uart_fd(); @@ -153,10 +155,14 @@ public: void set_mode(enum MAVLINK_MODE); enum MAVLINK_MODE get_mode() { return _mode; } - bool get_hil_enabled() { return _hil_enabled; }; + bool get_hil_enabled() { return _hil_enabled; } + + bool get_use_hil_gps() { return _use_hil_gps; } bool get_flow_control_enabled() { return _flow_control_enabled; } + bool get_forwarding_on() { return _forwarding_on; } + /** * Handle waypoint related messages. */ @@ -196,6 +202,16 @@ public: bool _task_should_exit; /**< if true, mavlink task should exit */ + int get_mavlink_fd() { return _mavlink_fd; } + + + /* Functions for waiting to start transmission until message received. */ + void set_has_received_messages(bool received_messages) { _received_messages = received_messages; } + bool get_has_received_messages() { return _received_messages; } + void set_wait_to_transmit(bool wait) { _wait_to_transmit = wait; } + bool get_wait_to_transmit() { return _wait_to_transmit; } + bool should_transmit() { return (!_wait_to_transmit || (_wait_to_transmit && _received_messages)); } + protected: Mavlink *next; @@ -209,7 +225,10 @@ private: /* states */ bool _hil_enabled; /**< Hardware In the Loop mode */ + bool _use_hil_gps; /**< Accept GPS HIL messages (for example from an external motion capturing system to fake indoor gps) */ bool _is_usb_uart; /**< Port is USB */ + bool _wait_to_transmit; /**< Wait to transmit until received messages. */ + bool _received_messages; /**< Whether we've received valid mavlink messages. */ unsigned _main_loop_delay; /**< mainloop delay, depends on data rate */ @@ -218,7 +237,6 @@ private: orb_advert_t _mission_pub; struct mission_s mission; - uint8_t missionlib_msg_buf[MAVLINK_MAX_PACKET_LEN]; MAVLINK_MODE _mode; uint8_t _mavlink_wpm_comp_id; @@ -234,6 +252,8 @@ private: mavlink_wpm_storage *_wpm; bool _verbose; + bool _forwarding_on; + bool _passing_on; int _uart_fd; int _baudrate; int _datarate; @@ -252,6 +272,18 @@ private: bool _flow_control_enabled; + struct mavlink_message_buffer { + int write_ptr; + int read_ptr; + int size; + char *data; + }; + mavlink_message_buffer _message_buffer; + + pthread_mutex_t _message_buffer_mutex; + + + /** * Send one parameter. * @@ -315,6 +347,22 @@ private: int configure_stream(const char *stream_name, const float rate); void configure_stream_threadsafe(const char *stream_name, const float rate); + int message_buffer_init(int size); + + void message_buffer_destroy(); + + int message_buffer_count(); + + int message_buffer_is_empty(); + + bool message_buffer_write(void *ptr, int size); + + int message_buffer_get_ptr(void **ptr, bool *is_part); + + void message_buffer_mark_read(int n); + + void pass_message(mavlink_message_t *msg); + static int mavlink_dev_ioctl(struct file *filep, int cmd, unsigned long arg); /** diff --git a/src/modules/mavlink/mavlink_messages.cpp b/src/modules/mavlink/mavlink_messages.cpp index 037999af7..79dd88657 100644 --- a/src/modules/mavlink/mavlink_messages.cpp +++ b/src/modules/mavlink/mavlink_messages.cpp @@ -71,6 +71,8 @@ #include <uORB/topics/battery_status.h> #include <uORB/topics/navigation_capabilities.h> #include <drivers/drv_rc_input.h> +#include <drivers/drv_pwm_output.h> +#include <drivers/drv_range_finder.h> #include "mavlink_messages.h" @@ -122,13 +124,13 @@ void get_mavlink_mode_state(struct vehicle_status_s *status, struct position_set *mavlink_base_mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED | (status->is_rotary_wing ? MAV_MODE_FLAG_STABILIZE_ENABLED : 0); custom_mode.main_mode = PX4_CUSTOM_MAIN_MODE_MANUAL; - } else if (status->main_state == MAIN_STATE_SEATBELT) { + } else if (status->main_state == MAIN_STATE_ALTCTL) { *mavlink_base_mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED | MAV_MODE_FLAG_STABILIZE_ENABLED; - custom_mode.main_mode = PX4_CUSTOM_MAIN_MODE_SEATBELT; + custom_mode.main_mode = PX4_CUSTOM_MAIN_MODE_ALTCTL; - } else if (status->main_state == MAIN_STATE_EASY) { + } else if (status->main_state == MAIN_STATE_POSCTL) { *mavlink_base_mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED | MAV_MODE_FLAG_STABILIZE_ENABLED | MAV_MODE_FLAG_GUIDED_ENABLED; - custom_mode.main_mode = PX4_CUSTOM_MAIN_MODE_EASY; + custom_mode.main_mode = PX4_CUSTOM_MAIN_MODE_POSCTL; } else if (status->main_state == MAIN_STATE_AUTO) { *mavlink_base_mode |= MAV_MODE_FLAG_AUTO_ENABLED | MAV_MODE_FLAG_STABILIZE_ENABLED | MAV_MODE_FLAG_GUIDED_ENABLED; @@ -261,22 +263,21 @@ protected: void send(const hrt_abstime t) { - if (status_sub->update(t)) { - mavlink_msg_sys_status_send(_channel, - status->onboard_control_sensors_present, - status->onboard_control_sensors_enabled, - status->onboard_control_sensors_health, - status->load * 1000.0f, - status->battery_voltage * 1000.0f, - status->battery_current * 1000.0f, - status->battery_remaining, - status->drop_rate_comm, - status->errors_comm, - status->errors_count1, - status->errors_count2, - status->errors_count3, - status->errors_count4); - } + status_sub->update(t); + mavlink_msg_sys_status_send(_channel, + status->onboard_control_sensors_present, + status->onboard_control_sensors_enabled, + status->onboard_control_sensors_health, + status->load * 1000.0f, + status->battery_voltage * 1000.0f, + status->battery_current * 1000.0f, + status->battery_remaining * 100.0f, + status->drop_rate_comm, + status->errors_comm, + status->errors_count1, + status->errors_count2, + status->errors_count3, + status->errors_count4); } }; @@ -640,6 +641,47 @@ protected: }; + +class MavlinkStreamViconPositionEstimate : public MavlinkStream +{ +public: + const char *get_name() + { + return "VICON_POSITION_ESTIMATE"; + } + + MavlinkStream *new_instance() + { + return new MavlinkStreamViconPositionEstimate(); + } + +private: + MavlinkOrbSubscription *pos_sub; + struct vehicle_vicon_position_s *pos; + +protected: + void subscribe(Mavlink *mavlink) + { + pos_sub = mavlink->add_orb_subscription(ORB_ID(vehicle_vicon_position)); + pos = (struct vehicle_vicon_position_s *)pos_sub->get_data(); + } + + void send(const hrt_abstime t) + { + if (pos_sub->update(t)) { + mavlink_msg_vicon_position_estimate_send(_channel, + pos->timestamp / 1000, + pos->x, + pos->y, + pos->z, + pos->roll, + pos->pitch, + pos->yaw); + } + } +}; + + class MavlinkStreamGPSGlobalOrigin : public MavlinkStream { public: @@ -777,58 +819,90 @@ protected: void send(const hrt_abstime t) { - bool updated = status_sub->update(t); - updated |= pos_sp_triplet_sub->update(t); - updated |= act_sub->update(t); + bool updated = act_sub->update(t); + (void)pos_sp_triplet_sub->update(t); + (void)status_sub->update(t); - if (updated) { + if (updated && (status->arming_state == ARMING_STATE_ARMED)) { /* translate the current syste state to mavlink state and mode */ uint8_t mavlink_state; uint8_t mavlink_base_mode; uint32_t mavlink_custom_mode; get_mavlink_mode_state(status, pos_sp_triplet, &mavlink_state, &mavlink_base_mode, &mavlink_custom_mode); - /* set number of valid outputs depending on vehicle type */ - unsigned n; + if (mavlink_system.type == MAV_TYPE_QUADROTOR || + mavlink_system.type == MAV_TYPE_HEXAROTOR || + mavlink_system.type == MAV_TYPE_OCTOROTOR) { + /* set number of valid outputs depending on vehicle type */ + unsigned n; - switch (mavlink_system.type) { - case MAV_TYPE_QUADROTOR: - n = 4; - break; + switch (mavlink_system.type) { + case MAV_TYPE_QUADROTOR: + n = 4; + break; - case MAV_TYPE_HEXAROTOR: - n = 6; - break; + case MAV_TYPE_HEXAROTOR: + n = 6; + break; - default: - n = 8; - break; - } + default: + n = 8; + break; + } + + /* scale / assign outputs depending on system type */ + float out[8]; - /* scale / assign outputs depending on system type */ - float out[8]; + for (unsigned i = 0; i < 8; i++) { + if (i < n) { + if (mavlink_base_mode & MAV_MODE_FLAG_SAFETY_ARMED) { + /* scale fake PWM out 900..2100 us to 0..1 for normal multirotors */ + out[i] = (act->output[i] - PWM_LOWEST_MIN) / (PWM_HIGHEST_MAX - PWM_LOWEST_MIN); - for (unsigned i = 0; i < 8; i++) { - if (i < n) { - if (mavlink_base_mode & MAV_MODE_FLAG_SAFETY_ARMED) { - /* scale fake PWM out 900..1200 us to 0..1*/ - out[i] = (act->output[i] - 900.0f) / 1200.0f; + } else { + /* send 0 when disarmed */ + out[i] = 0.0f; + } } else { - /* send 0 when disarmed */ - out[i] = 0.0f; + out[i] = -1.0f; + } + } + + mavlink_msg_hil_controls_send(_channel, + hrt_absolute_time(), + out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7], + mavlink_base_mode, + 0); + } else { + + /* fixed wing: scale all channels except throttle -1 .. 1 + * because we know that we set the mixers up this way + */ + + float out[8]; + + const float pwm_center = (PWM_HIGHEST_MAX + PWM_LOWEST_MIN) / 2; + + for (unsigned i = 0; i < 8; i++) { + if (i != 3) { + /* scale fake PWM out 900..2100 us to -1..+1 for normal channels */ + out[i] = (act->output[i] - pwm_center) / ((PWM_HIGHEST_MAX - PWM_LOWEST_MIN) / 2); + + } else { + + /* scale fake PWM out 900..2100 us to 0..1 for throttle */ + out[i] = (act->output[i] - PWM_LOWEST_MIN) / (PWM_HIGHEST_MAX - PWM_LOWEST_MIN); } - } else { - out[i] = -1.0f; } - } - mavlink_msg_hil_controls_send(_channel, - hrt_absolute_time(), - out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7], - mavlink_base_mode, - 0); + mavlink_msg_hil_controls_send(_channel, + hrt_absolute_time(), + out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7], + mavlink_base_mode, + 0); + } } } }; @@ -1064,10 +1138,10 @@ protected: if (manual_sub->update(t)) { mavlink_msg_manual_control_send(_channel, mavlink_system.sysid, - manual->roll * 1000, - manual->pitch * 1000, - manual->yaw * 1000, - manual->throttle * 1000, + manual->x * 1000, + manual->y * 1000, + manual->z * 1000, + manual->r * 1000, 0); } } @@ -1220,8 +1294,6 @@ protected: { status_sub = mavlink->add_orb_subscription(ORB_ID(vehicle_status)); status = (struct vehicle_status_s *)status_sub->get_data(); - - } void send(const hrt_abstime t) @@ -1232,11 +1304,57 @@ protected: || status->arming_state == ARMING_STATE_ARMED_ERROR) { /* send camera capture on */ - mavlink_msg_command_long_send(_channel, 42, 30, MAV_CMD_DO_CONTROL_VIDEO, 0, 0, 0, 0, 1, 0, 0, 0); + mavlink_msg_command_long_send(_channel, mavlink_system.sysid, 0, MAV_CMD_DO_CONTROL_VIDEO, 0, 0, 0, 0, 1, 0, 0, 0); } else { /* send camera capture off */ - mavlink_msg_command_long_send(_channel, 42, 30, MAV_CMD_DO_CONTROL_VIDEO, 0, 0, 0, 0, 0, 0, 0, 0); + mavlink_msg_command_long_send(_channel, mavlink_system.sysid, 0, MAV_CMD_DO_CONTROL_VIDEO, 0, 0, 0, 0, 0, 0, 0, 0); + } + } +}; + +class MavlinkStreamDistanceSensor : public MavlinkStream +{ +public: + const char *get_name() + { + return "DISTANCE_SENSOR"; + } + + MavlinkStream *new_instance() + { + return new MavlinkStreamDistanceSensor(); + } + +private: + MavlinkOrbSubscription *range_sub; + struct range_finder_report *range; + +protected: + void subscribe(Mavlink *mavlink) + { + range_sub = mavlink->add_orb_subscription(ORB_ID(sensor_range_finder)); + range = (struct range_finder_report *)range_sub->get_data(); + } + + void send(const hrt_abstime t) + { + if (range_sub->update(t)) { + + uint8_t type; + + switch (range->type) { + case RANGE_FINDER_TYPE_LASER: + type = MAV_DISTANCE_SENSOR_LASER; + break; + } + + uint8_t id = 0; + uint8_t orientation = 0; + uint8_t covariance = 20; + + mavlink_msg_distance_sensor_send(_channel, range->timestamp / 1000, type, id, orientation, + range->minimum_distance*100, range->maximum_distance*100, range->distance*100, covariance); } } }; @@ -1267,5 +1385,7 @@ MavlinkStream *streams_list[] = { new MavlinkStreamAttitudeControls(), new MavlinkStreamNamedValueFloat(), new MavlinkStreamCameraCapture(), + new MavlinkStreamDistanceSensor(), + new MavlinkStreamViconPositionEstimate(), nullptr }; diff --git a/src/modules/mavlink/mavlink_orb_subscription.cpp b/src/modules/mavlink/mavlink_orb_subscription.cpp index 4de722832..d432edd2b 100644 --- a/src/modules/mavlink/mavlink_orb_subscription.cpp +++ b/src/modules/mavlink/mavlink_orb_subscription.cpp @@ -88,6 +88,7 @@ MavlinkOrbSubscription::update(const hrt_abstime t) if (_updated) { orb_copy(_topic, _fd, _data); + _published = true; return true; } } diff --git a/src/modules/mavlink/mavlink_receiver.cpp b/src/modules/mavlink/mavlink_receiver.cpp index 489d2bdcb..72b9ee83a 100644 --- a/src/modules/mavlink/mavlink_receiver.cpp +++ b/src/modules/mavlink/mavlink_receiver.cpp @@ -88,8 +88,6 @@ static const float mg2ms2 = CONSTANTS_ONE_G / 1000.0f; MavlinkReceiver::MavlinkReceiver(Mavlink *parent) : _mavlink(parent), - _manual_sub(-1), - _global_pos_pub(-1), _local_pos_pub(-1), _attitude_pub(-1), @@ -162,6 +160,9 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg) * The HIL mode is enabled by the HIL bit flag * in the system mode. Either send a set mode * COMMAND_LONG message or a SET_MODE message + * + * Accept HIL GPS messages if use_hil_gps flag is true. + * This allows to provide fake gps measurements to the system. */ if (_mavlink->get_hil_enabled()) { switch (msg->msgid) { @@ -169,10 +170,6 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg) handle_message_hil_sensor(msg); break; - case MAVLINK_MSG_ID_HIL_GPS: - handle_message_hil_gps(msg); - break; - case MAVLINK_MSG_ID_HIL_STATE_QUATERNION: handle_message_hil_state_quaternion(msg); break; @@ -181,6 +178,23 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg) break; } } + + + if (_mavlink->get_hil_enabled() || (_mavlink->get_use_hil_gps() && msg->sysid == mavlink_system.sysid)) { + switch (msg->msgid) { + case MAVLINK_MSG_ID_HIL_GPS: + handle_message_hil_gps(msg); + break; + + default: + break; + } + + } + + /* If we've received a valid message, mark the flag indicating so. + This is used in the '-w' command-line flag. */ + _mavlink->set_has_received_messages(true); } void @@ -203,6 +217,12 @@ MavlinkReceiver::handle_message_command_long(mavlink_message_t *msg) _mavlink->_task_should_exit = true; } else { + + if (msg->sysid == mavlink_system.sysid && msg->compid == mavlink_system.compid) { + warnx("ignoring CMD spoofed with same SYS/COMP ID"); + return; + } + struct vehicle_command_s vcmd; memset(&vcmd, 0, sizeof(vcmd)); @@ -222,12 +242,10 @@ MavlinkReceiver::handle_message_command_long(mavlink_message_t *msg) vcmd.source_component = msg->compid; vcmd.confirmation = cmd_mavlink.confirmation; - /* check if topic is advertised */ - if (_cmd_pub <= 0) { + if (_cmd_pub < 0) { _cmd_pub = orb_advertise(ORB_ID(vehicle_command), &vcmd); } else { - /* publish */ orb_publish(ORB_ID(vehicle_command), _cmd_pub, &vcmd); } } @@ -245,6 +263,7 @@ MavlinkReceiver::handle_message_optical_flow(mavlink_message_t *msg) memset(&f, 0, sizeof(f)); f.timestamp = hrt_absolute_time(); + f.flow_timestamp = flow.time_usec; f.flow_raw_x = flow.flow_x; f.flow_raw_y = flow.flow_y; f.flow_comp_x_m = flow.flow_comp_m_x; @@ -253,7 +272,7 @@ MavlinkReceiver::handle_message_optical_flow(mavlink_message_t *msg) f.quality = flow.quality; f.sensor_id = flow.sensor_id; - if (_flow_pub <= 0) { + if (_flow_pub < 0) { _flow_pub = orb_advertise(ORB_ID(optical_flow), &f); } else { @@ -287,7 +306,7 @@ MavlinkReceiver::handle_message_set_mode(mavlink_message_t *msg) vcmd.source_component = msg->compid; vcmd.confirmation = 1; - if (_cmd_pub <= 0) { + if (_cmd_pub < 0) { _cmd_pub = orb_advertise(ORB_ID(vehicle_command), &vcmd); } else { @@ -312,7 +331,7 @@ MavlinkReceiver::handle_message_vicon_position_estimate(mavlink_message_t *msg) vicon_position.pitch = pos.pitch; vicon_position.yaw = pos.yaw; - if (_vicon_position_pub <= 0) { + if (_vicon_position_pub < 0) { _vicon_position_pub = orb_advertise(ORB_ID(vehicle_vicon_position), &vicon_position); } else { @@ -373,7 +392,7 @@ MavlinkReceiver::handle_message_quad_swarm_roll_pitch_yaw_thrust(mavlink_message offboard_control_sp.timestamp = hrt_absolute_time(); - if (_offboard_control_sp_pub <= 0) { + if (_offboard_control_sp_pub < 0) { _offboard_control_sp_pub = orb_advertise(ORB_ID(offboard_control_setpoint), &offboard_control_sp); } else { @@ -401,7 +420,7 @@ MavlinkReceiver::handle_message_radio_status(mavlink_message_t *msg) tstatus.rxerrors = rstatus.rxerrors; tstatus.fixed = rstatus.fixed; - if (_telemetry_status_pub <= 0) { + if (_telemetry_status_pub < 0) { _telemetry_status_pub = orb_advertise(ORB_ID(telemetry_status), &tstatus); } else { @@ -415,47 +434,20 @@ MavlinkReceiver::handle_message_manual_control(mavlink_message_t *msg) mavlink_manual_control_t man; mavlink_msg_manual_control_decode(msg, &man); - /* rc channels */ - { - struct rc_channels_s rc; - memset(&rc, 0, sizeof(rc)); - - rc.timestamp = hrt_absolute_time(); - rc.chan_count = 4; + struct manual_control_setpoint_s manual; + memset(&manual, 0, sizeof(manual)); - rc.chan[0].scaled = man.x / 1000.0f; - rc.chan[1].scaled = man.y / 1000.0f; - rc.chan[2].scaled = man.r / 1000.0f; - rc.chan[3].scaled = man.z / 1000.0f; + manual.timestamp = hrt_absolute_time(); + manual.x = man.x / 1000.0f; + manual.y = man.y / 1000.0f; + manual.r = man.r / 1000.0f; + manual.z = man.z / 1000.0f; - if (_rc_pub == 0) { - _rc_pub = orb_advertise(ORB_ID(rc_channels), &rc); + if (_manual_pub < 0) { + _manual_pub = orb_advertise(ORB_ID(manual_control_setpoint), &manual); - } else { - orb_publish(ORB_ID(rc_channels), _rc_pub, &rc); - } - } - - /* manual control */ - { - struct manual_control_setpoint_s manual; - memset(&manual, 0, sizeof(manual)); - - /* get a copy first, to prevent altering values that are not sent by the mavlink command */ - orb_copy(ORB_ID(manual_control_setpoint), _manual_sub, &manual); - - manual.timestamp = hrt_absolute_time(); - manual.roll = man.x / 1000.0f; - manual.pitch = man.y / 1000.0f; - manual.yaw = man.r / 1000.0f; - manual.throttle = man.z / 1000.0f; - - if (_manual_pub == 0) { - _manual_pub = orb_advertise(ORB_ID(manual_control_setpoint), &manual); - - } else { - orb_publish(ORB_ID(manual_control_setpoint), _manual_pub, &manual); - } + } else { + orb_publish(ORB_ID(manual_control_setpoint), _manual_pub, &manual); } } @@ -619,11 +611,11 @@ MavlinkReceiver::handle_message_hil_sensor(mavlink_message_t *msg) hil_sensors.differential_pressure_timestamp = timestamp; /* publish combined sensor topic */ - if (_sensors_pub > 0) { - orb_publish(ORB_ID(sensor_combined), _sensors_pub, &hil_sensors); + if (_sensors_pub < 0) { + _sensors_pub = orb_advertise(ORB_ID(sensor_combined), &hil_sensors); } else { - _sensors_pub = orb_advertise(ORB_ID(sensor_combined), &hil_sensors); + orb_publish(ORB_ID(sensor_combined), _sensors_pub, &hil_sensors); } } @@ -634,13 +626,15 @@ MavlinkReceiver::handle_message_hil_sensor(mavlink_message_t *msg) hil_battery_status.timestamp = timestamp; hil_battery_status.voltage_v = 11.1f; + hil_battery_status.voltage_filtered_v = 11.1f; hil_battery_status.current_a = 10.0f; + hil_battery_status.discharged_mah = -1.0f; - if (_battery_pub > 0) { - orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status); + if (_battery_pub < 0) { + _battery_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status); } else { - _baro_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status); + orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status); } } @@ -692,11 +686,11 @@ MavlinkReceiver::handle_message_hil_gps(mavlink_message_t *msg) hil_gps.fix_type = gps.fix_type; hil_gps.satellites_visible = gps.satellites_visible; - if (_gps_pub > 0) { - orb_publish(ORB_ID(vehicle_gps_position), _gps_pub, &hil_gps); + if (_gps_pub < 0) { + _gps_pub = orb_advertise(ORB_ID(vehicle_gps_position), &hil_gps); } else { - _gps_pub = orb_advertise(ORB_ID(vehicle_gps_position), &hil_gps); + orb_publish(ORB_ID(vehicle_gps_position), _gps_pub, &hil_gps); } } @@ -750,11 +744,11 @@ MavlinkReceiver::handle_message_hil_state_quaternion(mavlink_message_t *msg) hil_attitude.pitchspeed = hil_state.pitchspeed; hil_attitude.yawspeed = hil_state.yawspeed; - if (_attitude_pub > 0) { - orb_publish(ORB_ID(vehicle_attitude), _attitude_pub, &hil_attitude); + if (_attitude_pub < 0) { + _attitude_pub = orb_advertise(ORB_ID(vehicle_attitude), &hil_attitude); } else { - _attitude_pub = orb_advertise(ORB_ID(vehicle_attitude), &hil_attitude); + orb_publish(ORB_ID(vehicle_attitude), _attitude_pub, &hil_attitude); } } @@ -764,7 +758,6 @@ MavlinkReceiver::handle_message_hil_state_quaternion(mavlink_message_t *msg) memset(&hil_global_pos, 0, sizeof(hil_global_pos)); hil_global_pos.timestamp = timestamp; - hil_global_pos.global_valid = true; hil_global_pos.lat = hil_state.lat; hil_global_pos.lon = hil_state.lon; hil_global_pos.alt = hil_state.alt / 1000.0f; @@ -772,30 +765,35 @@ MavlinkReceiver::handle_message_hil_state_quaternion(mavlink_message_t *msg) hil_global_pos.vel_e = hil_state.vy / 100.0f; hil_global_pos.vel_d = hil_state.vz / 100.0f; hil_global_pos.yaw = hil_attitude.yaw; + hil_global_pos.eph = 2.0f; + hil_global_pos.epv = 4.0f; - if (_global_pos_pub > 0) { - orb_publish(ORB_ID(vehicle_global_position), _global_pos_pub, &hil_global_pos); + if (_global_pos_pub < 0) { + _global_pos_pub = orb_advertise(ORB_ID(vehicle_global_position), &hil_global_pos); } else { - _global_pos_pub = orb_advertise(ORB_ID(vehicle_global_position), &hil_global_pos); + orb_publish(ORB_ID(vehicle_global_position), _global_pos_pub, &hil_global_pos); } } /* local position */ { + double lat = hil_state.lat * 1e-7; + double lon = hil_state.lon * 1e-7; + if (!_hil_local_proj_inited) { _hil_local_proj_inited = true; _hil_local_alt0 = hil_state.alt / 1000.0f; - map_projection_init(hil_state.lat, hil_state.lon); + map_projection_init(&_hil_local_proj_ref, hil_state.lat, hil_state.lon); hil_local_pos.ref_timestamp = timestamp; - hil_local_pos.ref_lat = hil_state.lat; - hil_local_pos.ref_lon = hil_state.lon; + hil_local_pos.ref_lat = lat; + hil_local_pos.ref_lon = lon; hil_local_pos.ref_alt = _hil_local_alt0; } float x; float y; - map_projection_project(hil_state.lat * 1e-7, hil_state.lon * 1e-7, &x, &y); + map_projection_project(&_hil_local_proj_ref, lat, lon, &x, &y); hil_local_pos.timestamp = timestamp; hil_local_pos.xy_valid = true; hil_local_pos.z_valid = true; @@ -814,11 +812,11 @@ MavlinkReceiver::handle_message_hil_state_quaternion(mavlink_message_t *msg) bool landed = (float)(hil_state.alt) / 1000.0f < (_hil_local_alt0 + 0.1f); // XXX improve? hil_local_pos.landed = landed; - if (_local_pos_pub > 0) { - orb_publish(ORB_ID(vehicle_local_position), _local_pos_pub, &hil_local_pos); + if (_local_pos_pub < 0) { + _local_pos_pub = orb_advertise(ORB_ID(vehicle_local_position), &hil_local_pos); } else { - _local_pos_pub = orb_advertise(ORB_ID(vehicle_local_position), &hil_local_pos); + orb_publish(ORB_ID(vehicle_local_position), _local_pos_pub, &hil_local_pos); } } @@ -855,11 +853,11 @@ MavlinkReceiver::handle_message_hil_state_quaternion(mavlink_message_t *msg) hil_battery_status.current_a = 10.0f; hil_battery_status.discharged_mah = -1.0f; - if (_battery_pub > 0) { - orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status); + if (_battery_pub < 0) { + _battery_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status); } else { - _battery_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status); + orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status); } } } @@ -883,8 +881,6 @@ MavlinkReceiver::receive_thread(void *arg) sprintf(thread_name, "mavlink_rcv_if%d", _mavlink->get_instance_id()); prctl(PR_SET_NAME, thread_name, getpid()); - _manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); - struct pollfd fds[1]; fds[0].fd = uart_fd; fds[0].events = POLLIN; @@ -911,6 +907,11 @@ MavlinkReceiver::receive_thread(void *arg) /* handle packet with parameter component */ _mavlink->mavlink_pm_message_handler(_mavlink->get_channel(), &msg); + + if (_mavlink->get_forwarding_on()) { + /* forward any messages to other mavlink instances */ + Mavlink::forward_message(&msg, _mavlink); + } } } } @@ -948,7 +949,7 @@ MavlinkReceiver::receive_start(Mavlink *parent) param.sched_priority = SCHED_PRIORITY_MAX - 40; (void)pthread_attr_setschedparam(&receiveloop_attr, ¶m); - pthread_attr_setstacksize(&receiveloop_attr, 3000); + pthread_attr_setstacksize(&receiveloop_attr, 2900); pthread_t thread; pthread_create(&thread, &receiveloop_attr, MavlinkReceiver::start_helper, (void *)parent); diff --git a/src/modules/mavlink/mavlink_receiver.h b/src/modules/mavlink/mavlink_receiver.h index 0a5a1b5c7..9ab84b58a 100644 --- a/src/modules/mavlink/mavlink_receiver.h +++ b/src/modules/mavlink/mavlink_receiver.h @@ -120,7 +120,6 @@ private: mavlink_status_t status; struct vehicle_local_position_s hil_local_pos; - int _manual_sub; orb_advert_t _global_pos_pub; orb_advert_t _local_pos_pub; orb_advert_t _attitude_pub; @@ -143,4 +142,5 @@ private: uint64_t _old_timestamp; bool _hil_local_proj_inited; float _hil_local_alt0; + struct map_projection_reference_s _hil_local_proj_ref; }; diff --git a/src/modules/mavlink/mavlink_stream.h b/src/modules/mavlink/mavlink_stream.h index 135e1bce0..def40d9ad 100644 --- a/src/modules/mavlink/mavlink_stream.h +++ b/src/modules/mavlink/mavlink_stream.h @@ -32,7 +32,7 @@ ****************************************************************************/ /** - * @file mavlink_stream.cpp + * @file mavlink_stream.h * Mavlink messages stream definition. * * @author Anton Babushkin <anton.babushkin@me.com> diff --git a/src/modules/mavlink/module.mk b/src/modules/mavlink/module.mk index f09efa2e6..f532e26fe 100644 --- a/src/modules/mavlink/module.mk +++ b/src/modules/mavlink/module.mk @@ -42,6 +42,11 @@ SRCS += mavlink_main.cpp \ mavlink_orb_subscription.cpp \ mavlink_messages.cpp \ mavlink_stream.cpp \ - mavlink_rate_limiter.cpp + mavlink_rate_limiter.cpp \ + mavlink_commands.cpp INCLUDE_DIRS += $(MAVLINK_SRC)/include/mavlink + +MAXOPTIMIZATION = -Os + +MODULE_STACKSIZE = 1024 diff --git a/src/modules/mc_att_control/mc_att_control_main.cpp b/src/modules/mc_att_control/mc_att_control_main.cpp index 9cb8e8344..b23166a5e 100644 --- a/src/modules/mc_att_control/mc_att_control_main.cpp +++ b/src/modules/mc_att_control/mc_att_control_main.cpp @@ -1,9 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. - * Author: @author Tobias Naegeli <naegelit@student.ethz.ch> - * @author Lorenz Meier <lm@inf.ethz.ch> - * @author Anton Babushkin <anton.babushkin@me.com> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -35,9 +32,13 @@ ****************************************************************************/ /** - * @file mc_att_control_main.c + * @file mc_att_control_main.cpp * Multicopter attitude controller. * + * @author Tobias Naegeli <naegelit@student.ethz.ch> + * @author Lorenz Meier <lm@inf.ethz.ch> + * @author Anton Babushkin <anton.babushkin@me.com> + * * The controller has two loops: P loop for angular error and PD loop for angular rate error. * Desired rotation calculated keeping in mind that yaw response is normally slower than roll/pitch. * For small deviations controller rotates copter to have shortest path of thrust vector and independently rotates around yaw, @@ -71,7 +72,7 @@ #include <systemlib/err.h> #include <systemlib/perf_counter.h> #include <systemlib/systemlib.h> -#include <mathlib/mathlib.h> +#include <lib/mathlib/mathlib.h> #include <lib/geo/geo.h> /** @@ -156,8 +157,11 @@ private: param_t yaw_rate_i; param_t yaw_rate_d; param_t yaw_ff; + param_t yaw_rate_max; - param_t rc_scale_yaw; + param_t man_roll_max; + param_t man_pitch_max; + param_t man_yaw_max; } _params_handles; /**< handles for interesting parameters */ struct { @@ -166,8 +170,11 @@ private: math::Vector<3> rate_i; /**< I gain for angular rate error */ math::Vector<3> rate_d; /**< D gain for angular rate error */ float yaw_ff; /**< yaw control feed-forward */ + float yaw_rate_max; /**< max yaw rate */ - float rc_scale_yaw; + float man_roll_max; + float man_pitch_max; + float man_yaw_max; } _params; /** @@ -221,9 +228,9 @@ private: static void task_main_trampoline(int argc, char *argv[]); /** - * Main sensor collection task. + * Main attitude control task. */ - void task_main() __attribute__((noreturn)); + void task_main(); }; namespace mc_att_control @@ -272,6 +279,11 @@ MulticopterAttitudeControl::MulticopterAttitudeControl() : _params.rate_p.zero(); _params.rate_i.zero(); _params.rate_d.zero(); + _params.yaw_ff = 0.0f; + _params.yaw_rate_max = 0.0f; + _params.man_roll_max = 0.0f; + _params.man_pitch_max = 0.0f; + _params.man_yaw_max = 0.0f; _rates_prev.zero(); _rates_sp.zero(); @@ -294,8 +306,10 @@ MulticopterAttitudeControl::MulticopterAttitudeControl() : _params_handles.yaw_rate_i = param_find("MC_YAWRATE_I"); _params_handles.yaw_rate_d = param_find("MC_YAWRATE_D"); _params_handles.yaw_ff = param_find("MC_YAW_FF"); - - _params_handles.rc_scale_yaw = param_find("RC_SCALE_YAW"); + _params_handles.yaw_rate_max = param_find("MC_YAWRATE_MAX"); + _params_handles.man_roll_max = param_find("MC_MAN_R_MAX"); + _params_handles.man_pitch_max = param_find("MC_MAN_P_MAX"); + _params_handles.man_yaw_max = param_find("MC_MAN_Y_MAX"); /* fetch initial parameter values */ parameters_update(); @@ -330,7 +344,7 @@ MulticopterAttitudeControl::parameters_update() { float v; - /* roll */ + /* roll gains */ param_get(_params_handles.roll_p, &v); _params.att_p(0) = v; param_get(_params_handles.roll_rate_p, &v); @@ -340,7 +354,7 @@ MulticopterAttitudeControl::parameters_update() param_get(_params_handles.roll_rate_d, &v); _params.rate_d(0) = v; - /* pitch */ + /* pitch gains */ param_get(_params_handles.pitch_p, &v); _params.att_p(1) = v; param_get(_params_handles.pitch_rate_p, &v); @@ -350,7 +364,7 @@ MulticopterAttitudeControl::parameters_update() param_get(_params_handles.pitch_rate_d, &v); _params.rate_d(1) = v; - /* yaw */ + /* yaw gains */ param_get(_params_handles.yaw_p, &v); _params.att_p(2) = v; param_get(_params_handles.yaw_rate_p, &v); @@ -361,8 +375,16 @@ MulticopterAttitudeControl::parameters_update() _params.rate_d(2) = v; param_get(_params_handles.yaw_ff, &_params.yaw_ff); + param_get(_params_handles.yaw_rate_max, &_params.yaw_rate_max); + _params.yaw_rate_max = math::radians(_params.yaw_rate_max); - param_get(_params_handles.rc_scale_yaw, &_params.rc_scale_yaw); + /* manual control scale */ + param_get(_params_handles.man_roll_max, &_params.man_roll_max); + param_get(_params_handles.man_pitch_max, &_params.man_pitch_max); + param_get(_params_handles.man_yaw_max, &_params.man_yaw_max); + _params.man_roll_max = math::radians(_params.man_roll_max); + _params.man_pitch_max = math::radians(_params.man_pitch_max); + _params.man_yaw_max = math::radians(_params.man_yaw_max); return OK; } @@ -404,7 +426,6 @@ MulticopterAttitudeControl::vehicle_manual_poll() orb_check(_manual_control_sp_sub, &updated); if (updated) { - orb_copy(ORB_ID(manual_control_setpoint), _manual_control_sp_sub, &_manual_control_sp); } } @@ -466,7 +487,7 @@ MulticopterAttitudeControl::control_attitude(float dt) if (!_v_control_mode.flag_control_climb_rate_enabled) { /* pass throttle directly if not in altitude stabilized mode */ - _v_att_sp.thrust = _manual_control_sp.throttle; + _v_att_sp.thrust = _manual_control_sp.z; publish_att_sp = true; } @@ -483,24 +504,19 @@ MulticopterAttitudeControl::control_attitude(float dt) // reset_yaw_sp = true; //} } else { - float yaw_dz_scaled = YAW_DEADZONE * _params.rc_scale_yaw; - - if (_params.rc_scale_yaw > 0.001f && fabs(_manual_control_sp.yaw) > yaw_dz_scaled) { - /* move yaw setpoint */ - yaw_sp_move_rate = _manual_control_sp.yaw / _params.rc_scale_yaw; - - if (_manual_control_sp.yaw > 0.0f) { - yaw_sp_move_rate -= YAW_DEADZONE; - - } else { - yaw_sp_move_rate += YAW_DEADZONE; - } - - yaw_sp_move_rate *= _params.rc_scale_yaw; - _v_att_sp.yaw_body = _wrap_pi(_v_att_sp.yaw_body + yaw_sp_move_rate * dt); - _v_att_sp.R_valid = false; - publish_att_sp = true; + /* move yaw setpoint */ + yaw_sp_move_rate = _manual_control_sp.r * _params.man_yaw_max; + _v_att_sp.yaw_body = _wrap_pi(_v_att_sp.yaw_body + yaw_sp_move_rate * dt); + float yaw_offs_max = _params.man_yaw_max / _params.att_p(2); + float yaw_offs = _wrap_pi(_v_att_sp.yaw_body - _v_att.yaw); + if (yaw_offs < - yaw_offs_max) { + _v_att_sp.yaw_body = _wrap_pi(_v_att.yaw - yaw_offs_max); + + } else if (yaw_offs > yaw_offs_max) { + _v_att_sp.yaw_body = _wrap_pi(_v_att.yaw + yaw_offs_max); } + _v_att_sp.R_valid = false; + publish_att_sp = true; } /* reset yaw setpint to current position if needed */ @@ -513,8 +529,8 @@ MulticopterAttitudeControl::control_attitude(float dt) if (!_v_control_mode.flag_control_velocity_enabled) { /* update attitude setpoint if not in position control mode */ - _v_att_sp.roll_body = _manual_control_sp.roll; - _v_att_sp.pitch_body = _manual_control_sp.pitch; + _v_att_sp.roll_body = _manual_control_sp.y * _params.man_roll_max; + _v_att_sp.pitch_body = -_manual_control_sp.x * _params.man_pitch_max; _v_att_sp.R_valid = false; publish_att_sp = true; } @@ -627,6 +643,9 @@ MulticopterAttitudeControl::control_attitude(float dt) /* calculate angular rates setpoint */ _rates_sp = _params.att_p.emult(e_R); + /* limit yaw rate */ + _rates_sp(2) = math::constrain(_rates_sp(2), -_params.yaw_rate_max, _params.yaw_rate_max); + /* feed forward yaw setpoint rate */ _rates_sp(2) += yaw_sp_move_rate * yaw_w * _params.yaw_ff; } @@ -807,7 +826,7 @@ MulticopterAttitudeControl::start() _control_task = task_spawn_cmd("mc_att_control", SCHED_DEFAULT, SCHED_PRIORITY_MAX - 5, - 2048, + 2000, (main_t)&MulticopterAttitudeControl::task_main_trampoline, nullptr); diff --git a/src/modules/mc_att_control/mc_att_control_params.c b/src/modules/mc_att_control/mc_att_control_params.c index 488107d58..ad38a0a03 100644 --- a/src/modules/mc_att_control/mc_att_control_params.c +++ b/src/modules/mc_att_control/mc_att_control_params.c @@ -1,9 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. - * Author: @author Tobias Naegeli <naegelit@student.ethz.ch> - * @author Lorenz Meier <lm@inf.ethz.ch> - * @author Anton Babushkin <anton.babushkin@me.com> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -37,6 +34,10 @@ /** * @file mc_att_control_params.c * Parameters for multicopter attitude controller. + * + * @author Tobias Naegeli <naegelit@student.ethz.ch> + * @author Lorenz Meier <lm@inf.ethz.ch> + * @author Anton Babushkin <anton.babushkin@me.com> */ #include <systemlib/param/param.h> @@ -173,3 +174,44 @@ PARAM_DEFINE_FLOAT(MC_YAWRATE_D, 0.0f); * @group Multicopter Attitude Control */ PARAM_DEFINE_FLOAT(MC_YAW_FF, 0.5f); + +/** + * Max yaw rate + * + * Limit for yaw rate, has effect for large rotations in autonomous mode, to avoid large control output and mixer saturation. + * + * @unit deg/s + * @min 0.0 + * @max 360.0 + * @group Multicopter Attitude Control + */ +PARAM_DEFINE_FLOAT(MC_YAWRATE_MAX, 120.0f); + +/** + * Max manual roll + * + * @unit deg + * @min 0.0 + * @max 90.0 + * @group Multicopter Attitude Control + */ +PARAM_DEFINE_FLOAT(MC_MAN_R_MAX, 35.0f); + +/** + * Max manual pitch + * + * @unit deg + * @min 0.0 + * @max 90.0 + * @group Multicopter Attitude Control + */ +PARAM_DEFINE_FLOAT(MC_MAN_P_MAX, 35.0f); + +/** + * Max manual yaw rate + * + * @unit deg/s + * @min 0.0 + * @group Multicopter Attitude Control + */ +PARAM_DEFINE_FLOAT(MC_MAN_Y_MAX, 120.0f); diff --git a/src/modules/mc_pos_control/mc_pos_control_main.cpp b/src/modules/mc_pos_control/mc_pos_control_main.cpp index cefe5fc15..20a482620 100644 --- a/src/modules/mc_pos_control/mc_pos_control_main.cpp +++ b/src/modules/mc_pos_control/mc_pos_control_main.cpp @@ -1,7 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2013 PX4 Development Team. All rights reserved. - * Author: @author Anton Babushkin <anton.babushkin@me.com> + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -40,6 +39,8 @@ * Output of velocity controller is thrust vector that splitted to thrust direction * (i.e. rotation matrix for multicopter orientation) and thrust module (i.e. multicopter thrust itself). * Controller doesn't use Euler angles for work, they generated only for more human-friendly control and logging. + * + * @author Anton Babushkin <anton.babushkin@me.com> */ #include <nuttx/config.h> @@ -62,9 +63,10 @@ #include <uORB/topics/vehicle_control_mode.h> #include <uORB/topics/actuator_armed.h> #include <uORB/topics/parameter_update.h> -#include <uORB/topics/vehicle_global_position.h> +#include <uORB/topics/vehicle_local_position.h> #include <uORB/topics/position_setpoint_triplet.h> #include <uORB/topics/vehicle_global_velocity_setpoint.h> +#include <uORB/topics/vehicle_local_position_setpoint.h> #include <systemlib/param/param.h> #include <systemlib/err.h> #include <systemlib/systemlib.h> @@ -114,20 +116,21 @@ private: int _params_sub; /**< notification of parameter updates */ int _manual_sub; /**< notification of manual control updates */ int _arming_sub; /**< arming status of outputs */ - int _global_pos_sub; /**< vehicle local position */ + int _local_pos_sub; /**< vehicle local position */ int _pos_sp_triplet_sub; /**< position setpoint triplet */ orb_advert_t _att_sp_pub; /**< attitude setpoint publication */ - orb_advert_t _pos_sp_triplet_pub; /**< position setpoint triplet publication */ - orb_advert_t _global_vel_sp_pub; /**< vehicle global velocity setpoint */ + orb_advert_t _local_pos_sp_pub; /**< vehicle local position setpoint publication */ + orb_advert_t _global_vel_sp_pub; /**< vehicle global velocity setpoint publication */ struct vehicle_attitude_s _att; /**< vehicle attitude */ struct vehicle_attitude_setpoint_s _att_sp; /**< vehicle attitude setpoint */ struct manual_control_setpoint_s _manual; /**< r/c channel data */ struct vehicle_control_mode_s _control_mode; /**< vehicle control mode */ struct actuator_armed_s _arming; /**< actuator arming status */ - struct vehicle_global_position_s _global_pos; /**< vehicle global position */ + struct vehicle_local_position_s _local_pos; /**< vehicle local position */ struct position_setpoint_triplet_s _pos_sp_triplet; /**< vehicle global position setpoint triplet */ + struct vehicle_local_position_setpoint_s _local_pos_sp; /**< vehicle local position setpoint */ struct vehicle_global_velocity_setpoint_s _global_vel_sp; /**< vehicle global velocity setpoint */ struct { @@ -145,23 +148,17 @@ private: param_t xy_vel_d; param_t xy_vel_max; param_t xy_ff; - param_t tilt_max; + param_t tilt_max_air; param_t land_speed; - param_t land_tilt_max; - - param_t rc_scale_pitch; - param_t rc_scale_roll; + param_t tilt_max_land; } _params_handles; /**< handles for interesting parameters */ struct { float thr_min; float thr_max; - float tilt_max; + float tilt_max_air; float land_speed; - float land_tilt_max; - - float rc_scale_pitch; - float rc_scale_roll; + float tilt_max_land; math::Vector<3> pos_p; math::Vector<3> vel_p; @@ -172,14 +169,15 @@ private: math::Vector<3> sp_offs_max; } _params; - double _lat_sp; - double _lon_sp; - float _alt_sp; + struct map_projection_reference_s _ref_pos; + float _ref_alt; + hrt_abstime _ref_timestamp; - bool _reset_lat_lon_sp; + bool _reset_pos_sp; bool _reset_alt_sp; - bool _use_global_alt; /**< switch between global (AMSL) and barometric altitudes */ + math::Vector<3> _pos; + math::Vector<3> _pos_sp; math::Vector<3> _vel; math::Vector<3> _vel_sp; math::Vector<3> _vel_prev; /**< velocity on previous step */ @@ -202,9 +200,13 @@ private: static float scale_control(float ctl, float end, float dz); /** - * Reset lat/lon to current position + * Update reference for local position projection + */ + void update_ref(); + /** + * Reset position setpoint to current position */ - void reset_lat_lon_sp(); + void reset_pos_sp(); /** * Reset altitude setpoint to current altitude @@ -224,7 +226,7 @@ private: /** * Main sensor collection task. */ - void task_main() __attribute__((noreturn)); + void task_main(); }; namespace pos_control @@ -252,31 +254,32 @@ MulticopterPositionControl::MulticopterPositionControl() : _params_sub(-1), _manual_sub(-1), _arming_sub(-1), - _global_pos_sub(-1), + _local_pos_sub(-1), _pos_sp_triplet_sub(-1), /* publications */ _att_sp_pub(-1), - _pos_sp_triplet_pub(-1), + _local_pos_sp_pub(-1), _global_vel_sp_pub(-1), - _lat_sp(0.0), - _lon_sp(0.0), - _alt_sp(0.0f), + _ref_alt(0.0f), + _ref_timestamp(0), - _reset_lat_lon_sp(true), - _reset_alt_sp(true), - _use_global_alt(false) + _reset_pos_sp(true), + _reset_alt_sp(true) { memset(&_att, 0, sizeof(_att)); memset(&_att_sp, 0, sizeof(_att_sp)); memset(&_manual, 0, sizeof(_manual)); memset(&_control_mode, 0, sizeof(_control_mode)); memset(&_arming, 0, sizeof(_arming)); - memset(&_global_pos, 0, sizeof(_global_pos)); + memset(&_local_pos, 0, sizeof(_local_pos)); memset(&_pos_sp_triplet, 0, sizeof(_pos_sp_triplet)); + memset(&_local_pos_sp, 0, sizeof(_local_pos_sp)); memset(&_global_vel_sp, 0, sizeof(_global_vel_sp)); + memset(&_ref_pos, 0, sizeof(_ref_pos)); + _params.pos_p.zero(); _params.vel_p.zero(); _params.vel_i.zero(); @@ -285,6 +288,8 @@ MulticopterPositionControl::MulticopterPositionControl() : _params.vel_ff.zero(); _params.sp_offs_max.zero(); + _pos.zero(); + _pos_sp.zero(); _vel.zero(); _vel_sp.zero(); _vel_prev.zero(); @@ -303,11 +308,9 @@ MulticopterPositionControl::MulticopterPositionControl() : _params_handles.xy_vel_d = param_find("MPC_XY_VEL_D"); _params_handles.xy_vel_max = param_find("MPC_XY_VEL_MAX"); _params_handles.xy_ff = param_find("MPC_XY_FF"); - _params_handles.tilt_max = param_find("MPC_TILT_MAX"); + _params_handles.tilt_max_air = param_find("MPC_TILTMAX_AIR"); _params_handles.land_speed = param_find("MPC_LAND_SPEED"); - _params_handles.land_tilt_max = param_find("MPC_LAND_TILT"); - _params_handles.rc_scale_pitch = param_find("RC_SCALE_PITCH"); - _params_handles.rc_scale_roll = param_find("RC_SCALE_ROLL"); + _params_handles.tilt_max_land = param_find("MPC_TILTMAX_LND"); /* fetch initial parameter values */ parameters_update(true); @@ -345,17 +348,18 @@ MulticopterPositionControl::parameters_update(bool force) orb_check(_params_sub, &updated); - if (updated) + if (updated) { orb_copy(ORB_ID(parameter_update), _params_sub, ¶m_upd); + } if (updated || force) { param_get(_params_handles.thr_min, &_params.thr_min); param_get(_params_handles.thr_max, &_params.thr_max); - param_get(_params_handles.tilt_max, &_params.tilt_max); + param_get(_params_handles.tilt_max_air, &_params.tilt_max_air); + _params.tilt_max_air = math::radians(_params.tilt_max_air); param_get(_params_handles.land_speed, &_params.land_speed); - param_get(_params_handles.land_tilt_max, &_params.land_tilt_max); - param_get(_params_handles.rc_scale_pitch, &_params.rc_scale_pitch); - param_get(_params_handles.rc_scale_roll, &_params.rc_scale_roll); + param_get(_params_handles.tilt_max_land, &_params.tilt_max_land); + _params.tilt_max_land = math::radians(_params.tilt_max_land); float v; param_get(_params_handles.xy_p, &v); @@ -402,33 +406,39 @@ MulticopterPositionControl::poll_subscriptions() orb_check(_att_sub, &updated); - if (updated) + if (updated) { orb_copy(ORB_ID(vehicle_attitude), _att_sub, &_att); + } orb_check(_att_sp_sub, &updated); - if (updated) + if (updated) { orb_copy(ORB_ID(vehicle_attitude_setpoint), _att_sp_sub, &_att_sp); + } orb_check(_control_mode_sub, &updated); - if (updated) + if (updated) { orb_copy(ORB_ID(vehicle_control_mode), _control_mode_sub, &_control_mode); + } orb_check(_manual_sub, &updated); - if (updated) + if (updated) { orb_copy(ORB_ID(manual_control_setpoint), _manual_sub, &_manual); + } orb_check(_arming_sub, &updated); - if (updated) + if (updated) { orb_copy(ORB_ID(actuator_armed), _arming_sub, &_arming); + } - orb_check(_global_pos_sub, &updated); + orb_check(_local_pos_sub, &updated); - if (updated) - orb_copy(ORB_ID(vehicle_global_position), _global_pos_sub, &_global_pos); + if (updated) { + orb_copy(ORB_ID(vehicle_local_position), _local_pos_sub, &_local_pos); + } } float @@ -452,40 +462,50 @@ MulticopterPositionControl::task_main_trampoline(int argc, char *argv[]) } void -MulticopterPositionControl::reset_lat_lon_sp() +MulticopterPositionControl::update_ref() { - if (_reset_lat_lon_sp) { - _reset_lat_lon_sp = false; - _lat_sp = _global_pos.lat; - _lon_sp = _global_pos.lon; - mavlink_log_info(_mavlink_fd, "[mpc] reset lat/lon sp: %.7f, %.7f", _lat_sp, _lon_sp); + if (_local_pos.ref_timestamp != _ref_timestamp) { + double lat_sp, lon_sp; + float alt_sp; + + if (_ref_timestamp != 0) { + /* calculate current position setpoint in global frame */ + map_projection_reproject(&_ref_pos, _pos_sp(0), _pos_sp(1), &lat_sp, &lon_sp); + alt_sp = _ref_alt - _pos_sp(2); + } + + /* update local projection reference */ + map_projection_init(&_ref_pos, _local_pos.ref_lat, _local_pos.ref_lon); + _ref_alt = _local_pos.ref_alt; + + if (_ref_timestamp != 0) { + /* reproject position setpoint to new reference */ + map_projection_project(&_ref_pos, lat_sp, lon_sp, &_pos_sp.data[0], &_pos_sp.data[1]); + _pos_sp(2) = -(alt_sp - _ref_alt); + } + + _ref_timestamp = _local_pos.ref_timestamp; } } void -MulticopterPositionControl::reset_alt_sp() +MulticopterPositionControl::reset_pos_sp() { - if (_reset_alt_sp) { - _reset_alt_sp = false; - _alt_sp = _use_global_alt ? _global_pos.alt : _global_pos.baro_alt; - mavlink_log_info(_mavlink_fd, "[mpc] reset alt (%s) sp: %.2f", _use_global_alt ? "AMSL" : "baro", (double)_alt_sp); + if (_reset_pos_sp) { + _reset_pos_sp = false; + _pos_sp(0) = _pos(0); + _pos_sp(1) = _pos(1); + mavlink_log_info(_mavlink_fd, "[mpc] reset pos sp: %.2f, %.2f", (double)_pos_sp(0), (double)_pos_sp(1)); } } void -MulticopterPositionControl::select_alt(bool global) +MulticopterPositionControl::reset_alt_sp() { - if (global != _use_global_alt) { - _use_global_alt = global; - - if (global) { - /* switch from barometric to global altitude */ - _alt_sp += _global_pos.alt - _global_pos.baro_alt; - - } else { - /* switch from global to barometric altitude */ - _alt_sp += _global_pos.baro_alt - _global_pos.alt; - } + if (_reset_alt_sp) { + _reset_alt_sp = false; + _pos_sp(2) = _pos(2); + mavlink_log_info(_mavlink_fd, "[mpc] reset alt sp: %.2f", -(double)_pos_sp(2)); } } @@ -506,7 +526,7 @@ MulticopterPositionControl::task_main() _params_sub = orb_subscribe(ORB_ID(parameter_update)); _manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); _arming_sub = orb_subscribe(ORB_ID(actuator_armed)); - _global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position)); + _local_pos_sub = orb_subscribe(ORB_ID(vehicle_local_position)); _pos_sp_triplet_sub = orb_subscribe(ORB_ID(position_setpoint_triplet)); parameters_update(true); @@ -537,8 +557,7 @@ MulticopterPositionControl::task_main() /* wakeup source */ struct pollfd fds[1]; - /* Setup of loop */ - fds[0].fd = _global_pos_sub; + fds[0].fd = _local_pos_sub; fds[0].events = POLLIN; while (!_task_should_exit) { @@ -546,8 +565,9 @@ MulticopterPositionControl::task_main() int pret = poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 500); /* timed out - periodic check for _task_should_exit */ - if (pret == 0) + if (pret == 0) { continue; + } /* this is undesirable but not much we can do */ if (pret < 0) { @@ -564,7 +584,7 @@ MulticopterPositionControl::task_main() if (_control_mode.flag_armed && !was_armed) { /* reset setpoints and integrals on arming */ - _reset_lat_lon_sp = true; + _reset_pos_sp = true; _reset_alt_sp = true; reset_int_z = true; reset_int_xy = true; @@ -572,44 +592,41 @@ MulticopterPositionControl::task_main() was_armed = _control_mode.flag_armed; + update_ref(); + if (_control_mode.flag_control_altitude_enabled || _control_mode.flag_control_position_enabled || _control_mode.flag_control_climb_rate_enabled || _control_mode.flag_control_velocity_enabled) { - _vel(0) = _global_pos.vel_n; - _vel(1) = _global_pos.vel_e; - _vel(2) = _global_pos.vel_d; + _pos(0) = _local_pos.x; + _pos(1) = _local_pos.y; + _pos(2) = _local_pos.z; - sp_move_rate.zero(); + _vel(0) = _local_pos.vx; + _vel(1) = _local_pos.vy; + _vel(2) = _local_pos.vz; - float alt = _global_pos.alt; + sp_move_rate.zero(); /* select control source */ if (_control_mode.flag_control_manual_enabled) { - /* select altitude source and update setpoint */ - select_alt(_global_pos.global_valid); - - if (!_use_global_alt) { - alt = _global_pos.baro_alt; - } - /* manual control */ if (_control_mode.flag_control_altitude_enabled) { /* reset alt setpoint to current altitude if needed */ reset_alt_sp(); /* move altitude setpoint with throttle stick */ - sp_move_rate(2) = -scale_control(_manual.throttle - 0.5f, 0.5f, alt_ctl_dz); + sp_move_rate(2) = -scale_control(_manual.z - 0.5f, 0.5f, alt_ctl_dz); } if (_control_mode.flag_control_position_enabled) { - /* reset lat/lon setpoint to current position if needed */ - reset_lat_lon_sp(); + /* reset position setpoint to current position if needed */ + reset_pos_sp(); /* move position setpoint with roll/pitch stick */ - sp_move_rate(0) = scale_control(-_manual.pitch / _params.rc_scale_pitch, 1.0f, pos_ctl_dz); - sp_move_rate(1) = scale_control(_manual.roll / _params.rc_scale_roll, 1.0f, pos_ctl_dz); + sp_move_rate(0) = _manual.x; + sp_move_rate(1) = _manual.y; } /* limit setpoint move rate */ @@ -625,74 +642,47 @@ MulticopterPositionControl::task_main() sp_move_rate = R_yaw_sp * sp_move_rate.emult(_params.vel_max); /* move position setpoint */ - add_vector_to_global_position(_lat_sp, _lon_sp, sp_move_rate(0) * dt, sp_move_rate(1) * dt, &_lat_sp, &_lon_sp); - _alt_sp -= sp_move_rate(2) * dt; + _pos_sp += sp_move_rate * dt; /* check if position setpoint is too far from actual position */ math::Vector<3> pos_sp_offs; pos_sp_offs.zero(); if (_control_mode.flag_control_position_enabled) { - get_vector_to_next_waypoint_fast(_global_pos.lat, _global_pos.lon, _lat_sp, _lon_sp, &pos_sp_offs.data[0], &pos_sp_offs.data[1]); - pos_sp_offs(0) /= _params.sp_offs_max(0); - pos_sp_offs(1) /= _params.sp_offs_max(1); + pos_sp_offs(0) = (_pos_sp(0) - _pos(0)) / _params.sp_offs_max(0); + pos_sp_offs(1) = (_pos_sp(1) - _pos(1)) / _params.sp_offs_max(1); } if (_control_mode.flag_control_altitude_enabled) { - pos_sp_offs(2) = -(_alt_sp - alt) / _params.sp_offs_max(2); + pos_sp_offs(2) = (_pos_sp(2) - _pos(2)) / _params.sp_offs_max(2); } float pos_sp_offs_norm = pos_sp_offs.length(); if (pos_sp_offs_norm > 1.0f) { pos_sp_offs /= pos_sp_offs_norm; - add_vector_to_global_position(_global_pos.lat, _global_pos.lon, pos_sp_offs(0) * _params.sp_offs_max(0), pos_sp_offs(1) * _params.sp_offs_max(1), &_lat_sp, &_lon_sp); - _alt_sp = alt - pos_sp_offs(2) * _params.sp_offs_max(2); - } - - /* fill position setpoint triplet */ - _pos_sp_triplet.previous.valid = true; - _pos_sp_triplet.current.valid = true; - _pos_sp_triplet.next.valid = true; - - _pos_sp_triplet.nav_state = NAV_STATE_NONE; - _pos_sp_triplet.current.type = SETPOINT_TYPE_NORMAL; - _pos_sp_triplet.current.lat = _lat_sp; - _pos_sp_triplet.current.lon = _lon_sp; - _pos_sp_triplet.current.alt = _alt_sp; - _pos_sp_triplet.current.yaw = _att_sp.yaw_body; - _pos_sp_triplet.current.loiter_radius = 0.0f; - _pos_sp_triplet.current.loiter_direction = 1.0f; - _pos_sp_triplet.current.pitch_min = 0.0f; - - /* publish position setpoint triplet */ - if (_pos_sp_triplet_pub > 0) { - orb_publish(ORB_ID(position_setpoint_triplet), _pos_sp_triplet_pub, &_pos_sp_triplet); - - } else { - _pos_sp_triplet_pub = orb_advertise(ORB_ID(position_setpoint_triplet), &_pos_sp_triplet); + _pos_sp = _pos + pos_sp_offs.emult(_params.sp_offs_max); } } else { - /* always use AMSL altitude for AUTO */ - select_alt(true); - /* AUTO */ bool updated; orb_check(_pos_sp_triplet_sub, &updated); - if (updated) + if (updated) { orb_copy(ORB_ID(position_setpoint_triplet), _pos_sp_triplet_sub, &_pos_sp_triplet); + } if (_pos_sp_triplet.current.valid) { /* in case of interrupted mission don't go to waypoint but stay at current position */ - _reset_lat_lon_sp = true; + _reset_pos_sp = true; _reset_alt_sp = true; - /* update position setpoint */ - _lat_sp = _pos_sp_triplet.current.lat; - _lon_sp = _pos_sp_triplet.current.lon; - _alt_sp = _pos_sp_triplet.current.alt; + /* project setpoint to local frame */ + map_projection_project(&_ref_pos, + _pos_sp_triplet.current.lat, _pos_sp_triplet.current.lon, + &_pos_sp.data[0], &_pos_sp.data[1]); + _pos_sp(2) = -(_pos_sp_triplet.current.alt - _ref_alt); /* update yaw setpoint if needed */ if (isfinite(_pos_sp_triplet.current.yaw)) { @@ -701,11 +691,25 @@ MulticopterPositionControl::task_main() } else { /* no waypoint, loiter, reset position setpoint if needed */ - reset_lat_lon_sp(); + reset_pos_sp(); reset_alt_sp(); } } + /* fill local position setpoint */ + _local_pos_sp.x = _pos_sp(0); + _local_pos_sp.y = _pos_sp(1); + _local_pos_sp.z = _pos_sp(2); + _local_pos_sp.yaw = _att_sp.yaw_body; + + /* publish local position setpoint */ + if (_local_pos_sp_pub > 0) { + orb_publish(ORB_ID(vehicle_local_position_setpoint), _local_pos_sp_pub, &_local_pos_sp); + + } else { + _local_pos_sp_pub = orb_advertise(ORB_ID(vehicle_local_position_setpoint), &_local_pos_sp); + } + if (!_control_mode.flag_control_manual_enabled && _pos_sp_triplet.current.valid && _pos_sp_triplet.current.type == SETPOINT_TYPE_IDLE) { /* idle state, don't run controller and set zero thrust */ R.identity(); @@ -729,9 +733,7 @@ MulticopterPositionControl::task_main() } else { /* run position & altitude controllers, calculate velocity setpoint */ - math::Vector<3> pos_err; - get_vector_to_next_waypoint_fast(_global_pos.lat, _global_pos.lon, _lat_sp, _lon_sp, &pos_err.data[0], &pos_err.data[1]); - pos_err(2) = -(_alt_sp - alt); + math::Vector<3> pos_err = _pos_sp - _pos; _vel_sp = pos_err.emult(_params.pos_p) + sp_move_rate.emult(_params.vel_ff); @@ -741,7 +743,7 @@ MulticopterPositionControl::task_main() } if (!_control_mode.flag_control_position_enabled) { - _reset_lat_lon_sp = true; + _reset_pos_sp = true; _vel_sp(0) = 0.0f; _vel_sp(1) = 0.0f; } @@ -780,7 +782,7 @@ MulticopterPositionControl::task_main() float i = _params.thr_min; if (reset_int_z_manual) { - i = _manual.throttle; + i = _manual.z; if (i < _params.thr_min) { i = _params.thr_min; @@ -843,16 +845,17 @@ MulticopterPositionControl::task_main() thr_min = 0.0f; } - float tilt_max = _params.tilt_max; + float tilt_max = _params.tilt_max_air; /* adjust limits for landing mode */ if (!_control_mode.flag_control_manual_enabled && _pos_sp_triplet.current.valid && _pos_sp_triplet.current.type == SETPOINT_TYPE_LAND) { /* limit max tilt and min lift when landing */ - tilt_max = _params.land_tilt_max; + tilt_max = _params.tilt_max_land; - if (thr_min < 0.0f) + if (thr_min < 0.0f) { thr_min = 0.0f; + } } /* limit min lift */ @@ -943,8 +946,9 @@ MulticopterPositionControl::task_main() thrust_int(2) += vel_err(2) * _params.vel_i(2) * dt; /* protection against flipping on ground when landing */ - if (thrust_int(2) > 0.0f) + if (thrust_int(2) > 0.0f) { thrust_int(2) = 0.0f; + } } /* calculate attitude setpoint from thrust vector */ @@ -1003,6 +1007,18 @@ MulticopterPositionControl::task_main() _att_sp.roll_body = euler(0); _att_sp.pitch_body = euler(1); /* yaw already used to construct rot matrix, but actual rotation matrix can have different yaw near singularity */ + + } else if (!_control_mode.flag_control_manual_enabled) { + /* autonomous altitude control without position control (failsafe landing), + * force level attitude, don't change yaw */ + R.from_euler(0.0f, 0.0f, _att_sp.yaw_body); + + /* copy rotation matrix to attitude setpoint topic */ + memcpy(&_att_sp.R_body[0][0], R.data, sizeof(_att_sp.R_body)); + _att_sp.R_valid = true; + + _att_sp.roll_body = 0.0f; + _att_sp.pitch_body = 0.0f; } _att_sp.thrust = thrust_abs; @@ -1025,7 +1041,7 @@ MulticopterPositionControl::task_main() } else { /* position controller disabled, reset setpoints */ _reset_alt_sp = true; - _reset_lat_lon_sp = true; + _reset_pos_sp = true; reset_int_z = true; reset_int_xy = true; } @@ -1050,7 +1066,7 @@ MulticopterPositionControl::start() _control_task = task_spawn_cmd("mc_pos_control", SCHED_DEFAULT, SCHED_PRIORITY_MAX - 5, - 2048, + 2000, (main_t)&MulticopterPositionControl::task_main_trampoline, nullptr); @@ -1064,18 +1080,21 @@ MulticopterPositionControl::start() int mc_pos_control_main(int argc, char *argv[]) { - if (argc < 1) + if (argc < 1) { errx(1, "usage: mc_pos_control {start|stop|status}"); + } if (!strcmp(argv[1], "start")) { - if (pos_control::g_control != nullptr) + if (pos_control::g_control != nullptr) { errx(1, "already running"); + } pos_control::g_control = new MulticopterPositionControl; - if (pos_control::g_control == nullptr) + if (pos_control::g_control == nullptr) { errx(1, "alloc failed"); + } if (OK != pos_control::g_control->start()) { delete pos_control::g_control; @@ -1087,8 +1106,9 @@ int mc_pos_control_main(int argc, char *argv[]) } if (!strcmp(argv[1], "stop")) { - if (pos_control::g_control == nullptr) + if (pos_control::g_control == nullptr) { errx(1, "not running"); + } delete pos_control::g_control; pos_control::g_control = nullptr; diff --git a/src/modules/mc_pos_control/mc_pos_control_params.c b/src/modules/mc_pos_control/mc_pos_control_params.c index ae62ebb67..bbca690e9 100644 --- a/src/modules/mc_pos_control/mc_pos_control_params.c +++ b/src/modules/mc_pos_control/mc_pos_control_params.c @@ -35,6 +35,8 @@ /** * @file mc_pos_control_params.c * Multicopter position controller parameters. + * + * @author Anton Babushkin <anton.babushkin@me.com> */ #include <systemlib/param/param.h> @@ -98,8 +100,9 @@ PARAM_DEFINE_FLOAT(MPC_Z_VEL_D, 0.0f); /** * Maximum vertical velocity * - * Maximum vertical velocity in AUTO mode and endpoint for stabilized modes (SEATBELT, EASY). + * Maximum vertical velocity in AUTO mode and endpoint for stabilized modes (ALTCTRL, POSCTRL). * + * @unit m/s * @min 0.0 * @group Multicopter Position Control */ @@ -108,7 +111,7 @@ PARAM_DEFINE_FLOAT(MPC_Z_VEL_MAX, 5.0f); /** * Vertical velocity feed forward * - * Feed forward weight for altitude control in stabilized modes (SEATBELT, EASY). 0 will give slow responce and no overshot, 1 - fast responce and big overshot. + * Feed forward weight for altitude control in stabilized modes (ALTCTRL, POSCTRL). 0 will give slow responce and no overshot, 1 - fast responce and big overshot. * * @min 0.0 * @max 1.0 @@ -153,8 +156,9 @@ PARAM_DEFINE_FLOAT(MPC_XY_VEL_D, 0.2f); /** * Maximum horizontal velocity * - * Maximum horizontal velocity in AUTO mode and endpoint for position stabilized mode (EASY). + * Maximum horizontal velocity in AUTO mode and endpoint for position stabilized mode (POSCTRL). * + * @unit m/s * @min 0.0 * @group Multicopter Position Control */ @@ -163,7 +167,7 @@ PARAM_DEFINE_FLOAT(MPC_XY_VEL_MAX, 5.0f); /** * Horizontal velocity feed forward * - * Feed forward weight for position control in position control mode (EASY). 0 will give slow responce and no overshot, 1 - fast responce and big overshot. + * Feed forward weight for position control in position control mode (POSCTRL). 0 will give slow responce and no overshot, 1 - fast responce and big overshot. * * @min 0.0 * @max 1.0 @@ -172,31 +176,35 @@ PARAM_DEFINE_FLOAT(MPC_XY_VEL_MAX, 5.0f); PARAM_DEFINE_FLOAT(MPC_XY_FF, 0.5f); /** - * Maximum tilt + * Maximum tilt angle in air * - * Limits maximum tilt in AUTO and EASY modes. + * Limits maximum tilt in AUTO and POSCTRL modes during flight. * + * @unit deg * @min 0.0 - * @max 1.57 + * @max 90.0 * @group Multicopter Position Control */ -PARAM_DEFINE_FLOAT(MPC_TILT_MAX, 1.0f); +PARAM_DEFINE_FLOAT(MPC_TILTMAX_AIR, 45.0f); /** - * Landing descend rate + * Maximum tilt during landing * + * Limits maximum tilt angle on landing. + * + * @unit deg * @min 0.0 + * @max 90.0 * @group Multicopter Position Control */ -PARAM_DEFINE_FLOAT(MPC_LAND_SPEED, 1.0f); +PARAM_DEFINE_FLOAT(MPC_TILTMAX_LND, 15.0f); /** - * Maximum landing tilt - * - * Limits maximum tilt on landing. + * Landing descend rate * + * @unit m/s * @min 0.0 - * @max 1.57 * @group Multicopter Position Control */ -PARAM_DEFINE_FLOAT(MPC_LAND_TILT, 0.3f); +PARAM_DEFINE_FLOAT(MPC_LAND_SPEED, 1.0f); + diff --git a/src/modules/navigator/geofence.cpp b/src/modules/navigator/geofence.cpp index f452a85f7..bc8dbca50 100644 --- a/src/modules/navigator/geofence.cpp +++ b/src/modules/navigator/geofence.cpp @@ -1,8 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013 PX4 Development Team. All rights reserved. - * Author: @author Jean Cyr <jean.m.cyr@gmail.com> - * @author Thomas Gubler <thomasgubler@gmail.com> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -35,6 +33,9 @@ /** * @file geofence.cpp * Provides functions for handling the geofence + * + * @author Jean Cyr <jean.m.cyr@gmail.com> + * @author Thomas Gubler <thomasgubler@gmail.com> */ #include "geofence.h" diff --git a/src/modules/navigator/geofence.h b/src/modules/navigator/geofence.h index 9628b7271..2eb126ab5 100644 --- a/src/modules/navigator/geofence.h +++ b/src/modules/navigator/geofence.h @@ -1,8 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013 PX4 Development Team. All rights reserved. - * Author: @author Jean Cyr <jean.m.cyr@gmail.com> - * @author Thomas Gubler <thomasgubler@gmail.com> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -35,6 +33,9 @@ /** * @file geofence.h * Provides functions for handling the geofence + * + * @author Jean Cyr <jean.m.cyr@gmail.com> + * @author Thomas Gubler <thomasgubler@gmail.com> */ #ifndef GEOFENCE_H_ diff --git a/src/modules/navigator/geofence_params.c b/src/modules/navigator/geofence_params.c index 5831a0ca9..653b1ad84 100644 --- a/src/modules/navigator/geofence_params.c +++ b/src/modules/navigator/geofence_params.c @@ -1,7 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013 PX4 Development Team. All rights reserved. - * Author: Lorenz Meier <lm@inf.ethz.ch> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions diff --git a/src/modules/navigator/mission_feasibility_checker.cpp b/src/modules/navigator/mission_feasibility_checker.cpp index eaafa217d..2f45f2267 100644 --- a/src/modules/navigator/mission_feasibility_checker.cpp +++ b/src/modules/navigator/mission_feasibility_checker.cpp @@ -1,8 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013 PX4 Development Team. All rights reserved. - * Author: @author Lorenz Meier <lm@inf.ethz.ch> - * @author Thomas Gubler <thomasgubler@student.ethz.ch> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -35,6 +33,9 @@ /** * @file mission_feasibility_checker.cpp * Provides checks if mission is feasible given the navigation capabilities + * + * @author Lorenz Meier <lm@inf.ethz.ch> + * @author Thomas Gubler <thomasgubler@student.ethz.ch> */ #include "mission_feasibility_checker.h" @@ -100,8 +101,8 @@ bool MissionFeasibilityChecker::checkGeofence(dm_item_t dm_current, size_t nMiss /* Check if all mission items are inside the geofence (if we have a valid geofence) */ if (geofence.valid()) { for (size_t i = 0; i < nMissionItems; i++) { - static struct mission_item_s missionitem; - const ssize_t len = sizeof(struct mission_item_s); + struct mission_item_s missionitem; + const ssize_t len = sizeof(missionitem); if (dm_read(dm_current, i, &missionitem, len) != len) { /* not supposed to happen unless the datamanager can't access the SD card, etc. */ @@ -125,8 +126,8 @@ bool MissionFeasibilityChecker::checkFixedWingLanding(dm_item_t dm_current, size for (size_t i = 0; i < nMissionItems; i++) { - static struct mission_item_s missionitem; - const ssize_t len = sizeof(struct mission_item_s); + struct mission_item_s missionitem; + const ssize_t len = sizeof(missionitem); if (dm_read(dm_current, i, &missionitem, len) != len) { /* not supposed to happen unless the datamanager can't access the SD card, etc. */ return false; diff --git a/src/modules/navigator/mission_feasibility_checker.h b/src/modules/navigator/mission_feasibility_checker.h index 7a0b2a296..f98e28462 100644 --- a/src/modules/navigator/mission_feasibility_checker.h +++ b/src/modules/navigator/mission_feasibility_checker.h @@ -1,8 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013 PX4 Development Team. All rights reserved. - * Author: @author Lorenz Meier <lm@inf.ethz.ch> - * @author Thomas Gubler <thomasgubler@student.ethz.ch> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -35,7 +33,11 @@ /** * @file mission_feasibility_checker.h * Provides checks if mission is feasible given the navigation capabilities + * + * @author Lorenz Meier <lm@inf.ethz.ch> + * @author Thomas Gubler <thomasgubler@student.ethz.ch> */ + #ifndef MISSION_FEASIBILITY_CHECKER_H_ #define MISSION_FEASIBILITY_CHECKER_H_ diff --git a/src/modules/navigator/module.mk b/src/modules/navigator/module.mk index 55f8a4caa..6ea9dec2b 100644 --- a/src/modules/navigator/module.mk +++ b/src/modules/navigator/module.mk @@ -45,3 +45,5 @@ SRCS = navigator_main.cpp \ geofence_params.c INCLUDE_DIRS += $(MAVLINK_SRC)/include/mavlink + +MODULE_STACKSIZE = 1200 diff --git a/src/modules/navigator/navigator_main.cpp b/src/modules/navigator/navigator_main.cpp index c45cafc1b..87c893079 100644 --- a/src/modules/navigator/navigator_main.cpp +++ b/src/modules/navigator/navigator_main.cpp @@ -1,10 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. - * Author: @author Lorenz Meier <lm@inf.ethz.ch> - * @author Jean Cyr <jean.m.cyr@gmail.com> - * @author Julian Oes <joes@student.ethz.ch> - * @author Anton Babushkin <anton.babushkin@me.com> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -35,7 +31,7 @@ * ****************************************************************************/ /** - * @file navigator_main.c + * @file navigator_main.cpp * Implementation of the main navigation state machine. * * Handles missions, geo fencing and failsafe navigation behavior. @@ -177,7 +173,7 @@ private: class Mission _mission; bool _mission_item_valid; /**< current mission item valid */ - bool _global_pos_valid; /**< track changes of global_position.global_valid flag */ + bool _global_pos_valid; /**< track changes of global_position */ bool _reset_loiter_pos; /**< if true then loiter position should be set to current position */ bool _waypoint_position_reached; bool _waypoint_yaw_reached; @@ -510,7 +506,7 @@ Navigator::offboard_mission_update(bool isrotaryWing) { struct mission_s offboard_mission; - if (orb_copy(ORB_ID(mission), _offboard_mission_sub, &offboard_mission) == OK) { + if (orb_copy(ORB_ID(offboard_mission), _offboard_mission_sub, &offboard_mission) == OK) { /* Check mission feasibility, for now do not handle the return value, * however warnings are issued to the gcs via mavlink from inside the MissionFeasiblityChecker */ @@ -543,7 +539,7 @@ Navigator::onboard_mission_update() { struct mission_s onboard_mission; - if (orb_copy(ORB_ID(mission), _onboard_mission_sub, &onboard_mission) == OK) { + if (orb_copy(ORB_ID(onboard_mission), _onboard_mission_sub, &onboard_mission) == OK) { _mission.set_onboard_mission_count(onboard_mission.count); _mission.set_current_onboard_mission_index(onboard_mission.current_index); @@ -611,7 +607,7 @@ Navigator::task_main() * do subscriptions */ _global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position)); - _offboard_mission_sub = orb_subscribe(ORB_ID(mission)); + _offboard_mission_sub = orb_subscribe(ORB_ID(offboard_mission)); _onboard_mission_sub = orb_subscribe(ORB_ID(onboard_mission)); _capabilities_sub = orb_subscribe(ORB_ID(navigation_capabilities)); _vstatus_sub = orb_subscribe(ORB_ID(vehicle_status)); @@ -690,84 +686,56 @@ Navigator::task_main() if (fds[6].revents & POLLIN) { vehicle_status_update(); - /* evaluate state machine from commander and set the navigator mode accordingly */ + /* evaluate state requested by commander */ if (_control_mode.flag_armed && _control_mode.flag_control_auto_enabled) { - bool stick_mode = false; - - if (!_vstatus.rc_signal_lost) { - /* RC signal available, use control switches to set mode */ - /* RETURN switch, overrides MISSION switch */ - if (_vstatus.return_switch == RETURN_SWITCH_RETURN) { - /* switch to RTL if not already landed after RTL and home position set */ - if (!(_rtl_state == RTL_STATE_DESCEND && - (myState == NAV_STATE_LAND || myState == NAV_STATE_LOITER)) && - _vstatus.condition_home_position_valid) { - dispatch(EVENT_RTL_REQUESTED); - } + /* publish position setpoint triplet on each status update if navigator active */ + _pos_sp_triplet_updated = true; - stick_mode = true; + if (_vstatus.set_nav_state_timestamp != _set_nav_state_timestamp) { + /* commander requested new navigation mode, try to set it */ + switch (_vstatus.set_nav_state) { + case NAV_STATE_NONE: + /* nothing to do */ + break; - } else { - /* MISSION switch */ - if (_vstatus.mission_switch == MISSION_SWITCH_LOITER) { - request_loiter_or_ready(); - stick_mode = true; + case NAV_STATE_LOITER: + request_loiter_or_ready(); + break; - } else if (_vstatus.mission_switch == MISSION_SWITCH_MISSION) { - request_mission_if_available(); - stick_mode = true; - } + case NAV_STATE_MISSION: + request_mission_if_available(); + break; - if (!stick_mode && _vstatus.return_switch == RETURN_SWITCH_NORMAL && myState == NAV_STATE_RTL) { - /* RETURN switch is in normal mode, no MISSION switch mapped, interrupt if in RTL state */ - request_mission_if_available(); - stick_mode = true; + case NAV_STATE_RTL: + if (!(_rtl_state == RTL_STATE_DESCEND && + (myState == NAV_STATE_LAND || myState == NAV_STATE_LOITER)) && + _vstatus.condition_home_position_valid) { + dispatch(EVENT_RTL_REQUESTED); } - } - } - - if (!stick_mode) { - if (_vstatus.set_nav_state_timestamp != _set_nav_state_timestamp) { - /* commander requested new navigation mode, try to set it */ - _set_nav_state_timestamp = _vstatus.set_nav_state_timestamp; - - switch (_vstatus.set_nav_state) { - case NAV_STATE_NONE: - /* nothing to do */ - break; - - case NAV_STATE_LOITER: - request_loiter_or_ready(); - break; - - case NAV_STATE_MISSION: - request_mission_if_available(); - break; - case NAV_STATE_RTL: - if (!(_rtl_state == RTL_STATE_DESCEND && - (myState == NAV_STATE_LAND || myState == NAV_STATE_LOITER)) && - _vstatus.condition_home_position_valid) { - dispatch(EVENT_RTL_REQUESTED); - } + break; - break; + case NAV_STATE_LAND: + dispatch(EVENT_LAND_REQUESTED); - case NAV_STATE_LAND: - dispatch(EVENT_LAND_REQUESTED); + break; - break; + default: + warnx("ERROR: Requested navigation state not supported"); + break; + } - default: - warnx("ERROR: Requested navigation state not supported"); - break; - } + } else { + /* on first switch to AUTO try mission by default, if none is available fallback to loiter */ + if (myState == NAV_STATE_NONE) { + request_mission_if_available(); + } + } - } else { - /* on first switch to AUTO try mission by default, if none is available fallback to loiter */ - if (myState == NAV_STATE_NONE) { - request_mission_if_available(); - } + /* check if waypoint has been reached in MISSION, RTL and LAND modes */ + if (myState == NAV_STATE_MISSION || myState == NAV_STATE_RTL || myState == NAV_STATE_LAND) { + if (check_mission_item_reached()) { + on_mission_item_reached(); } } @@ -775,6 +743,8 @@ Navigator::task_main() /* navigator shouldn't act */ dispatch(EVENT_NONE_REQUESTED); } + + _set_nav_state_timestamp = _vstatus.set_nav_state_timestamp; } /* parameters updated */ @@ -813,17 +783,15 @@ Navigator::task_main() if (fds[1].revents & POLLIN) { global_position_update(); - /* publish position setpoint triplet on each position update if navigator active */ if (_control_mode.flag_armed && _control_mode.flag_control_auto_enabled) { + /* publish position setpoint triplet on each position update if navigator active */ _pos_sp_triplet_updated = true; - if (myState == NAV_STATE_LAND && _global_pos.global_valid && !_global_pos_valid) { + if (myState == NAV_STATE_LAND && !_global_pos_valid) { /* got global position when landing, update setpoint */ start_land(); } - _global_pos_valid = _global_pos.global_valid; - /* check if waypoint has been reached in MISSION, RTL and LAND modes */ if (myState == NAV_STATE_MISSION || myState == NAV_STATE_RTL || myState == NAV_STATE_LAND) { if (check_mission_item_reached()) { @@ -848,6 +816,8 @@ Navigator::task_main() } } + _global_pos_valid = _vstatus.condition_global_position_valid; + /* publish position setpoint triplet if updated */ if (_pos_sp_triplet_updated) { _pos_sp_triplet_updated = false; @@ -878,7 +848,7 @@ Navigator::start() _navigator_task = task_spawn_cmd("navigator", SCHED_DEFAULT, SCHED_PRIORITY_MAX - 5, - 2048, + 2000, (main_t)&Navigator::task_main_trampoline, nullptr); @@ -893,9 +863,9 @@ Navigator::start() void Navigator::status() { - warnx("Global position is %svalid", _global_pos.global_valid ? "" : "in"); + warnx("Global position: %svalid", _global_pos_valid ? "" : "in"); - if (_global_pos.global_valid) { + if (_global_pos_valid) { warnx("Longitude %5.5f degrees, latitude %5.5f degrees", _global_pos.lon, _global_pos.lat); warnx("Altitude %5.5f meters, altitude above home %5.5f meters", (double)_global_pos.alt, (double)(_global_pos.alt - _home_pos.alt)); @@ -1317,7 +1287,7 @@ Navigator::set_rtl_item() _mission_item.yaw = NAN; _mission_item.loiter_radius = _parameters.loiter_radius; _mission_item.loiter_direction = 1; - _mission_item.nav_cmd = NAV_CMD_TAKEOFF; + _mission_item.nav_cmd = NAV_CMD_WAYPOINT; _mission_item.acceptance_radius = _parameters.acceptance_radius; _mission_item.time_inside = 0.0f; _mission_item.pitch_min = 0.0f; @@ -1377,7 +1347,7 @@ Navigator::set_rtl_item() _mission_item.yaw = NAN; _mission_item.loiter_radius = _parameters.loiter_radius; _mission_item.loiter_direction = 1; - _mission_item.nav_cmd = NAV_CMD_WAYPOINT; + _mission_item.nav_cmd = NAV_CMD_LOITER_TIME_LIMIT; _mission_item.acceptance_radius = _parameters.acceptance_radius; _mission_item.time_inside = _parameters.rtl_land_delay < 0.0f ? 0.0f : _parameters.rtl_land_delay; _mission_item.pitch_min = 0.0f; @@ -1539,7 +1509,7 @@ Navigator::check_mission_item_reached() /* check yaw if defined only for rotary wing except takeoff */ float yaw_err = _wrap_pi(_mission_item.yaw - _global_pos.yaw); - if (fabsf(yaw_err) < 0.05f) { /* XXX get rid of magic number */ + if (fabsf(yaw_err) < 0.2f) { /* XXX get rid of magic number */ _waypoint_yaw_reached = true; } diff --git a/src/modules/navigator/navigator_mission.cpp b/src/modules/navigator/navigator_mission.cpp index 72dddebfe..49fc62785 100644 --- a/src/modules/navigator/navigator_mission.cpp +++ b/src/modules/navigator/navigator_mission.cpp @@ -1,7 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013 PX4 Development Team. All rights reserved. - * Author: @author Julian Oes <joes@student.ethz.ch> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -34,6 +33,8 @@ /** * @file navigator_mission.cpp * Helper class to access missions + * + * @author Julian Oes <joes@student.ethz.ch> */ #include <string.h> diff --git a/src/modules/navigator/navigator_mission.h b/src/modules/navigator/navigator_mission.h index 2bd4da82e..b0f88e016 100644 --- a/src/modules/navigator/navigator_mission.h +++ b/src/modules/navigator/navigator_mission.h @@ -1,7 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013 PX4 Development Team. All rights reserved. - * Author: @author Julian Oes <joes@student.ethz.ch> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -34,6 +33,8 @@ /** * @file navigator_mission.h * Helper class to access missions + * + * @author Julian Oes <joes@student.ethz.ch> */ #ifndef NAVIGATOR_MISSION_H diff --git a/src/modules/navigator/navigator_params.c b/src/modules/navigator/navigator_params.c index 9ef359c6d..5139283b6 100644 --- a/src/modules/navigator/navigator_params.c +++ b/src/modules/navigator/navigator_params.c @@ -1,9 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013 PX4 Development Team. All rights reserved. - * Author: @author Lorenz Meier <lm@inf.ethz.ch> - * @author Julian Oes <joes@student.ethz.ch> - * @author Anton Babushkin <anton.babushkin@me.com> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions diff --git a/src/modules/navigator/navigator_state.h b/src/modules/navigator/navigator_state.h index 6a1475c9b..476f93414 100644 --- a/src/modules/navigator/navigator_state.h +++ b/src/modules/navigator/navigator_state.h @@ -1,8 +1,42 @@ -/* - * navigator_state.h +/**************************************************************************** * - * Created on: 27.01.2014 - * Author: ton + * Copyright (c) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file navigator_state.h + * + * Navigator state + * + * @author Anton Babushkin <anton.babushkin@me.com> */ #ifndef NAVIGATOR_STATE_H_ diff --git a/src/modules/position_estimator/position_estimator_main.c b/src/modules/position_estimator/position_estimator_main.c deleted file mode 100644 index e84945299..000000000 --- a/src/modules/position_estimator/position_estimator_main.c +++ /dev/null @@ -1,423 +0,0 @@ -/**************************************************************************** - * - * Copyright (C) 2008-2012 PX4 Development Team. All rights reserved. - * Author: Tobias Naegeli <naegelit@student.ethz.ch> - * Thomas Gubler <thomasgubler@student.ethz.ch> - * Julian Oes <joes@student.ethz.ch> - * Lorenz Meier <lm@inf.ethz.ch> - * - * Redistribution and use in source and binary forms, with or without - * modification, are permitted provided that the following conditions - * are met: - * - * 1. Redistributions of source code must retain the above copyright - * notice, this list of conditions and the following disclaimer. - * 2. Redistributions in binary form must reproduce the above copyright - * notice, this list of conditions and the following disclaimer in - * the documentation and/or other materials provided with the - * distribution. - * 3. Neither the name PX4 nor the names of its contributors may be - * used to endorse or promote products derived from this software - * without specific prior written permission. - * - * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS - * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT - * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS - * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE - * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, - * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, - * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS - * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED - * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT - * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN - * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE - * POSSIBILITY OF SUCH DAMAGE. - * - ****************************************************************************/ - -/** - * @file position_estimator_main.c - * Model-identification based position estimator for multirotors - */ - -#include <nuttx/config.h> -#include <unistd.h> -#include <stdlib.h> -#include <stdio.h> -#include <stdbool.h> -#include <fcntl.h> -#include <float.h> -#include <nuttx/sched.h> -#include <sys/prctl.h> -#include <termios.h> -#include <errno.h> -#include <limits.h> -#include <math.h> -#include <uORB/uORB.h> -#include <uORB/topics/vehicle_status.h> -#include <uORB/topics/vehicle_attitude.h> -#include <uORB/topics/vehicle_gps_position.h> -#include <uORB/topics/vehicle_global_position.h> -#include <uORB/topics/vehicle_local_position.h> -#include <poll.h> - -#define N_STATES 6 -#define ERROR_COVARIANCE_INIT 3 -#define R_EARTH 6371000.0 - -#define PROJECTION_INITIALIZE_COUNTER_LIMIT 5000 -#define REPROJECTION_COUNTER_LIMIT 125 - -__EXPORT int position_estimator_main(int argc, char *argv[]); - -static uint16_t position_estimator_counter_position_information; - -/* values for map projection */ -static double phi_1; -static double sin_phi_1; -static double cos_phi_1; -static double lambda_0; -static double scale; - -/** - * Initializes the map transformation. - * - * Initializes the transformation between the geographic coordinate system and the azimuthal equidistant plane - * @param lat in degrees (47.1234567°, not 471234567°) - * @param lon in degrees (8.1234567°, not 81234567°) - */ -static void map_projection_init(double lat_0, double lon_0) //lat_0, lon_0 are expected to be in correct format: -> 47.1234567 and not 471234567 -{ - /* notation and formulas according to: http://mathworld.wolfram.com/AzimuthalEquidistantProjection.html */ - phi_1 = lat_0 / 180.0 * M_PI; - lambda_0 = lon_0 / 180.0 * M_PI; - - sin_phi_1 = sin(phi_1); - cos_phi_1 = cos(phi_1); - - /* calculate local scale by using the relation of true distance and the distance on plane */ //TODO: this is a quick solution, there are probably easier ways to determine the scale - - /* 1) calculate true distance d on sphere to a point: http://www.movable-type.co.uk/scripts/latlong.html */ - const double r_earth = 6371000; - - double lat1 = phi_1; - double lon1 = lambda_0; - - double lat2 = phi_1 + 0.5 / 180 * M_PI; - double lon2 = lambda_0 + 0.5 / 180 * M_PI; - double sin_lat_2 = sin(lat2); - double cos_lat_2 = cos(lat2); - double d = acos(sin(lat1) * sin_lat_2 + cos(lat1) * cos_lat_2 * cos(lon2 - lon1)) * r_earth; - - /* 2) calculate distance rho on plane */ - double k_bar = 0; - double c = acos(sin_phi_1 * sin_lat_2 + cos_phi_1 * cos_lat_2 * cos(lon2 - lambda_0)); - - if (0 != c) - k_bar = c / sin(c); - - double x2 = k_bar * (cos_lat_2 * sin(lon2 - lambda_0)); //Projection of point 2 on plane - double y2 = k_bar * ((cos_phi_1 * sin_lat_2 - sin_phi_1 * cos_lat_2 * cos(lon2 - lambda_0))); - double rho = sqrt(pow(x2, 2) + pow(y2, 2)); - - scale = d / rho; - -} - -/** - * Transforms a point in the geographic coordinate system to the local azimuthal equidistant plane - * @param x north - * @param y east - * @param lat in degrees (47.1234567°, not 471234567°) - * @param lon in degrees (8.1234567°, not 81234567°) - */ -static void map_projection_project(double lat, double lon, float *x, float *y) -{ - /* notation and formulas accoring to: http://mathworld.wolfram.com/AzimuthalEquidistantProjection.html */ - double phi = lat / 180.0 * M_PI; - double lambda = lon / 180.0 * M_PI; - - double sin_phi = sin(phi); - double cos_phi = cos(phi); - - double k_bar = 0; - /* using small angle approximation (formula in comment is without aproximation) */ - double c = acos(sin_phi_1 * sin_phi + cos_phi_1 * cos_phi * (1 - pow((lambda - lambda_0), 2) / 2)); //double c = acos( sin_phi_1 * sin_phi + cos_phi_1 * cos_phi * cos(lambda - lambda_0) ); - - if (0 != c) - k_bar = c / sin(c); - - /* using small angle approximation (formula in comment is without aproximation) */ - *y = k_bar * (cos_phi * (lambda - lambda_0)) * scale;//*y = k_bar * (cos_phi * sin(lambda - lambda_0)) * scale; - *x = k_bar * ((cos_phi_1 * sin_phi - sin_phi_1 * cos_phi * (1 - pow((lambda - lambda_0), 2) / 2))) * scale; // *x = k_bar * ((cos_phi_1 * sin_phi - sin_phi_1 * cos_phi * cos(lambda - lambda_0))) * scale; - -// printf("%phi_1=%.10f, lambda_0 =%.10f\n", phi_1, lambda_0); -} - -/** - * Transforms a point in the local azimuthal equidistant plane to the geographic coordinate system - * - * @param x north - * @param y east - * @param lat in degrees (47.1234567°, not 471234567°) - * @param lon in degrees (8.1234567°, not 81234567°) - */ -static void map_projection_reproject(float x, float y, double *lat, double *lon) -{ - /* notation and formulas accoring to: http://mathworld.wolfram.com/AzimuthalEquidistantProjection.html */ - - double x_descaled = x / scale; - double y_descaled = y / scale; - - double c = sqrt(pow(x_descaled, 2) + pow(y_descaled, 2)); - double sin_c = sin(c); - double cos_c = cos(c); - - double lat_sphere = 0; - - if (c != 0) - lat_sphere = asin(cos_c * sin_phi_1 + (x_descaled * sin_c * cos_phi_1) / c); - else - lat_sphere = asin(cos_c * sin_phi_1); - -// printf("lat_sphere = %.10f\n",lat_sphere); - - double lon_sphere = 0; - - if (phi_1 == M_PI / 2) { - //using small angle approximation (formula in comment is without aproximation) - lon_sphere = (lambda_0 - y_descaled / x_descaled); //lon_sphere = (lambda_0 + atan2(-y_descaled, x_descaled)); - - } else if (phi_1 == -M_PI / 2) { - //using small angle approximation (formula in comment is without aproximation) - lon_sphere = (lambda_0 + y_descaled / x_descaled); //lon_sphere = (lambda_0 + atan2(y_descaled, x_descaled)); - - } else { - - lon_sphere = (lambda_0 + atan2(y_descaled * sin_c , c * cos_phi_1 * cos_c - x_descaled * sin_phi_1 * sin_c)); - //using small angle approximation -// double denominator = (c * cos_phi_1 * cos_c - x_descaled * sin_phi_1 * sin_c); -// if(denominator != 0) -// { -// lon_sphere = (lambda_0 + (y_descaled * sin_c) / denominator); -// } -// else -// { -// ... -// } - } - -// printf("lon_sphere = %.10f\n",lon_sphere); - - *lat = lat_sphere * 180.0 / M_PI; - *lon = lon_sphere * 180.0 / M_PI; - -} - -/**************************************************************************** - * main - ****************************************************************************/ - -int position_estimator_main(int argc, char *argv[]) -{ - - /* welcome user */ - printf("[multirotor position_estimator] started\n"); - - /* initialize values */ - static float u[2] = {0, 0}; - static float z[3] = {0, 0, 0}; - static float xapo[N_STATES] = {0, 0, 0, 0, 0, 0}; - static float Papo[N_STATES * N_STATES] = {ERROR_COVARIANCE_INIT, 0, 0, 0, 0, 0, - ERROR_COVARIANCE_INIT, 0, 0, 0, 0, 0, - ERROR_COVARIANCE_INIT, 0, 0, 0, 0, 0, - ERROR_COVARIANCE_INIT, 0, 0, 0, 0, 0, - ERROR_COVARIANCE_INIT, 0, 0, 0, 0, 0, - ERROR_COVARIANCE_INIT, 0, 0, 0, 0, 0 - }; - - static float xapo1[N_STATES]; - static float Papo1[36]; - - static float gps_covariance[3] = {0.0f, 0.0f, 0.0f}; - - static uint16_t counter = 0; - position_estimator_counter_position_information = 0; - - uint8_t predict_only = 1; - - bool gps_valid = false; - - bool new_initialization = true; - - static double lat_current = 0.0d;//[°]] --> 47.0 - static double lon_current = 0.0d; //[°]] -->8.5 - float alt_current = 0.0f; - - - //TODO: handle flight without gps but with estimator - - /* subscribe to vehicle status, attitude, gps */ - struct vehicle_gps_position_s gps; - gps.fix_type = 0; - struct vehicle_status_s vstatus; - struct vehicle_attitude_s att; - - int vehicle_gps_sub = orb_subscribe(ORB_ID(vehicle_gps_position)); - int vehicle_status_sub = orb_subscribe(ORB_ID(vehicle_status)); - - /* subscribe to attitude at 100 Hz */ - int vehicle_attitude_sub = orb_subscribe(ORB_ID(vehicle_attitude)); - - /* wait until gps signal turns valid, only then can we initialize the projection */ - while (gps.fix_type < 3) { - struct pollfd fds[1] = { {.fd = vehicle_gps_sub, .events = POLLIN} }; - - /* wait for GPS updates, BUT READ VEHICLE STATUS (!) - * this choice is critical, since the vehicle status might not - * actually change, if this app is started after GPS lock was - * aquired. - */ - if (poll(fds, 1, 5000)) { - /* Wait for the GPS update to propagate (we have some time) */ - usleep(5000); - /* Read wether the vehicle status changed */ - orb_copy(ORB_ID(vehicle_gps_position), vehicle_gps_sub, &gps); - gps_valid = (gps.fix_type > 2); - } - } - - /* get gps value for first initialization */ - orb_copy(ORB_ID(vehicle_gps_position), vehicle_gps_sub, &gps); - lat_current = ((double)(gps.lat)) * 1e-7; - lon_current = ((double)(gps.lon)) * 1e-7; - alt_current = gps.alt * 1e-3; - - /* initialize coordinates */ - map_projection_init(lat_current, lon_current); - - /* publish global position messages only after first GPS message */ - struct vehicle_local_position_s local_pos = { - .x = 0, - .y = 0, - .z = 0 - }; - orb_advert_t local_pos_pub = orb_advertise(ORB_ID(vehicle_local_position), &local_pos); - - printf("[multirotor position estimator] initialized projection with: lat: %.10f, lon:%.10f\n", lat_current, lon_current); - - while (1) { - - /*This runs at the rate of the sensors, if we have also a new gps update this is used in the position_estimator function */ - struct pollfd fds[1] = { {.fd = vehicle_attitude_sub, .events = POLLIN} }; - - if (poll(fds, 1, 5000) <= 0) { - /* error / timeout */ - } else { - - orb_copy(ORB_ID(vehicle_attitude), vehicle_attitude_sub, &att); - /* got attitude, updating pos as well */ - orb_copy(ORB_ID(vehicle_gps_position), vehicle_gps_sub, &gps); - orb_copy(ORB_ID(vehicle_status), vehicle_status_sub, &vstatus); - - /*copy attitude */ - u[0] = att.roll; - u[1] = att.pitch; - - /* initialize map projection with the last estimate (not at full rate) */ - if (gps.fix_type > 2) { - /* Project gps lat lon (Geographic coordinate system) to plane*/ - map_projection_project(((double)(gps.lat)) * 1e-7, ((double)(gps.lon)) * 1e-7, &(z[0]), &(z[1])); - - local_pos.x = z[0]; - local_pos.y = z[1]; - /* negative offset from initialization altitude */ - local_pos.z = alt_current - (gps.alt) * 1e-3; - - - orb_publish(ORB_ID(vehicle_local_position), local_pos_pub, &local_pos); - } - - - // gps_covariance[0] = gps.eph; //TODO: needs scaling - // gps_covariance[1] = gps.eph; - // gps_covariance[2] = gps.epv; - - // } else { - // /* we can not use the gps signal (it is of low quality) */ - // predict_only = 1; - // } - - // // predict_only = 0; //TODO: only for testing, removeme, XXX - // // z[0] = sinf(((float)counter)/180.0f*3.14159265f); //TODO: only for testing, removeme, XXX - // // usleep(100000); //TODO: only for testing, removeme, XXX - - - // /*Get new estimation (this is calculated in the plane) */ - // //TODO: if new_initialization == true: use 0,0,0, else use xapo - // if (true == new_initialization) { //TODO,XXX: uncomment! - // xapo[0] = 0; //we have a new plane initialization. the current estimate is in the center of the plane - // xapo[2] = 0; - // xapo[4] = 0; - // position_estimator(u, z, xapo, Papo, gps_covariance, predict_only, xapo1, Papo1); - - // } else { - // position_estimator(u, z, xapo, Papo, gps_covariance, predict_only, xapo1, Papo1); - // } - - - - // /* Copy values from xapo1 to xapo */ - // int i; - - // for (i = 0; i < N_STATES; i++) { - // xapo[i] = xapo1[i]; - // } - - // if ((counter % REPROJECTION_COUNTER_LIMIT == 0) || (counter % (PROJECTION_INITIALIZE_COUNTER_LIMIT - 1) == 0)) { - // /* Reproject from plane to geographic coordinate system */ - // // map_projection_reproject(xapo1[0], xapo1[2], map_scale, phi_1, lambda_0, &lat_current, &lon_current) //TODO,XXX: uncomment! - // map_projection_reproject(z[0], z[1], &lat_current, &lon_current); //do not use estimator for projection testing, removeme - // // //DEBUG - // // if(counter%500 == 0) - // // { - // // printf("phi_1: %.10f\n", phi_1); - // // printf("lambda_0: %.10f\n", lambda_0); - // // printf("lat_estimated: %.10f\n", lat_current); - // // printf("lon_estimated: %.10f\n", lon_current); - // // printf("z[0]=%.10f, z[1]=%.10f, z[2]=%f\n", z[0], z[1], z[2]); - // // fflush(stdout); - // // - // // } - - // // if(!isnan(lat_current) && !isnan(lon_current))// && !isnan(xapo1[4]) && !isnan(xapo1[1]) && !isnan(xapo1[3]) && !isnan(xapo1[5])) - // // { - // /* send out */ - - // global_pos.lat = lat_current; - // global_pos.lon = lon_current; - // global_pos.alt = xapo1[4]; - // global_pos.vx = xapo1[1]; - // global_pos.vy = xapo1[3]; - // global_pos.vz = xapo1[5]; - - /* publish current estimate */ - // orb_publish(ORB_ID(vehicle_global_position), global_pos_pub, &global_pos); - // } - // else - // { - // printf("[position estimator] ERROR: nan values, lat_current=%.4f, lon_current=%.4f, z[0]=%.4f z[1]=%.4f\n", lat_current, lon_current, z[0], z[1]); - // fflush(stdout); - // } - - // } - - counter++; - } - - } - - return 0; -} - - diff --git a/src/modules/position_estimator_inav/module.mk b/src/modules/position_estimator_inav/module.mk index 939d76849..0658d3f09 100644 --- a/src/modules/position_estimator_inav/module.mk +++ b/src/modules/position_estimator_inav/module.mk @@ -39,3 +39,5 @@ MODULE_COMMAND = position_estimator_inav SRCS = position_estimator_inav_main.c \ position_estimator_inav_params.c \ inertial_filter.c + +MODULE_STACKSIZE = 1200 diff --git a/src/modules/position_estimator_inav/position_estimator_inav_main.c b/src/modules/position_estimator_inav/position_estimator_inav_main.c index 368fa6ee2..d8d0ff37d 100644 --- a/src/modules/position_estimator_inav/position_estimator_inav_main.c +++ b/src/modules/position_estimator_inav/position_estimator_inav_main.c @@ -1,7 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 Anton Babushkin. All rights reserved. - * Author: Anton Babushkin <rk3dov@gmail.com> + * Copyright (C) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -35,6 +34,8 @@ /** * @file position_estimator_inav_main.c * Model-identification based position estimator for multirotors + * + * @author Anton Babushkin <anton.babushkin@me.com> */ #include <unistd.h> @@ -57,6 +58,7 @@ #include <uORB/topics/vehicle_local_position.h> #include <uORB/topics/vehicle_global_position.h> #include <uORB/topics/vehicle_gps_position.h> +#include <uORB/topics/home_position.h> #include <uORB/topics/optical_flow.h> #include <mavlink/mavlink_log.h> #include <poll.h> @@ -95,8 +97,9 @@ static void usage(const char *reason); */ static void usage(const char *reason) { - if (reason) + if (reason) { fprintf(stderr, "%s\n", reason); + } fprintf(stderr, "usage: position_estimator_inav {start|stop|status} [-v]\n\n"); exit(1); @@ -112,8 +115,9 @@ static void usage(const char *reason) */ int position_estimator_inav_main(int argc, char *argv[]) { - if (argc < 1) + if (argc < 1) { usage("missing command"); + } if (!strcmp(argv[1], "start")) { if (thread_running) { @@ -125,12 +129,13 @@ int position_estimator_inav_main(int argc, char *argv[]) verbose_mode = false; if (argc > 1) - if (!strcmp(argv[2], "-v")) + if (!strcmp(argv[2], "-v")) { verbose_mode = true; + } thread_should_exit = false; position_estimator_inav_task = task_spawn_cmd("position_estimator_inav", - SCHED_RR, SCHED_PRIORITY_MAX - 5, 4096, + SCHED_DEFAULT, SCHED_PRIORITY_MAX - 5, 4000, position_estimator_inav_thread_main, (argv) ? (const char **) &argv[2] : (const char **) NULL); exit(0); @@ -163,16 +168,19 @@ int position_estimator_inav_main(int argc, char *argv[]) exit(1); } -void write_debug_log(const char *msg, float dt, float x_est[3], float y_est[3], float z_est[3], float corr_acc[3], float corr_gps[3][2], float w_xy_gps_p, float w_xy_gps_v) { +void write_debug_log(const char *msg, float dt, float x_est[3], float y_est[3], float z_est[3], float x_est_prev[3], float y_est_prev[3], float z_est_prev[3], float corr_acc[3], float corr_gps[3][2], float w_xy_gps_p, float w_xy_gps_v) +{ FILE *f = fopen("/fs/microsd/inav.log", "a"); + if (f) { char *s = malloc(256); - unsigned n = snprintf(s, 256, "%llu %s\n\tdt=%.5f x_est=[%.5f %.5f %.5f] y_est=[%.5f %.5f %.5f] z_est=[%.5f %.5f %.5f]\n", hrt_absolute_time(), msg, dt, x_est[0], x_est[1], x_est[2], y_est[0], y_est[1], y_est[2], z_est[0], z_est[1], z_est[2]); + unsigned n = snprintf(s, 256, "%llu %s\n\tdt=%.5f x_est=[%.5f %.5f %.5f] y_est=[%.5f %.5f %.5f] z_est=[%.5f %.5f %.5f] x_est_prev=[%.5f %.5f %.5f] y_est_prev=[%.5f %.5f %.5f] z_est_prev=[%.5f %.5f %.5f]\n", hrt_absolute_time(), msg, dt, x_est[0], x_est[1], x_est[2], y_est[0], y_est[1], y_est[2], z_est[0], z_est[1], z_est[2], x_est_prev[0], x_est_prev[1], x_est_prev[2], y_est_prev[0], y_est_prev[1], y_est_prev[2], z_est_prev[0], z_est_prev[1], z_est_prev[2]); fwrite(s, 1, n, f); n = snprintf(s, 256, "\tacc_corr=[%.5f %.5f %.5f] gps_pos_corr=[%.5f %.5f %.5f] gps_vel_corr=[%.5f %.5f %.5f] w_xy_gps_p=%.5f w_xy_gps_v=%.5f\n", corr_acc[0], corr_acc[1], corr_acc[2], corr_gps[0][0], corr_gps[1][0], corr_gps[2][0], corr_gps[0][1], corr_gps[1][1], corr_gps[2][1], w_xy_gps_p, w_xy_gps_v); fwrite(s, 1, n, f); free(s); } + fsync(fileno(f)); fclose(f); } @@ -191,6 +199,11 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) float y_est[3] = { 0.0f, 0.0f, 0.0f }; float z_est[3] = { 0.0f, 0.0f, 0.0f }; + float x_est_prev[3], y_est_prev[3], z_est_prev[3]; + memset(x_est_prev, 0, sizeof(x_est_prev)); + memset(y_est_prev, 0, sizeof(y_est_prev)); + memset(z_est_prev, 0, sizeof(z_est_prev)); + int baro_init_cnt = 0; int baro_init_num = 200; float baro_offset = 0.0f; // baro offset for reference altitude, initialized on start, then adjusted @@ -206,6 +219,9 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) bool ref_inited = false; hrt_abstime ref_init_start = 0; const hrt_abstime ref_init_delay = 1000000; // wait for 1s after 3D fix + struct map_projection_reference_s ref; + memset(&ref, 0, sizeof(ref)); + hrt_abstime home_timestamp = 0; uint16_t accel_updates = 0; uint16_t baro_updates = 0; @@ -238,7 +254,11 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) float corr_flow[] = { 0.0f, 0.0f }; // N E float w_flow = 0.0f; + static float min_eph_epv = 2.0f; // min EPH/EPV, used for weight calculation + static float max_eph_epv = 10.0f; // max EPH/EPV acceptable for estimation + float sonar_prev = 0.0f; + hrt_abstime flow_prev = 0; // time of last flow measurement hrt_abstime sonar_time = 0; // time of last sonar measurement (not filtered) hrt_abstime sonar_valid_time = 0; // time of last sonar measurement used for correction (filtered) hrt_abstime xy_src_time = 0; // time of last available position data @@ -257,6 +277,8 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) memset(&sensor, 0, sizeof(sensor)); struct vehicle_gps_position_s gps; memset(&gps, 0, sizeof(gps)); + struct home_position_s home; + memset(&home, 0, sizeof(home)); struct vehicle_attitude_s att; memset(&att, 0, sizeof(att)); struct vehicle_local_position_s local_pos; @@ -274,10 +296,11 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) int vehicle_attitude_sub = orb_subscribe(ORB_ID(vehicle_attitude)); int optical_flow_sub = orb_subscribe(ORB_ID(optical_flow)); int vehicle_gps_position_sub = orb_subscribe(ORB_ID(vehicle_gps_position)); + int home_position_sub = orb_subscribe(ORB_ID(home_position)); /* advertise */ orb_advert_t vehicle_local_position_pub = orb_advertise(ORB_ID(vehicle_local_position), &local_pos); - orb_advert_t vehicle_global_position_pub = orb_advertise(ORB_ID(vehicle_global_position), &global_pos); + orb_advert_t vehicle_global_position_pub = -1; struct position_estimator_inav_params params; struct position_estimator_inav_param_handles pos_inav_param_handles; @@ -325,7 +348,6 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) mavlink_log_info(mavlink_fd, "[inav] baro offs: %.2f", baro_offset); local_pos.z_valid = true; local_pos.v_z_valid = true; - global_pos.baro_valid = true; } } } @@ -425,6 +447,10 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) if (updated) { orb_copy(ORB_ID(optical_flow), optical_flow_sub, &flow); + /* calculate time from previous update */ + float flow_dt = flow_prev > 0 ? (flow.flow_timestamp - flow_prev) * 1e-6f : 0.1f; + flow_prev = flow.flow_timestamp; + if (flow.ground_distance_m > 0.31f && flow.ground_distance_m < 4.0f && att.R[2][2] > 0.7 && flow.ground_distance_m != sonar_prev) { sonar_time = t; sonar_prev = flow.ground_distance_m; @@ -475,10 +501,10 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) flow_accurate = fabsf(body_v_est[1] / flow_dist - att.rollspeed) < max_flow && fabsf(body_v_est[0] / flow_dist + att.pitchspeed) < max_flow; - /* convert raw flow to angular flow */ + /* convert raw flow to angular flow (rad/s) */ float flow_ang[2]; - flow_ang[0] = flow.flow_raw_x * params.flow_k; - flow_ang[1] = flow.flow_raw_y * params.flow_k; + flow_ang[0] = flow.flow_raw_x * params.flow_k / 1000.0f / flow_dt; + flow_ang[1] = flow.flow_raw_y * params.flow_k / 1000.0f / flow_dt; /* flow measurements vector */ float flow_m[3]; flow_m[0] = -flow_ang[0] * flow_dist; @@ -503,8 +529,9 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) /* if flow is not accurate, reduce weight for it */ // TODO make this more fuzzy - if (!flow_accurate) + if (!flow_accurate) { w_flow *= 0.05f; + } flow_valid = true; @@ -516,32 +543,73 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) flow_updates++; } + /* home position */ + orb_check(home_position_sub, &updated); + + if (updated) { + orb_copy(ORB_ID(home_position), home_position_sub, &home); + + if (home.timestamp != home_timestamp) { + home_timestamp = home.timestamp; + + double est_lat, est_lon; + float est_alt; + + if (ref_inited) { + /* calculate current estimated position in global frame */ + est_alt = local_pos.ref_alt - local_pos.z; + map_projection_reproject(&ref, local_pos.x, local_pos.y, &est_lat, &est_lon); + } + + /* update reference */ + map_projection_init(&ref, home.lat, home.lon); + + /* update baro offset */ + baro_offset += home.alt - local_pos.ref_alt; + + local_pos.ref_lat = home.lat; + local_pos.ref_lon = home.lon; + local_pos.ref_alt = home.alt; + local_pos.ref_timestamp = home.timestamp; + + if (ref_inited) { + /* reproject position estimate with new reference */ + map_projection_project(&ref, est_lat, est_lon, &x_est[0], &y_est[0]); + z_est[0] = -(est_alt - local_pos.ref_alt); + } + + ref_inited = true; + } + } + /* vehicle GPS position */ orb_check(vehicle_gps_position_sub, &updated); if (updated) { orb_copy(ORB_ID(vehicle_gps_position), vehicle_gps_position_sub, &gps); - if (gps.fix_type >= 3) { - /* hysteresis for GPS quality */ - if (gps_valid) { - if (gps.eph_m > 10.0f || gps.epv_m > 20.0f) { - gps_valid = false; - mavlink_log_info(mavlink_fd, "[inav] GPS signal lost"); - } + bool reset_est = false; - } else { - if (gps.eph_m < 5.0f && gps.epv_m < 10.0f) { - gps_valid = true; - mavlink_log_info(mavlink_fd, "[inav] GPS signal found"); - } + /* hysteresis for GPS quality */ + if (gps_valid) { + if (gps.eph_m > max_eph_epv * 1.5f || gps.epv_m > max_eph_epv * 1.5f || gps.fix_type < 3) { + gps_valid = false; + mavlink_log_info(mavlink_fd, "[inav] GPS signal lost"); } } else { - gps_valid = false; + if (gps.eph_m < max_eph_epv && gps.epv_m < max_eph_epv && gps.fix_type >= 3) { + gps_valid = true; + reset_est = true; + mavlink_log_info(mavlink_fd, "[inav] GPS signal found"); + } } if (gps_valid) { + double lat = gps.lat * 1e-7; + double lon = gps.lon * 1e-7; + float alt = gps.alt * 1e-3; + /* initialize reference position if needed */ if (!ref_inited) { if (ref_init_start == 0) { @@ -549,18 +617,25 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) } else if (t > ref_init_start + ref_init_delay) { ref_inited = true; - /* reference GPS position */ - double lat = gps.lat * 1e-7; - double lon = gps.lon * 1e-7; - float alt = gps.alt * 1e-3; - - local_pos.ref_lat = gps.lat; - local_pos.ref_lon = gps.lon; - local_pos.ref_alt = alt + z_est[0]; + /* update baro offset */ + baro_offset -= z_est[0]; + + /* set position estimate to (0, 0, 0), use GPS velocity for XY */ + x_est[0] = 0.0f; + x_est[1] = gps.vel_n_m_s; + x_est[2] = accel_NED[0]; + y_est[0] = 0.0f; + y_est[1] = gps.vel_e_m_s; + z_est[0] = 0.0f; + y_est[2] = accel_NED[1]; + + local_pos.ref_lat = lat; + local_pos.ref_lon = lon; + local_pos.ref_alt = alt; local_pos.ref_timestamp = t; /* initialize projection */ - map_projection_init(lat, lon); + map_projection_init(&ref, lat, lon); warnx("init ref: lat=%.7f, lon=%.7f, alt=%.2f", lat, lon, alt); mavlink_log_info(mavlink_fd, "[inav] init ref: lat=%.7f, lon=%.7f, alt=%.2f", lat, lon, alt); } @@ -569,11 +644,22 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) if (ref_inited) { /* project GPS lat lon to plane */ float gps_proj[2]; - map_projection_project(gps.lat * 1e-7, gps.lon * 1e-7, &(gps_proj[0]), &(gps_proj[1])); + map_projection_project(&ref, lat, lon, &(gps_proj[0]), &(gps_proj[1])); + + /* reset position estimate when GPS becomes good */ + if (reset_est) { + x_est[0] = gps_proj[0]; + x_est[1] = gps.vel_n_m_s; + x_est[2] = accel_NED[0]; + y_est[0] = gps_proj[1]; + y_est[1] = gps.vel_e_m_s; + y_est[2] = accel_NED[1]; + } + /* calculate correction for position */ corr_gps[0][0] = gps_proj[0] - x_est[0]; corr_gps[1][0] = gps_proj[1] - y_est[0]; - corr_gps[2][0] = local_pos.ref_alt - gps.alt * 1e-3 - z_est[0]; + corr_gps[2][0] = local_pos.ref_alt - alt - z_est[0]; /* calculate correction for velocity */ if (gps.vel_ned_valid) { @@ -587,8 +673,8 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) corr_gps[2][1] = 0.0f; } - w_gps_xy = 2.0f / fmaxf(2.0f, gps.eph_m); - w_gps_z = 4.0f / fmaxf(4.0f, gps.epv_m); + w_gps_xy = min_eph_epv / fmaxf(min_eph_epv, gps.eph_m); + w_gps_z = min_eph_epv / fmaxf(min_eph_epv, gps.epv_m); } } else { @@ -704,23 +790,34 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) /* inertial filter prediction for altitude */ inertial_filter_predict(dt, z_est); + if (!(isfinite(z_est[0]) && isfinite(z_est[1]) && isfinite(z_est[2]))) { + write_debug_log("BAD ESTIMATE AFTER Z PREDICTION", dt, x_est, y_est, z_est, x_est_prev, y_est_prev, z_est_prev, corr_acc, corr_gps, w_xy_gps_p, w_xy_gps_v); + memcpy(z_est, z_est_prev, sizeof(z_est)); + } + /* inertial filter correction for altitude */ inertial_filter_correct(corr_baro, dt, z_est, 0, params.w_z_baro); inertial_filter_correct(corr_gps[2][0], dt, z_est, 0, w_z_gps_p); inertial_filter_correct(corr_acc[2], dt, z_est, 2, params.w_z_acc); - float x_est_prev[3], y_est_prev[3]; + if (!(isfinite(z_est[0]) && isfinite(z_est[1]) && isfinite(z_est[2]))) { + write_debug_log("BAD ESTIMATE AFTER Z CORRECTION", dt, x_est, y_est, z_est, x_est_prev, y_est_prev, z_est_prev, corr_acc, corr_gps, w_xy_gps_p, w_xy_gps_v); + memcpy(z_est, z_est_prev, sizeof(z_est)); + memset(corr_acc, 0, sizeof(corr_acc)); + memset(corr_gps, 0, sizeof(corr_gps)); + corr_baro = 0; - memcpy(x_est_prev, x_est, sizeof(x_est)); - memcpy(y_est_prev, y_est, sizeof(y_est)); + } else { + memcpy(z_est_prev, z_est, sizeof(z_est)); + } if (can_estimate_xy) { /* inertial filter prediction for position */ inertial_filter_predict(dt, x_est); inertial_filter_predict(dt, y_est); - if (!isfinite(x_est[0]) || !isfinite(y_est[0])) { - write_debug_log("BAD ESTIMATE AFTER PREDICTION", dt, x_est, y_est, z_est, corr_acc, corr_gps, w_xy_gps_p, w_xy_gps_v); + if (!(isfinite(x_est[0]) && isfinite(x_est[1]) && isfinite(x_est[2]) && isfinite(y_est[0]) && isfinite(y_est[1]) && isfinite(y_est[2]))) { + write_debug_log("BAD ESTIMATE AFTER PREDICTION", dt, x_est, y_est, z_est, x_est_prev, y_est_prev, z_est_prev, corr_acc, corr_gps, w_xy_gps_p, w_xy_gps_v); memcpy(x_est, x_est_prev, sizeof(x_est)); memcpy(y_est, y_est_prev, sizeof(y_est)); } @@ -744,13 +841,17 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) } } - if (!isfinite(x_est[0]) || !isfinite(y_est[0])) { - write_debug_log("BAD ESTIMATE AFTER CORRECTION", dt, x_est, y_est, z_est, corr_acc, corr_gps, w_xy_gps_p, w_xy_gps_v); + if (!(isfinite(x_est[0]) && isfinite(x_est[1]) && isfinite(x_est[2]) && isfinite(y_est[0]) && isfinite(y_est[1]) && isfinite(y_est[2]))) { + write_debug_log("BAD ESTIMATE AFTER CORRECTION", dt, x_est, y_est, z_est, x_est_prev, y_est_prev, z_est_prev, corr_acc, corr_gps, w_xy_gps_p, w_xy_gps_v); memcpy(x_est, x_est_prev, sizeof(x_est)); memcpy(y_est, y_est_prev, sizeof(y_est)); memset(corr_acc, 0, sizeof(corr_acc)); memset(corr_gps, 0, sizeof(corr_gps)); memset(corr_flow, 0, sizeof(corr_flow)); + + } else { + memcpy(x_est_prev, x_est, sizeof(x_est)); + memcpy(y_est_prev, y_est, sizeof(y_est)); } } @@ -763,7 +864,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) float thrust = armed.armed ? actuator.control[3] : 0.0f; if (landed) { - if (alt_disp2 > land_disp2 && thrust > params.land_thr) { + if (alt_disp2 > land_disp2 || thrust > params.land_thr) { landed = false; landed_time = 0; } @@ -808,7 +909,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) if (t > pub_last + pub_interval) { pub_last = t; /* publish local position */ - local_pos.xy_valid = can_estimate_xy && use_gps_xy; + local_pos.xy_valid = can_estimate_xy; local_pos.v_xy_valid = can_estimate_xy; local_pos.xy_global = local_pos.xy_valid && use_gps_xy; local_pos.z_global = local_pos.z_valid && use_gps_z; @@ -831,40 +932,35 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) orb_publish(ORB_ID(vehicle_local_position), vehicle_local_position_pub, &local_pos); - /* publish global position */ - global_pos.global_valid = local_pos.xy_global; + if (local_pos.xy_global && local_pos.z_global) { + /* publish global position */ + global_pos.timestamp = t; + global_pos.time_gps_usec = gps.time_gps_usec; - if (local_pos.xy_global) { double est_lat, est_lon; - map_projection_reproject(local_pos.x, local_pos.y, &est_lat, &est_lon); + map_projection_reproject(&ref, local_pos.x, local_pos.y, &est_lat, &est_lon); + global_pos.lat = est_lat; global_pos.lon = est_lon; - global_pos.time_gps_usec = gps.time_gps_usec; - } + global_pos.alt = local_pos.ref_alt - local_pos.z; - /* set valid values even if position is not valid */ - if (local_pos.v_xy_valid) { global_pos.vel_n = local_pos.vx; global_pos.vel_e = local_pos.vy; - } - - if (local_pos.z_global) { - global_pos.alt = local_pos.ref_alt - local_pos.z; - } - - if (local_pos.z_valid) { - global_pos.baro_alt = baro_offset - local_pos.z; - } - - if (local_pos.v_z_valid) { global_pos.vel_d = local_pos.vz; - } - global_pos.yaw = local_pos.yaw; + global_pos.yaw = local_pos.yaw; + + // TODO implement dead-reckoning + global_pos.eph = gps.eph_m; + global_pos.epv = gps.epv_m; - global_pos.timestamp = t; + if (vehicle_global_position_pub < 0) { + vehicle_global_position_pub = orb_advertise(ORB_ID(vehicle_global_position), &global_pos); - orb_publish(ORB_ID(vehicle_global_position), vehicle_global_position_pub, &global_pos); + } else { + orb_publish(ORB_ID(vehicle_global_position), vehicle_global_position_pub, &global_pos); + } + } } } diff --git a/src/modules/position_estimator_inav/position_estimator_inav_params.c b/src/modules/position_estimator_inav/position_estimator_inav_params.c index b71f9472f..2e4f26661 100644 --- a/src/modules/position_estimator_inav/position_estimator_inav_params.c +++ b/src/modules/position_estimator_inav/position_estimator_inav_params.c @@ -50,13 +50,13 @@ PARAM_DEFINE_FLOAT(INAV_W_XY_ACC, 20.0f); PARAM_DEFINE_FLOAT(INAV_W_XY_FLOW, 5.0f); PARAM_DEFINE_FLOAT(INAV_W_GPS_FLOW, 0.1f); PARAM_DEFINE_FLOAT(INAV_W_ACC_BIAS, 0.05f); -PARAM_DEFINE_FLOAT(INAV_FLOW_K, 0.0165f); +PARAM_DEFINE_FLOAT(INAV_FLOW_K, 0.15f); PARAM_DEFINE_FLOAT(INAV_FLOW_Q_MIN, 0.5f); PARAM_DEFINE_FLOAT(INAV_SONAR_FILT, 0.05f); PARAM_DEFINE_FLOAT(INAV_SONAR_ERR, 0.5f); PARAM_DEFINE_FLOAT(INAV_LAND_T, 3.0f); PARAM_DEFINE_FLOAT(INAV_LAND_DISP, 0.7f); -PARAM_DEFINE_FLOAT(INAV_LAND_THR, 0.3f); +PARAM_DEFINE_FLOAT(INAV_LAND_THR, 0.2f); int parameters_init(struct position_estimator_inav_param_handles *h) { diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe1.c b/src/modules/position_estimator_mc/codegen/kalman_dlqe1.c deleted file mode 100755 index 977565b8e..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe1.c +++ /dev/null @@ -1,58 +0,0 @@ -/* - * kalman_dlqe1.c - * - * Code generation for function 'kalman_dlqe1' - * - * C source code generated on: Wed Feb 13 20:34:32 2013 - * - */ - -/* Include files */ -#include "rt_nonfinite.h" -#include "kalman_dlqe1.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ - -/* Function Definitions */ -void kalman_dlqe1(const real32_T A[9], const real32_T C[3], const real32_T K[3], - const real32_T x_aposteriori_k[3], real32_T z, real32_T - x_aposteriori[3]) -{ - printf("[dlqe input]: x_aposteriori_k %12.8f\t %12.8f\t %12.8f\t z:%12.8f\n", (double)(x_aposteriori_k[0]), (double)(x_aposteriori_k[1]), (double)(x_aposteriori_k[2]), (double)z); - printf("[dlqe input]: C[0]: %12.8f\tC[1] %12.8f\tC[2] %12.8f\n", (double)(C[0]), (double)(C[1]), (double)(C[2])); - real32_T y; - int32_T i0; - real32_T b_y[3]; - int32_T i1; - real32_T f0; - y = 0.0F; - for (i0 = 0; i0 < 3; i0++) { - b_y[i0] = 0.0F; - for (i1 = 0; i1 < 3; i1++) { - b_y[i0] += C[i1] * A[i1 + 3 * i0]; - } - - y += b_y[i0] * x_aposteriori_k[i0]; - } - - y = z - y; - for (i0 = 0; i0 < 3; i0++) { - f0 = 0.0F; - for (i1 = 0; i1 < 3; i1++) { - f0 += A[i0 + 3 * i1] * x_aposteriori_k[i1]; - } - - x_aposteriori[i0] = f0 + K[i0] * y; - } - //printf("[dlqe output]: x_aposteriori %12.8f\t %12.8f\t %12.8f\n", (double)(x_aposteriori[0]), (double)(x_aposteriori[1]), (double)(x_aposteriori[2])); -} - -/* End of code generation (kalman_dlqe1.c) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe1.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe1.h deleted file mode 100755 index 2f5330563..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe1.h +++ /dev/null @@ -1,30 +0,0 @@ -/* - * kalman_dlqe1.h - * - * Code generation for function 'kalman_dlqe1' - * - * C source code generated on: Wed Feb 13 20:34:32 2013 - * - */ - -#ifndef __KALMAN_DLQE1_H__ -#define __KALMAN_DLQE1_H__ -/* Include files */ -#include <stddef.h> -#include <stdlib.h> - -#include "rtwtypes.h" -#include "kalman_dlqe1_types.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -extern void kalman_dlqe1(const real32_T A[9], const real32_T C[3], const real32_T K[3], const real32_T x_aposteriori_k[3], real32_T z, real32_T x_aposteriori[3]); -#endif -/* End of code generation (kalman_dlqe1.h) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe1_initialize.c b/src/modules/position_estimator_mc/codegen/kalman_dlqe1_initialize.c deleted file mode 100755 index 6627f76e9..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe1_initialize.c +++ /dev/null @@ -1,31 +0,0 @@ -/* - * kalman_dlqe1_initialize.c - * - * Code generation for function 'kalman_dlqe1_initialize' - * - * C source code generated on: Wed Feb 13 20:34:31 2013 - * - */ - -/* Include files */ -#include "rt_nonfinite.h" -#include "kalman_dlqe1.h" -#include "kalman_dlqe1_initialize.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ - -/* Function Definitions */ -void kalman_dlqe1_initialize(void) -{ - rt_InitInfAndNaN(8U); -} - -/* End of code generation (kalman_dlqe1_initialize.c) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe1_initialize.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe1_initialize.h deleted file mode 100755 index a77eb5712..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe1_initialize.h +++ /dev/null @@ -1,30 +0,0 @@ -/* - * kalman_dlqe1_initialize.h - * - * Code generation for function 'kalman_dlqe1_initialize' - * - * C source code generated on: Wed Feb 13 20:34:31 2013 - * - */ - -#ifndef __KALMAN_DLQE1_INITIALIZE_H__ -#define __KALMAN_DLQE1_INITIALIZE_H__ -/* Include files */ -#include <stddef.h> -#include <stdlib.h> - -#include "rtwtypes.h" -#include "kalman_dlqe1_types.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -extern void kalman_dlqe1_initialize(void); -#endif -/* End of code generation (kalman_dlqe1_initialize.h) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe1_terminate.c b/src/modules/position_estimator_mc/codegen/kalman_dlqe1_terminate.c deleted file mode 100755 index a65536f79..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe1_terminate.c +++ /dev/null @@ -1,31 +0,0 @@ -/* - * kalman_dlqe1_terminate.c - * - * Code generation for function 'kalman_dlqe1_terminate' - * - * C source code generated on: Wed Feb 13 20:34:31 2013 - * - */ - -/* Include files */ -#include "rt_nonfinite.h" -#include "kalman_dlqe1.h" -#include "kalman_dlqe1_terminate.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ - -/* Function Definitions */ -void kalman_dlqe1_terminate(void) -{ - /* (no terminate code required) */ -} - -/* End of code generation (kalman_dlqe1_terminate.c) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe1_terminate.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe1_terminate.h deleted file mode 100755 index 100c7f76c..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe1_terminate.h +++ /dev/null @@ -1,30 +0,0 @@ -/* - * kalman_dlqe1_terminate.h - * - * Code generation for function 'kalman_dlqe1_terminate' - * - * C source code generated on: Wed Feb 13 20:34:32 2013 - * - */ - -#ifndef __KALMAN_DLQE1_TERMINATE_H__ -#define __KALMAN_DLQE1_TERMINATE_H__ -/* Include files */ -#include <stddef.h> -#include <stdlib.h> - -#include "rtwtypes.h" -#include "kalman_dlqe1_types.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -extern void kalman_dlqe1_terminate(void); -#endif -/* End of code generation (kalman_dlqe1_terminate.h) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe1_types.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe1_types.h deleted file mode 100755 index d4b2c2d61..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe1_types.h +++ /dev/null @@ -1,16 +0,0 @@ -/* - * kalman_dlqe1_types.h - * - * Code generation for function 'kalman_dlqe1' - * - * C source code generated on: Wed Feb 13 20:34:31 2013 - * - */ - -#ifndef __KALMAN_DLQE1_TYPES_H__ -#define __KALMAN_DLQE1_TYPES_H__ - -/* Type Definitions */ - -#endif -/* End of code generation (kalman_dlqe1_types.h) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe2.c b/src/modules/position_estimator_mc/codegen/kalman_dlqe2.c deleted file mode 100755 index 11b999064..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe2.c +++ /dev/null @@ -1,119 +0,0 @@ -/* - * kalman_dlqe2.c - * - * Code generation for function 'kalman_dlqe2' - * - * C source code generated on: Thu Feb 14 12:52:28 2013 - * - */ - -/* Include files */ -#include "rt_nonfinite.h" -#include "kalman_dlqe2.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -static real32_T rt_powf_snf(real32_T u0, real32_T u1); - -/* Function Definitions */ -static real32_T rt_powf_snf(real32_T u0, real32_T u1) -{ - real32_T y; - real32_T f1; - real32_T f2; - if (rtIsNaNF(u0) || rtIsNaNF(u1)) { - y = ((real32_T)rtNaN); - } else { - f1 = (real32_T)fabs(u0); - f2 = (real32_T)fabs(u1); - if (rtIsInfF(u1)) { - if (f1 == 1.0F) { - y = ((real32_T)rtNaN); - } else if (f1 > 1.0F) { - if (u1 > 0.0F) { - y = ((real32_T)rtInf); - } else { - y = 0.0F; - } - } else if (u1 > 0.0F) { - y = 0.0F; - } else { - y = ((real32_T)rtInf); - } - } else if (f2 == 0.0F) { - y = 1.0F; - } else if (f2 == 1.0F) { - if (u1 > 0.0F) { - y = u0; - } else { - y = 1.0F / u0; - } - } else if (u1 == 2.0F) { - y = u0 * u0; - } else if ((u1 == 0.5F) && (u0 >= 0.0F)) { - y = (real32_T)sqrt(u0); - } else if ((u0 < 0.0F) && (u1 > (real32_T)floor(u1))) { - y = ((real32_T)rtNaN); - } else { - y = (real32_T)pow(u0, u1); - } - } - - return y; -} - -void kalman_dlqe2(real32_T dt, real32_T k1, real32_T k2, real32_T k3, const - real32_T x_aposteriori_k[3], real32_T z, real32_T - x_aposteriori[3]) -{ - //printf("[dqle2] dt: %12.8f\tvk1 %12.8f\tk2: %12.8f\tk3: %12.8f\n", (double)(dt), (double)(k1), (double)(k2), (double)(k3)); - //printf("[dqle2] dt: %8.4f\n", (double)(dt));//, (double)(k1), (double)(k2), (double)(k3)); - real32_T A[9]; - real32_T y; - int32_T i0; - static const int8_T iv0[3] = { 0, 0, 1 }; - - real32_T b_k1[3]; - int32_T i1; - static const int8_T iv1[3] = { 1, 0, 0 }; - - real32_T f0; - A[0] = 1.0F; - A[3] = dt; - A[6] = 0.5F * rt_powf_snf(dt, 2.0F); - A[1] = 0.0F; - A[4] = 1.0F; - A[7] = dt; - y = 0.0F; - for (i0 = 0; i0 < 3; i0++) { - A[2 + 3 * i0] = (real32_T)iv0[i0]; - b_k1[i0] = 0.0F; - for (i1 = 0; i1 < 3; i1++) { - b_k1[i0] += (real32_T)iv1[i1] * A[i1 + 3 * i0]; - } - - y += b_k1[i0] * x_aposteriori_k[i0]; - } - - y = z - y; - b_k1[0] = k1; - b_k1[1] = k2; - b_k1[2] = k3; - for (i0 = 0; i0 < 3; i0++) { - f0 = 0.0F; - for (i1 = 0; i1 < 3; i1++) { - f0 += A[i0 + 3 * i1] * x_aposteriori_k[i1]; - } - - x_aposteriori[i0] = f0 + b_k1[i0] * y; - } -} - -/* End of code generation (kalman_dlqe2.c) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe2.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe2.h deleted file mode 100755 index 30170ae22..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe2.h +++ /dev/null @@ -1,32 +0,0 @@ -/* - * kalman_dlqe2.h - * - * Code generation for function 'kalman_dlqe2' - * - * C source code generated on: Thu Feb 14 12:52:29 2013 - * - */ - -#ifndef __KALMAN_DLQE2_H__ -#define __KALMAN_DLQE2_H__ -/* Include files */ -#include <math.h> -#include <stddef.h> -#include <stdlib.h> -#include "rt_nonfinite.h" - -#include "rtwtypes.h" -#include "kalman_dlqe2_types.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -extern void kalman_dlqe2(real32_T dt, real32_T k1, real32_T k2, real32_T k3, const real32_T x_aposteriori_k[3], real32_T z, real32_T x_aposteriori[3]); -#endif -/* End of code generation (kalman_dlqe2.h) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe2_initialize.c b/src/modules/position_estimator_mc/codegen/kalman_dlqe2_initialize.c deleted file mode 100755 index de5a1d8aa..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe2_initialize.c +++ /dev/null @@ -1,31 +0,0 @@ -/* - * kalman_dlqe2_initialize.c - * - * Code generation for function 'kalman_dlqe2_initialize' - * - * C source code generated on: Thu Feb 14 12:52:28 2013 - * - */ - -/* Include files */ -#include "rt_nonfinite.h" -#include "kalman_dlqe2.h" -#include "kalman_dlqe2_initialize.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ - -/* Function Definitions */ -void kalman_dlqe2_initialize(void) -{ - rt_InitInfAndNaN(8U); -} - -/* End of code generation (kalman_dlqe2_initialize.c) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe2_initialize.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe2_initialize.h deleted file mode 100755 index 3d507ff31..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe2_initialize.h +++ /dev/null @@ -1,32 +0,0 @@ -/* - * kalman_dlqe2_initialize.h - * - * Code generation for function 'kalman_dlqe2_initialize' - * - * C source code generated on: Thu Feb 14 12:52:28 2013 - * - */ - -#ifndef __KALMAN_DLQE2_INITIALIZE_H__ -#define __KALMAN_DLQE2_INITIALIZE_H__ -/* Include files */ -#include <math.h> -#include <stddef.h> -#include <stdlib.h> -#include "rt_nonfinite.h" - -#include "rtwtypes.h" -#include "kalman_dlqe2_types.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -extern void kalman_dlqe2_initialize(void); -#endif -/* End of code generation (kalman_dlqe2_initialize.h) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe2_terminate.c b/src/modules/position_estimator_mc/codegen/kalman_dlqe2_terminate.c deleted file mode 100755 index 0757c878c..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe2_terminate.c +++ /dev/null @@ -1,31 +0,0 @@ -/* - * kalman_dlqe2_terminate.c - * - * Code generation for function 'kalman_dlqe2_terminate' - * - * C source code generated on: Thu Feb 14 12:52:28 2013 - * - */ - -/* Include files */ -#include "rt_nonfinite.h" -#include "kalman_dlqe2.h" -#include "kalman_dlqe2_terminate.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ - -/* Function Definitions */ -void kalman_dlqe2_terminate(void) -{ - /* (no terminate code required) */ -} - -/* End of code generation (kalman_dlqe2_terminate.c) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe2_terminate.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe2_terminate.h deleted file mode 100755 index 23995020b..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe2_terminate.h +++ /dev/null @@ -1,32 +0,0 @@ -/* - * kalman_dlqe2_terminate.h - * - * Code generation for function 'kalman_dlqe2_terminate' - * - * C source code generated on: Thu Feb 14 12:52:28 2013 - * - */ - -#ifndef __KALMAN_DLQE2_TERMINATE_H__ -#define __KALMAN_DLQE2_TERMINATE_H__ -/* Include files */ -#include <math.h> -#include <stddef.h> -#include <stdlib.h> -#include "rt_nonfinite.h" - -#include "rtwtypes.h" -#include "kalman_dlqe2_types.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -extern void kalman_dlqe2_terminate(void); -#endif -/* End of code generation (kalman_dlqe2_terminate.h) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe2_types.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe2_types.h deleted file mode 100755 index f7a04d908..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe2_types.h +++ /dev/null @@ -1,16 +0,0 @@ -/* - * kalman_dlqe2_types.h - * - * Code generation for function 'kalman_dlqe2' - * - * C source code generated on: Thu Feb 14 12:52:28 2013 - * - */ - -#ifndef __KALMAN_DLQE2_TYPES_H__ -#define __KALMAN_DLQE2_TYPES_H__ - -/* Type Definitions */ - -#endif -/* End of code generation (kalman_dlqe2_types.h) */ diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe3.c b/src/modules/position_estimator_mc/codegen/kalman_dlqe3.c deleted file mode 100755 index 9efe2ea7a..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe3.c +++ /dev/null @@ -1,137 +0,0 @@ -/*
- * kalman_dlqe3.c
- *
- * Code generation for function 'kalman_dlqe3'
- *
- * C source code generated on: Tue Feb 19 15:26:31 2013
- *
- */
-
-/* Include files */
-#include "rt_nonfinite.h"
-#include "kalman_dlqe3.h"
-#include "randn.h"
-
-/* Type Definitions */
-
-/* Named Constants */
-
-/* Variable Declarations */
-
-/* Variable Definitions */
-
-/* Function Declarations */
-static real32_T rt_powf_snf(real32_T u0, real32_T u1);
-
-/* Function Definitions */
-static real32_T rt_powf_snf(real32_T u0, real32_T u1)
-{
- real32_T y;
- real32_T f1;
- real32_T f2;
- if (rtIsNaNF(u0) || rtIsNaNF(u1)) {
- y = ((real32_T)rtNaN);
- } else {
- f1 = (real32_T)fabs(u0);
- f2 = (real32_T)fabs(u1);
- if (rtIsInfF(u1)) {
- if (f1 == 1.0F) {
- y = ((real32_T)rtNaN);
- } else if (f1 > 1.0F) {
- if (u1 > 0.0F) {
- y = ((real32_T)rtInf);
- } else {
- y = 0.0F;
- }
- } else if (u1 > 0.0F) {
- y = 0.0F;
- } else {
- y = ((real32_T)rtInf);
- }
- } else if (f2 == 0.0F) {
- y = 1.0F;
- } else if (f2 == 1.0F) {
- if (u1 > 0.0F) {
- y = u0;
- } else {
- y = 1.0F / u0;
- }
- } else if (u1 == 2.0F) {
- y = u0 * u0;
- } else if ((u1 == 0.5F) && (u0 >= 0.0F)) {
- y = (real32_T)sqrt(u0);
- } else if ((u0 < 0.0F) && (u1 > (real32_T)floor(u1))) {
- y = ((real32_T)rtNaN);
- } else {
- y = (real32_T)pow(u0, u1);
- }
- }
-
- return y;
-}
-
-void kalman_dlqe3(real32_T dt, real32_T k1, real32_T k2, real32_T k3, const
- real32_T x_aposteriori_k[3], real32_T z, real32_T posUpdate,
- real32_T addNoise, real32_T sigma, real32_T x_aposteriori[3])
-{
- real32_T A[9];
- int32_T i0;
- static const int8_T iv0[3] = { 0, 0, 1 };
-
- real_T b;
- real32_T y;
- real32_T b_y[3];
- int32_T i1;
- static const int8_T iv1[3] = { 1, 0, 0 };
-
- real32_T b_k1[3];
- real32_T f0;
- A[0] = 1.0F;
- A[3] = dt;
- A[6] = 0.5F * rt_powf_snf(dt, 2.0F);
- A[1] = 0.0F;
- A[4] = 1.0F;
- A[7] = dt;
- for (i0 = 0; i0 < 3; i0++) {
- A[2 + 3 * i0] = (real32_T)iv0[i0];
- }
-
- if (addNoise == 1.0F) {
- b = randn();
- z += sigma * (real32_T)b;
- }
-
- if (posUpdate != 0.0F) {
- y = 0.0F;
- for (i0 = 0; i0 < 3; i0++) {
- b_y[i0] = 0.0F;
- for (i1 = 0; i1 < 3; i1++) {
- b_y[i0] += (real32_T)iv1[i1] * A[i1 + 3 * i0];
- }
-
- y += b_y[i0] * x_aposteriori_k[i0];
- }
-
- y = z - y;
- b_k1[0] = k1;
- b_k1[1] = k2;
- b_k1[2] = k3;
- for (i0 = 0; i0 < 3; i0++) {
- f0 = 0.0F;
- for (i1 = 0; i1 < 3; i1++) {
- f0 += A[i0 + 3 * i1] * x_aposteriori_k[i1];
- }
-
- x_aposteriori[i0] = f0 + b_k1[i0] * y;
- }
- } else {
- for (i0 = 0; i0 < 3; i0++) {
- x_aposteriori[i0] = 0.0F;
- for (i1 = 0; i1 < 3; i1++) {
- x_aposteriori[i0] += A[i0 + 3 * i1] * x_aposteriori_k[i1];
- }
- }
- }
-}
-
-/* End of code generation (kalman_dlqe3.c) */
diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe3.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe3.h deleted file mode 100755 index 9bbffbbb3..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe3.h +++ /dev/null @@ -1,33 +0,0 @@ -/*
- * kalman_dlqe3.h
- *
- * Code generation for function 'kalman_dlqe3'
- *
- * C source code generated on: Tue Feb 19 15:26:32 2013
- *
- */
-
-#ifndef __KALMAN_DLQE3_H__
-#define __KALMAN_DLQE3_H__
-/* Include files */
-#include <math.h>
-#include <stddef.h>
-#include <stdlib.h>
-#include <string.h>
-#include "rt_nonfinite.h"
-
-#include "rtwtypes.h"
-#include "kalman_dlqe3_types.h"
-
-/* Type Definitions */
-
-/* Named Constants */
-
-/* Variable Declarations */
-
-/* Variable Definitions */
-
-/* Function Declarations */
-extern void kalman_dlqe3(real32_T dt, real32_T k1, real32_T k2, real32_T k3, const real32_T x_aposteriori_k[3], real32_T z, real32_T posUpdate, real32_T addNoise, real32_T sigma, real32_T x_aposteriori[3]);
-#endif
-/* End of code generation (kalman_dlqe3.h) */
diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_data.c b/src/modules/position_estimator_mc/codegen/kalman_dlqe3_data.c deleted file mode 100755 index 8f2275c13..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_data.c +++ /dev/null @@ -1,32 +0,0 @@ -/*
- * kalman_dlqe3_data.c
- *
- * Code generation for function 'kalman_dlqe3_data'
- *
- * C source code generated on: Tue Feb 19 15:26:31 2013
- *
- */
-
-/* Include files */
-#include "rt_nonfinite.h"
-#include "kalman_dlqe3.h"
-#include "kalman_dlqe3_data.h"
-
-/* Type Definitions */
-
-/* Named Constants */
-
-/* Variable Declarations */
-
-/* Variable Definitions */
-uint32_T method;
-uint32_T state[2];
-uint32_T b_method;
-uint32_T b_state;
-uint32_T c_state[2];
-boolean_T state_not_empty;
-
-/* Function Declarations */
-
-/* Function Definitions */
-/* End of code generation (kalman_dlqe3_data.c) */
diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_data.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe3_data.h deleted file mode 100755 index 952eb7b89..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_data.h +++ /dev/null @@ -1,38 +0,0 @@ -/*
- * kalman_dlqe3_data.h
- *
- * Code generation for function 'kalman_dlqe3_data'
- *
- * C source code generated on: Tue Feb 19 15:26:31 2013
- *
- */
-
-#ifndef __KALMAN_DLQE3_DATA_H__
-#define __KALMAN_DLQE3_DATA_H__
-/* Include files */
-#include <math.h>
-#include <stddef.h>
-#include <stdlib.h>
-#include <string.h>
-#include "rt_nonfinite.h"
-
-#include "rtwtypes.h"
-#include "kalman_dlqe3_types.h"
-
-/* Type Definitions */
-
-/* Named Constants */
-
-/* Variable Declarations */
-extern uint32_T method;
-extern uint32_T state[2];
-extern uint32_T b_method;
-extern uint32_T b_state;
-extern uint32_T c_state[2];
-extern boolean_T state_not_empty;
-
-/* Variable Definitions */
-
-/* Function Declarations */
-#endif
-/* End of code generation (kalman_dlqe3_data.h) */
diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_initialize.c b/src/modules/position_estimator_mc/codegen/kalman_dlqe3_initialize.c deleted file mode 100755 index b87d604c4..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_initialize.c +++ /dev/null @@ -1,47 +0,0 @@ -/*
- * kalman_dlqe3_initialize.c
- *
- * Code generation for function 'kalman_dlqe3_initialize'
- *
- * C source code generated on: Tue Feb 19 15:26:31 2013
- *
- */
-
-/* Include files */
-#include "rt_nonfinite.h"
-#include "kalman_dlqe3.h"
-#include "kalman_dlqe3_initialize.h"
-#include "kalman_dlqe3_data.h"
-
-/* Type Definitions */
-
-/* Named Constants */
-
-/* Variable Declarations */
-
-/* Variable Definitions */
-
-/* Function Declarations */
-
-/* Function Definitions */
-void kalman_dlqe3_initialize(void)
-{
- int32_T i;
- static const uint32_T uv0[2] = { 362436069U, 0U };
-
- rt_InitInfAndNaN(8U);
- state_not_empty = FALSE;
- b_state = 1144108930U;
- b_method = 7U;
- method = 0U;
- for (i = 0; i < 2; i++) {
- c_state[i] = 362436069U + 158852560U * (uint32_T)i;
- state[i] = uv0[i];
- }
-
- if (state[1] == 0U) {
- state[1] = 521288629U;
- }
-}
-
-/* End of code generation (kalman_dlqe3_initialize.c) */
diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_initialize.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe3_initialize.h deleted file mode 100755 index 9dee90f9e..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_initialize.h +++ /dev/null @@ -1,33 +0,0 @@ -/*
- * kalman_dlqe3_initialize.h
- *
- * Code generation for function 'kalman_dlqe3_initialize'
- *
- * C source code generated on: Tue Feb 19 15:26:31 2013
- *
- */
-
-#ifndef __KALMAN_DLQE3_INITIALIZE_H__
-#define __KALMAN_DLQE3_INITIALIZE_H__
-/* Include files */
-#include <math.h>
-#include <stddef.h>
-#include <stdlib.h>
-#include <string.h>
-#include "rt_nonfinite.h"
-
-#include "rtwtypes.h"
-#include "kalman_dlqe3_types.h"
-
-/* Type Definitions */
-
-/* Named Constants */
-
-/* Variable Declarations */
-
-/* Variable Definitions */
-
-/* Function Declarations */
-extern void kalman_dlqe3_initialize(void);
-#endif
-/* End of code generation (kalman_dlqe3_initialize.h) */
diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_terminate.c b/src/modules/position_estimator_mc/codegen/kalman_dlqe3_terminate.c deleted file mode 100755 index b00858205..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_terminate.c +++ /dev/null @@ -1,31 +0,0 @@ -/*
- * kalman_dlqe3_terminate.c
- *
- * Code generation for function 'kalman_dlqe3_terminate'
- *
- * C source code generated on: Tue Feb 19 15:26:31 2013
- *
- */
-
-/* Include files */
-#include "rt_nonfinite.h"
-#include "kalman_dlqe3.h"
-#include "kalman_dlqe3_terminate.h"
-
-/* Type Definitions */
-
-/* Named Constants */
-
-/* Variable Declarations */
-
-/* Variable Definitions */
-
-/* Function Declarations */
-
-/* Function Definitions */
-void kalman_dlqe3_terminate(void)
-{
- /* (no terminate code required) */
-}
-
-/* End of code generation (kalman_dlqe3_terminate.c) */
diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_terminate.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe3_terminate.h deleted file mode 100755 index 69cc85c76..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_terminate.h +++ /dev/null @@ -1,33 +0,0 @@ -/*
- * kalman_dlqe3_terminate.h
- *
- * Code generation for function 'kalman_dlqe3_terminate'
- *
- * C source code generated on: Tue Feb 19 15:26:31 2013
- *
- */
-
-#ifndef __KALMAN_DLQE3_TERMINATE_H__
-#define __KALMAN_DLQE3_TERMINATE_H__
-/* Include files */
-#include <math.h>
-#include <stddef.h>
-#include <stdlib.h>
-#include <string.h>
-#include "rt_nonfinite.h"
-
-#include "rtwtypes.h"
-#include "kalman_dlqe3_types.h"
-
-/* Type Definitions */
-
-/* Named Constants */
-
-/* Variable Declarations */
-
-/* Variable Definitions */
-
-/* Function Declarations */
-extern void kalman_dlqe3_terminate(void);
-#endif
-/* End of code generation (kalman_dlqe3_terminate.h) */
diff --git a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_types.h b/src/modules/position_estimator_mc/codegen/kalman_dlqe3_types.h deleted file mode 100755 index f36ea4557..000000000 --- a/src/modules/position_estimator_mc/codegen/kalman_dlqe3_types.h +++ /dev/null @@ -1,16 +0,0 @@ -/*
- * kalman_dlqe3_types.h
- *
- * Code generation for function 'kalman_dlqe3'
- *
- * C source code generated on: Tue Feb 19 15:26:30 2013
- *
- */
-
-#ifndef __KALMAN_DLQE3_TYPES_H__
-#define __KALMAN_DLQE3_TYPES_H__
-
-/* Type Definitions */
-
-#endif
-/* End of code generation (kalman_dlqe3_types.h) */
diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D.c b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D.c deleted file mode 100755 index 5139848bc..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D.c +++ /dev/null @@ -1,136 +0,0 @@ -/* - * positionKalmanFilter1D.c - * - * Code generation for function 'positionKalmanFilter1D' - * - * C source code generated on: Fri Nov 30 14:26:11 2012 - * - */ - -/* Include files */ -#include "rt_nonfinite.h" -#include "positionKalmanFilter1D.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ - -/* Function Definitions */ -void positionKalmanFilter1D(const real32_T A[9], const real32_T B[3], const - real32_T C[3], const real32_T x_aposteriori_k[3], const real32_T - P_aposteriori_k[9], real32_T u, real32_T z, uint8_T gps_update, const real32_T - Q[9], real32_T R, real32_T thresh, real32_T decay, real32_T x_aposteriori[3], - real32_T P_aposteriori[9]) -{ - int32_T i0; - real32_T f0; - int32_T k; - real32_T b_A[9]; - int32_T i1; - real32_T P_apriori[9]; - real32_T y; - real32_T K[3]; - real32_T S; - int8_T I[9]; - - /* prediction */ - for (i0 = 0; i0 < 3; i0++) { - f0 = 0.0F; - for (k = 0; k < 3; k++) { - f0 += A[i0 + 3 * k] * x_aposteriori_k[k]; - } - - x_aposteriori[i0] = f0 + B[i0] * u; - } - - for (i0 = 0; i0 < 3; i0++) { - for (k = 0; k < 3; k++) { - b_A[i0 + 3 * k] = 0.0F; - for (i1 = 0; i1 < 3; i1++) { - b_A[i0 + 3 * k] += A[i0 + 3 * i1] * P_aposteriori_k[i1 + 3 * k]; - } - } - } - - for (i0 = 0; i0 < 3; i0++) { - for (k = 0; k < 3; k++) { - f0 = 0.0F; - for (i1 = 0; i1 < 3; i1++) { - f0 += b_A[i0 + 3 * i1] * A[k + 3 * i1]; - } - - P_apriori[i0 + 3 * k] = f0 + Q[i0 + 3 * k]; - } - } - - if ((real32_T)fabs(u) < thresh) { - x_aposteriori[1] *= decay; - } - - /* update */ - if (gps_update == 1) { - y = 0.0F; - for (k = 0; k < 3; k++) { - y += C[k] * x_aposteriori[k]; - K[k] = 0.0F; - for (i0 = 0; i0 < 3; i0++) { - K[k] += C[i0] * P_apriori[i0 + 3 * k]; - } - } - - y = z - y; - S = 0.0F; - for (k = 0; k < 3; k++) { - S += K[k] * C[k]; - } - - S += R; - for (i0 = 0; i0 < 3; i0++) { - f0 = 0.0F; - for (k = 0; k < 3; k++) { - f0 += P_apriori[i0 + 3 * k] * C[k]; - } - - K[i0] = f0 / S; - } - - for (i0 = 0; i0 < 3; i0++) { - x_aposteriori[i0] += K[i0] * y; - } - - for (i0 = 0; i0 < 9; i0++) { - I[i0] = 0; - } - - for (k = 0; k < 3; k++) { - I[k + 3 * k] = 1; - } - - for (i0 = 0; i0 < 3; i0++) { - for (k = 0; k < 3; k++) { - b_A[k + 3 * i0] = (real32_T)I[k + 3 * i0] - K[k] * C[i0]; - } - } - - for (i0 = 0; i0 < 3; i0++) { - for (k = 0; k < 3; k++) { - P_aposteriori[i0 + 3 * k] = 0.0F; - for (i1 = 0; i1 < 3; i1++) { - P_aposteriori[i0 + 3 * k] += b_A[i0 + 3 * i1] * P_apriori[i1 + 3 * k]; - } - } - } - } else { - for (i0 = 0; i0 < 9; i0++) { - P_aposteriori[i0] = P_apriori[i0]; - } - } -} - -/* End of code generation (positionKalmanFilter1D.c) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D.h b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D.h deleted file mode 100755 index 205c8eb4e..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D.h +++ /dev/null @@ -1,31 +0,0 @@ -/* - * positionKalmanFilter1D.h - * - * Code generation for function 'positionKalmanFilter1D' - * - * C source code generated on: Fri Nov 30 14:26:11 2012 - * - */ - -#ifndef __POSITIONKALMANFILTER1D_H__ -#define __POSITIONKALMANFILTER1D_H__ -/* Include files */ -#include <math.h> -#include <stddef.h> -#include <stdlib.h> - -#include "rtwtypes.h" -#include "positionKalmanFilter1D_types.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -extern void positionKalmanFilter1D(const real32_T A[9], const real32_T B[3], const real32_T C[3], const real32_T x_aposteriori_k[3], const real32_T P_aposteriori_k[9], real32_T u, real32_T z, uint8_T gps_update, const real32_T Q[9], real32_T R, real32_T thresh, real32_T decay, real32_T x_aposteriori[3], real32_T P_aposteriori[9]); -#endif -/* End of code generation (positionKalmanFilter1D.h) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT.c b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT.c deleted file mode 100755 index 4c535618a..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT.c +++ /dev/null @@ -1,157 +0,0 @@ -/* - * positionKalmanFilter1D_dT.c - * - * Code generation for function 'positionKalmanFilter1D_dT' - * - * C source code generated on: Fri Nov 30 17:37:33 2012 - * - */ - -/* Include files */ -#include "rt_nonfinite.h" -#include "positionKalmanFilter1D_dT.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ - -/* Function Definitions */ -void positionKalmanFilter1D_dT(real32_T dT, const real32_T x_aposteriori_k[3], - const real32_T P_aposteriori_k[9], real32_T u, real32_T z, uint8_T gps_update, - const real32_T Q[9], real_T R, real32_T thresh, real32_T decay, real32_T - x_aposteriori[3], real32_T P_aposteriori[9]) -{ - real32_T A[9]; - int32_T i; - static const int8_T iv0[3] = { 0, 0, 1 }; - - real32_T K[3]; - real32_T f0; - int32_T i0; - real32_T b_A[9]; - int32_T i1; - real32_T P_apriori[9]; - static const int8_T iv1[3] = { 1, 0, 0 }; - - real32_T fv0[3]; - real32_T y; - static const int8_T iv2[3] = { 1, 0, 0 }; - - real32_T S; - int8_T I[9]; - - /* dynamics */ - A[0] = 1.0F; - A[3] = dT; - A[6] = -0.5F * dT * dT; - A[1] = 0.0F; - A[4] = 1.0F; - A[7] = -dT; - for (i = 0; i < 3; i++) { - A[2 + 3 * i] = (real32_T)iv0[i]; - } - - /* prediction */ - K[0] = 0.5F * dT * dT; - K[1] = dT; - K[2] = 0.0F; - for (i = 0; i < 3; i++) { - f0 = 0.0F; - for (i0 = 0; i0 < 3; i0++) { - f0 += A[i + 3 * i0] * x_aposteriori_k[i0]; - } - - x_aposteriori[i] = f0 + K[i] * u; - } - - for (i = 0; i < 3; i++) { - for (i0 = 0; i0 < 3; i0++) { - b_A[i + 3 * i0] = 0.0F; - for (i1 = 0; i1 < 3; i1++) { - b_A[i + 3 * i0] += A[i + 3 * i1] * P_aposteriori_k[i1 + 3 * i0]; - } - } - } - - for (i = 0; i < 3; i++) { - for (i0 = 0; i0 < 3; i0++) { - f0 = 0.0F; - for (i1 = 0; i1 < 3; i1++) { - f0 += b_A[i + 3 * i1] * A[i0 + 3 * i1]; - } - - P_apriori[i + 3 * i0] = f0 + Q[i + 3 * i0]; - } - } - - if ((real32_T)fabs(u) < thresh) { - x_aposteriori[1] *= decay; - } - - /* update */ - if (gps_update == 1) { - f0 = 0.0F; - for (i = 0; i < 3; i++) { - f0 += (real32_T)iv1[i] * x_aposteriori[i]; - fv0[i] = 0.0F; - for (i0 = 0; i0 < 3; i0++) { - fv0[i] += (real32_T)iv1[i0] * P_apriori[i0 + 3 * i]; - } - } - - y = z - f0; - f0 = 0.0F; - for (i = 0; i < 3; i++) { - f0 += fv0[i] * (real32_T)iv2[i]; - } - - S = f0 + (real32_T)R; - for (i = 0; i < 3; i++) { - f0 = 0.0F; - for (i0 = 0; i0 < 3; i0++) { - f0 += P_apriori[i + 3 * i0] * (real32_T)iv2[i0]; - } - - K[i] = f0 / S; - } - - for (i = 0; i < 3; i++) { - x_aposteriori[i] += K[i] * y; - } - - for (i = 0; i < 9; i++) { - I[i] = 0; - } - - for (i = 0; i < 3; i++) { - I[i + 3 * i] = 1; - } - - for (i = 0; i < 3; i++) { - for (i0 = 0; i0 < 3; i0++) { - A[i0 + 3 * i] = (real32_T)I[i0 + 3 * i] - K[i0] * (real32_T)iv1[i]; - } - } - - for (i = 0; i < 3; i++) { - for (i0 = 0; i0 < 3; i0++) { - P_aposteriori[i + 3 * i0] = 0.0F; - for (i1 = 0; i1 < 3; i1++) { - P_aposteriori[i + 3 * i0] += A[i + 3 * i1] * P_apriori[i1 + 3 * i0]; - } - } - } - } else { - for (i = 0; i < 9; i++) { - P_aposteriori[i] = P_apriori[i]; - } - } -} - -/* End of code generation (positionKalmanFilter1D_dT.c) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT.h b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT.h deleted file mode 100755 index 94cbe2ce6..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT.h +++ /dev/null @@ -1,31 +0,0 @@ -/* - * positionKalmanFilter1D_dT.h - * - * Code generation for function 'positionKalmanFilter1D_dT' - * - * C source code generated on: Fri Nov 30 17:37:33 2012 - * - */ - -#ifndef __POSITIONKALMANFILTER1D_DT_H__ -#define __POSITIONKALMANFILTER1D_DT_H__ -/* Include files */ -#include <math.h> -#include <stddef.h> -#include <stdlib.h> - -#include "rtwtypes.h" -#include "positionKalmanFilter1D_dT_types.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -extern void positionKalmanFilter1D_dT(real32_T dT, const real32_T x_aposteriori_k[3], const real32_T P_aposteriori_k[9], real32_T u, real32_T z, uint8_T gps_update, const real32_T Q[9], real_T R, real32_T thresh, real32_T decay, real32_T x_aposteriori[3], real32_T P_aposteriori[9]); -#endif -/* End of code generation (positionKalmanFilter1D_dT.h) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_initialize.c b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_initialize.c deleted file mode 100755 index aa89f8a9d..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_initialize.c +++ /dev/null @@ -1,31 +0,0 @@ -/* - * positionKalmanFilter1D_dT_initialize.c - * - * Code generation for function 'positionKalmanFilter1D_dT_initialize' - * - * C source code generated on: Fri Nov 30 17:37:33 2012 - * - */ - -/* Include files */ -#include "rt_nonfinite.h" -#include "positionKalmanFilter1D_dT.h" -#include "positionKalmanFilter1D_dT_initialize.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ - -/* Function Definitions */ -void positionKalmanFilter1D_dT_initialize(void) -{ - rt_InitInfAndNaN(8U); -} - -/* End of code generation (positionKalmanFilter1D_dT_initialize.c) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_initialize.h b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_initialize.h deleted file mode 100755 index 8d358a9a3..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_initialize.h +++ /dev/null @@ -1,31 +0,0 @@ -/* - * positionKalmanFilter1D_dT_initialize.h - * - * Code generation for function 'positionKalmanFilter1D_dT_initialize' - * - * C source code generated on: Fri Nov 30 17:37:33 2012 - * - */ - -#ifndef __POSITIONKALMANFILTER1D_DT_INITIALIZE_H__ -#define __POSITIONKALMANFILTER1D_DT_INITIALIZE_H__ -/* Include files */ -#include <math.h> -#include <stddef.h> -#include <stdlib.h> - -#include "rtwtypes.h" -#include "positionKalmanFilter1D_dT_types.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -extern void positionKalmanFilter1D_dT_initialize(void); -#endif -/* End of code generation (positionKalmanFilter1D_dT_initialize.h) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_terminate.c b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_terminate.c deleted file mode 100755 index 20ed2edbb..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_terminate.c +++ /dev/null @@ -1,31 +0,0 @@ -/* - * positionKalmanFilter1D_dT_terminate.c - * - * Code generation for function 'positionKalmanFilter1D_dT_terminate' - * - * C source code generated on: Fri Nov 30 17:37:33 2012 - * - */ - -/* Include files */ -#include "rt_nonfinite.h" -#include "positionKalmanFilter1D_dT.h" -#include "positionKalmanFilter1D_dT_terminate.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ - -/* Function Definitions */ -void positionKalmanFilter1D_dT_terminate(void) -{ - /* (no terminate code required) */ -} - -/* End of code generation (positionKalmanFilter1D_dT_terminate.c) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_terminate.h b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_terminate.h deleted file mode 100755 index 5eb5807a0..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_terminate.h +++ /dev/null @@ -1,31 +0,0 @@ -/* - * positionKalmanFilter1D_dT_terminate.h - * - * Code generation for function 'positionKalmanFilter1D_dT_terminate' - * - * C source code generated on: Fri Nov 30 17:37:33 2012 - * - */ - -#ifndef __POSITIONKALMANFILTER1D_DT_TERMINATE_H__ -#define __POSITIONKALMANFILTER1D_DT_TERMINATE_H__ -/* Include files */ -#include <math.h> -#include <stddef.h> -#include <stdlib.h> - -#include "rtwtypes.h" -#include "positionKalmanFilter1D_dT_types.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -extern void positionKalmanFilter1D_dT_terminate(void); -#endif -/* End of code generation (positionKalmanFilter1D_dT_terminate.h) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_types.h b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_types.h deleted file mode 100755 index 43e5f016c..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_dT_types.h +++ /dev/null @@ -1,16 +0,0 @@ -/* - * positionKalmanFilter1D_dT_types.h - * - * Code generation for function 'positionKalmanFilter1D_dT' - * - * C source code generated on: Fri Nov 30 17:37:33 2012 - * - */ - -#ifndef __POSITIONKALMANFILTER1D_DT_TYPES_H__ -#define __POSITIONKALMANFILTER1D_DT_TYPES_H__ - -/* Type Definitions */ - -#endif -/* End of code generation (positionKalmanFilter1D_dT_types.h) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_initialize.c b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_initialize.c deleted file mode 100755 index 5bd87c390..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_initialize.c +++ /dev/null @@ -1,31 +0,0 @@ -/* - * positionKalmanFilter1D_initialize.c - * - * Code generation for function 'positionKalmanFilter1D_initialize' - * - * C source code generated on: Fri Nov 30 14:26:11 2012 - * - */ - -/* Include files */ -#include "rt_nonfinite.h" -#include "positionKalmanFilter1D.h" -#include "positionKalmanFilter1D_initialize.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ - -/* Function Definitions */ -void positionKalmanFilter1D_initialize(void) -{ - rt_InitInfAndNaN(8U); -} - -/* End of code generation (positionKalmanFilter1D_initialize.c) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_initialize.h b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_initialize.h deleted file mode 100755 index 44bce472f..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_initialize.h +++ /dev/null @@ -1,31 +0,0 @@ -/* - * positionKalmanFilter1D_initialize.h - * - * Code generation for function 'positionKalmanFilter1D_initialize' - * - * C source code generated on: Fri Nov 30 14:26:11 2012 - * - */ - -#ifndef __POSITIONKALMANFILTER1D_INITIALIZE_H__ -#define __POSITIONKALMANFILTER1D_INITIALIZE_H__ -/* Include files */ -#include <math.h> -#include <stddef.h> -#include <stdlib.h> - -#include "rtwtypes.h" -#include "positionKalmanFilter1D_types.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -extern void positionKalmanFilter1D_initialize(void); -#endif -/* End of code generation (positionKalmanFilter1D_initialize.h) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_terminate.c b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_terminate.c deleted file mode 100755 index 41e11936f..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_terminate.c +++ /dev/null @@ -1,31 +0,0 @@ -/* - * positionKalmanFilter1D_terminate.c - * - * Code generation for function 'positionKalmanFilter1D_terminate' - * - * C source code generated on: Fri Nov 30 14:26:11 2012 - * - */ - -/* Include files */ -#include "rt_nonfinite.h" -#include "positionKalmanFilter1D.h" -#include "positionKalmanFilter1D_terminate.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ - -/* Function Definitions */ -void positionKalmanFilter1D_terminate(void) -{ - /* (no terminate code required) */ -} - -/* End of code generation (positionKalmanFilter1D_terminate.c) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_terminate.h b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_terminate.h deleted file mode 100755 index e84ea01bc..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_terminate.h +++ /dev/null @@ -1,31 +0,0 @@ -/* - * positionKalmanFilter1D_terminate.h - * - * Code generation for function 'positionKalmanFilter1D_terminate' - * - * C source code generated on: Fri Nov 30 14:26:11 2012 - * - */ - -#ifndef __POSITIONKALMANFILTER1D_TERMINATE_H__ -#define __POSITIONKALMANFILTER1D_TERMINATE_H__ -/* Include files */ -#include <math.h> -#include <stddef.h> -#include <stdlib.h> - -#include "rtwtypes.h" -#include "positionKalmanFilter1D_types.h" - -/* Type Definitions */ - -/* Named Constants */ - -/* Variable Declarations */ - -/* Variable Definitions */ - -/* Function Declarations */ -extern void positionKalmanFilter1D_terminate(void); -#endif -/* End of code generation (positionKalmanFilter1D_terminate.h) */ diff --git a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_types.h b/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_types.h deleted file mode 100755 index 4b473f56f..000000000 --- a/src/modules/position_estimator_mc/codegen/positionKalmanFilter1D_types.h +++ /dev/null @@ -1,16 +0,0 @@ -/* - * positionKalmanFilter1D_types.h - * - * Code generation for function 'positionKalmanFilter1D' - * - * C source code generated on: Fri Nov 30 14:26:11 2012 - * - */ - -#ifndef __POSITIONKALMANFILTER1D_TYPES_H__ -#define __POSITIONKALMANFILTER1D_TYPES_H__ - -/* Type Definitions */ - -#endif -/* End of code generation (positionKalmanFilter1D_types.h) */ diff --git a/src/modules/position_estimator_mc/codegen/randn.c b/src/modules/position_estimator_mc/codegen/randn.c deleted file mode 100755 index 51aef7b76..000000000 --- a/src/modules/position_estimator_mc/codegen/randn.c +++ /dev/null @@ -1,524 +0,0 @@ -/*
- * randn.c
- *
- * Code generation for function 'randn'
- *
- * C source code generated on: Tue Feb 19 15:26:32 2013
- *
- */
-
-/* Include files */
-#include "rt_nonfinite.h"
-#include "kalman_dlqe3.h"
-#include "randn.h"
-#include "kalman_dlqe3_data.h"
-
-/* Type Definitions */
-
-/* Named Constants */
-
-/* Variable Declarations */
-
-/* Variable Definitions */
-static uint32_T d_state[625];
-
-/* Function Declarations */
-static real_T b_genrandu(uint32_T mt[625]);
-static real_T eml_rand_mt19937ar(uint32_T e_state[625]);
-static real_T eml_rand_shr3cong(uint32_T e_state[2]);
-static void genrand_uint32_vector(uint32_T mt[625], uint32_T u[2]);
-static void genrandu(uint32_T s, uint32_T *e_state, real_T *r);
-static void twister_state_vector(uint32_T mt[625], real_T seed);
-
-/* Function Definitions */
-static real_T b_genrandu(uint32_T mt[625])
-{
- real_T r;
- int32_T exitg1;
- uint32_T u[2];
- boolean_T isvalid;
- int32_T k;
- boolean_T exitg2;
-
- /* <LEGAL> This is a uniform (0,1) pseudorandom number generator based on: */
- /* <LEGAL> */
- /* <LEGAL> A C-program for MT19937, with initialization improved 2002/1/26. */
- /* <LEGAL> Coded by Takuji Nishimura and Makoto Matsumoto. */
- /* <LEGAL> */
- /* <LEGAL> Copyright (C) 1997 - 2002, Makoto Matsumoto and Takuji Nishimura, */
- /* <LEGAL> All rights reserved. */
- /* <LEGAL> */
- /* <LEGAL> Redistribution and use in source and binary forms, with or without */
- /* <LEGAL> modification, are permitted provided that the following conditions */
- /* <LEGAL> are met: */
- /* <LEGAL> */
- /* <LEGAL> 1. Redistributions of source code must retain the above copyright */
- /* <LEGAL> notice, this list of conditions and the following disclaimer. */
- /* <LEGAL> */
- /* <LEGAL> 2. Redistributions in binary form must reproduce the above copyright */
- /* <LEGAL> notice, this list of conditions and the following disclaimer in the */
- /* <LEGAL> documentation and/or other materials provided with the distribution. */
- /* <LEGAL> */
- /* <LEGAL> 3. The names of its contributors may not be used to endorse or promote */
- /* <LEGAL> products derived from this software without specific prior written */
- /* <LEGAL> permission. */
- /* <LEGAL> */
- /* <LEGAL> THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS */
- /* <LEGAL> "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT */
- /* <LEGAL> LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR */
- /* <LEGAL> A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT OWNER OR */
- /* <LEGAL> CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, */
- /* <LEGAL> EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, */
- /* <LEGAL> PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR */
- /* <LEGAL> PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF */
- /* <LEGAL> LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING */
- /* <LEGAL> NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS */
- /* <LEGAL> SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE. */
- do {
- exitg1 = 0;
- genrand_uint32_vector(mt, u);
- r = 1.1102230246251565E-16 * ((real_T)(u[0] >> 5U) * 6.7108864E+7 + (real_T)
- (u[1] >> 6U));
- if (r == 0.0) {
- if ((mt[624] >= 1U) && (mt[624] < 625U)) {
- isvalid = TRUE;
- } else {
- isvalid = FALSE;
- }
-
- if (isvalid) {
- isvalid = FALSE;
- k = 1;
- exitg2 = FALSE;
- while ((exitg2 == FALSE) && (k < 625)) {
- if (mt[k - 1] == 0U) {
- k++;
- } else {
- isvalid = TRUE;
- exitg2 = TRUE;
- }
- }
- }
-
- if (!isvalid) {
- twister_state_vector(mt, 5489.0);
- }
- } else {
- exitg1 = 1;
- }
- } while (exitg1 == 0);
-
- return r;
-}
-
-static real_T eml_rand_mt19937ar(uint32_T e_state[625])
-{
- real_T r;
- int32_T exitg1;
- uint32_T u32[2];
- int32_T i;
- static const real_T dv1[257] = { 0.0, 0.215241895984875, 0.286174591792068,
- 0.335737519214422, 0.375121332878378, 0.408389134611989, 0.43751840220787,
- 0.46363433679088, 0.487443966139235, 0.50942332960209, 0.529909720661557,
- 0.549151702327164, 0.567338257053817, 0.584616766106378, 0.601104617755991,
- 0.61689699000775, 0.63207223638606, 0.646695714894993, 0.660822574244419,
- 0.674499822837293, 0.687767892795788, 0.700661841106814, 0.713212285190975,
- 0.725446140909999, 0.737387211434295, 0.749056662017815, 0.760473406430107,
- 0.771654424224568, 0.782615023307232, 0.793369058840623, 0.80392911698997,
- 0.814306670135215, 0.824512208752291, 0.834555354086381, 0.844444954909153,
- 0.854189171008163, 0.863795545553308, 0.87327106808886, 0.882622229585165,
- 0.891855070732941, 0.900975224461221, 0.909987953496718, 0.91889818364959,
- 0.927710533401999, 0.936429340286575, 0.945058684468165, 0.953602409881086,
- 0.96206414322304, 0.970447311064224, 0.978755155294224, 0.986990747099062,
- 0.99515699963509, 1.00325667954467, 1.01129241744, 1.01926671746548,
- 1.02718196603564, 1.03504043983344, 1.04284431314415, 1.05059566459093,
- 1.05829648333067, 1.06594867476212, 1.07355406579244, 1.0811144097034,
- 1.08863139065398, 1.09610662785202, 1.10354167942464, 1.11093804601357,
- 1.11829717411934, 1.12562045921553, 1.13290924865253, 1.14016484436815,
- 1.14738850542085, 1.15458145035993, 1.16174485944561, 1.16887987673083,
- 1.17598761201545, 1.18306914268269, 1.19012551542669, 1.19715774787944,
- 1.20416683014438, 1.2111537262437, 1.21811937548548, 1.22506469375653,
- 1.23199057474614, 1.23889789110569, 1.24578749554863, 1.2526602218949,
- 1.25951688606371, 1.26635828701823, 1.27318520766536, 1.27999841571382,
- 1.28679866449324, 1.29358669373695, 1.30036323033084, 1.30712898903073,
- 1.31388467315022, 1.32063097522106, 1.32736857762793, 1.33409815321936,
- 1.3408203658964, 1.34753587118059, 1.35424531676263, 1.36094934303328,
- 1.36764858359748, 1.37434366577317, 1.38103521107586, 1.38772383568998,
- 1.39441015092814, 1.40109476367925, 1.4077782768464, 1.41446128977547,
- 1.42114439867531, 1.42782819703026, 1.43451327600589, 1.44120022484872,
- 1.44788963128058, 1.45458208188841, 1.46127816251028, 1.46797845861808,
- 1.47468355569786, 1.48139403962819, 1.48811049705745, 1.49483351578049,
- 1.50156368511546, 1.50830159628131, 1.51504784277671, 1.521803020761,
- 1.52856772943771, 1.53534257144151, 1.542128153229, 1.54892508547417,
- 1.55573398346918, 1.56255546753104, 1.56939016341512, 1.57623870273591,
- 1.58310172339603, 1.58997987002419, 1.59687379442279, 1.60378415602609,
- 1.61071162236983, 1.61765686957301, 1.62462058283303, 1.63160345693487,
- 1.63860619677555, 1.64562951790478, 1.65267414708306, 1.65974082285818,
- 1.66683029616166, 1.67394333092612, 1.68108070472517, 1.68824320943719,
- 1.69543165193456, 1.70264685479992, 1.7098896570713, 1.71716091501782,
- 1.72446150294804, 1.73179231405296, 1.73915426128591, 1.74654827828172,
- 1.75397532031767, 1.76143636531891, 1.76893241491127, 1.77646449552452,
- 1.78403365954944, 1.79164098655216, 1.79928758454972, 1.80697459135082,
- 1.81470317596628, 1.82247454009388, 1.83028991968276, 1.83815058658281,
- 1.84605785028518, 1.8540130597602, 1.86201760539967, 1.87007292107127,
- 1.878180486293, 1.88634182853678, 1.8945585256707, 1.90283220855043,
- 1.91116456377125, 1.91955733659319, 1.92801233405266, 1.93653142827569,
- 1.94511656000868, 1.95376974238465, 1.96249306494436, 1.97128869793366,
- 1.98015889690048, 1.98910600761744, 1.99813247135842, 2.00724083056053,
- 2.0164337349062, 2.02571394786385, 2.03508435372962, 2.04454796521753,
- 2.05410793165065, 2.06376754781173, 2.07353026351874, 2.0833996939983,
- 2.09337963113879, 2.10347405571488, 2.11368715068665, 2.12402331568952,
- 2.13448718284602, 2.14508363404789, 2.15581781987674, 2.16669518035431,
- 2.17772146774029, 2.18890277162636, 2.20024554661128, 2.21175664288416,
- 2.22344334009251, 2.23531338492992, 2.24737503294739, 2.25963709517379,
- 2.27210899022838, 2.28480080272449, 2.29772334890286, 2.31088825060137,
- 2.32430801887113, 2.33799614879653, 2.35196722737914, 2.36623705671729,
- 2.38082279517208, 2.39574311978193, 2.41101841390112, 2.42667098493715,
- 2.44272531820036, 2.4592083743347, 2.47614993967052, 2.49358304127105,
- 2.51154444162669, 2.53007523215985, 2.54922155032478, 2.56903545268184,
- 2.58957598670829, 2.61091051848882, 2.63311639363158, 2.65628303757674,
- 2.68051464328574, 2.70593365612306, 2.73268535904401, 2.76094400527999,
- 2.79092117400193, 2.82287739682644, 2.85713873087322, 2.89412105361341,
- 2.93436686720889, 2.97860327988184, 3.02783779176959, 3.08352613200214,
- 3.147889289518, 3.2245750520478, 3.32024473383983, 3.44927829856143,
- 3.65415288536101, 3.91075795952492 };
-
- real_T u;
- static const real_T dv2[257] = { 1.0, 0.977101701267673, 0.959879091800108,
- 0.9451989534423, 0.932060075959231, 0.919991505039348, 0.908726440052131,
- 0.898095921898344, 0.887984660755834, 0.878309655808918, 0.869008688036857,
- 0.860033621196332, 0.851346258458678, 0.842915653112205, 0.834716292986884,
- 0.826726833946222, 0.818929191603703, 0.811307874312656, 0.803849483170964,
- 0.796542330422959, 0.789376143566025, 0.782341832654803, 0.775431304981187,
- 0.768637315798486, 0.761953346836795, 0.755373506507096, 0.748892447219157,
- 0.742505296340151, 0.736207598126863, 0.729995264561476, 0.72386453346863,
- 0.717811932630722, 0.711834248878248, 0.705928501332754, 0.700091918136512,
- 0.694321916126117, 0.688616083004672, 0.682972161644995, 0.677388036218774,
- 0.671861719897082, 0.66639134390875, 0.660975147776663, 0.655611470579697,
- 0.650298743110817, 0.645035480820822, 0.639820277453057, 0.634651799287624,
- 0.629528779924837, 0.624450015547027, 0.619414360605834, 0.614420723888914,
- 0.609468064925773, 0.604555390697468, 0.599681752619125, 0.594846243767987,
- 0.590047996332826, 0.585286179263371, 0.580559996100791, 0.575868682972354,
- 0.571211506735253, 0.566587763256165, 0.561996775814525, 0.557437893618766,
- 0.552910490425833, 0.548413963255266, 0.543947731190026, 0.539511234256952,
- 0.535103932380458, 0.530725304403662, 0.526374847171684, 0.522052074672322,
- 0.517756517229756, 0.513487720747327, 0.509245245995748, 0.505028667943468,
- 0.500837575126149, 0.49667156905249, 0.492530263643869, 0.488413284705458,
- 0.484320269426683, 0.480250865909047, 0.476204732719506, 0.47218153846773,
- 0.468180961405694, 0.464202689048174, 0.460246417812843, 0.456311852678716,
- 0.452398706861849, 0.448506701507203, 0.444635565395739, 0.440785034665804,
- 0.436954852547985, 0.433144769112652, 0.429354541029442, 0.425583931338022,
- 0.421832709229496, 0.418100649837848, 0.414387534040891, 0.410693148270188,
- 0.407017284329473, 0.403359739221114, 0.399720314980197, 0.396098818515832,
- 0.392495061459315, 0.388908860018789, 0.385340034840077, 0.381788410873393,
- 0.378253817245619, 0.374736087137891, 0.371235057668239, 0.367750569779032,
- 0.364282468129004, 0.360830600989648, 0.357394820145781, 0.353974980800077,
- 0.350570941481406, 0.347182563956794, 0.343809713146851, 0.340452257044522,
- 0.337110066637006, 0.333783015830718, 0.330470981379163, 0.327173842813601,
- 0.323891482376391, 0.320623784956905, 0.317370638029914, 0.314131931596337,
- 0.310907558126286, 0.307697412504292, 0.30450139197665, 0.301319396100803,
- 0.298151326696685, 0.294997087799962, 0.291856585617095, 0.288729728482183,
- 0.285616426815502, 0.282516593083708, 0.279430141761638, 0.276356989295668,
- 0.273297054068577, 0.270250256365875, 0.267216518343561, 0.264195763997261,
- 0.261187919132721, 0.258192911337619, 0.255210669954662, 0.252241126055942,
- 0.249284212418529, 0.246339863501264, 0.24340801542275, 0.240488605940501,
- 0.237581574431238, 0.23468686187233, 0.231804410824339, 0.228934165414681,
- 0.226076071322381, 0.223230075763918, 0.220396127480152, 0.217574176724331,
- 0.214764175251174, 0.211966076307031, 0.209179834621125, 0.206405406397881,
- 0.203642749310335, 0.200891822494657, 0.198152586545776, 0.195425003514135,
- 0.192709036903589, 0.190004651670465, 0.187311814223801, 0.1846304924268,
- 0.181960655599523, 0.179302274522848, 0.176655321443735, 0.174019770081839,
- 0.171395595637506, 0.168782774801212, 0.166181285764482, 0.163591108232366,
- 0.161012223437511, 0.158444614155925, 0.15588826472448, 0.153343161060263,
- 0.150809290681846, 0.148286642732575, 0.145775208005994, 0.143274978973514,
- 0.140785949814445, 0.138308116448551, 0.135841476571254, 0.133386029691669,
- 0.130941777173644, 0.12850872228, 0.126086870220186, 0.123676228201597,
- 0.12127680548479, 0.11888861344291, 0.116511665625611, 0.114145977827839,
- 0.111791568163838, 0.109448457146812, 0.107116667774684, 0.104796225622487,
- 0.102487158941935, 0.10018949876881, 0.0979032790388625, 0.095628536713009,
- 0.093365311912691, 0.0911136480663738, 0.0888735920682759,
- 0.0866451944505581, 0.0844285095703535, 0.082223595813203,
- 0.0800305158146631, 0.0778493367020961, 0.0756801303589272,
- 0.0735229737139814, 0.0713779490588905, 0.0692451443970068,
- 0.0671246538277886, 0.065016577971243, 0.0629210244377582, 0.06083810834954,
- 0.0587679529209339, 0.0567106901062031, 0.0546664613248891,
- 0.0526354182767924, 0.0506177238609479, 0.0486135532158687,
- 0.0466230949019305, 0.0446465522512946, 0.0426841449164746,
- 0.0407361106559411, 0.0388027074045262, 0.0368842156885674,
- 0.0349809414617162, 0.0330932194585786, 0.0312214171919203,
- 0.0293659397581334, 0.0275272356696031, 0.0257058040085489,
- 0.0239022033057959, 0.0221170627073089, 0.0203510962300445,
- 0.0186051212757247, 0.0168800831525432, 0.0151770883079353,
- 0.0134974506017399, 0.0118427578579079, 0.0102149714397015,
- 0.00861658276939875, 0.00705087547137324, 0.00552240329925101,
- 0.00403797259336304, 0.00260907274610216, 0.0012602859304986,
- 0.000477467764609386 };
-
- real_T x;
- do {
- exitg1 = 0;
- genrand_uint32_vector(e_state, u32);
- i = (int32_T)((u32[1] >> 24U) + 1U);
- r = (((real_T)(u32[0] >> 3U) * 1.6777216E+7 + (real_T)((int32_T)u32[1] &
- 16777215)) * 2.2204460492503131E-16 - 1.0) * dv1[i];
- if (fabs(r) <= dv1[i - 1]) {
- exitg1 = 1;
- } else if (i < 256) {
- u = b_genrandu(e_state);
- if (dv2[i] + u * (dv2[i - 1] - dv2[i]) < exp(-0.5 * r * r)) {
- exitg1 = 1;
- }
- } else {
- do {
- u = b_genrandu(e_state);
- x = log(u) * 0.273661237329758;
- u = b_genrandu(e_state);
- } while (!(-2.0 * log(u) > x * x));
-
- if (r < 0.0) {
- r = x - 3.65415288536101;
- } else {
- r = 3.65415288536101 - x;
- }
-
- exitg1 = 1;
- }
- } while (exitg1 == 0);
-
- return r;
-}
-
-static real_T eml_rand_shr3cong(uint32_T e_state[2])
-{
- real_T r;
- uint32_T icng;
- uint32_T jsr;
- uint32_T ui;
- int32_T j;
- static const real_T dv0[65] = { 0.340945, 0.4573146, 0.5397793, 0.6062427,
- 0.6631691, 0.7136975, 0.7596125, 0.8020356, 0.8417227, 0.8792102, 0.9148948,
- 0.9490791, 0.9820005, 1.0138492, 1.044781, 1.0749254, 1.1043917, 1.1332738,
- 1.161653, 1.189601, 1.2171815, 1.2444516, 1.2714635, 1.298265, 1.3249008,
- 1.3514125, 1.3778399, 1.4042211, 1.4305929, 1.4569915, 1.4834527, 1.5100122,
- 1.5367061, 1.5635712, 1.5906454, 1.617968, 1.6455802, 1.6735255, 1.7018503,
- 1.7306045, 1.7598422, 1.7896223, 1.8200099, 1.851077, 1.8829044, 1.9155831,
- 1.9492166, 1.9839239, 2.0198431, 2.0571356, 2.095993, 2.136645, 2.1793713,
- 2.2245175, 2.2725186, 2.3239338, 2.3795008, 2.4402218, 2.5075117, 2.5834658,
- 2.6713916, 2.7769942, 2.7769942, 2.7769942, 2.7769942 };
-
- real_T x;
- real_T y;
- real_T s;
- icng = 69069U * e_state[0] + 1234567U;
- jsr = e_state[1] ^ e_state[1] << 13U;
- jsr ^= jsr >> 17U;
- jsr ^= jsr << 5U;
- ui = icng + jsr;
- j = (int32_T)(ui & 63U);
- r = (real_T)(int32_T)ui * 4.6566128730773926E-10 * dv0[j + 1];
- if (fabs(r) <= dv0[j]) {
- } else {
- x = (fabs(r) - dv0[j]) / (dv0[j + 1] - dv0[j]);
- icng = 69069U * icng + 1234567U;
- jsr ^= jsr << 13U;
- jsr ^= jsr >> 17U;
- jsr ^= jsr << 5U;
- y = (real_T)(int32_T)(icng + jsr) * 2.328306436538696E-10;
- s = x + (0.5 + y);
- if (s > 1.301198) {
- if (r < 0.0) {
- r = 0.4878992 * x - 0.4878992;
- } else {
- r = 0.4878992 - 0.4878992 * x;
- }
- } else if (s <= 0.9689279) {
- } else {
- s = 0.4878992 * x;
- x = 0.4878992 - 0.4878992 * x;
- if (0.5 + y > 12.67706 - 12.37586 * exp(-0.5 * (0.4878992 - s) * x)) {
- if (r < 0.0) {
- r = -(0.4878992 - s);
- } else {
- r = 0.4878992 - s;
- }
- } else if (exp(-0.5 * dv0[j + 1] * dv0[j + 1]) + (0.5 + y) * 0.01958303 /
- dv0[j + 1] <= exp(-0.5 * r * r)) {
- } else {
- do {
- icng = 69069U * icng + 1234567U;
- jsr ^= jsr << 13U;
- jsr ^= jsr >> 17U;
- jsr ^= jsr << 5U;
- x = log(0.5 + (real_T)(int32_T)(icng + jsr) * 2.328306436538696E-10) /
- 2.776994;
- icng = 69069U * icng + 1234567U;
- jsr ^= jsr << 13U;
- jsr ^= jsr >> 17U;
- jsr ^= jsr << 5U;
- } while (!(-2.0 * log(0.5 + (real_T)(int32_T)(icng + jsr) *
- 2.328306436538696E-10) > x * x));
-
- if (r < 0.0) {
- r = x - 2.776994;
- } else {
- r = 2.776994 - x;
- }
- }
- }
- }
-
- e_state[0] = icng;
- e_state[1] = jsr;
- return r;
-}
-
-static void genrand_uint32_vector(uint32_T mt[625], uint32_T u[2])
-{
- int32_T i;
- uint32_T mti;
- int32_T kk;
- uint32_T y;
- uint32_T b_y;
- uint32_T c_y;
- uint32_T d_y;
- for (i = 0; i < 2; i++) {
- u[i] = 0U;
- }
-
- for (i = 0; i < 2; i++) {
- mti = mt[624] + 1U;
- if (mti >= 625U) {
- for (kk = 0; kk < 227; kk++) {
- y = (mt[kk] & 2147483648U) | (mt[1 + kk] & 2147483647U);
- if ((int32_T)(y & 1U) == 0) {
- b_y = y >> 1U;
- } else {
- b_y = y >> 1U ^ 2567483615U;
- }
-
- mt[kk] = mt[397 + kk] ^ b_y;
- }
-
- for (kk = 0; kk < 396; kk++) {
- y = (mt[227 + kk] & 2147483648U) | (mt[228 + kk] & 2147483647U);
- if ((int32_T)(y & 1U) == 0) {
- c_y = y >> 1U;
- } else {
- c_y = y >> 1U ^ 2567483615U;
- }
-
- mt[227 + kk] = mt[kk] ^ c_y;
- }
-
- y = (mt[623] & 2147483648U) | (mt[0] & 2147483647U);
- if ((int32_T)(y & 1U) == 0) {
- d_y = y >> 1U;
- } else {
- d_y = y >> 1U ^ 2567483615U;
- }
-
- mt[623] = mt[396] ^ d_y;
- mti = 1U;
- }
-
- y = mt[(int32_T)mti - 1];
- mt[624] = mti;
- y ^= y >> 11U;
- y ^= y << 7U & 2636928640U;
- y ^= y << 15U & 4022730752U;
- y ^= y >> 18U;
- u[i] = y;
- }
-}
-
-static void genrandu(uint32_T s, uint32_T *e_state, real_T *r)
-{
- int32_T hi;
- uint32_T test1;
- uint32_T test2;
- hi = (int32_T)(s / 127773U);
- test1 = 16807U * (s - (uint32_T)hi * 127773U);
- test2 = 2836U * (uint32_T)hi;
- if (test1 < test2) {
- *e_state = (test1 - test2) + 2147483647U;
- } else {
- *e_state = test1 - test2;
- }
-
- *r = (real_T)*e_state * 4.6566128752457969E-10;
-}
-
-static void twister_state_vector(uint32_T mt[625], real_T seed)
-{
- uint32_T r;
- int32_T mti;
- if (seed < 4.294967296E+9) {
- if (seed >= 0.0) {
- r = (uint32_T)seed;
- } else {
- r = 0U;
- }
- } else if (seed >= 4.294967296E+9) {
- r = MAX_uint32_T;
- } else {
- r = 0U;
- }
-
- mt[0] = r;
- for (mti = 0; mti < 623; mti++) {
- r = (r ^ r >> 30U) * 1812433253U + (uint32_T)(1 + mti);
- mt[1 + mti] = r;
- }
-
- mt[624] = 624U;
-}
-
-real_T randn(void)
-{
- real_T r;
- uint32_T e_state;
- real_T t;
- real_T b_r;
- uint32_T f_state;
- if (method == 0U) {
- if (b_method == 4U) {
- do {
- genrandu(b_state, &e_state, &r);
- genrandu(e_state, &b_state, &t);
- b_r = 2.0 * r - 1.0;
- t = 2.0 * t - 1.0;
- t = t * t + b_r * b_r;
- } while (!(t <= 1.0));
-
- r = (2.0 * r - 1.0) * sqrt(-2.0 * log(t) / t);
- } else if (b_method == 5U) {
- r = eml_rand_shr3cong(c_state);
- } else {
- if (!state_not_empty) {
- memset(&d_state[0], 0, 625U * sizeof(uint32_T));
- twister_state_vector(d_state, 5489.0);
- state_not_empty = TRUE;
- }
-
- r = eml_rand_mt19937ar(d_state);
- }
- } else if (method == 4U) {
- e_state = state[0];
- do {
- genrandu(e_state, &f_state, &r);
- genrandu(f_state, &e_state, &t);
- b_r = 2.0 * r - 1.0;
- t = 2.0 * t - 1.0;
- t = t * t + b_r * b_r;
- } while (!(t <= 1.0));
-
- state[0] = e_state;
- r = (2.0 * r - 1.0) * sqrt(-2.0 * log(t) / t);
- } else {
- r = eml_rand_shr3cong(state);
- }
-
- return r;
-}
-
-/* End of code generation (randn.c) */
diff --git a/src/modules/position_estimator_mc/codegen/randn.h b/src/modules/position_estimator_mc/codegen/randn.h deleted file mode 100755 index 8a2aa9277..000000000 --- a/src/modules/position_estimator_mc/codegen/randn.h +++ /dev/null @@ -1,33 +0,0 @@ -/*
- * randn.h
- *
- * Code generation for function 'randn'
- *
- * C source code generated on: Tue Feb 19 15:26:32 2013
- *
- */
-
-#ifndef __RANDN_H__
-#define __RANDN_H__
-/* Include files */
-#include <math.h>
-#include <stddef.h>
-#include <stdlib.h>
-#include <string.h>
-#include "rt_nonfinite.h"
-
-#include "rtwtypes.h"
-#include "kalman_dlqe3_types.h"
-
-/* Type Definitions */
-
-/* Named Constants */
-
-/* Variable Declarations */
-
-/* Variable Definitions */
-
-/* Function Declarations */
-extern real_T randn(void);
-#endif
-/* End of code generation (randn.h) */
diff --git a/src/modules/position_estimator_mc/codegen/rtGetInf.c b/src/modules/position_estimator_mc/codegen/rtGetInf.c deleted file mode 100755 index c6fa7884e..000000000 --- a/src/modules/position_estimator_mc/codegen/rtGetInf.c +++ /dev/null @@ -1,139 +0,0 @@ -/* - * rtGetInf.c - * - * Code generation for function 'kalman_dlqe2' - * - * C source code generated on: Thu Feb 14 12:52:29 2013 - * - */ - -/* - * Abstract: - * MATLAB for code generation function to initialize non-finite, Inf and MinusInf - */ -#include "rtGetInf.h" -#define NumBitsPerChar 8U - -/* Function: rtGetInf ================================================== - * Abstract: - * Initialize rtInf needed by the generated code. - * Inf is initialized as non-signaling. Assumes IEEE. - */ -real_T rtGetInf(void) -{ - size_t bitsPerReal = sizeof(real_T) * (NumBitsPerChar); - real_T inf = 0.0; - if (bitsPerReal == 32U) { - inf = rtGetInfF(); - } else { - uint16_T one = 1U; - enum { - LittleEndian, - BigEndian - } machByteOrder = (*((uint8_T *) &one) == 1U) ? LittleEndian : BigEndian; - switch (machByteOrder) { - case LittleEndian: - { - union { - LittleEndianIEEEDouble bitVal; - real_T fltVal; - } tmpVal; - - tmpVal.bitVal.words.wordH = 0x7FF00000U; - tmpVal.bitVal.words.wordL = 0x00000000U; - inf = tmpVal.fltVal; - break; - } - - case BigEndian: - { - union { - BigEndianIEEEDouble bitVal; - real_T fltVal; - } tmpVal; - - tmpVal.bitVal.words.wordH = 0x7FF00000U; - tmpVal.bitVal.words.wordL = 0x00000000U; - inf = tmpVal.fltVal; - break; - } - } - } - - return inf; -} - -/* Function: rtGetInfF ================================================== - * Abstract: - * Initialize rtInfF needed by the generated code. - * Inf is initialized as non-signaling. Assumes IEEE. - */ -real32_T rtGetInfF(void) -{ - IEEESingle infF; - infF.wordL.wordLuint = 0x7F800000U; - return infF.wordL.wordLreal; -} - -/* Function: rtGetMinusInf ================================================== - * Abstract: - * Initialize rtMinusInf needed by the generated code. - * Inf is initialized as non-signaling. Assumes IEEE. - */ -real_T rtGetMinusInf(void) -{ - size_t bitsPerReal = sizeof(real_T) * (NumBitsPerChar); - real_T minf = 0.0; - if (bitsPerReal == 32U) { - minf = rtGetMinusInfF(); - } else { - uint16_T one = 1U; - enum { - LittleEndian, - BigEndian - } machByteOrder = (*((uint8_T *) &one) == 1U) ? LittleEndian : BigEndian; - switch (machByteOrder) { - case LittleEndian: - { - union { - LittleEndianIEEEDouble bitVal; - real_T fltVal; - } tmpVal; - - tmpVal.bitVal.words.wordH = 0xFFF00000U; - tmpVal.bitVal.words.wordL = 0x00000000U; - minf = tmpVal.fltVal; - break; - } - - case BigEndian: - { - union { - BigEndianIEEEDouble bitVal; - real_T fltVal; - } tmpVal; - - tmpVal.bitVal.words.wordH = 0xFFF00000U; - tmpVal.bitVal.words.wordL = 0x00000000U; - minf = tmpVal.fltVal; - break; - } - } - } - - return minf; -} - -/* Function: rtGetMinusInfF ================================================== - * Abstract: - * Initialize rtMinusInfF needed by the generated code. - * Inf is initialized as non-signaling. Assumes IEEE. - */ -real32_T rtGetMinusInfF(void) -{ - IEEESingle minfF; - minfF.wordL.wordLuint = 0xFF800000U; - return minfF.wordL.wordLreal; -} - -/* End of code generation (rtGetInf.c) */ diff --git a/src/modules/position_estimator_mc/codegen/rtGetInf.h b/src/modules/position_estimator_mc/codegen/rtGetInf.h deleted file mode 100755 index e7b2a2d1c..000000000 --- a/src/modules/position_estimator_mc/codegen/rtGetInf.h +++ /dev/null @@ -1,23 +0,0 @@ -/* - * rtGetInf.h - * - * Code generation for function 'kalman_dlqe2' - * - * C source code generated on: Thu Feb 14 12:52:29 2013 - * - */ - -#ifndef __RTGETINF_H__ -#define __RTGETINF_H__ - -#include <stddef.h> -#include "rtwtypes.h" -#include "rt_nonfinite.h" - -extern real_T rtGetInf(void); -extern real32_T rtGetInfF(void); -extern real_T rtGetMinusInf(void); -extern real32_T rtGetMinusInfF(void); - -#endif -/* End of code generation (rtGetInf.h) */ diff --git a/src/modules/position_estimator_mc/codegen/rtGetNaN.c b/src/modules/position_estimator_mc/codegen/rtGetNaN.c deleted file mode 100755 index 552770149..000000000 --- a/src/modules/position_estimator_mc/codegen/rtGetNaN.c +++ /dev/null @@ -1,96 +0,0 @@ -/* - * rtGetNaN.c - * - * Code generation for function 'kalman_dlqe2' - * - * C source code generated on: Thu Feb 14 12:52:29 2013 - * - */ - -/* - * Abstract: - * MATLAB for code generation function to initialize non-finite, NaN - */ -#include "rtGetNaN.h" -#define NumBitsPerChar 8U - -/* Function: rtGetNaN ================================================== - * Abstract: - * Initialize rtNaN needed by the generated code. - * NaN is initialized as non-signaling. Assumes IEEE. - */ -real_T rtGetNaN(void) -{ - size_t bitsPerReal = sizeof(real_T) * (NumBitsPerChar); - real_T nan = 0.0; - if (bitsPerReal == 32U) { - nan = rtGetNaNF(); - } else { - uint16_T one = 1U; - enum { - LittleEndian, - BigEndian - } machByteOrder = (*((uint8_T *) &one) == 1U) ? LittleEndian : BigEndian; - switch (machByteOrder) { - case LittleEndian: - { - union { - LittleEndianIEEEDouble bitVal; - real_T fltVal; - } tmpVal; - - tmpVal.bitVal.words.wordH = 0xFFF80000U; - tmpVal.bitVal.words.wordL = 0x00000000U; - nan = tmpVal.fltVal; - break; - } - - case BigEndian: - { - union { - BigEndianIEEEDouble bitVal; - real_T fltVal; - } tmpVal; - - tmpVal.bitVal.words.wordH = 0x7FFFFFFFU; - tmpVal.bitVal.words.wordL = 0xFFFFFFFFU; - nan = tmpVal.fltVal; - break; - } - } - } - - return nan; -} - -/* Function: rtGetNaNF ================================================== - * Abstract: - * Initialize rtNaNF needed by the generated code. - * NaN is initialized as non-signaling. Assumes IEEE. - */ -real32_T rtGetNaNF(void) -{ - IEEESingle nanF = { { 0 } }; - uint16_T one = 1U; - enum { - LittleEndian, - BigEndian - } machByteOrder = (*((uint8_T *) &one) == 1U) ? LittleEndian : BigEndian; - switch (machByteOrder) { - case LittleEndian: - { - nanF.wordL.wordLuint = 0xFFC00000U; - break; - } - - case BigEndian: - { - nanF.wordL.wordLuint = 0x7FFFFFFFU; - break; - } - } - - return nanF.wordL.wordLreal; -} - -/* End of code generation (rtGetNaN.c) */ diff --git a/src/modules/position_estimator_mc/codegen/rtGetNaN.h b/src/modules/position_estimator_mc/codegen/rtGetNaN.h deleted file mode 100755 index 5acdd9790..000000000 --- a/src/modules/position_estimator_mc/codegen/rtGetNaN.h +++ /dev/null @@ -1,21 +0,0 @@ -/* - * rtGetNaN.h - * - * Code generation for function 'kalman_dlqe2' - * - * C source code generated on: Thu Feb 14 12:52:29 2013 - * - */ - -#ifndef __RTGETNAN_H__ -#define __RTGETNAN_H__ - -#include <stddef.h> -#include "rtwtypes.h" -#include "rt_nonfinite.h" - -extern real_T rtGetNaN(void); -extern real32_T rtGetNaNF(void); - -#endif -/* End of code generation (rtGetNaN.h) */ diff --git a/src/modules/position_estimator_mc/codegen/rt_nonfinite.c b/src/modules/position_estimator_mc/codegen/rt_nonfinite.c deleted file mode 100755 index de121c4a0..000000000 --- a/src/modules/position_estimator_mc/codegen/rt_nonfinite.c +++ /dev/null @@ -1,87 +0,0 @@ -/* - * rt_nonfinite.c - * - * Code generation for function 'kalman_dlqe2' - * - * C source code generated on: Thu Feb 14 12:52:29 2013 - * - */ - -/* - * Abstract: - * MATLAB for code generation function to initialize non-finites, - * (Inf, NaN and -Inf). - */ -#include "rt_nonfinite.h" -#include "rtGetNaN.h" -#include "rtGetInf.h" - -real_T rtInf; -real_T rtMinusInf; -real_T rtNaN; -real32_T rtInfF; -real32_T rtMinusInfF; -real32_T rtNaNF; - -/* Function: rt_InitInfAndNaN ================================================== - * Abstract: - * Initialize the rtInf, rtMinusInf, and rtNaN needed by the - * generated code. NaN is initialized as non-signaling. Assumes IEEE. - */ -void rt_InitInfAndNaN(size_t realSize) -{ - (void) (realSize); - rtNaN = rtGetNaN(); - rtNaNF = rtGetNaNF(); - rtInf = rtGetInf(); - rtInfF = rtGetInfF(); - rtMinusInf = rtGetMinusInf(); - rtMinusInfF = rtGetMinusInfF(); -} - -/* Function: rtIsInf ================================================== - * Abstract: - * Test if value is infinite - */ -boolean_T rtIsInf(real_T value) -{ - return ((value==rtInf || value==rtMinusInf) ? 1U : 0U); -} - -/* Function: rtIsInfF ================================================= - * Abstract: - * Test if single-precision value is infinite - */ -boolean_T rtIsInfF(real32_T value) -{ - return(((value)==rtInfF || (value)==rtMinusInfF) ? 1U : 0U); -} - -/* Function: rtIsNaN ================================================== - * Abstract: - * Test if value is not a number - */ -boolean_T rtIsNaN(real_T value) -{ -#if defined(_MSC_VER) && (_MSC_VER <= 1200) - return _isnan(value)? TRUE:FALSE; -#else - return (value!=value)? 1U:0U; -#endif -} - -/* Function: rtIsNaNF ================================================= - * Abstract: - * Test if single-precision value is not a number - */ -boolean_T rtIsNaNF(real32_T value) -{ -#if defined(_MSC_VER) && (_MSC_VER <= 1200) - return _isnan((real_T)value)? true:false; -#else - return (value!=value)? 1U:0U; -#endif -} - - -/* End of code generation (rt_nonfinite.c) */ diff --git a/src/modules/position_estimator_mc/codegen/rt_nonfinite.h b/src/modules/position_estimator_mc/codegen/rt_nonfinite.h deleted file mode 100755 index 3bbcfd087..000000000 --- a/src/modules/position_estimator_mc/codegen/rt_nonfinite.h +++ /dev/null @@ -1,53 +0,0 @@ -/* - * rt_nonfinite.h - * - * Code generation for function 'kalman_dlqe2' - * - * C source code generated on: Thu Feb 14 12:52:29 2013 - * - */ - -#ifndef __RT_NONFINITE_H__ -#define __RT_NONFINITE_H__ - -#if defined(_MSC_VER) && (_MSC_VER <= 1200) -#include <float.h> -#endif -#include <stddef.h> -#include "rtwtypes.h" - -extern real_T rtInf; -extern real_T rtMinusInf; -extern real_T rtNaN; -extern real32_T rtInfF; -extern real32_T rtMinusInfF; -extern real32_T rtNaNF; -extern void rt_InitInfAndNaN(size_t realSize); -extern boolean_T rtIsInf(real_T value); -extern boolean_T rtIsInfF(real32_T value); -extern boolean_T rtIsNaN(real_T value); -extern boolean_T rtIsNaNF(real32_T value); - -typedef struct { - struct { - uint32_T wordH; - uint32_T wordL; - } words; -} BigEndianIEEEDouble; - -typedef struct { - struct { - uint32_T wordL; - uint32_T wordH; - } words; -} LittleEndianIEEEDouble; - -typedef struct { - union { - real32_T wordLreal; - uint32_T wordLuint; - } wordL; -} IEEESingle; - -#endif -/* End of code generation (rt_nonfinite.h) */ diff --git a/src/modules/position_estimator_mc/codegen/rtwtypes.h b/src/modules/position_estimator_mc/codegen/rtwtypes.h deleted file mode 100755 index 8916e8572..000000000 --- a/src/modules/position_estimator_mc/codegen/rtwtypes.h +++ /dev/null @@ -1,159 +0,0 @@ -/* - * rtwtypes.h - * - * Code generation for function 'kalman_dlqe2' - * - * C source code generated on: Thu Feb 14 12:52:29 2013 - * - */ - -#ifndef __RTWTYPES_H__ -#define __RTWTYPES_H__ -#ifndef TRUE -# define TRUE (1U) -#endif -#ifndef FALSE -# define FALSE (0U) -#endif -#ifndef __TMWTYPES__ -#define __TMWTYPES__ - -#include <limits.h> - -/*=======================================================================* - * Target hardware information - * Device type: Generic->MATLAB Host Computer - * Number of bits: char: 8 short: 16 int: 32 - * long: 32 native word size: 32 - * Byte ordering: LittleEndian - * Signed integer division rounds to: Undefined - * Shift right on a signed integer as arithmetic shift: off - *=======================================================================*/ - -/*=======================================================================* - * Fixed width word size data types: * - * int8_T, int16_T, int32_T - signed 8, 16, or 32 bit integers * - * uint8_T, uint16_T, uint32_T - unsigned 8, 16, or 32 bit integers * - * real32_T, real64_T - 32 and 64 bit floating point numbers * - *=======================================================================*/ - -typedef signed char int8_T; -typedef unsigned char uint8_T; -typedef short int16_T; -typedef unsigned short uint16_T; -typedef int int32_T; -typedef unsigned int uint32_T; -typedef float real32_T; -typedef double real64_T; - -/*===========================================================================* - * Generic type definitions: real_T, time_T, boolean_T, int_T, uint_T, * - * ulong_T, char_T and byte_T. * - *===========================================================================*/ - -typedef double real_T; -typedef double time_T; -typedef unsigned char boolean_T; -typedef int int_T; -typedef unsigned int uint_T; -typedef unsigned long ulong_T; -typedef char char_T; -typedef char_T byte_T; - -/*===========================================================================* - * Complex number type definitions * - *===========================================================================*/ -#define CREAL_T - typedef struct { - real32_T re; - real32_T im; - } creal32_T; - - typedef struct { - real64_T re; - real64_T im; - } creal64_T; - - typedef struct { - real_T re; - real_T im; - } creal_T; - - typedef struct { - int8_T re; - int8_T im; - } cint8_T; - - typedef struct { - uint8_T re; - uint8_T im; - } cuint8_T; - - typedef struct { - int16_T re; - int16_T im; - } cint16_T; - - typedef struct { - uint16_T re; - uint16_T im; - } cuint16_T; - - typedef struct { - int32_T re; - int32_T im; - } cint32_T; - - typedef struct { - uint32_T re; - uint32_T im; - } cuint32_T; - - -/*=======================================================================* - * Min and Max: * - * int8_T, int16_T, int32_T - signed 8, 16, or 32 bit integers * - * uint8_T, uint16_T, uint32_T - unsigned 8, 16, or 32 bit integers * - *=======================================================================*/ - -#define MAX_int8_T ((int8_T)(127)) -#define MIN_int8_T ((int8_T)(-128)) -#define MAX_uint8_T ((uint8_T)(255)) -#define MIN_uint8_T ((uint8_T)(0)) -#define MAX_int16_T ((int16_T)(32767)) -#define MIN_int16_T ((int16_T)(-32768)) -#define MAX_uint16_T ((uint16_T)(65535)) -#define MIN_uint16_T ((uint16_T)(0)) -#define MAX_int32_T ((int32_T)(2147483647)) -#define MIN_int32_T ((int32_T)(-2147483647-1)) -#define MAX_uint32_T ((uint32_T)(0xFFFFFFFFU)) -#define MIN_uint32_T ((uint32_T)(0)) - -/* Logical type definitions */ -#if !defined(__cplusplus) && !defined(__true_false_are_keywords) -# ifndef false -# define false (0U) -# endif -# ifndef true -# define true (1U) -# endif -#endif - -/* - * MATLAB for code generation assumes the code is compiled on a target using a 2's compliment representation - * for signed integer values. - */ -#if ((SCHAR_MIN + 1) != -SCHAR_MAX) -#error "This code must be compiled using a 2's complement representation for signed integer values" -#endif - -/* - * Maximum length of a MATLAB identifier (function/variable) - * including the null-termination character. Referenced by - * rt_logging.c and rt_matrx.c. - */ -#define TMW_NAME_LENGTH_MAX 64 - -#endif -#endif -/* End of code generation (rtwtypes.h) */ diff --git a/src/modules/position_estimator_mc/kalman_dlqe1.m b/src/modules/position_estimator_mc/kalman_dlqe1.m deleted file mode 100755 index ff939d029..000000000 --- a/src/modules/position_estimator_mc/kalman_dlqe1.m +++ /dev/null @@ -1,3 +0,0 @@ -function [x_aposteriori] = kalman_dlqe1(A,C,K,x_aposteriori_k,z) - x_aposteriori=A*x_aposteriori_k+K*(z-C*A*x_aposteriori_k); -end
\ No newline at end of file diff --git a/src/modules/position_estimator_mc/kalman_dlqe2.m b/src/modules/position_estimator_mc/kalman_dlqe2.m deleted file mode 100755 index 2a50164ef..000000000 --- a/src/modules/position_estimator_mc/kalman_dlqe2.m +++ /dev/null @@ -1,9 +0,0 @@ -function [x_aposteriori] = kalman_dlqe2(dt,k1,k2,k3,x_aposteriori_k,z) - st = 1/2*dt^2; - A = [1,dt,st; - 0,1,dt; - 0,0,1]; - C=[1,0,0]; - K = [k1;k2;k3]; - x_aposteriori=A*x_aposteriori_k+K*(z-C*A*x_aposteriori_k); -end
\ No newline at end of file diff --git a/src/modules/position_estimator_mc/kalman_dlqe3.m b/src/modules/position_estimator_mc/kalman_dlqe3.m deleted file mode 100755 index 4c6421b7f..000000000 --- a/src/modules/position_estimator_mc/kalman_dlqe3.m +++ /dev/null @@ -1,17 +0,0 @@ -function [x_aposteriori] = kalman_dlqe3(dt,k1,k2,k3,x_aposteriori_k,z,posUpdate,addNoise,sigma)
- st = 1/2*dt^2;
- A = [1,dt,st;
- 0,1,dt;
- 0,0,1];
- C=[1,0,0];
- K = [k1;k2;k3];
- if addNoise==1
- noise = sigma*randn(1,1);
- z = z + noise;
- end
- if(posUpdate)
- x_aposteriori=A*x_aposteriori_k+K*(z-C*A*x_aposteriori_k);
- else
- x_aposteriori=A*x_aposteriori_k;
- end
-end
\ No newline at end of file diff --git a/src/modules/position_estimator_mc/module.mk b/src/modules/position_estimator_mc/module.mk deleted file mode 100644 index 40b135ea4..000000000 --- a/src/modules/position_estimator_mc/module.mk +++ /dev/null @@ -1,60 +0,0 @@ -############################################################################ -# -# Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved. -# -# Redistribution and use in source and binary forms, with or without -# modification, are permitted provided that the following conditions -# are met: -# -# 1. Redistributions of source code must retain the above copyright -# notice, this list of conditions and the following disclaimer. -# 2. Redistributions in binary form must reproduce the above copyright -# notice, this list of conditions and the following disclaimer in -# the documentation and/or other materials provided with the -# distribution. -# 3. Neither the name PX4 nor the names of its contributors may be -# used to endorse or promote products derived from this software -# without specific prior written permission. -# -# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS -# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT -# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS -# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE -# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, -# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, -# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS -# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED -# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT -# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN -# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE -# POSSIBILITY OF SUCH DAMAGE. -# -############################################################################ - -# -# Makefile to build the position estimator -# - -MODULE_COMMAND = position_estimator_mc - -SRCS = position_estimator_mc_main.c \ - position_estimator_mc_params.c \ - codegen/positionKalmanFilter1D_initialize.c \ - codegen/positionKalmanFilter1D_terminate.c \ - codegen/positionKalmanFilter1D.c \ - codegen/rt_nonfinite.c \ - codegen/rtGetInf.c \ - codegen/rtGetNaN.c \ - codegen/positionKalmanFilter1D_dT_initialize.c \ - codegen/positionKalmanFilter1D_dT_terminate.c \ - codegen/kalman_dlqe1.c \ - codegen/kalman_dlqe1_initialize.c \ - codegen/kalman_dlqe1_terminate.c \ - codegen/kalman_dlqe2.c \ - codegen/kalman_dlqe2_initialize.c \ - codegen/kalman_dlqe2_terminate.c \ - codegen/kalman_dlqe3.c \ - codegen/kalman_dlqe3_initialize.c \ - codegen/kalman_dlqe3_terminate.c \ - codegen/kalman_dlqe3_data.c \ - codegen/randn.c diff --git a/src/modules/position_estimator_mc/positionKalmanFilter1D.m b/src/modules/position_estimator_mc/positionKalmanFilter1D.m deleted file mode 100755 index 144ff8c7c..000000000 --- a/src/modules/position_estimator_mc/positionKalmanFilter1D.m +++ /dev/null @@ -1,19 +0,0 @@ -function [x_aposteriori,P_aposteriori]=positionKalmanFilter1D(A,B,C,x_aposteriori_k,P_aposteriori_k,u,z,gps_update,Q,R,thresh,decay) -%prediction - x_apriori=A*x_aposteriori_k+B*u; - P_apriori=A*P_aposteriori_k*A'+Q; - if abs(u)<thresh - x_apriori(2)=decay*x_apriori(2); - end - %update - if gps_update==1 - y=z-C*x_apriori; - S=C*P_apriori*C'+R; - K=(P_apriori*C')/S; - x_aposteriori=x_apriori+K*y; - P_aposteriori=(eye(size(P_apriori))-K*C)*P_apriori; - else - x_aposteriori=x_apriori; - P_aposteriori=P_apriori; - end -end diff --git a/src/modules/position_estimator_mc/positionKalmanFilter1D_dT.m b/src/modules/position_estimator_mc/positionKalmanFilter1D_dT.m deleted file mode 100755 index f94cce1fb..000000000 --- a/src/modules/position_estimator_mc/positionKalmanFilter1D_dT.m +++ /dev/null @@ -1,26 +0,0 @@ -function [x_aposteriori,P_aposteriori]=positionKalmanFilter1D_dT(dT,x_aposteriori_k,P_aposteriori_k,u,z,gps_update,Q,R,thresh,decay) - %dynamics - A = [1 dT -0.5*dT*dT; - 0 1 -dT; - 0 0 1]; - B = [0.5*dT*dT; dT; 0]; - C = [1 0 0]; - %prediction - x_apriori=A*x_aposteriori_k+B*u; - P_apriori=A*P_aposteriori_k*A'+Q; - if abs(u)<thresh - x_apriori(2)=decay*x_apriori(2); - end - %update - if gps_update==1 - y=z-C*x_apriori; - S=C*P_apriori*C'+R; - K=(P_apriori*C')/S; - x_aposteriori=x_apriori+K*y; - P_aposteriori=(eye(size(P_apriori))-K*C)*P_apriori; - else - x_aposteriori=x_apriori; - P_aposteriori=P_apriori; - end -end - diff --git a/src/modules/position_estimator_mc/position_estimator_mc_main.c b/src/modules/position_estimator_mc/position_estimator_mc_main.c deleted file mode 100755 index 363961819..000000000 --- a/src/modules/position_estimator_mc/position_estimator_mc_main.c +++ /dev/null @@ -1,515 +0,0 @@ -/**************************************************************************** - * - * Copyright (C) 2008-2012 PX4 Development Team. All rights reserved. - * Author: Damian Aregger <daregger@student.ethz.ch> - * Tobias Naegeli <naegelit@student.ethz.ch> -* Lorenz Meier <lm@inf.ethz.ch> - * - * Redistribution and use in source and binary forms, with or without - * modification, are permitted provided that the following conditions - * are met: - * - * 1. Redistributions of source code must retain the above copyright - * notice, this list of conditions and the following disclaimer. - * 2. Redistributions in binary form must reproduce the above copyright - * notice, this list of conditions and the following disclaimer in - * the documentation and/or other materials provided with the - * distribution. - * 3. Neither the name PX4 nor the names of its contributors may be - * used to endorse or promote products derived from this software - * without specific prior written permission. - * - * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS - * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT - * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS - * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE - * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, - * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, - * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS - * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED - * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT - * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN - * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE - * POSSIBILITY OF SUCH DAMAGE. - * - ****************************************************************************/ - -/** - * @file position_estimator_main.c - * Model-identification based position estimator for multirotors - */ - -#include <unistd.h> -#include <stdlib.h> -#include <stdio.h> -#include <stdbool.h> -#include <fcntl.h> -#include <float.h> -#include <string.h> -#include <nuttx/config.h> -#include <nuttx/sched.h> -#include <sys/prctl.h> -#include <termios.h> -#include <errno.h> -#include <limits.h> -#include <math.h> -#include <uORB/uORB.h> -#include <uORB/topics/sensor_combined.h> -#include <uORB/topics/parameter_update.h> -#include <uORB/topics/vehicle_attitude.h> -#include <uORB/topics/actuator_outputs.h> -#include <uORB/topics/actuator_controls_effective.h> -#include <uORB/topics/vehicle_status.h> -#include <uORB/topics/vehicle_vicon_position.h> -#include <uORB/topics/vehicle_local_position.h> -#include <uORB/topics/vehicle_global_position.h> -#include <uORB/topics/vehicle_local_position_setpoint.h> -#include <uORB/topics/vehicle_gps_position.h> -#include <mavlink/mavlink_log.h> -#include <poll.h> -#include <systemlib/geo/geo.h> -#include <systemlib/err.h> -#include <systemlib/systemlib.h> - -#include <drivers/drv_hrt.h> - -#include "position_estimator_mc_params.h" -//#include <uORB/topics/debug_key_value.h> -#include "codegen/kalman_dlqe2.h" -#include "codegen/kalman_dlqe2_initialize.h" -#include "codegen/kalman_dlqe3.h" -#include "codegen/kalman_dlqe3_initialize.h" - -static bool thread_should_exit = false; /**< Deamon exit flag */ -static bool thread_running = false; /**< Deamon status flag */ -static int position_estimator_mc_task; /**< Handle of deamon task / thread */ - -__EXPORT int position_estimator_mc_main(int argc, char *argv[]); - -int position_estimator_mc_thread_main(int argc, char *argv[]); -/** - * Print the correct usage. - */ -static void usage(const char *reason); - -static void -usage(const char *reason) -{ - if (reason) - warnx("%s\n", reason); - warnx("usage: position_estimator_mc {start|stop|status}"); - exit(1); -} - -/** - * The position_estimator_mc_thread only briefly exists to start - * the background job. The stack size assigned in the - * Makefile does only apply to this management task. - * - * The actual stack size should be set in the call - * to task_create(). - */ -int position_estimator_mc_main(int argc, char *argv[]) -{ - if (argc < 1) - usage("missing command"); - - if (!strcmp(argv[1], "start")) { - - if (thread_running) { - printf("position_estimator_mc already running\n"); - /* this is not an error */ - exit(0); - } - - thread_should_exit = false; - position_estimator_mc_task = task_spawn_cmd("position_estimator_mc", - SCHED_RR, - SCHED_PRIORITY_MAX - 5, - 4096, - position_estimator_mc_thread_main, - (argv) ? (const char **)&argv[2] : (const char **)NULL); - exit(0); - } - if (!strcmp(argv[1], "stop")) { - thread_should_exit = true; - exit(0); - } - - if (!strcmp(argv[1], "status")) { - if (thread_running) { - warnx("position_estimator_mc is running"); - } else { - warnx("position_estimator_mc not started"); - } - exit(0); - } - - usage("unrecognized command"); - exit(1); -} - -/**************************************************************************** - * main - ****************************************************************************/ -int position_estimator_mc_thread_main(int argc, char *argv[]) -{ - /* welcome user */ - warnx("[position_estimator_mc] started"); - int mavlink_fd; - mavlink_fd = open(MAVLINK_LOG_DEVICE, 0); - mavlink_log_info(mavlink_fd, "[position_estimator_mc] started"); - - /* initialize values */ - float z[3] = {0, 0, 0}; /* output variables from tangent plane mapping */ - // float rotMatrix[4] = {1.0f, 0.0f, 0.0f, 1.0f}; - float x_x_aposteriori_k[3] = {1.0f, 0.0f, 0.0f}; - float x_y_aposteriori_k[3] = {1.0f, 0.0f, 0.0f}; - float x_z_aposteriori_k[3] = {1.0f, 0.0f, 0.0f}; - float x_x_aposteriori[3] = {0.0f, 0.0f, 0.0f}; - float x_y_aposteriori[3] = {1.0f, 0.0f, 0.0f}; - float x_z_aposteriori[3] = {1.0f, 0.0f, 0.0f}; - - // XXX this is terribly wrong and should actual dT instead - const float dT_const_50 = 1.0f/50.0f; - - float addNoise = 0.0f; - float sigma = 0.0f; - //computed from dlqe in matlab - const float K_vicon_50Hz[3] = {0.5297f, 0.9873f, 0.9201f}; - // XXX implement baro filter - const float K_baro[3] = {0.0248f, 0.0377f, 0.0287f}; - float K[3] = {0.0f, 0.0f, 0.0f}; - int baro_loop_cnt = 0; - int baro_loop_end = 70; /* measurement for 1 second */ - float p0_Pa = 0.0f; /* to determin while start up */ - float rho0 = 1.293f; /* standard pressure */ - const float const_earth_gravity = 9.81f; - - float posX = 0.0f; - float posY = 0.0f; - float posZ = 0.0f; - - double lat_current; - double lon_current; - float alt_current; - - float gps_origin_altitude = 0.0f; - - /* Initialize filter */ - kalman_dlqe2_initialize(); - kalman_dlqe3_initialize(); - - /* declare and safely initialize all structs */ - struct sensor_combined_s sensor; - memset(&sensor, 0, sizeof(sensor)); - struct vehicle_attitude_s att; - memset(&att, 0, sizeof(att)); - struct vehicle_status_s vehicle_status; - memset(&vehicle_status, 0, sizeof(vehicle_status)); /* make sure that baroINITdone = false */ - struct vehicle_vicon_position_s vicon_pos; - memset(&vicon_pos, 0, sizeof(vicon_pos)); - struct actuator_controls_effective_s act_eff; - memset(&act_eff, 0, sizeof(act_eff)); - struct vehicle_gps_position_s gps; - memset(&gps, 0, sizeof(gps)); - struct vehicle_local_position_s local_pos_est; - memset(&local_pos_est, 0, sizeof(local_pos_est)); - struct vehicle_global_position_s global_pos_est; - memset(&global_pos_est, 0, sizeof(global_pos_est)); - - /* subscribe */ - int sensor_sub = orb_subscribe(ORB_ID(sensor_combined)); - int sub_params = orb_subscribe(ORB_ID(parameter_update)); - int vehicle_attitude_sub = orb_subscribe(ORB_ID(vehicle_attitude)); - int vicon_pos_sub = orb_subscribe(ORB_ID(vehicle_vicon_position)); - int actuator_eff_sub = orb_subscribe(ORB_ID(actuator_controls_effective_0)); - int vehicle_gps_sub = orb_subscribe(ORB_ID(vehicle_gps_position)); - int vehicle_status_sub = orb_subscribe(ORB_ID(vehicle_status)); - - /* advertise */ - orb_advert_t local_pos_est_pub = 0; - orb_advert_t global_pos_est_pub = 0; - - struct position_estimator_mc_params pos1D_params; - struct position_estimator_mc_param_handles pos1D_param_handles; - /* initialize parameter handles */ - parameters_init(&pos1D_param_handles); - - bool flag_use_gps = false; - bool flag_use_baro = false; - bool flag_baro_initialized = false; /* in any case disable baroINITdone */ - /* FIRST PARAMETER READ at START UP*/ - struct parameter_update_s update; - orb_copy(ORB_ID(parameter_update), sub_params, &update); /* read from param to clear updated flag */ - /* FIRST PARAMETER UPDATE */ - parameters_update(&pos1D_param_handles, &pos1D_params); - flag_use_baro = pos1D_params.baro; - sigma = pos1D_params.sigma; - addNoise = pos1D_params.addNoise; - /* END FIRST PARAMETER UPDATE */ - - /* try to grab a vicon message - if it fails, go for GPS. */ - - /* make sure the next orb_check() can't return true unless we get a timely update */ - orb_copy(ORB_ID(vehicle_vicon_position), vicon_pos_sub, &vicon_pos); - /* allow 200 ms for vicon to come in */ - usleep(200000); - /* check if we got vicon */ - bool update_check; - orb_check(vicon_pos_sub, &update_check); - /* if no update was available, use GPS */ - flag_use_gps = !update_check; - - if (flag_use_gps) { - mavlink_log_info(mavlink_fd, "[pos_est_mc] GPS locked"); - /* wait until gps signal turns valid, only then can we initialize the projection */ - - // XXX magic number - float hdop_threshold_m = 4.0f; - float vdop_threshold_m = 8.0f; - - /* - * If horizontal dilution of precision (hdop / eph) - * and vertical diluation of precision (vdop / epv) - * are below a certain threshold (e.g. 4 m), AND - * home position is not yet set AND the last GPS - * GPS measurement is not older than two seconds AND - * the system is currently not armed, set home - * position to the current position. - */ - - while (!(gps.fix_type == 3 - && (gps.eph_m < hdop_threshold_m) - && (gps.epv_m < vdop_threshold_m) - && (hrt_absolute_time() - gps.timestamp_position < 2000000))) { - - struct pollfd fds1[2] = { - { .fd = vehicle_gps_sub, .events = POLLIN }, - { .fd = sub_params, .events = POLLIN }, - }; - - /* wait for GPS updates, BUT READ VEHICLE STATUS (!) - * this choice is critical, since the vehicle status might not - * actually change, if this app is started after GPS lock was - * aquired. - */ - if (poll(fds1, 2, 5000)) { - if (fds1[0].revents & POLLIN){ - /* Read gps position */ - orb_copy(ORB_ID(vehicle_gps_position), vehicle_gps_sub, &gps); - } - if (fds1[1].revents & POLLIN){ - /* Read out parameters to check for an update there, e.g. useGPS variable */ - /* read from param to clear updated flag */ - struct parameter_update_s updated; - orb_copy(ORB_ID(parameter_update), sub_params, &updated); - /* update parameters */ - parameters_update(&pos1D_param_handles, &pos1D_params); - } - } - static int printcounter = 0; - if (printcounter == 100) { - printcounter = 0; - warnx("[pos_est_mc] wait for GPS fix"); - } - printcounter++; - } - - /* get gps value for first initialization */ - orb_copy(ORB_ID(vehicle_gps_position), vehicle_gps_sub, &gps); - lat_current = ((double)(gps.lat)) * 1e-7d; - lon_current = ((double)(gps.lon)) * 1e-7d; - alt_current = gps.alt * 1e-3f; - gps_origin_altitude = alt_current; - /* initialize coordinates */ - map_projection_init(lat_current, lon_current); - /* publish global position messages only after first GPS message */ - printf("[pos_est_mc] initialized projection with: lat: %.10f, lon:%.10f\n", lat_current, lon_current); - - } else { - mavlink_log_info(mavlink_fd, "[pos_est_mc] I'm NOT using GPS - I use VICON"); - /* onboard calculated position estimations */ - } - thread_running = true; - - struct pollfd fds2[3] = { - { .fd = vehicle_gps_sub, .events = POLLIN }, - { .fd = vicon_pos_sub, .events = POLLIN }, - { .fd = sub_params, .events = POLLIN }, - }; - - bool vicon_updated = false; - bool gps_updated = false; - - /**< main_loop */ - while (!thread_should_exit) { - int ret = poll(fds2, 3, 20); //wait maximal this 20 ms = 50 Hz minimum rate - if (ret < 0) { - /* poll error */ - } else { - if (fds2[2].revents & POLLIN){ - /* new parameter */ - /* read from param to clear updated flag */ - struct parameter_update_s updated; - orb_copy(ORB_ID(parameter_update), sub_params, &updated); - /* update parameters */ - parameters_update(&pos1D_param_handles, &pos1D_params); - flag_use_baro = pos1D_params.baro; - sigma = pos1D_params.sigma; - addNoise = pos1D_params.addNoise; - } - vicon_updated = false; /* default is no vicon_updated */ - if (fds2[1].revents & POLLIN) { - /* new vicon position */ - orb_copy(ORB_ID(vehicle_vicon_position), vicon_pos_sub, &vicon_pos); - posX = vicon_pos.x; - posY = vicon_pos.y; - posZ = vicon_pos.z; - vicon_updated = true; /* set flag for vicon update */ - } /* end of poll call for vicon updates */ - gps_updated = false; - if (fds2[0].revents & POLLIN) { - /* new GPS value */ - orb_copy(ORB_ID(vehicle_gps_position), vehicle_gps_sub, &gps); - /* Project gps lat lon (Geographic coordinate system) to plane*/ - map_projection_project(((double)(gps.lat)) * 1e-7d, ((double)(gps.lon)) * 1e-7d, &(z[0]), &(z[1])); - posX = z[0]; - posY = z[1]; - posZ = (float)(gps.alt * 1e-3f); - gps_updated = true; - } - - /* Main estimator loop */ - orb_copy(ORB_ID(actuator_controls_effective_0), actuator_eff_sub, &act_eff); - orb_copy(ORB_ID(vehicle_attitude), vehicle_attitude_sub, &att); - orb_copy(ORB_ID(vehicle_status), vehicle_status_sub, &vehicle_status); - orb_copy(ORB_ID(sensor_combined), sensor_sub, &sensor); - // barometric pressure estimation at start up - if (!flag_baro_initialized){ - // mean calculation over several measurements - if (baro_loop_cnt<baro_loop_end) { - p0_Pa += (sensor.baro_pres_mbar*100); - baro_loop_cnt++; - } else { - p0_Pa /= (float)(baro_loop_cnt); - flag_baro_initialized = true; - char *baro_m_start = "barometer initialized with p0 = "; - char p0_char[15]; - sprintf(p0_char, "%8.2f", (double)(p0_Pa/100)); - char *baro_m_end = " mbar"; - char str[80]; - strcpy(str,baro_m_start); - strcat(str,p0_char); - strcat(str,baro_m_end); - mavlink_log_info(mavlink_fd, str); - } - } - if (flag_use_gps) { - /* initialize map projection with the last estimate (not at full rate) */ - if (gps.fix_type > 2) { - /* x-y-position/velocity estimation in earth frame = gps frame */ - kalman_dlqe3(dT_const_50,K_vicon_50Hz[0],K_vicon_50Hz[1],K_vicon_50Hz[2],x_x_aposteriori_k,posX,gps_updated,0.0f,0.0f,x_x_aposteriori); - memcpy(x_x_aposteriori_k, x_x_aposteriori, sizeof(x_x_aposteriori)); - kalman_dlqe3(dT_const_50,K_vicon_50Hz[0],K_vicon_50Hz[1],K_vicon_50Hz[2],x_y_aposteriori_k,posY,gps_updated,0.0f,0.0f,x_y_aposteriori); - memcpy(x_y_aposteriori_k, x_y_aposteriori, sizeof(x_y_aposteriori)); - /* z-position/velocity estimation in earth frame = vicon frame */ - float z_est = 0.0f; - if (flag_baro_initialized && flag_use_baro) { - z_est = -p0_Pa*logf(p0_Pa/(sensor.baro_pres_mbar*100))/(rho0*const_earth_gravity); - K[0] = K_vicon_50Hz[0]; - K[1] = K_vicon_50Hz[1]; - K[2] = K_vicon_50Hz[2]; - gps_updated = 1.0f; /* always enable the update, cause baro update = 200 Hz */ - } else { - z_est = posZ; - K[0] = K_vicon_50Hz[0]; - K[1] = K_vicon_50Hz[1]; - K[2] = K_vicon_50Hz[2]; - } - - kalman_dlqe3(dT_const_50,K[0],K[1],K[2],x_z_aposteriori_k,z_est,gps_updated,0.0f,0.0f,x_z_aposteriori); - memcpy(x_z_aposteriori_k, x_z_aposteriori, sizeof(x_z_aposteriori)); - local_pos_est.x = x_x_aposteriori_k[0]; - local_pos_est.vx = x_x_aposteriori_k[1]; - local_pos_est.y = x_y_aposteriori_k[0]; - local_pos_est.vy = x_y_aposteriori_k[1]; - local_pos_est.z = x_z_aposteriori_k[0]; - local_pos_est.vz = x_z_aposteriori_k[1]; - local_pos_est.timestamp = hrt_absolute_time(); - if ((isfinite(x_x_aposteriori_k[0])) && (isfinite(x_x_aposteriori_k[1])) && (isfinite(x_y_aposteriori_k[0])) && (isfinite(x_y_aposteriori_k[1])) && (isfinite(x_z_aposteriori_k[0])) && (isfinite(x_z_aposteriori_k[1]))) { - /* publish local position estimate */ - if (local_pos_est_pub > 0) { - orb_publish(ORB_ID(vehicle_local_position), local_pos_est_pub, &local_pos_est); - } else { - local_pos_est_pub = orb_advertise(ORB_ID(vehicle_local_position), &local_pos_est); - } - /* publish on GPS updates */ - if (gps_updated) { - - double lat, lon; - float alt = z_est + gps_origin_altitude; - - map_projection_reproject(local_pos_est.x, local_pos_est.y, &lat, &lon); - - global_pos_est.lat = lat; - global_pos_est.lon = lon; - global_pos_est.alt = alt; - - if (global_pos_est_pub > 0) { - orb_publish(ORB_ID(vehicle_global_position), global_pos_est_pub, &global_pos_est); - } else { - global_pos_est_pub = orb_advertise(ORB_ID(vehicle_global_position), &global_pos_est); - } - } - } - } - } else { - /* x-y-position/velocity estimation in earth frame = vicon frame */ - kalman_dlqe3(dT_const_50,K_vicon_50Hz[0],K_vicon_50Hz[1],K_vicon_50Hz[2],x_x_aposteriori_k,posX,vicon_updated,addNoise,sigma,x_x_aposteriori); - memcpy(x_x_aposteriori_k, x_x_aposteriori, sizeof(x_x_aposteriori)); - kalman_dlqe3(dT_const_50,K_vicon_50Hz[0],K_vicon_50Hz[1],K_vicon_50Hz[2],x_y_aposteriori_k,posY,vicon_updated,addNoise,sigma,x_y_aposteriori); - memcpy(x_y_aposteriori_k, x_y_aposteriori, sizeof(x_y_aposteriori)); - /* z-position/velocity estimation in earth frame = vicon frame */ - float z_est = 0.0f; - float local_sigma = 0.0f; - if (flag_baro_initialized && flag_use_baro) { - z_est = -p0_Pa*logf(p0_Pa/(sensor.baro_pres_mbar*100.0f))/(rho0*const_earth_gravity); - K[0] = K_vicon_50Hz[0]; - K[1] = K_vicon_50Hz[1]; - K[2] = K_vicon_50Hz[2]; - vicon_updated = 1; /* always enable the update, cause baro update = 200 Hz */ - local_sigma = 0.0f; /* don't add noise on barometer in any case */ - } else { - z_est = posZ; - K[0] = K_vicon_50Hz[0]; - K[1] = K_vicon_50Hz[1]; - K[2] = K_vicon_50Hz[2]; - local_sigma = sigma; - } - kalman_dlqe3(dT_const_50,K[0],K[1],K[2],x_z_aposteriori_k,z_est,vicon_updated,addNoise,local_sigma,x_z_aposteriori); - memcpy(x_z_aposteriori_k, x_z_aposteriori, sizeof(x_z_aposteriori)); - local_pos_est.x = x_x_aposteriori_k[0]; - local_pos_est.vx = x_x_aposteriori_k[1]; - local_pos_est.y = x_y_aposteriori_k[0]; - local_pos_est.vy = x_y_aposteriori_k[1]; - local_pos_est.z = x_z_aposteriori_k[0]; - local_pos_est.vz = x_z_aposteriori_k[1]; - local_pos_est.timestamp = hrt_absolute_time(); - if ((isfinite(x_x_aposteriori_k[0])) && (isfinite(x_x_aposteriori_k[1])) && (isfinite(x_y_aposteriori_k[0])) && (isfinite(x_y_aposteriori_k[1])) && (isfinite(x_z_aposteriori_k[0])) && (isfinite(x_z_aposteriori_k[1]))){ - if(local_pos_est_pub > 0) - orb_publish(ORB_ID(vehicle_local_position), local_pos_est_pub, &local_pos_est); - else - local_pos_est_pub = orb_advertise(ORB_ID(vehicle_local_position), &local_pos_est); - //char buf[0xff]; sprintf(buf,"[pos_est_mc] x:%f, y:%f, z:%f",x_x_aposteriori_k[0],x_y_aposteriori_k[0],x_z_aposteriori_k[0]); - //mavlink_log_info(mavlink_fd, buf); - } - } - } /* end of poll return value check */ - } - - printf("[pos_est_mc] exiting.\n"); - mavlink_log_info(mavlink_fd, "[pos_est_mc] exiting"); - thread_running = false; - return 0; -} diff --git a/src/modules/px4iofirmware/controls.c b/src/modules/px4iofirmware/controls.c index 941500f0d..62e6b12cb 100644 --- a/src/modules/px4iofirmware/controls.c +++ b/src/modules/px4iofirmware/controls.c @@ -134,8 +134,6 @@ controls_tick() { perf_begin(c_gather_sbus); - bool sbus_status = (r_status_flags & PX4IO_P_STATUS_FLAGS_RC_SBUS); - bool sbus_failsafe, sbus_frame_drop; bool sbus_updated = sbus_input(r_raw_rc_values, &r_raw_rc_count, &sbus_failsafe, &sbus_frame_drop, PX4IO_RC_INPUT_CHANNELS); @@ -201,94 +199,105 @@ controls_tick() { /* update RC-received timestamp */ system_state.rc_channels_timestamp_received = hrt_absolute_time(); - /* do not command anything in failsafe, kick in the RC loss counter */ - if (!(r_raw_rc_flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE)) { - - /* update RC-received timestamp */ - system_state.rc_channels_timestamp_valid = system_state.rc_channels_timestamp_received; - - /* map raw inputs to mapped inputs */ - /* XXX mapping should be atomic relative to protocol */ - for (unsigned i = 0; i < r_raw_rc_count; i++) { - - /* map the input channel */ - uint16_t *conf = &r_page_rc_input_config[i * PX4IO_P_RC_CONFIG_STRIDE]; - - if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_ENABLED) { - - uint16_t raw = r_raw_rc_values[i]; - - int16_t scaled; - - /* - * 1) Constrain to min/max values, as later processing depends on bounds. - */ - if (raw < conf[PX4IO_P_RC_CONFIG_MIN]) - raw = conf[PX4IO_P_RC_CONFIG_MIN]; - if (raw > conf[PX4IO_P_RC_CONFIG_MAX]) - raw = conf[PX4IO_P_RC_CONFIG_MAX]; - - /* - * 2) Scale around the mid point differently for lower and upper range. - * - * This is necessary as they don't share the same endpoints and slope. - * - * First normalize to 0..1 range with correct sign (below or above center), - * then scale to 20000 range (if center is an actual center, -10000..10000, - * if parameters only support half range, scale to 10000 range, e.g. if - * center == min 0..10000, if center == max -10000..0). - * - * As the min and max bounds were enforced in step 1), division by zero - * cannot occur, as for the case of center == min or center == max the if - * statement is mutually exclusive with the arithmetic NaN case. - * - * DO NOT REMOVE OR ALTER STEP 1! - */ - if (raw > (conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE])) { - scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_MAX] - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE])); - - } else if (raw < (conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE])) { - scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE] - conf[PX4IO_P_RC_CONFIG_MIN])); - - } else { - /* in the configured dead zone, output zero */ - scaled = 0; - } - - /* invert channel if requested */ - if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_REVERSE) - scaled = -scaled; + /* update RC-received timestamp */ + system_state.rc_channels_timestamp_valid = system_state.rc_channels_timestamp_received; + + /* map raw inputs to mapped inputs */ + /* XXX mapping should be atomic relative to protocol */ + for (unsigned i = 0; i < r_raw_rc_count; i++) { + + /* map the input channel */ + uint16_t *conf = &r_page_rc_input_config[i * PX4IO_P_RC_CONFIG_STRIDE]; + + if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_ENABLED) { + + uint16_t raw = r_raw_rc_values[i]; + + int16_t scaled; + + /* + * 1) Constrain to min/max values, as later processing depends on bounds. + */ + if (raw < conf[PX4IO_P_RC_CONFIG_MIN]) + raw = conf[PX4IO_P_RC_CONFIG_MIN]; + if (raw > conf[PX4IO_P_RC_CONFIG_MAX]) + raw = conf[PX4IO_P_RC_CONFIG_MAX]; + + /* + * 2) Scale around the mid point differently for lower and upper range. + * + * This is necessary as they don't share the same endpoints and slope. + * + * First normalize to 0..1 range with correct sign (below or above center), + * then scale to 20000 range (if center is an actual center, -10000..10000, + * if parameters only support half range, scale to 10000 range, e.g. if + * center == min 0..10000, if center == max -10000..0). + * + * As the min and max bounds were enforced in step 1), division by zero + * cannot occur, as for the case of center == min or center == max the if + * statement is mutually exclusive with the arithmetic NaN case. + * + * DO NOT REMOVE OR ALTER STEP 1! + */ + if (raw > (conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE])) { + scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_MAX] - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE])); + + } else if (raw < (conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE])) { + scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE] - conf[PX4IO_P_RC_CONFIG_MIN])); + + } else { + /* in the configured dead zone, output zero */ + scaled = 0; + } - /* and update the scaled/mapped version */ - unsigned mapped = conf[PX4IO_P_RC_CONFIG_ASSIGNMENT]; - if (mapped < PX4IO_CONTROL_CHANNELS) { + /* invert channel if requested */ + if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_REVERSE) { + scaled = -scaled; + } - /* invert channel if pitch - pulling the lever down means pitching up by convention */ - if (mapped == 1) /* roll, pitch, yaw, throttle, override is the standard order */ - scaled = -scaled; + /* and update the scaled/mapped version */ + unsigned mapped = conf[PX4IO_P_RC_CONFIG_ASSIGNMENT]; + if (mapped < PX4IO_CONTROL_CHANNELS) { - r_rc_values[mapped] = SIGNED_TO_REG(scaled); - assigned_channels |= (1 << mapped); + /* invert channel if pitch - pulling the lever down means pitching up by convention */ + if (mapped == 1) { + /* roll, pitch, yaw, throttle, override is the standard order */ + scaled = -scaled; + } + if (mapped == 3 && r_setup_rc_thr_failsafe) { + /* throttle failsafe detection */ + if (((raw < conf[PX4IO_P_RC_CONFIG_MIN]) && (raw < r_setup_rc_thr_failsafe)) || + ((raw > conf[PX4IO_P_RC_CONFIG_MAX]) && (raw > r_setup_rc_thr_failsafe))) { + r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_FAILSAFE; + } else { + r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FAILSAFE); + } } + + r_rc_values[mapped] = SIGNED_TO_REG(scaled); + assigned_channels |= (1 << mapped); + } } + } - /* set un-assigned controls to zero */ - for (unsigned i = 0; i < PX4IO_CONTROL_CHANNELS; i++) { - if (!(assigned_channels & (1 << i))) - r_rc_values[i] = 0; + /* set un-assigned controls to zero */ + for (unsigned i = 0; i < PX4IO_CONTROL_CHANNELS; i++) { + if (!(assigned_channels & (1 << i))) { + r_rc_values[i] = 0; } + } - /* set RC OK flag, as we got an update */ - r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_OK; + /* set RC OK flag, as we got an update */ + r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_OK; + r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_RC_OK; - /* if we have enough channels (5) to control the vehicle, the mapping is ok */ - if (assigned_channels > 4) { - r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_MAPPING_OK; - } else { - r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_MAPPING_OK); - } + /* if we have enough channels (5) to control the vehicle, the mapping is ok */ + if (assigned_channels > 4) { + r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_MAPPING_OK; + } else { + r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_MAPPING_OK); } /* @@ -316,37 +325,42 @@ controls_tick() { * Handle losing RC input */ - /* this kicks in if the receiver is gone or the system went to failsafe */ - if (rc_input_lost || (r_raw_rc_flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE)) { + /* if we are in failsafe, clear the override flag */ + if (r_raw_rc_flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE) { + r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_OVERRIDE); + } + + /* this kicks in if the receiver is gone, but there is not on failsafe (indicated by separate flag) */ + if (rc_input_lost) { /* Clear the RC input status flag, clear manual override flag */ r_status_flags &= ~( PX4IO_P_STATUS_FLAGS_OVERRIDE | PX4IO_P_STATUS_FLAGS_RC_OK); + /* flag raw RC as lost */ + r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_RC_OK); + /* Mark all channels as invalid, as we just lost the RX */ r_rc_valid = 0; + /* Set raw channel count to zero */ + r_raw_rc_count = 0; + /* Set the RC_LOST alarm */ r_status_alarms |= PX4IO_P_STATUS_ALARMS_RC_LOST; } - /* this kicks in if the receiver is completely gone */ - if (rc_input_lost) { - - /* Set channel count to zero */ - r_raw_rc_count = 0; - } - /* * Check for manual override. * * The PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK flag must be set, and we - * must have R/C input. + * must have R/C input (NO FAILSAFE!). * Override is enabled if either the hardcoded channel / value combination * is selected, or the AP has requested it. */ if ((r_setup_arming & PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK) && - (r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK)) { + (r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK) && + !(r_raw_rc_flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE)) { bool override = false; @@ -369,10 +383,10 @@ controls_tick() { mixer_tick(); } else { - r_status_flags &= ~PX4IO_P_STATUS_FLAGS_OVERRIDE; + r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_OVERRIDE); } } else { - r_status_flags &= ~PX4IO_P_STATUS_FLAGS_OVERRIDE; + r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_OVERRIDE); } } @@ -395,8 +409,9 @@ ppm_input(uint16_t *values, uint16_t *num_values, uint16_t *frame_len) if (*num_values > PX4IO_RC_INPUT_CHANNELS) *num_values = PX4IO_RC_INPUT_CHANNELS; - for (unsigned i = 0; i < *num_values; i++) + for (unsigned i = 0; i < *num_values; i++) { values[i] = ppm_buffer[i]; + } /* clear validity */ ppm_last_valid_decode = 0; diff --git a/src/modules/px4iofirmware/mixer.cpp b/src/modules/px4iofirmware/mixer.cpp index 9558198f3..ebf4f3e8e 100644 --- a/src/modules/px4iofirmware/mixer.cpp +++ b/src/modules/px4iofirmware/mixer.cpp @@ -254,10 +254,25 @@ mixer_tick(void) for (unsigned i = 0; i < PX4IO_SERVO_COUNT; i++) up_pwm_servo_set(i, r_page_servos[i]); + /* set S.BUS1 or S.BUS2 outputs */ + + if (r_setup_features & PX4IO_P_SETUP_FEATURES_SBUS2_OUT) { + sbus2_output(r_page_servos, PX4IO_SERVO_COUNT); + } else if (r_setup_features & PX4IO_P_SETUP_FEATURES_SBUS1_OUT) { + sbus1_output(r_page_servos, PX4IO_SERVO_COUNT); + } + } else if (mixer_servos_armed && should_always_enable_pwm) { /* set the disarmed servo outputs. */ for (unsigned i = 0; i < PX4IO_SERVO_COUNT; i++) up_pwm_servo_set(i, r_page_servo_disarmed[i]); + + /* set S.BUS1 or S.BUS2 outputs */ + if (r_setup_features & PX4IO_P_SETUP_FEATURES_SBUS1_OUT) + sbus1_output(r_page_servos, PX4IO_SERVO_COUNT); + + if (r_setup_features & PX4IO_P_SETUP_FEATURES_SBUS2_OUT) + sbus2_output(r_page_servos, PX4IO_SERVO_COUNT); } } diff --git a/src/modules/px4iofirmware/protocol.h b/src/modules/px4iofirmware/protocol.h index d48c6c529..7471faec7 100644 --- a/src/modules/px4iofirmware/protocol.h +++ b/src/modules/px4iofirmware/protocol.h @@ -142,6 +142,7 @@ #define PX4IO_P_RAW_RC_FLAGS_FAILSAFE (1 << 1) /* receiver is in failsafe mode */ #define PX4IO_P_RAW_RC_FLAGS_RC_DSM11 (1 << 2) /* DSM decoding is 11 bit mode */ #define PX4IO_P_RAW_RC_FLAGS_MAPPING_OK (1 << 3) /* Channel mapping is ok */ +#define PX4IO_P_RAW_RC_FLAGS_RC_OK (1 << 4) /* RC reception ok */ #define PX4IO_P_RAW_RC_NRSSI 2 /* [2] Normalized RSSI value, 0: no reception, 255: perfect reception */ #define PX4IO_P_RAW_RC_DATA 3 /* [1] + [2] Details about the RC source (PPM frame length, Spektrum protocol type) */ @@ -164,10 +165,10 @@ /* setup page */ #define PX4IO_PAGE_SETUP 50 #define PX4IO_P_SETUP_FEATURES 0 -#define PX4IO_P_SETUP_FEATURES_SBUS1_OUT (1 << 0) /* enable S.Bus v1 output */ -#define PX4IO_P_SETUP_FEATURES_SBUS2_OUT (1 << 1) /* enable S.Bus v2 output */ -#define PX4IO_P_SETUP_FEATURES_PWM_RSSI (1 << 2) /* enable PWM RSSI parsing */ -#define PX4IO_P_SETUP_FEATURES_ADC_RSSI (1 << 3) /* enable ADC RSSI parsing */ +#define PX4IO_P_SETUP_FEATURES_SBUS1_OUT (1 << 0) /**< enable S.Bus v1 output */ +#define PX4IO_P_SETUP_FEATURES_SBUS2_OUT (1 << 1) /**< enable S.Bus v2 output */ +#define PX4IO_P_SETUP_FEATURES_PWM_RSSI (1 << 2) /**< enable PWM RSSI parsing */ +#define PX4IO_P_SETUP_FEATURES_ADC_RSSI (1 << 3) /**< enable ADC RSSI parsing */ #define PX4IO_P_SETUP_ARMING 1 /* arming controls */ #define PX4IO_P_SETUP_ARMING_IO_ARM_OK (1 << 0) /* OK to arm the IO side */ @@ -189,6 +190,8 @@ #define PX4IO_P_SETUP_RELAYS_POWER2 (1<<1) /* hardware rev [1] power relay 2 */ #define PX4IO_P_SETUP_RELAYS_ACC1 (1<<2) /* hardware rev [1] accessory power 1 */ #define PX4IO_P_SETUP_RELAYS_ACC2 (1<<3) /* hardware rev [1] accessory power 2 */ +#else +#define PX4IO_P_SETUP_RELAYS_PAD 5 #endif #define PX4IO_P_SETUP_VBATT_SCALE 6 /* hardware rev [1] battery voltage correction factor (float) */ @@ -201,26 +204,33 @@ enum { /* DSM bind states */ dsm_bind_send_pulses, dsm_bind_reinit_uart }; - /* 8 */ -#define PX4IO_P_SETUP_SET_DEBUG 9 /* debug level for IO board */ + /* 8 */ +#define PX4IO_P_SETUP_SET_DEBUG 9 /* debug level for IO board */ -#define PX4IO_P_SETUP_REBOOT_BL 10 /* reboot IO into bootloader */ -#define PX4IO_REBOOT_BL_MAGIC 14662 /* required argument for reboot (random) */ +#define PX4IO_P_SETUP_REBOOT_BL 10 /* reboot IO into bootloader */ +#define PX4IO_REBOOT_BL_MAGIC 14662 /* required argument for reboot (random) */ -#define PX4IO_P_SETUP_CRC 11 /* get CRC of IO firmware */ +#define PX4IO_P_SETUP_CRC 11 /* get CRC of IO firmware */ + /* storage space of 12 occupied by CRC */ +#define PX4IO_P_SETUP_FORCE_SAFETY_OFF 12 /* force safety switch into + 'armed' (PWM enabled) state - this is a non-data write and + hence index 12 can safely be used. */ +#define PX4IO_P_SETUP_RC_THR_FAILSAFE_US 13 /**< the throttle failsafe pulse length in microseconds */ + +#define PX4IO_FORCE_SAFETY_MAGIC 22027 /* required argument for force safety (random) */ /* autopilot control values, -10000..10000 */ -#define PX4IO_PAGE_CONTROLS 51 /**< actuator control groups, one after the other, 8 wide */ +#define PX4IO_PAGE_CONTROLS 51 /**< actuator control groups, one after the other, 8 wide */ #define PX4IO_P_CONTROLS_GROUP_0 (PX4IO_PROTOCOL_MAX_CONTROL_COUNT * 0) /**< 0..PX4IO_PROTOCOL_MAX_CONTROL_COUNT - 1 */ #define PX4IO_P_CONTROLS_GROUP_1 (PX4IO_PROTOCOL_MAX_CONTROL_COUNT * 1) /**< 0..PX4IO_PROTOCOL_MAX_CONTROL_COUNT - 1 */ #define PX4IO_P_CONTROLS_GROUP_2 (PX4IO_PROTOCOL_MAX_CONTROL_COUNT * 2) /**< 0..PX4IO_PROTOCOL_MAX_CONTROL_COUNT - 1 */ #define PX4IO_P_CONTROLS_GROUP_3 (PX4IO_PROTOCOL_MAX_CONTROL_COUNT * 3) /**< 0..PX4IO_PROTOCOL_MAX_CONTROL_COUNT - 1 */ #define PX4IO_P_CONTROLS_GROUP_VALID 64 -#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP0 (1 << 0) /* group 0 is valid / received */ -#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP1 (1 << 1) /* group 1 is valid / received */ -#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP2 (1 << 2) /* group 2 is valid / received */ -#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP3 (1 << 3) /* group 3 is valid / received */ +#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP0 (1 << 0) /**< group 0 is valid / received */ +#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP1 (1 << 1) /**< group 1 is valid / received */ +#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP2 (1 << 2) /**< group 2 is valid / received */ +#define PX4IO_P_CONTROLS_GROUP_VALID_GROUP3 (1 << 3) /**< group 3 is valid / received */ /* raw text load to the mixer parser - ignores offset */ #define PX4IO_PAGE_MIXERLOAD 52 diff --git a/src/modules/px4iofirmware/px4io.h b/src/modules/px4iofirmware/px4io.h index 54c5663a5..ca175bfbc 100644 --- a/src/modules/px4iofirmware/px4io.h +++ b/src/modules/px4iofirmware/px4io.h @@ -108,6 +108,7 @@ extern uint16_t r_page_servo_disarmed[]; /* PX4IO_PAGE_DISARMED_PWM */ #ifdef CONFIG_ARCH_BOARD_PX4IO_V1 #define r_setup_relays r_page_setup[PX4IO_P_SETUP_RELAYS] #endif +#define r_setup_rc_thr_failsafe r_page_setup[PX4IO_P_SETUP_RC_THR_FAILSAFE_US] #define r_control_values (&r_page_controls[0]) @@ -218,6 +219,8 @@ extern bool dsm_input(uint16_t *values, uint16_t *num_values); extern void dsm_bind(uint16_t cmd, int pulses); extern int sbus_init(const char *device); extern bool sbus_input(uint16_t *values, uint16_t *num_values, bool *sbus_failsafe, bool *sbus_frame_drop, uint16_t max_channels); +extern bool sbus1_output(uint16_t *values, uint16_t num_values); +extern bool sbus2_output(uint16_t *values, uint16_t num_values); /** global debug level for isr_debug() */ extern volatile uint8_t debug_level; diff --git a/src/modules/px4iofirmware/registers.c b/src/modules/px4iofirmware/registers.c index 97d25bbfa..db1836f4a 100644 --- a/src/modules/px4iofirmware/registers.c +++ b/src/modules/px4iofirmware/registers.c @@ -160,6 +160,9 @@ volatile uint16_t r_page_setup[] = [PX4IO_P_SETUP_PWM_ALTRATE] = 200, #ifdef CONFIG_ARCH_BOARD_PX4IO_V1 [PX4IO_P_SETUP_RELAYS] = 0, +#else + /* this is unused, but we will pad it for readability (the compiler pads it automatically) */ + [PX4IO_P_SETUP_RELAYS_PAD] = 0, #endif #ifdef ADC_VSERVO [PX4IO_P_SETUP_VSERVO_SCALE] = 10000, @@ -169,6 +172,7 @@ volatile uint16_t r_page_setup[] = [PX4IO_P_SETUP_SET_DEBUG] = 0, [PX4IO_P_SETUP_REBOOT_BL] = 0, [PX4IO_P_SETUP_CRC ... (PX4IO_P_SETUP_CRC+1)] = 0, + [PX4IO_P_SETUP_RC_THR_FAILSAFE_US] = 0, }; #ifdef CONFIG_ARCH_BOARD_PX4IO_V2 @@ -462,9 +466,18 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value) #ifdef ENABLE_SBUS_OUT ENABLE_SBUS_OUT(value & (PX4IO_P_SETUP_FEATURES_SBUS1_OUT | PX4IO_P_SETUP_FEATURES_SBUS2_OUT)); - /* disable the conflicting options */ - if (value & (PX4IO_P_SETUP_FEATURES_SBUS1_OUT | PX4IO_P_SETUP_FEATURES_SBUS2_OUT)) { - value &= ~(PX4IO_P_SETUP_FEATURES_PWM_RSSI | PX4IO_P_SETUP_FEATURES_ADC_RSSI); + /* disable the conflicting options with SBUS 1 */ + if (value & (PX4IO_P_SETUP_FEATURES_SBUS1_OUT)) { + value &= ~(PX4IO_P_SETUP_FEATURES_PWM_RSSI | + PX4IO_P_SETUP_FEATURES_ADC_RSSI | + PX4IO_P_SETUP_FEATURES_SBUS2_OUT); + } + + /* disable the conflicting options with SBUS 2 */ + if (value & (PX4IO_P_SETUP_FEATURES_SBUS2_OUT)) { + value &= ~(PX4IO_P_SETUP_FEATURES_PWM_RSSI | + PX4IO_P_SETUP_FEATURES_ADC_RSSI | + PX4IO_P_SETUP_FEATURES_SBUS1_OUT); } #endif @@ -513,18 +526,22 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value) break; case PX4IO_P_SETUP_PWM_DEFAULTRATE: - if (value < 50) + if (value < 50) { value = 50; - if (value > 400) + } + if (value > 400) { value = 400; + } pwm_configure_rates(r_setup_pwm_rates, value, r_setup_pwm_altrate); break; case PX4IO_P_SETUP_PWM_ALTRATE: - if (value < 50) + if (value < 50) { value = 50; - if (value > 400) + } + if (value > 400) { value = 400; + } pwm_configure_rates(r_setup_pwm_rates, r_setup_pwm_defaultrate, value); break; @@ -556,8 +573,9 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value) } // check the magic value - if (value != PX4IO_REBOOT_BL_MAGIC) + if (value != PX4IO_REBOOT_BL_MAGIC) { break; + } // we schedule a reboot rather than rebooting // immediately to allow the IO board to ACK @@ -569,6 +587,18 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value) dsm_bind(value & 0x0f, (value >> 4) & 0xF); break; + case PX4IO_P_SETUP_FORCE_SAFETY_OFF: + if (value == PX4IO_FORCE_SAFETY_MAGIC) { + r_status_flags |= PX4IO_P_STATUS_FLAGS_SAFETY_OFF; + } + break; + + case PX4IO_P_SETUP_RC_THR_FAILSAFE_US: + if (value > 650 && value < 2350) { + r_page_setup[PX4IO_P_SETUP_RC_THR_FAILSAFE_US] = value; + } + break; + default: return -1; } diff --git a/src/modules/px4iofirmware/sbus.c b/src/modules/px4iofirmware/sbus.c index f6ec542eb..0e7dc621c 100644 --- a/src/modules/px4iofirmware/sbus.c +++ b/src/modules/px4iofirmware/sbus.c @@ -93,7 +93,7 @@ int sbus_init(const char *device) { if (sbus_fd < 0) - sbus_fd = open(device, O_RDONLY | O_NONBLOCK); + sbus_fd = open(device, O_RDWR | O_NONBLOCK); if (sbus_fd >= 0) { struct termios t; @@ -113,11 +113,22 @@ sbus_init(const char *device) } else { debug("S.Bus: open failed"); } - return sbus_fd; } bool +sbus1_output(uint16_t *values, uint16_t num_values) +{ + write(sbus_fd, 'A', 1); +} + +bool +sbus2_output(uint16_t *values, uint16_t num_values) +{ + write(sbus_fd, 'B', 1); +} + +bool sbus_input(uint16_t *values, uint16_t *num_values, bool *sbus_failsafe, bool *sbus_frame_drop, uint16_t max_channels) { ssize_t ret; diff --git a/src/modules/sdlog/module.mk b/src/modules/sdlog/module.mk deleted file mode 100644 index 89da2d827..000000000 --- a/src/modules/sdlog/module.mk +++ /dev/null @@ -1,43 +0,0 @@ -############################################################################ -# -# Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved. -# -# Redistribution and use in source and binary forms, with or without -# modification, are permitted provided that the following conditions -# are met: -# -# 1. Redistributions of source code must retain the above copyright -# notice, this list of conditions and the following disclaimer. -# 2. Redistributions in binary form must reproduce the above copyright -# notice, this list of conditions and the following disclaimer in -# the documentation and/or other materials provided with the -# distribution. -# 3. Neither the name PX4 nor the names of its contributors may be -# used to endorse or promote products derived from this software -# without specific prior written permission. -# -# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS -# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT -# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS -# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE -# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, -# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, -# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS -# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED -# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT -# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN -# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE -# POSSIBILITY OF SUCH DAMAGE. -# -############################################################################ - -# -# sdlog Application -# - -MODULE_COMMAND = sdlog -# The main thread only buffers to RAM, needs a high priority -MODULE_PRIORITY = "SCHED_PRIORITY_MAX-30" - -SRCS = sdlog.c \ - sdlog_ringbuffer.c diff --git a/src/modules/sdlog/sdlog.c b/src/modules/sdlog/sdlog.c deleted file mode 100644 index c22523bf2..000000000 --- a/src/modules/sdlog/sdlog.c +++ /dev/null @@ -1,840 +0,0 @@ -/**************************************************************************** - * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: Lorenz Meier <lm@inf.ethz.ch> - * - * Redistribution and use in source and binary forms, with or without - * modification, are permitted provided that the following conditions - * are met: - * - * 1. Redistributions of source code must retain the above copyright - * notice, this list of conditions and the following disclaimer. - * 2. Redistributions in binary form must reproduce the above copyright - * notice, this list of conditions and the following disclaimer in - * the documentation and/or other materials provided with the - * distribution. - * 3. Neither the name PX4 nor the names of its contributors may be - * used to endorse or promote products derived from this software - * without specific prior written permission. - * - * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS - * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT - * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS - * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE - * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, - * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, - * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS - * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED - * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT - * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN - * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE - * POSSIBILITY OF SUCH DAMAGE. - * - ****************************************************************************/ - -/** - * @file sdlog.c - * @author Lorenz Meier <lm@inf.ethz.ch> - * - * Simple SD logger for flight data. Buffers new sensor values and - * does the heavy SD I/O in a low-priority worker thread. - */ - -#include <nuttx/config.h> -#include <sys/types.h> -#include <sys/stat.h> -#include <sys/prctl.h> -#include <fcntl.h> -#include <errno.h> -#include <unistd.h> -#include <stdio.h> -#include <poll.h> -#include <stdlib.h> -#include <string.h> -#include <ctype.h> -#include <systemlib/err.h> -#include <unistd.h> -#include <drivers/drv_hrt.h> - -#include <uORB/uORB.h> -#include <uORB/topics/sensor_combined.h> -#include <uORB/topics/vehicle_attitude.h> -#include <uORB/topics/vehicle_attitude_setpoint.h> -#include <uORB/topics/actuator_outputs.h> -#include <uORB/topics/actuator_controls.h> -#include <uORB/topics/actuator_controls_effective.h> -#include <uORB/topics/vehicle_command.h> -#include <uORB/topics/vehicle_local_position.h> -#include <uORB/topics/vehicle_global_position.h> -#include <uORB/topics/vehicle_gps_position.h> -#include <uORB/topics/vehicle_vicon_position.h> -#include <uORB/topics/optical_flow.h> -#include <uORB/topics/battery_status.h> -#include <uORB/topics/differential_pressure.h> -#include <uORB/topics/airspeed.h> - -#include <systemlib/systemlib.h> - -#include <mavlink/mavlink_log.h> - -#include "sdlog_ringbuffer.h" - -static bool thread_should_exit = false; /**< Deamon exit flag */ -static bool thread_running = false; /**< Deamon status flag */ -static int deamon_task; /**< Handle of deamon task / thread */ -static const int MAX_NO_LOGFOLDER = 999; /**< Maximum number of log folders */ - -static const char *mountpoint = "/fs/microsd"; -static const char *mfile_in = "/etc/logging/logconv.m"; -int sysvector_file = -1; -int mavlink_fd = -1; -struct sdlog_logbuffer lb; - -/* mutex / condition to synchronize threads */ -pthread_mutex_t sysvector_mutex; -pthread_cond_t sysvector_cond; - -/** - * System state vector log buffer writing - */ -static void *sdlog_sysvector_write_thread(void *arg); - -/** - * Create the thread to write the system vector - */ -pthread_t sysvector_write_start(struct sdlog_logbuffer *logbuf); - -/** - * SD log management function. - */ -__EXPORT int sdlog_main(int argc, char *argv[]); - -/** - * Mainloop of sd log deamon. - */ -int sdlog_thread_main(int argc, char *argv[]); - -/** - * Print the correct usage. - */ -static void usage(const char *reason); - -static int file_exist(const char *filename); - -static int file_copy(const char *file_old, const char *file_new); - -static void handle_command(struct vehicle_command_s *cmd); - -/** - * Print the current status. - */ -static void print_sdlog_status(void); - -/** - * Create folder for current logging session. - */ -static int create_logfolder(char *folder_path); - -static void -usage(const char *reason) -{ - if (reason) - fprintf(stderr, "%s\n", reason); - - errx(1, "usage: sdlog {start|stop|status} [-s <number of skipped lines>]\n\n"); -} - -// XXX turn this into a C++ class -unsigned sensor_combined_bytes = 0; -unsigned actuator_outputs_bytes = 0; -unsigned actuator_controls_bytes = 0; -unsigned sysvector_bytes = 0; -unsigned blackbox_file_bytes = 0; -uint64_t starttime = 0; - -/* logging on or off, default to true */ -bool logging_enabled = true; - -/** - * The sd log deamon app only briefly exists to start - * the background job. The stack size assigned in the - * Makefile does only apply to this management task. - * - * The actual stack size should be set in the call - * to task_spawn_cmd(). - */ -int sdlog_main(int argc, char *argv[]) -{ - if (argc < 1) - usage("missing command"); - - if (!strcmp(argv[1], "start")) { - - if (thread_running) { - printf("sdlog already running\n"); - /* this is not an error */ - exit(0); - } - - thread_should_exit = false; - deamon_task = task_spawn_cmd("sdlog", - SCHED_DEFAULT, - SCHED_PRIORITY_DEFAULT - 30, - 4096, - sdlog_thread_main, - (const char **)argv); - exit(0); - } - - if (!strcmp(argv[1], "stop")) { - if (!thread_running) { - printf("\tsdlog is not started\n"); - } - - thread_should_exit = true; - exit(0); - } - - if (!strcmp(argv[1], "status")) { - if (thread_running) { - print_sdlog_status(); - - } else { - printf("\tsdlog not started\n"); - } - - exit(0); - } - - usage("unrecognized command"); - exit(1); -} - -int create_logfolder(char *folder_path) -{ - /* make folder on sdcard */ - uint16_t foldernumber = 1; // start with folder 0001 - int mkdir_ret; - - /* look for the next folder that does not exist */ - while (foldernumber < MAX_NO_LOGFOLDER) { - /* set up file path: e.g. /mnt/sdcard/sensorfile0001.txt */ - sprintf(folder_path, "%s/session%04u", mountpoint, foldernumber); - mkdir_ret = mkdir(folder_path, S_IRWXU | S_IRWXG | S_IRWXO); - /* the result is -1 if the folder exists */ - - if (mkdir_ret == 0) { - /* folder does not exist, success */ - - /* now copy the Matlab/Octave file */ - char mfile_out[100]; - sprintf(mfile_out, "%s/session%04u/run_to_plot_data.m", mountpoint, foldernumber); - int ret = file_copy(mfile_in, mfile_out); - - if (!ret) { - warnx("copied m file to %s", mfile_out); - - } else { - warnx("failed copying m file from %s to\n %s", mfile_in, mfile_out); - } - - break; - - } else if (mkdir_ret == -1) { - /* folder exists already */ - foldernumber++; - continue; - - } else { - warn("failed creating new folder"); - return -1; - } - } - - if (foldernumber >= MAX_NO_LOGFOLDER) { - /* we should not end up here, either we have more than MAX_NO_LOGFOLDER on the SD card, or another problem */ - warn("all %d possible folders exist already", MAX_NO_LOGFOLDER); - return -1; - } - - return 0; -} - - -static void * -sdlog_sysvector_write_thread(void *arg) -{ - /* set name */ - prctl(PR_SET_NAME, "sdlog microSD I/O", 0); - - struct sdlog_logbuffer *logbuf = (struct sdlog_logbuffer *)arg; - - int poll_count = 0; - struct sdlog_sysvector sysvect; - memset(&sysvect, 0, sizeof(sysvect)); - - while (!thread_should_exit) { - - /* make sure threads are synchronized */ - pthread_mutex_lock(&sysvector_mutex); - - /* only wait if no data is available to process */ - if (sdlog_logbuffer_is_empty(logbuf)) { - /* blocking wait for new data at this line */ - pthread_cond_wait(&sysvector_cond, &sysvector_mutex); - } - - /* only quickly load data, do heavy I/O a few lines down */ - int ret = sdlog_logbuffer_read(logbuf, &sysvect); - /* continue */ - pthread_mutex_unlock(&sysvector_mutex); - - if (ret == OK) { - sysvector_bytes += write(sysvector_file, (const char *)&sysvect, sizeof(sysvect)); - } - - if (poll_count % 100 == 0) { - fsync(sysvector_file); - } - - poll_count++; - } - - fsync(sysvector_file); - - return OK; -} - -pthread_t -sysvector_write_start(struct sdlog_logbuffer *logbuf) -{ - pthread_attr_t receiveloop_attr; - pthread_attr_init(&receiveloop_attr); - - struct sched_param param; - /* low priority, as this is expensive disk I/O */ - param.sched_priority = SCHED_PRIORITY_DEFAULT - 40; - (void)pthread_attr_setschedparam(&receiveloop_attr, ¶m); - - pthread_attr_setstacksize(&receiveloop_attr, 2048); - - pthread_t thread; - pthread_create(&thread, &receiveloop_attr, sdlog_sysvector_write_thread, logbuf); - return thread; - - // XXX we have to destroy the attr at some point -} - - -int sdlog_thread_main(int argc, char *argv[]) -{ - mavlink_fd = open(MAVLINK_LOG_DEVICE, 0); - - if (mavlink_fd < 0) { - warnx("ERROR: Failed to open MAVLink log stream, start mavlink app first.\n"); - } - - /* log every n'th value (skip three per default) */ - int skip_value = 3; - - /* work around some stupidity in task_create's argv handling */ - argc -= 2; - argv += 2; - int ch; - - while ((ch = getopt(argc, argv, "s:r")) != EOF) { - switch (ch) { - case 's': - { - /* log only every n'th (gyro clocked) value */ - unsigned s = strtoul(optarg, NULL, 10); - - if (s < 1 || s > 250) { - errx(1, "Wrong skip value of %d, out of range (1..250)\n", s); - } else { - skip_value = s; - } - } - break; - - case 'r': - /* log only on request, disable logging per default */ - logging_enabled = false; - break; - - case '?': - if (optopt == 'c') { - warnx("Option -%c requires an argument.\n", optopt); - } else if (isprint(optopt)) { - warnx("Unknown option `-%c'.\n", optopt); - } else { - warnx("Unknown option character `\\x%x'.\n", optopt); - } - - default: - usage("unrecognized flag"); - errx(1, "exiting."); - } - } - - if (file_exist(mountpoint) != OK) { - errx(1, "logging mount point %s not present, exiting.", mountpoint); - } - - char folder_path[64]; - - if (create_logfolder(folder_path)) - errx(1, "unable to create logging folder, exiting."); - - FILE *gpsfile; - FILE *blackbox_file; - - /* string to hold the path to the sensorfile */ - char path_buf[64] = ""; - - /* only print logging path, important to find log file later */ - warnx("logging to directory %s\n", folder_path); - - /* set up file path: e.g. /mnt/sdcard/session0001/actuator_controls0.bin */ - sprintf(path_buf, "%s/%s.bin", folder_path, "sysvector"); - - if (0 == (sysvector_file = open(path_buf, O_CREAT | O_WRONLY | O_DSYNC))) { - errx(1, "opening %s failed.\n", path_buf); - } - - /* set up file path: e.g. /mnt/sdcard/session0001/gps.txt */ - sprintf(path_buf, "%s/%s.txt", folder_path, "gps"); - - if (NULL == (gpsfile = fopen(path_buf, "w"))) { - errx(1, "opening %s failed.\n", path_buf); - } - - int gpsfile_no = fileno(gpsfile); - - /* set up file path: e.g. /mnt/sdcard/session0001/blackbox.txt */ - sprintf(path_buf, "%s/%s.txt", folder_path, "blackbox"); - - if (NULL == (blackbox_file = fopen(path_buf, "w"))) { - errx(1, "opening %s failed.\n", path_buf); - } - - // XXX for fsync() calls - int blackbox_file_no = fileno(blackbox_file); - - /* --- IMPORTANT: DEFINE NUMBER OF ORB STRUCTS TO WAIT FOR HERE --- */ - /* number of messages */ - const ssize_t fdsc = 25; - /* Sanity check variable and index */ - ssize_t fdsc_count = 0; - /* file descriptors to wait for */ - struct pollfd fds[fdsc]; - - - struct { - struct sensor_combined_s raw; - struct vehicle_attitude_s att; - struct vehicle_attitude_setpoint_s att_sp; - struct actuator_outputs_s act_outputs; - struct actuator_controls_s act_controls; - struct actuator_controls_effective_s act_controls_effective; - struct vehicle_command_s cmd; - struct vehicle_local_position_s local_pos; - struct vehicle_global_position_s global_pos; - struct vehicle_gps_position_s gps_pos; - struct vehicle_vicon_position_s vicon_pos; - struct optical_flow_s flow; - struct battery_status_s batt; - struct differential_pressure_s diff_pres; - struct airspeed_s airspeed; - } buf; - memset(&buf, 0, sizeof(buf)); - - struct { - int cmd_sub; - int sensor_sub; - int att_sub; - int spa_sub; - int act_0_sub; - int controls_0_sub; - int controls_effective_0_sub; - int local_pos_sub; - int global_pos_sub; - int gps_pos_sub; - int vicon_pos_sub; - int flow_sub; - int batt_sub; - int diff_pres_sub; - int airspeed_sub; - } subs; - - /* --- MANAGEMENT - LOGGING COMMAND --- */ - /* subscribe to ORB for vehicle command */ - subs.cmd_sub = orb_subscribe(ORB_ID(vehicle_command)); - fds[fdsc_count].fd = subs.cmd_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- GPS POSITION --- */ - /* subscribe to ORB for global position */ - subs.gps_pos_sub = orb_subscribe(ORB_ID(vehicle_gps_position)); - fds[fdsc_count].fd = subs.gps_pos_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- SENSORS RAW VALUE --- */ - /* subscribe to ORB for sensors raw */ - subs.sensor_sub = orb_subscribe(ORB_ID(sensor_combined)); - fds[fdsc_count].fd = subs.sensor_sub; - /* do not rate limit, instead use skip counter (aliasing on rate limit) */ - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- ATTITUDE VALUE --- */ - /* subscribe to ORB for attitude */ - subs.att_sub = orb_subscribe(ORB_ID(vehicle_attitude)); - fds[fdsc_count].fd = subs.att_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- ATTITUDE SETPOINT VALUE --- */ - /* subscribe to ORB for attitude setpoint */ - /* struct already allocated */ - subs.spa_sub = orb_subscribe(ORB_ID(vehicle_attitude_setpoint)); - fds[fdsc_count].fd = subs.spa_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /** --- ACTUATOR OUTPUTS --- */ - subs.act_0_sub = orb_subscribe(ORB_ID(actuator_outputs_0)); - fds[fdsc_count].fd = subs.act_0_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- ACTUATOR CONTROL VALUE --- */ - /* subscribe to ORB for actuator control */ - subs.controls_0_sub = orb_subscribe(ORB_ID_VEHICLE_ATTITUDE_CONTROLS); - fds[fdsc_count].fd = subs.controls_0_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- ACTUATOR CONTROL EFFECTIVE VALUE --- */ - /* subscribe to ORB for actuator control */ - subs.controls_effective_0_sub = orb_subscribe(ORB_ID_VEHICLE_ATTITUDE_CONTROLS_EFFECTIVE); - fds[fdsc_count].fd = subs.controls_effective_0_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- LOCAL POSITION --- */ - /* subscribe to ORB for local position */ - subs.local_pos_sub = orb_subscribe(ORB_ID(vehicle_local_position)); - fds[fdsc_count].fd = subs.local_pos_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- GLOBAL POSITION --- */ - /* subscribe to ORB for global position */ - subs.global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position)); - fds[fdsc_count].fd = subs.global_pos_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- VICON POSITION --- */ - /* subscribe to ORB for vicon position */ - subs.vicon_pos_sub = orb_subscribe(ORB_ID(vehicle_vicon_position)); - fds[fdsc_count].fd = subs.vicon_pos_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- FLOW measurements --- */ - /* subscribe to ORB for flow measurements */ - subs.flow_sub = orb_subscribe(ORB_ID(optical_flow)); - fds[fdsc_count].fd = subs.flow_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- BATTERY STATUS --- */ - /* subscribe to ORB for flow measurements */ - subs.batt_sub = orb_subscribe(ORB_ID(battery_status)); - fds[fdsc_count].fd = subs.batt_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- DIFFERENTIAL PRESSURE --- */ - /* subscribe to ORB for flow measurements */ - subs.diff_pres_sub = orb_subscribe(ORB_ID(differential_pressure)); - fds[fdsc_count].fd = subs.diff_pres_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* --- AIRSPEED --- */ - /* subscribe to ORB for airspeed */ - subs.airspeed_sub = orb_subscribe(ORB_ID(airspeed)); - fds[fdsc_count].fd = subs.airspeed_sub; - fds[fdsc_count].events = POLLIN; - fdsc_count++; - - /* WARNING: If you get the error message below, - * then the number of registered messages (fdsc) - * differs from the number of messages in the above list. - */ - if (fdsc_count > fdsc) { - warn("WARNING: Not enough space for poll fds allocated. Check %s:%d.\n", __FILE__, __LINE__); - fdsc_count = fdsc; - } - - /* - * set up poll to block for new data, - * wait for a maximum of 1000 ms (1 second) - */ - // const int timeout = 1000; - - thread_running = true; - - /* initialize log buffer with a size of 10 */ - sdlog_logbuffer_init(&lb, 10); - - /* initialize thread synchronization */ - pthread_mutex_init(&sysvector_mutex, NULL); - pthread_cond_init(&sysvector_cond, NULL); - - /* start logbuffer emptying thread */ - pthread_t sysvector_pthread = sysvector_write_start(&lb); - - starttime = hrt_absolute_time(); - - /* track skipping */ - int skip_count = 0; - - while (!thread_should_exit) { - - /* only poll for commands, gps and sensor_combined */ - int poll_ret = poll(fds, 3, 1000); - - /* handle the poll result */ - if (poll_ret == 0) { - /* XXX this means none of our providers is giving us data - might be an error? */ - } else if (poll_ret < 0) { - /* XXX this is seriously bad - should be an emergency */ - } else { - - int ifds = 0; - - /* --- VEHICLE COMMAND VALUE --- */ - if (fds[ifds++].revents & POLLIN) { - /* copy command into local buffer */ - orb_copy(ORB_ID(vehicle_command), subs.cmd_sub, &buf.cmd); - - /* always log to blackbox, even when logging disabled */ - blackbox_file_bytes += fprintf(blackbox_file, "[%10.4f\tVCMD] CMD #%d [%f\t%f\t%f\t%f\t%f\t%f\t%f]\n", hrt_absolute_time()/1000000.0d, - buf.cmd.command, (double)buf.cmd.param1, (double)buf.cmd.param2, (double)buf.cmd.param3, (double)buf.cmd.param4, - (double)buf.cmd.param5, (double)buf.cmd.param6, (double)buf.cmd.param7); - - handle_command(&buf.cmd); - } - - /* --- VEHICLE GPS VALUE --- */ - if (fds[ifds++].revents & POLLIN) { - /* copy gps position into local buffer */ - orb_copy(ORB_ID(vehicle_gps_position), subs.gps_pos_sub, &buf.gps_pos); - - /* if logging disabled, continue */ - if (logging_enabled) { - - /* write KML line */ - } - } - - /* --- SENSORS RAW VALUE --- */ - if (fds[ifds++].revents & POLLIN) { - - // /* copy sensors raw data into local buffer */ - // orb_copy(ORB_ID(sensor_combined), subs.sensor_sub, &buf.raw); - // /* write out */ - // sensor_combined_bytes += write(sensorfile, (const char*)&(buf.raw), sizeof(buf.raw)); - - /* always copy sensors raw data into local buffer, since poll flags won't clear else */ - orb_copy(ORB_ID(sensor_combined), subs.sensor_sub, &buf.raw); - orb_copy(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, subs.controls_0_sub, &buf.act_controls); - orb_copy(ORB_ID_VEHICLE_ATTITUDE_CONTROLS_EFFECTIVE, subs.controls_effective_0_sub, &buf.act_controls_effective); - orb_copy(ORB_ID(actuator_outputs_0), subs.act_0_sub, &buf.act_outputs); - orb_copy(ORB_ID(vehicle_attitude_setpoint), subs.spa_sub, &buf.att_sp); - orb_copy(ORB_ID(vehicle_gps_position), subs.gps_pos_sub, &buf.gps_pos); - orb_copy(ORB_ID(vehicle_local_position), subs.local_pos_sub, &buf.local_pos); - orb_copy(ORB_ID(vehicle_global_position), subs.global_pos_sub, &buf.global_pos); - orb_copy(ORB_ID(vehicle_attitude), subs.att_sub, &buf.att); - orb_copy(ORB_ID(vehicle_vicon_position), subs.vicon_pos_sub, &buf.vicon_pos); - orb_copy(ORB_ID(optical_flow), subs.flow_sub, &buf.flow); - orb_copy(ORB_ID(differential_pressure), subs.diff_pres_sub, &buf.diff_pres); - orb_copy(ORB_ID(airspeed), subs.airspeed_sub, &buf.airspeed); - orb_copy(ORB_ID(battery_status), subs.batt_sub, &buf.batt); - - /* if skipping is on or logging is disabled, ignore */ - if (skip_count < skip_value || !logging_enabled) { - skip_count++; - /* do not log data */ - continue; - } else { - /* log data, reset */ - skip_count = 0; - } - - struct sdlog_sysvector sysvect = { - .timestamp = buf.raw.timestamp, - .gyro = {buf.raw.gyro_rad_s[0], buf.raw.gyro_rad_s[1], buf.raw.gyro_rad_s[2]}, - .accel = {buf.raw.accelerometer_m_s2[0], buf.raw.accelerometer_m_s2[1], buf.raw.accelerometer_m_s2[2]}, - .mag = {buf.raw.magnetometer_ga[0], buf.raw.magnetometer_ga[1], buf.raw.magnetometer_ga[2]}, - .baro = buf.raw.baro_pres_mbar, - .baro_alt = buf.raw.baro_alt_meter, - .baro_temp = buf.raw.baro_temp_celcius, - .control = {buf.act_controls.control[0], buf.act_controls.control[1], buf.act_controls.control[2], buf.act_controls.control[3]}, - .actuators = { - buf.act_outputs.output[0], buf.act_outputs.output[1], buf.act_outputs.output[2], buf.act_outputs.output[3], - buf.act_outputs.output[4], buf.act_outputs.output[5], buf.act_outputs.output[6], buf.act_outputs.output[7] - }, - .vbat = buf.batt.voltage_v, - .bat_current = buf.batt.current_a, - .bat_discharged = buf.batt.discharged_mah, - .adc = {buf.raw.adc_voltage_v[0], buf.raw.adc_voltage_v[1], buf.raw.adc_voltage_v[2], buf.raw.adc_voltage_v[3]}, - .local_position = {buf.local_pos.x, buf.local_pos.y, buf.local_pos.z}, - .gps_raw_position = {buf.gps_pos.lat, buf.gps_pos.lon, buf.gps_pos.alt}, - .attitude = {buf.att.pitch, buf.att.roll, buf.att.yaw}, - .rotMatrix = {buf.att.R[0][0], buf.att.R[0][1], buf.att.R[0][2], buf.att.R[1][0], buf.att.R[1][1], buf.att.R[1][2], buf.att.R[2][0], buf.att.R[2][1], buf.att.R[2][2]}, - .vicon = {buf.vicon_pos.x, buf.vicon_pos.y, buf.vicon_pos.z, buf.vicon_pos.roll, buf.vicon_pos.pitch, buf.vicon_pos.yaw}, - .control_effective = {buf.act_controls_effective.control_effective[0], buf.act_controls_effective.control_effective[1], buf.act_controls_effective.control_effective[2], buf.act_controls_effective.control_effective[3]}, - .flow = {buf.flow.flow_raw_x, buf.flow.flow_raw_y, buf.flow.flow_comp_x_m, buf.flow.flow_comp_y_m, buf.flow.ground_distance_m, buf.flow.quality}, - .diff_pressure = buf.diff_pres.differential_pressure_pa, - .ind_airspeed = buf.airspeed.indicated_airspeed_m_s, - .true_airspeed = buf.airspeed.true_airspeed_m_s - }; - - /* put into buffer for later IO */ - pthread_mutex_lock(&sysvector_mutex); - sdlog_logbuffer_write(&lb, &sysvect); - /* signal the other thread new data, but not yet unlock */ - if ((unsigned)lb.count > (lb.size / 2)) { - /* only request write if several packets can be written at once */ - pthread_cond_signal(&sysvector_cond); - } - /* unlock, now the writer thread may run */ - pthread_mutex_unlock(&sysvector_mutex); - } - - } - - } - - print_sdlog_status(); - - /* wake up write thread one last time */ - pthread_mutex_lock(&sysvector_mutex); - pthread_cond_signal(&sysvector_cond); - /* unlock, now the writer thread may return */ - pthread_mutex_unlock(&sysvector_mutex); - - /* wait for write thread to return */ - (void)pthread_join(sysvector_pthread, NULL); - - pthread_mutex_destroy(&sysvector_mutex); - pthread_cond_destroy(&sysvector_cond); - - warnx("exiting.\n\n"); - - /* finish KML file */ - // XXX - fclose(gpsfile); - fclose(blackbox_file); - - thread_running = false; - - return 0; -} - -void print_sdlog_status() -{ - unsigned bytes = sysvector_bytes + sensor_combined_bytes + actuator_outputs_bytes + blackbox_file_bytes + actuator_controls_bytes; - float mebibytes = bytes / 1024.0f / 1024.0f; - float seconds = ((float)(hrt_absolute_time() - starttime)) / 1000000.0f; - - warnx("wrote %4.2f MiB (average %5.3f MiB/s).\n", (double)mebibytes, (double)(mebibytes / seconds)); -} - -/** - * @return 0 if file exists - */ -int file_exist(const char *filename) -{ - struct stat buffer; - return stat(filename, &buffer); -} - -int file_copy(const char *file_old, const char *file_new) -{ - FILE *source, *target; - source = fopen(file_old, "r"); - int ret = 0; - - if (source == NULL) { - warnx("failed opening input file to copy"); - return 1; - } - - target = fopen(file_new, "w"); - - if (target == NULL) { - fclose(source); - warnx("failed to open output file to copy"); - return 1; - } - - char buf[128]; - int nread; - - while ((nread = fread(buf, 1, sizeof(buf), source)) > 0) { - int ret = fwrite(buf, 1, nread, target); - - if (ret <= 0) { - warnx("error writing file"); - ret = 1; - break; - } - } - - fsync(fileno(target)); - - fclose(source); - fclose(target); - - return ret; -} - -void handle_command(struct vehicle_command_s *cmd) -{ - /* result of the command */ - uint8_t result = VEHICLE_CMD_RESULT_UNSUPPORTED; - - /* request to set different system mode */ - switch (cmd->command) { - - case VEHICLE_CMD_PREFLIGHT_STORAGE: - - if (((int)(cmd->param3)) == 1) { - - /* enable logging */ - mavlink_log_info(mavlink_fd, "[log] file:"); - mavlink_log_info(mavlink_fd, "logdir"); - logging_enabled = true; - } - if (((int)(cmd->param3)) == 0) { - - /* disable logging */ - mavlink_log_info(mavlink_fd, "[log] stopped."); - logging_enabled = false; - } - break; - - default: - /* silently ignore */ - break; - } - -} diff --git a/src/modules/sdlog/sdlog_ringbuffer.h b/src/modules/sdlog/sdlog_ringbuffer.h deleted file mode 100644 index b65916459..000000000 --- a/src/modules/sdlog/sdlog_ringbuffer.h +++ /dev/null @@ -1,91 +0,0 @@ -/**************************************************************************** - * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. - * Author: Lorenz Meier <lm@inf.ethz.ch> - * - * Redistribution and use in source and binary forms, with or without - * modification, are permitted provided that the following conditions - * are met: - * - * 1. Redistributions of source code must retain the above copyright - * notice, this list of conditions and the following disclaimer. - * 2. Redistributions in binary form must reproduce the above copyright - * notice, this list of conditions and the following disclaimer in - * the documentation and/or other materials provided with the - * distribution. - * 3. Neither the name PX4 nor the names of its contributors may be - * used to endorse or promote products derived from this software - * without specific prior written permission. - * - * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS - * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT - * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS - * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE - * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, - * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, - * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS - * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED - * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT - * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN - * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE - * POSSIBILITY OF SUCH DAMAGE. - * - ****************************************************************************/ - -/** - * @file sdlog_ringbuffer.h - * microSD logging - * - * @author Lorenz Meier <lm@inf.ethz.ch> - */ - -#ifndef SDLOG_RINGBUFFER_H_ -#define SDLOG_RINGBUFFER_H_ - -#pragma pack(push, 1) -struct sdlog_sysvector { - uint64_t timestamp; /**< time [us] */ - float gyro[3]; /**< [rad/s] */ - float accel[3]; /**< [m/s^2] */ - float mag[3]; /**< [gauss] */ - float baro; /**< pressure [millibar] */ - float baro_alt; /**< altitude above MSL [meter] */ - float baro_temp; /**< [degree celcius] */ - float control[4]; /**< roll, pitch, yaw [-1..1], thrust [0..1] */ - float actuators[8]; /**< motor 1-8, in motor units (PWM: 1000-2000,AR.Drone: 0-512) */ - float vbat; /**< battery voltage in [volt] */ - float bat_current; /**< battery discharge current */ - float bat_discharged; /**< discharged energy in mAh */ - float adc[4]; /**< ADC ports [volt] */ - float local_position[3]; /**< tangent plane mapping into x,y,z [m] */ - int32_t gps_raw_position[3]; /**< latitude [degrees] north, longitude [degrees] east, altitude above MSL [millimeter] */ - float attitude[3]; /**< roll, pitch, yaw [rad] */ - float rotMatrix[9]; /**< unitvectors */ - float vicon[6]; /**< Vicon ground truth x, y, z and roll, pitch, yaw */ - float control_effective[4]; /**< roll, pitch, yaw [-1..1], thrust [0..1] */ - float flow[6]; /**< flow raw x, y, flow metric x, y, flow ground dist, flow quality */ - float diff_pressure; /**< differential pressure */ - float ind_airspeed; /**< indicated airspeed */ - float true_airspeed; /**< true airspeed */ -}; -#pragma pack(pop) - -struct sdlog_logbuffer { - unsigned int start; - // unsigned int end; - unsigned int size; - int count; - struct sdlog_sysvector *elems; -}; - -void sdlog_logbuffer_init(struct sdlog_logbuffer *lb, int size); - -int sdlog_logbuffer_is_full(struct sdlog_logbuffer *lb); - -int sdlog_logbuffer_is_empty(struct sdlog_logbuffer *lb); - -void sdlog_logbuffer_write(struct sdlog_logbuffer *lb, const struct sdlog_sysvector *elem); - -int sdlog_logbuffer_read(struct sdlog_logbuffer *lb, struct sdlog_sysvector *elem); - -#endif diff --git a/src/modules/sdlog2/module.mk b/src/modules/sdlog2/module.mk index f53129688..a28d43e72 100644 --- a/src/modules/sdlog2/module.mk +++ b/src/modules/sdlog2/module.mk @@ -41,3 +41,5 @@ MODULE_PRIORITY = "SCHED_PRIORITY_MAX-30" SRCS = sdlog2.c \ logbuffer.c + +MODULE_STACKSIZE = 1200 diff --git a/src/modules/sdlog2/sdlog2.c b/src/modules/sdlog2/sdlog2.c index ee3ec7216..39f433eb5 100644 --- a/src/modules/sdlog2/sdlog2.c +++ b/src/modules/sdlog2/sdlog2.c @@ -83,6 +83,9 @@ #include <uORB/topics/rc_channels.h> #include <uORB/topics/esc_status.h> #include <uORB/topics/telemetry_status.h> +#include <uORB/topics/estimator_status.h> +#include <uORB/topics/system_power.h> +#include <uORB/topics/servorail_status.h> #include <systemlib/systemlib.h> #include <systemlib/param/param.h> @@ -223,11 +226,11 @@ sdlog2_usage(const char *reason) } errx(1, "usage: sdlog2 {start|stop|status} [-r <log rate>] [-b <buffer size>] -e -a -t\n" - "\t-r\tLog rate in Hz, 0 means unlimited rate\n" - "\t-b\tLog buffer size in KiB, default is 8\n" - "\t-e\tEnable logging by default (if not, can be started by command)\n" - "\t-a\tLog only when armed (can be still overriden by command)\n" - "\t-t\tUse date/time for naming log directories and files\n"); + "\t-r\tLog rate in Hz, 0 means unlimited rate\n" + "\t-b\tLog buffer size in KiB, default is 8\n" + "\t-e\tEnable logging by default (if not, can be started by command)\n" + "\t-a\tLog only when armed (can be still overriden by command)\n" + "\t-t\tUse date/time for naming log directories and files\n"); } /** @@ -254,11 +257,11 @@ int sdlog2_main(int argc, char *argv[]) main_thread_should_exit = false; deamon_task = task_spawn_cmd("sdlog2", - SCHED_DEFAULT, - SCHED_PRIORITY_DEFAULT - 30, - 3000, - sdlog2_thread_main, - (const char **)argv); + SCHED_DEFAULT, + SCHED_PRIORITY_DEFAULT - 30, + 3000, + sdlog2_thread_main, + (const char **)argv); exit(0); } @@ -681,7 +684,7 @@ int sdlog2_thread_main(int argc, char *argv[]) case 'r': { unsigned long r = strtoul(optarg, NULL, 10); - if (r <= 0) { + if (r == 0) { r = 1; } @@ -794,6 +797,9 @@ int sdlog2_thread_main(int argc, char *argv[]) struct battery_status_s battery; struct telemetry_status_s telemetry; struct range_finder_report range_finder; + struct estimator_status_report estimator_status; + struct system_power_s system_power; + struct servorail_status_s servorail_status; } buf; memset(&buf, 0, sizeof(buf)); @@ -825,6 +831,11 @@ int sdlog2_thread_main(int argc, char *argv[]) struct log_BATT_s log_BATT; struct log_DIST_s log_DIST; struct log_TELE_s log_TELE; + struct log_ESTM_s log_ESTM; + struct log_PWR_s log_PWR; + struct log_VICN_s log_VICN; + struct log_GSN0_s log_GSN0; + struct log_GSN1_s log_GSN1; } body; } log_msg = { LOG_PACKET_HEADER_INIT(0) @@ -855,6 +866,9 @@ int sdlog2_thread_main(int argc, char *argv[]) int battery_sub; int telemetry_sub; int range_finder_sub; + int estimator_status_sub; + int system_power_sub; + int servorail_status_sub; } subs; subs.cmd_sub = orb_subscribe(ORB_ID(vehicle_command)); @@ -879,6 +893,9 @@ int sdlog2_thread_main(int argc, char *argv[]) subs.battery_sub = orb_subscribe(ORB_ID(battery_status)); subs.telemetry_sub = orb_subscribe(ORB_ID(telemetry_status)); subs.range_finder_sub = orb_subscribe(ORB_ID(sensor_range_finder)); + subs.estimator_status_sub = orb_subscribe(ORB_ID(estimator_status)); + subs.system_power_sub = orb_subscribe(ORB_ID(system_power)); + subs.servorail_status_sub = orb_subscribe(ORB_ID(servorail_status)); thread_running = true; @@ -893,9 +910,6 @@ int sdlog2_thread_main(int argc, char *argv[]) hrt_abstime barometer_timestamp = 0; hrt_abstime differential_pressure_timestamp = 0; - /* track changes in distance status */ - bool dist_bottom_present = false; - /* enable logging on start if needed */ if (log_on_start) { /* check GPS topic to get GPS time */ @@ -948,6 +962,7 @@ int sdlog2_thread_main(int argc, char *argv[]) log_msg.msg_type = LOG_STAT_MSG; log_msg.body.log_STAT.main_state = (uint8_t) buf_status.main_state; log_msg.body.log_STAT.arming_state = (uint8_t) buf_status.arming_state; + log_msg.body.log_STAT.failsafe_state = (uint8_t) buf_status.failsafe_state; log_msg.body.log_STAT.battery_remaining = buf_status.battery_remaining; log_msg.body.log_STAT.battery_warning = (uint8_t) buf_status.battery_warning; log_msg.body.log_STAT.landed = (uint8_t) buf_status.condition_landed; @@ -969,6 +984,18 @@ int sdlog2_thread_main(int argc, char *argv[]) log_msg.body.log_GPS.vel_d = buf_gps_pos.vel_d_m_s; log_msg.body.log_GPS.cog = buf_gps_pos.cog_rad; LOGBUFFER_WRITE_AND_COUNT(GPS); + + /* log the SNR of each satellite for a detailed view of signal quality */ + log_msg.msg_type = LOG_GSN0_MSG; + /* pick the smaller number so we do not overflow any of the arrays */ + unsigned gps_msg_max_snr = sizeof(buf_gps_pos.satellite_snr) / sizeof(buf_gps_pos.satellite_snr[0]); + unsigned log_max_snr = sizeof(log_msg.body.log_GSN0.satellite_snr) / sizeof(log_msg.body.log_GSN0.satellite_snr[0]); + unsigned sat_max_snr = (gps_msg_max_snr < log_max_snr) ? gps_msg_max_snr : log_max_snr; + + for (unsigned i = 0; i < sat_max_snr; i++) { + log_msg.body.log_GSN0.satellite_snr[i] = buf_gps_pos.satellite_snr[i]; + } + LOGBUFFER_WRITE_AND_COUNT(GSN0); } /* --- SENSOR COMBINED --- */ @@ -1021,6 +1048,7 @@ int sdlog2_thread_main(int argc, char *argv[]) log_msg.body.log_SENS.baro_alt = buf.sensor.baro_alt_meter; log_msg.body.log_SENS.baro_temp = buf.sensor.baro_temp_celcius; log_msg.body.log_SENS.diff_pres = buf.sensor.differential_pressure_pa; + log_msg.body.log_SENS.diff_pres_filtered = buf.sensor.differential_pressure_filtered_pa; LOGBUFFER_WRITE_AND_COUNT(SENS); } @@ -1083,28 +1111,19 @@ int sdlog2_thread_main(int argc, char *argv[]) log_msg.body.log_LPOS.x = buf.local_pos.x; log_msg.body.log_LPOS.y = buf.local_pos.y; log_msg.body.log_LPOS.z = buf.local_pos.z; + log_msg.body.log_LPOS.ground_dist = buf.local_pos.dist_bottom; + log_msg.body.log_LPOS.ground_dist_rate = buf.local_pos.dist_bottom_rate; log_msg.body.log_LPOS.vx = buf.local_pos.vx; log_msg.body.log_LPOS.vy = buf.local_pos.vy; log_msg.body.log_LPOS.vz = buf.local_pos.vz; - log_msg.body.log_LPOS.ref_lat = buf.local_pos.ref_lat; - log_msg.body.log_LPOS.ref_lon = buf.local_pos.ref_lon; + log_msg.body.log_LPOS.ref_lat = buf.local_pos.ref_lat * 1e7; + log_msg.body.log_LPOS.ref_lon = buf.local_pos.ref_lon * 1e7; log_msg.body.log_LPOS.ref_alt = buf.local_pos.ref_alt; log_msg.body.log_LPOS.xy_flags = (buf.local_pos.xy_valid ? 1 : 0) | (buf.local_pos.v_xy_valid ? 2 : 0) | (buf.local_pos.xy_global ? 8 : 0); log_msg.body.log_LPOS.z_flags = (buf.local_pos.z_valid ? 1 : 0) | (buf.local_pos.v_z_valid ? 2 : 0) | (buf.local_pos.z_global ? 8 : 0); log_msg.body.log_LPOS.landed = buf.local_pos.landed; + log_msg.body.log_LPOS.ground_dist_flags = (buf.local_pos.dist_bottom_valid ? 1 : 0); LOGBUFFER_WRITE_AND_COUNT(LPOS); - - if (buf.local_pos.dist_bottom_valid) { - dist_bottom_present = true; - } - - if (dist_bottom_present) { - log_msg.msg_type = LOG_DIST_MSG; - log_msg.body.log_DIST.bottom = buf.local_pos.dist_bottom; - log_msg.body.log_DIST.bottom_rate = buf.local_pos.dist_bottom_rate; - log_msg.body.log_DIST.flags = (buf.local_pos.dist_bottom_valid ? 1 : 0); - LOGBUFFER_WRITE_AND_COUNT(DIST); - } } /* --- LOCAL POSITION SETPOINT --- */ @@ -1126,8 +1145,8 @@ int sdlog2_thread_main(int argc, char *argv[]) log_msg.body.log_GPOS.vel_n = buf.global_pos.vel_n; log_msg.body.log_GPOS.vel_e = buf.global_pos.vel_e; log_msg.body.log_GPOS.vel_d = buf.global_pos.vel_d; - log_msg.body.log_GPOS.baro_alt = buf.global_pos.baro_alt; - log_msg.body.log_GPOS.flags = (buf.global_pos.baro_valid ? 1 : 0) | (buf.global_pos.global_valid ? 2 : 0); + log_msg.body.log_GPOS.eph = buf.global_pos.eph; + log_msg.body.log_GPOS.epv = buf.global_pos.epv; LOGBUFFER_WRITE_AND_COUNT(GPOS); } @@ -1148,7 +1167,14 @@ int sdlog2_thread_main(int argc, char *argv[]) /* --- VICON POSITION --- */ if (copy_if_updated(ORB_ID(vehicle_vicon_position), subs.vicon_pos_sub, &buf.vicon_pos)) { - // TODO not implemented yet + log_msg.msg_type = LOG_VICN_MSG; + log_msg.body.log_VICN.x = buf.vicon_pos.x; + log_msg.body.log_VICN.y = buf.vicon_pos.y; + log_msg.body.log_VICN.z = buf.vicon_pos.z; + log_msg.body.log_VICN.pitch = buf.vicon_pos.pitch; + log_msg.body.log_VICN.roll = buf.vicon_pos.roll; + log_msg.body.log_VICN.yaw = buf.vicon_pos.yaw; + LOGBUFFER_WRITE_AND_COUNT(VICN); } /* --- FLOW --- */ @@ -1170,6 +1196,7 @@ int sdlog2_thread_main(int argc, char *argv[]) /* Copy only the first 8 channels of 14 */ memcpy(log_msg.body.log_RC.channel, buf.rc.chan, sizeof(log_msg.body.log_RC.channel)); log_msg.body.log_RC.channel_count = buf.rc.chan_count; + log_msg.body.log_RC.signal_lost = buf.rc.signal_lost; LOGBUFFER_WRITE_AND_COUNT(RC); } @@ -1178,6 +1205,7 @@ int sdlog2_thread_main(int argc, char *argv[]) log_msg.msg_type = LOG_AIRS_MSG; log_msg.body.log_AIRS.indicated_airspeed = buf.airspeed.indicated_airspeed_m_s; log_msg.body.log_AIRS.true_airspeed = buf.airspeed.true_airspeed_m_s; + log_msg.body.log_AIRS.air_temperature_celsius = buf.airspeed.air_temperature_celsius; LOGBUFFER_WRITE_AND_COUNT(AIRS); } @@ -1220,6 +1248,24 @@ int sdlog2_thread_main(int argc, char *argv[]) LOGBUFFER_WRITE_AND_COUNT(BATT); } + /* --- SYSTEM POWER RAILS --- */ + if (copy_if_updated(ORB_ID(system_power), subs.system_power_sub, &buf.system_power)) { + log_msg.msg_type = LOG_PWR_MSG; + log_msg.body.log_PWR.peripherals_5v = buf.system_power.voltage5V_v; + log_msg.body.log_PWR.usb_ok = buf.system_power.usb_connected; + log_msg.body.log_PWR.brick_ok = buf.system_power.brick_valid; + log_msg.body.log_PWR.servo_ok = buf.system_power.servo_valid; + log_msg.body.log_PWR.low_power_rail_overcurrent = buf.system_power.periph_5V_OC; + log_msg.body.log_PWR.high_power_rail_overcurrent = buf.system_power.hipower_5V_OC; + + /* copy servo rail status topic here too */ + orb_copy(ORB_ID(servorail_status), subs.servorail_status_sub, &buf.servorail_status); + log_msg.body.log_PWR.servo_rail_5v = buf.servorail_status.voltage_v; + log_msg.body.log_PWR.servo_rssi = buf.servorail_status.rssi_v; + + LOGBUFFER_WRITE_AND_COUNT(PWR); + } + /* --- TELEMETRY --- */ if (copy_if_updated(ORB_ID(telemetry_status), subs.telemetry_sub, &buf.telemetry)) { log_msg.msg_type = LOG_TELE_MSG; @@ -1242,6 +1288,19 @@ int sdlog2_thread_main(int argc, char *argv[]) LOGBUFFER_WRITE_AND_COUNT(DIST); } + /* --- ESTIMATOR STATUS --- */ + if (copy_if_updated(ORB_ID(estimator_status), subs.estimator_status_sub, &buf.estimator_status)) { + log_msg.msg_type = LOG_ESTM_MSG; + unsigned maxcopy = (sizeof(buf.estimator_status.states) < sizeof(log_msg.body.log_ESTM.s)) ? sizeof(buf.estimator_status.states) : sizeof(log_msg.body.log_ESTM.s); + memset(&(log_msg.body.log_ESTM.s), 0, sizeof(log_msg.body.log_ESTM.s)); + memcpy(&(log_msg.body.log_ESTM.s), buf.estimator_status.states, maxcopy); + log_msg.body.log_ESTM.n_states = buf.estimator_status.n_states; + log_msg.body.log_ESTM.states_nan = buf.estimator_status.states_nan; + log_msg.body.log_ESTM.covariance_nan = buf.estimator_status.covariance_nan; + log_msg.body.log_ESTM.kalman_gain_nan = buf.estimator_status.kalman_gain_nan; + LOGBUFFER_WRITE_AND_COUNT(ESTM); + } + /* signal the other thread new data, but not yet unlock */ if (logbuffer_count(&lb) > MIN_BYTES_TO_WRITE) { /* only request write if several packets can be written at once */ diff --git a/src/modules/sdlog2/sdlog2_messages.h b/src/modules/sdlog2/sdlog2_messages.h index e27518aa0..0c6188657 100644 --- a/src/modules/sdlog2/sdlog2_messages.h +++ b/src/modules/sdlog2/sdlog2_messages.h @@ -92,6 +92,7 @@ struct log_SENS_s { float baro_alt; float baro_temp; float diff_pres; + float diff_pres_filtered; }; /* --- LPOS - LOCAL POSITION --- */ @@ -100,6 +101,8 @@ struct log_LPOS_s { float x; float y; float z; + float ground_dist; + float ground_dist_rate; float vx; float vy; float vz; @@ -109,6 +112,7 @@ struct log_LPOS_s { uint8_t xy_flags; uint8_t z_flags; uint8_t landed; + uint8_t ground_dist_flags; }; /* --- LPSP - LOCAL POSITION SETPOINT --- */ @@ -150,6 +154,7 @@ struct log_ATTC_s { struct log_STAT_s { uint8_t main_state; uint8_t arming_state; + uint8_t failsafe_state; float battery_remaining; uint8_t battery_warning; uint8_t landed; @@ -160,6 +165,7 @@ struct log_STAT_s { struct log_RC_s { float channel[8]; uint8_t channel_count; + uint8_t signal_lost; }; /* --- OUT0 - ACTUATOR_0 OUTPUT --- */ @@ -173,6 +179,7 @@ struct log_OUT0_s { struct log_AIRS_s { float indicated_airspeed; float true_airspeed; + float air_temperature_celsius; }; /* --- ARSP - ATTITUDE RATE SET POINT --- */ @@ -204,8 +211,8 @@ struct log_GPOS_s { float vel_n; float vel_e; float vel_d; - float baro_alt; - uint8_t flags; + float eph; + float epv; }; /* --- GPSP - GLOBAL POSITION SETPOINT --- */ @@ -276,6 +283,52 @@ struct log_TELE_s { uint8_t txbuf; }; +/* --- ESTM - ESTIMATOR STATUS --- */ +#define LOG_ESTM_MSG 23 +struct log_ESTM_s { + float s[10]; + uint8_t n_states; + uint8_t states_nan; + uint8_t covariance_nan; + uint8_t kalman_gain_nan; +}; + +/* --- PWR - ONBOARD POWER SYSTEM --- */ +#define LOG_PWR_MSG 24 +struct log_PWR_s { + float peripherals_5v; + float servo_rail_5v; + float servo_rssi; + uint8_t usb_ok; + uint8_t brick_ok; + uint8_t servo_ok; + uint8_t low_power_rail_overcurrent; + uint8_t high_power_rail_overcurrent; +}; + +/* --- VICN - VICON POSITION --- */ +#define LOG_VICN_MSG 25 +struct log_VICN_s { + float x; + float y; + float z; + float roll; + float pitch; + float yaw; +}; + +/* --- GSN0 - GPS SNR #0 --- */ +#define LOG_GSN0_MSG 26 +struct log_GSN0_s { + uint8_t satellite_snr[16]; /**< Signal to noise ratio of satellite. 0 for none, 255 for max. */ +}; + +/* --- GSN1 - GPS SNR #1 --- */ +#define LOG_GSN1_MSG 27 +struct log_GSN1_s { + uint8_t satellite_snr[16]; /**< Signal to noise ratio of satellite. 0 for none, 255 for max. */ +}; + /********** SYSTEM MESSAGES, ID > 0x80 **********/ /* --- TIME - TIME STAMP --- */ @@ -303,35 +356,40 @@ struct log_PARM_s { /* construct list of all message formats */ static const struct log_format_s log_formats[] = { /* business-level messages, ID < 0x80 */ - LOG_FORMAT(ATT, "fffffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate,GX,GY,GZ"), - LOG_FORMAT(ATSP, "ffff", "RollSP,PitchSP,YawSP,ThrustSP"), - LOG_FORMAT(IMU, "fffffffff", "AccX,AccY,AccZ,GyroX,GyroY,GyroZ,MagX,MagY,MagZ"), - LOG_FORMAT(SENS, "ffff", "BaroPres,BaroAlt,BaroTemp,DiffPres"), - LOG_FORMAT(LPOS, "ffffffLLfBBB", "X,Y,Z,VX,VY,VZ,RefLat,RefLon,RefAlt,XYFlags,ZFlags,Landed"), - LOG_FORMAT(LPSP, "ffff", "X,Y,Z,Yaw"), - LOG_FORMAT(GPS, "QBffLLfffff", "GPSTime,FixType,EPH,EPV,Lat,Lon,Alt,VelN,VelE,VelD,Cog"), - LOG_FORMAT(ATTC, "ffff", "Roll,Pitch,Yaw,Thrust"), - LOG_FORMAT(STAT, "BBfBB", "MainState,ArmState,BatRem,BatWarn,Landed"), - LOG_FORMAT(RC, "ffffffffB", "Ch0,Ch1,Ch2,Ch3,Ch4,Ch5,Ch6,Ch7,Count"), - LOG_FORMAT(OUT0, "ffffffff", "Out0,Out1,Out2,Out3,Out4,Out5,Out6,Out7"), - LOG_FORMAT(AIRS, "ff", "IndSpeed,TrueSpeed"), - LOG_FORMAT(ARSP, "fff", "RollRateSP,PitchRateSP,YawRateSP"), - LOG_FORMAT(FLOW, "hhfffBB", "RawX,RawY,CompX,CompY,Dist,Q,SensID"), - LOG_FORMAT(GPOS, "LLfffffB", "Lat,Lon,Alt,VelN,VelE,VelD,BaroAlt,Flags"), - LOG_FORMAT(GPSP, "BLLffBfbf", "NavState,Lat,Lon,Alt,Yaw,Type,LoitR,LoitDir,PitMin"), - LOG_FORMAT(ESC, "HBBBHHHHHHfH", "Counter,NumESC,Conn,N,Ver,Adr,Volt,Amp,RPM,Temp,SetP,SetPRAW"), - LOG_FORMAT(GVSP, "fff", "VX,VY,VZ"), - LOG_FORMAT(BATT, "ffff", "V,VFilt,C,Discharged"), - LOG_FORMAT(DIST, "ffB", "Bottom,BottomRate,Flags"), - LOG_FORMAT(TELE, "BBBBHHB", "RSSI,RemRSSI,Noise,RemNoise,RXErr,Fixed,TXBuf"), + LOG_FORMAT(ATT, "fffffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate,GX,GY,GZ"), + LOG_FORMAT(ATSP, "ffff", "RollSP,PitchSP,YawSP,ThrustSP"), + LOG_FORMAT(IMU, "fffffffff", "AccX,AccY,AccZ,GyroX,GyroY,GyroZ,MagX,MagY,MagZ"), + LOG_FORMAT(SENS, "fffff", "BaroPres,BaroAlt,BaroTemp,DiffPres,DiffPresFilt"), + LOG_FORMAT(LPOS, "ffffffffLLfBBBB", "X,Y,Z,dist,distR,VX,VY,VZ,RLat,RLon,RAlt,XYFlg,ZFlg,LFlg,GFlg"), + LOG_FORMAT(LPSP, "ffff", "X,Y,Z,Yaw"), + LOG_FORMAT(GPS, "QBffLLfffff", "GPSTime,FixType,EPH,EPV,Lat,Lon,Alt,VelN,VelE,VelD,Cog"), + LOG_FORMAT(ATTC, "ffff", "Roll,Pitch,Yaw,Thrust"), + LOG_FORMAT(STAT, "BBBfBB", "MainState,ArmState,FailsafeState,BatRem,BatWarn,Landed"), + LOG_FORMAT(RC, "ffffffffBB", "Ch0,Ch1,Ch2,Ch3,Ch4,Ch5,Ch6,Ch7,Count,SignalLost"), + LOG_FORMAT(OUT0, "ffffffff", "Out0,Out1,Out2,Out3,Out4,Out5,Out6,Out7"), + LOG_FORMAT(AIRS, "fff", "IndSpeed,TrueSpeed,AirTemp"), + LOG_FORMAT(ARSP, "fff", "RollRateSP,PitchRateSP,YawRateSP"), + LOG_FORMAT(FLOW, "hhfffBB", "RawX,RawY,CompX,CompY,Dist,Q,SensID"), + LOG_FORMAT(GPOS, "LLffffff", "Lat,Lon,Alt,VelN,VelE,VelD,EPH,EPV"), + LOG_FORMAT(GPSP, "BLLffBfbf", "NavState,Lat,Lon,Alt,Yaw,Type,LoitR,LoitDir,PitMin"), + LOG_FORMAT(ESC, "HBBBHHHHHHfH", "count,nESC,Conn,N,Ver,Adr,Volt,Amp,RPM,Temp,SetP,SetPRAW"), + LOG_FORMAT(GVSP, "fff", "VX,VY,VZ"), + LOG_FORMAT(BATT, "ffff", "V,VFilt,C,Discharged"), + LOG_FORMAT(DIST, "ffB", "Bottom,BottomRate,Flags"), + LOG_FORMAT(TELE, "BBBBHHB", "RSSI,RemRSSI,Noise,RemNoise,RXErr,Fixed,TXBuf"), + LOG_FORMAT(ESTM, "ffffffffffBBBB", "s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,nStat,statNaN,covNaN,kGainNaN"), + LOG_FORMAT(PWR, "fffBBBBB", "Periph5V,Servo5V,RSSI,UsbOk,BrickOk,ServoOk,PeriphOC,HipwrOC"), + LOG_FORMAT(VICN, "ffffff", "X,Y,Z,Roll,Pitch,Yaw"), + LOG_FORMAT(GSN0, "BBBBBBBBBBBBBBBB", "s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,s10,s11,s12,s13,s14,s15"), + LOG_FORMAT(GSN1, "BBBBBBBBBBBBBBBB", "s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,s10,s11,s12,s13,s14,s15"), /* system-level messages, ID >= 0x80 */ - // FMT: don't write format of format message, it's useless + /* FMT: don't write format of format message, it's useless */ LOG_FORMAT(TIME, "Q", "StartTime"), LOG_FORMAT(VER, "NZ", "Arch,FwGit"), - LOG_FORMAT(PARM, "Nf", "Name,Value"), + LOG_FORMAT(PARM, "Nf", "Name,Value") }; -static const int log_formats_num = sizeof(log_formats) / sizeof(struct log_format_s); +static const unsigned log_formats_num = sizeof(log_formats) / sizeof(log_formats[0]); #endif /* SDLOG2_MESSAGES_H_ */ diff --git a/src/modules/segway/BlockSegwayController.cpp b/src/modules/segway/BlockSegwayController.cpp index 96a443c6e..91230a37c 100644 --- a/src/modules/segway/BlockSegwayController.cpp +++ b/src/modules/segway/BlockSegwayController.cpp @@ -35,8 +35,8 @@ void BlockSegwayController::update() { // handle autopilot modes if (_status.main_state == MAIN_STATE_AUTO || - _status.main_state == MAIN_STATE_SEATBELT || - _status.main_state == MAIN_STATE_EASY) { + _status.main_state == MAIN_STATE_ALTCTL || + _status.main_state == MAIN_STATE_POSCTL) { _actuators.control[0] = spdCmd; _actuators.control[1] = spdCmd; diff --git a/src/modules/sensors/module.mk b/src/modules/sensors/module.mk index aa538fd6b..5b1bc5e86 100644 --- a/src/modules/sensors/module.mk +++ b/src/modules/sensors/module.mk @@ -40,3 +40,5 @@ MODULE_PRIORITY = "SCHED_PRIORITY_MAX-5" SRCS = sensors.cpp \ sensor_params.c + +MODULE_STACKSIZE = 1200 diff --git a/src/modules/sensors/sensor_params.c b/src/modules/sensors/sensor_params.c index 288c6e00a..c021e1fde 100644 --- a/src/modules/sensors/sensor_params.c +++ b/src/modules/sensors/sensor_params.c @@ -488,6 +488,15 @@ PARAM_DEFINE_INT32(BAT_V_SCALE_IO, 10000); * @group Battery Calibration */ PARAM_DEFINE_FLOAT(BAT_V_SCALING, 0.0082f); +#elif CONFIG_ARCH_BOARD_AEROCORE +/** + * Scaling factor for battery voltage sensor on AeroCore. + * + * For R70 = 133K, R71 = 10K --> scale = 1.8 * 143 / (4096*10) = 0.0063 + * + * @group Battery Calibration + */ +PARAM_DEFINE_FLOAT(BAT_V_SCALING, 0.0063f); #else /** * Scaling factor for battery voltage sensor on FMU v1. @@ -536,6 +545,20 @@ PARAM_DEFINE_INT32(RC_MAP_ROLL, 1); PARAM_DEFINE_INT32(RC_MAP_PITCH, 2); /** + * Failsafe channel mapping. + * + * The RC mapping index indicates which channel is used for failsafe + * If 0, whichever channel is mapped to throttle is used + * otherwise the value indicates the specific rc channel to use + * + * @min 0 + * @max 18 + * + * + */ +PARAM_DEFINE_INT32(RC_MAP_FAILSAFE, 0); //Default to throttle function + +/** * Throttle control channel mapping. * * The channel index (starting from 1 for channel 1) indicates @@ -585,24 +608,22 @@ PARAM_DEFINE_INT32(RC_MAP_MODE_SW, 0); PARAM_DEFINE_INT32(RC_MAP_RETURN_SW, 0); /** - * Assist switch channel mapping. + * Posctl switch channel mapping. * * @min 0 * @max 18 * @group Radio Calibration */ -PARAM_DEFINE_INT32(RC_MAP_ASSIST_SW, 0); +PARAM_DEFINE_INT32(RC_MAP_POSCTL_SW, 0); /** - * Mission switch channel mapping. + * Loiter switch channel mapping. * * @min 0 * @max 18 * @group Radio Calibration */ -PARAM_DEFINE_INT32(RC_MAP_MISSIO_SW, 0); - -//PARAM_DEFINE_INT32(RC_MAP_OFFB_SW, 0); +PARAM_DEFINE_INT32(RC_MAP_LOITER_SW, 0); /** * Flaps channel mapping. @@ -648,53 +669,90 @@ PARAM_DEFINE_INT32(RC_MAP_AUX3, 0); /** - * Roll scaling factor + * Failsafe channel PWM threshold. * + * @min 800 + * @max 2200 * @group Radio Calibration */ -PARAM_DEFINE_FLOAT(RC_SCALE_ROLL, 0.6f); +PARAM_DEFINE_INT32(RC_FAILS_THR, 0); /** - * Pitch scaling factor + * Threshold for selecting assist mode + * + * min:-1 + * max:+1 + * + * 0-1 indicate where in the full channel range the threshold sits + * 0 : min + * 1 : max + * sign indicates polarity of comparison + * positive : true when channel>th + * negative : true when channel<th * - * @group Radio Calibration */ -PARAM_DEFINE_FLOAT(RC_SCALE_PITCH, 0.6f); +PARAM_DEFINE_FLOAT(RC_ASSIST_TH, 0.25f); /** - * Yaw scaling factor + * Threshold for selecting auto mode + * + * min:-1 + * max:+1 + * + * 0-1 indicate where in the full channel range the threshold sits + * 0 : min + * 1 : max + * sign indicates polarity of comparison + * positive : true when channel>th + * negative : true when channel<th * - * @group Radio Calibration */ -PARAM_DEFINE_FLOAT(RC_SCALE_YAW, 2.0f); - +PARAM_DEFINE_FLOAT(RC_AUTO_TH, 0.75f); /** - * Failsafe channel mapping. + * Threshold for selecting posctl mode + * + * min:-1 + * max:+1 + * + * 0-1 indicate where in the full channel range the threshold sits + * 0 : min + * 1 : max + * sign indicates polarity of comparison + * positive : true when channel>th + * negative : true when channel<th * - * @min 0 - * @max 18 - * @group Radio Calibration */ -PARAM_DEFINE_INT32(RC_FS_CH, 0); +PARAM_DEFINE_FLOAT(RC_POSCTL_TH, 0.5f); /** - * Failsafe channel mode. + * Threshold for selecting return to launch mode * - * 0 = too low means signal loss, - * 1 = too high means signal loss + * min:-1 + * max:+1 + * + * 0-1 indicate where in the full channel range the threshold sits + * 0 : min + * 1 : max + * sign indicates polarity of comparison + * positive : true when channel>th + * negative : true when channel<th * - * @min 0 - * @max 1 - * @group Radio Calibration */ -PARAM_DEFINE_INT32(RC_FS_MODE, 0); +PARAM_DEFINE_FLOAT(RC_RETURN_TH, 0.5f); /** - * Failsafe channel PWM threshold. + * Threshold for selecting loiter mode + * + * min:-1 + * max:+1 + * + * 0-1 indicate where in the full channel range the threshold sits + * 0 : min + * 1 : max + * sign indicates polarity of comparison + * positive : true when channel>th + * negative : true when channel<th * - * @min 0 - * @max 1 - * @group Radio Calibration */ -PARAM_DEFINE_FLOAT(RC_FS_THR, 800); +PARAM_DEFINE_FLOAT(RC_LOITER_TH, 0.5f); diff --git a/src/modules/sensors/sensors.cpp b/src/modules/sensors/sensors.cpp index 520ea3137..c5954d02a 100644 --- a/src/modules/sensors/sensors.cpp +++ b/src/modules/sensors/sensors.cpp @@ -36,6 +36,8 @@ * Sensor readout process. * * @author Lorenz Meier <lm@inf.ethz.ch> + * @author Julian Oes <joes@student.ethz.ch> + * @author Thomas Gubler <thomasgubler@student.ethz.ch> */ #include <nuttx/config.h> @@ -124,6 +126,12 @@ #define ADC_AIRSPEED_VOLTAGE_CHANNEL 15 #endif +#ifdef CONFIG_ARCH_BOARD_AEROCORE +#define ADC_BATTERY_VOLTAGE_CHANNEL 10 +#define ADC_BATTERY_CURRENT_CHANNEL -1 +#define ADC_AIRSPEED_VOLTAGE_CHANNEL -1 +#endif + #define BATT_V_LOWPASS 0.001f #define BATT_V_IGNORE_THRESHOLD 3.5f @@ -133,7 +141,7 @@ */ #define PCB_TEMP_ESTIMATE_DEG 5.0f -#define limit_minus_one_to_one(arg) (arg < -1.0f) ? -1.0f : ((arg > 1.0f) ? 1.0f : arg) +#define STICK_ON_OFF_LIMIT 0.75f /** * Sensor app start / stop handling function @@ -165,7 +173,16 @@ public: private: static const unsigned _rc_max_chan_count = RC_INPUT_MAX_CHANNELS; /**< maximum number of r/c channels we handle */ - hrt_abstime _rc_last_valid; /**< last time we got a valid RC signal */ + /** + * Get and limit value for specified RC function. Returns NAN if not mapped. + */ + float get_rc_value(enum RC_CHANNELS_FUNCTION func, float min_value, float max_value); + + /** + * Get switch position for specified function. + */ + switch_pos_t get_rc_sw3pos_position(enum RC_CHANNELS_FUNCTION func, float on_th, bool on_inv, float mid_th, bool mid_inv); + switch_pos_t get_rc_sw2pos_position(enum RC_CHANNELS_FUNCTION func, float on_th, bool on_inv); /** * Gather and publish RC input data. @@ -209,8 +226,8 @@ private: struct differential_pressure_s _diff_pres; struct airspeed_s _airspeed; - math::Matrix<3,3> _board_rotation; /**< rotation matrix for the orientation that the board is mounted */ - math::Matrix<3,3> _external_mag_rotation; /**< rotation matrix for the orientation that an external mag is mounted */ + math::Matrix<3, 3> _board_rotation; /**< rotation matrix for the orientation that the board is mounted */ + math::Matrix<3, 3> _external_mag_rotation; /**< rotation matrix for the orientation that an external mag is mounted */ bool _mag_is_external; /**< true if the active mag is on an external board */ uint64_t _battery_discharged; /**< battery discharged current in mA*ms */ @@ -240,13 +257,12 @@ private: int rc_map_pitch; int rc_map_yaw; int rc_map_throttle; + int rc_map_failsafe; int rc_map_mode_sw; int rc_map_return_sw; - int rc_map_assisted_sw; - int rc_map_mission_sw; - -// int rc_map_offboard_ctrl_mode_sw; + int rc_map_posctl_sw; + int rc_map_loiter_sw; int rc_map_flaps; @@ -256,14 +272,17 @@ private: int rc_map_aux4; int rc_map_aux5; - float rc_scale_roll; - float rc_scale_pitch; - float rc_scale_yaw; - float rc_scale_flaps; - - int rc_fs_ch; - int rc_fs_mode; - float rc_fs_thr; + int32_t rc_fails_thr; + float rc_assist_th; + float rc_auto_th; + float rc_posctl_th; + float rc_return_th; + float rc_loiter_th; + bool rc_assist_inv; + bool rc_auto_inv; + bool rc_posctl_inv; + bool rc_return_inv; + bool rc_loiter_inv; float battery_voltage_scaling; float battery_current_scaling; @@ -290,13 +309,12 @@ private: param_t rc_map_pitch; param_t rc_map_yaw; param_t rc_map_throttle; + param_t rc_map_failsafe; param_t rc_map_mode_sw; param_t rc_map_return_sw; - param_t rc_map_assisted_sw; - param_t rc_map_mission_sw; - -// param_t rc_map_offboard_ctrl_mode_sw; + param_t rc_map_posctl_sw; + param_t rc_map_loiter_sw; param_t rc_map_flaps; @@ -306,14 +324,12 @@ private: param_t rc_map_aux4; param_t rc_map_aux5; - param_t rc_scale_roll; - param_t rc_scale_pitch; - param_t rc_scale_yaw; - param_t rc_scale_flaps; - - param_t rc_fs_ch; - param_t rc_fs_mode; - param_t rc_fs_thr; + param_t rc_fails_thr; + param_t rc_assist_th; + param_t rc_auto_th; + param_t rc_posctl_th; + param_t rc_return_th; + param_t rc_loiter_th; param_t battery_voltage_scaling; param_t battery_current_scaling; @@ -420,7 +436,7 @@ private: /** * Main sensor collection task. */ - void task_main() __attribute__((noreturn)); + void task_main(); }; namespace sensors @@ -436,8 +452,6 @@ Sensors *g_sensors = nullptr; } Sensors::Sensors() : - _rc_last_valid(0), - _fd_adc(-1), _last_adc(0), @@ -472,6 +486,7 @@ Sensors::Sensors() : _battery_discharged(0), _battery_current_timestamp(0) { + memset(&_rc, 0, sizeof(_rc)); /* basic r/c parameters */ for (unsigned i = 0; i < _rc_max_chan_count; i++) { @@ -504,6 +519,7 @@ Sensors::Sensors() : _parameter_handles.rc_map_pitch = param_find("RC_MAP_PITCH"); _parameter_handles.rc_map_yaw = param_find("RC_MAP_YAW"); _parameter_handles.rc_map_throttle = param_find("RC_MAP_THROTTLE"); + _parameter_handles.rc_map_failsafe = param_find("RC_MAP_FAILSAFE"); /* mandatory mode switches, mapped to channel 5 and 6 per default */ _parameter_handles.rc_map_mode_sw = param_find("RC_MAP_MODE_SW"); @@ -512,10 +528,8 @@ Sensors::Sensors() : _parameter_handles.rc_map_flaps = param_find("RC_MAP_FLAPS"); /* optional mode switches, not mapped per default */ - _parameter_handles.rc_map_assisted_sw = param_find("RC_MAP_ASSIST_SW"); - _parameter_handles.rc_map_mission_sw = param_find("RC_MAP_MISSIO_SW"); - -// _parameter_handles.rc_map_offboard_ctrl_mode_sw = param_find("RC_MAP_OFFB_SW"); + _parameter_handles.rc_map_posctl_sw = param_find("RC_MAP_POSCTL_SW"); + _parameter_handles.rc_map_loiter_sw = param_find("RC_MAP_LOITER_SW"); _parameter_handles.rc_map_aux1 = param_find("RC_MAP_AUX1"); _parameter_handles.rc_map_aux2 = param_find("RC_MAP_AUX2"); @@ -523,15 +537,13 @@ Sensors::Sensors() : _parameter_handles.rc_map_aux4 = param_find("RC_MAP_AUX4"); _parameter_handles.rc_map_aux5 = param_find("RC_MAP_AUX5"); - _parameter_handles.rc_scale_roll = param_find("RC_SCALE_ROLL"); - _parameter_handles.rc_scale_pitch = param_find("RC_SCALE_PITCH"); - _parameter_handles.rc_scale_yaw = param_find("RC_SCALE_YAW"); - _parameter_handles.rc_scale_flaps = param_find("RC_SCALE_FLAPS"); - - /* RC failsafe */ - _parameter_handles.rc_fs_ch = param_find("RC_FS_CH"); - _parameter_handles.rc_fs_mode = param_find("RC_FS_MODE"); - _parameter_handles.rc_fs_thr = param_find("RC_FS_THR"); + /* RC thresholds */ + _parameter_handles.rc_fails_thr = param_find("RC_FAILS_THR"); + _parameter_handles.rc_assist_th = param_find("RC_ASSIST_TH"); + _parameter_handles.rc_auto_th = param_find("RC_AUTO_TH"); + _parameter_handles.rc_posctl_th = param_find("RC_POSCTL_TH"); + _parameter_handles.rc_return_th = param_find("RC_RETURN_TH"); + _parameter_handles.rc_loiter_th = param_find("RC_LOITER_TH"); /* gyro offsets */ _parameter_handles.gyro_offset[0] = param_find("SENS_GYRO_XOFF"); @@ -632,64 +644,74 @@ Sensors::parameters_update() } /* handle wrong values */ - if (!rc_valid) + if (!rc_valid) { warnx("WARNING WARNING WARNING\n\nRC CALIBRATION NOT SANE!\n\n"); + } const char *paramerr = "FAIL PARM LOAD"; /* channel mapping */ if (param_get(_parameter_handles.rc_map_roll, &(_parameters.rc_map_roll)) != OK) { - warnx(paramerr); + warnx("%s", paramerr); } if (param_get(_parameter_handles.rc_map_pitch, &(_parameters.rc_map_pitch)) != OK) { - warnx(paramerr); + warnx("%s", paramerr); } if (param_get(_parameter_handles.rc_map_yaw, &(_parameters.rc_map_yaw)) != OK) { - warnx(paramerr); + warnx("%s", paramerr); } if (param_get(_parameter_handles.rc_map_throttle, &(_parameters.rc_map_throttle)) != OK) { - warnx(paramerr); + warnx("%s", paramerr); + } + + if (param_get(_parameter_handles.rc_map_failsafe, &(_parameters.rc_map_failsafe)) != OK) { + warnx("%s", paramerr); } if (param_get(_parameter_handles.rc_map_mode_sw, &(_parameters.rc_map_mode_sw)) != OK) { - warnx(paramerr); + warnx("%s", paramerr); } if (param_get(_parameter_handles.rc_map_return_sw, &(_parameters.rc_map_return_sw)) != OK) { - warnx(paramerr); + warnx("%s", paramerr); } - if (param_get(_parameter_handles.rc_map_assisted_sw, &(_parameters.rc_map_assisted_sw)) != OK) { - warnx(paramerr); + if (param_get(_parameter_handles.rc_map_posctl_sw, &(_parameters.rc_map_posctl_sw)) != OK) { + warnx("%s", paramerr); } - if (param_get(_parameter_handles.rc_map_mission_sw, &(_parameters.rc_map_mission_sw)) != OK) { - warnx(paramerr); + if (param_get(_parameter_handles.rc_map_loiter_sw, &(_parameters.rc_map_loiter_sw)) != OK) { + warnx("%s", paramerr); } if (param_get(_parameter_handles.rc_map_flaps, &(_parameters.rc_map_flaps)) != OK) { - warnx(paramerr); + warnx("%s", paramerr); } -// if (param_get(_parameter_handles.rc_map_offboard_ctrl_mode_sw, &(_parameters.rc_map_offboard_ctrl_mode_sw)) != OK) { -// warnx("Failed getting offboard control mode sw chan index"); -// } - param_get(_parameter_handles.rc_map_aux1, &(_parameters.rc_map_aux1)); param_get(_parameter_handles.rc_map_aux2, &(_parameters.rc_map_aux2)); param_get(_parameter_handles.rc_map_aux3, &(_parameters.rc_map_aux3)); param_get(_parameter_handles.rc_map_aux4, &(_parameters.rc_map_aux4)); param_get(_parameter_handles.rc_map_aux5, &(_parameters.rc_map_aux5)); - param_get(_parameter_handles.rc_scale_roll, &(_parameters.rc_scale_roll)); - param_get(_parameter_handles.rc_scale_pitch, &(_parameters.rc_scale_pitch)); - param_get(_parameter_handles.rc_scale_yaw, &(_parameters.rc_scale_yaw)); - param_get(_parameter_handles.rc_scale_flaps, &(_parameters.rc_scale_flaps)); - param_get(_parameter_handles.rc_fs_ch, &(_parameters.rc_fs_ch)); - param_get(_parameter_handles.rc_fs_mode, &(_parameters.rc_fs_mode)); - param_get(_parameter_handles.rc_fs_thr, &(_parameters.rc_fs_thr)); + param_get(_parameter_handles.rc_fails_thr, &(_parameters.rc_fails_thr)); + param_get(_parameter_handles.rc_assist_th, &(_parameters.rc_assist_th)); + _parameters.rc_assist_inv = (_parameters.rc_assist_th < 0); + _parameters.rc_assist_th = fabs(_parameters.rc_assist_th); + param_get(_parameter_handles.rc_auto_th, &(_parameters.rc_auto_th)); + _parameters.rc_auto_inv = (_parameters.rc_auto_th < 0); + _parameters.rc_auto_th = fabs(_parameters.rc_auto_th); + param_get(_parameter_handles.rc_posctl_th, &(_parameters.rc_posctl_th)); + _parameters.rc_posctl_inv = (_parameters.rc_posctl_th < 0); + _parameters.rc_posctl_th = fabs(_parameters.rc_posctl_th); + param_get(_parameter_handles.rc_return_th, &(_parameters.rc_return_th)); + _parameters.rc_return_inv = (_parameters.rc_return_th < 0); + _parameters.rc_return_th = fabs(_parameters.rc_return_th); + param_get(_parameter_handles.rc_loiter_th, &(_parameters.rc_loiter_th)); + _parameters.rc_loiter_inv = (_parameters.rc_loiter_th < 0); + _parameters.rc_loiter_th = fabs(_parameters.rc_loiter_th); /* update RC function mappings */ _rc.function[THROTTLE] = _parameters.rc_map_throttle - 1; @@ -699,13 +721,11 @@ Sensors::parameters_update() _rc.function[MODE] = _parameters.rc_map_mode_sw - 1; _rc.function[RETURN] = _parameters.rc_map_return_sw - 1; - _rc.function[ASSISTED] = _parameters.rc_map_assisted_sw - 1; - _rc.function[MISSION] = _parameters.rc_map_mission_sw - 1; + _rc.function[POSCTL] = _parameters.rc_map_posctl_sw - 1; + _rc.function[LOITER] = _parameters.rc_map_loiter_sw - 1; _rc.function[FLAPS] = _parameters.rc_map_flaps - 1; -// _rc.function[OFFBOARD_MODE] = _parameters.rc_map_offboard_ctrl_mode_sw - 1; - _rc.function[AUX_1] = _parameters.rc_map_aux1 - 1; _rc.function[AUX_2] = _parameters.rc_map_aux2 - 1; _rc.function[AUX_3] = _parameters.rc_map_aux3 - 1; @@ -743,12 +763,12 @@ Sensors::parameters_update() /* scaling of ADC ticks to battery voltage */ if (param_get(_parameter_handles.battery_voltage_scaling, &(_parameters.battery_voltage_scaling)) != OK) { - warnx(paramerr); + warnx("%s", paramerr); } /* scaling of ADC ticks to battery current */ if (param_get(_parameter_handles.battery_current_scaling, &(_parameters.battery_current_scaling)) != OK) { - warnx(paramerr); + warnx("%s", paramerr); } param_get(_parameter_handles.board_rotation, &(_parameters.board_rotation)); @@ -783,7 +803,7 @@ Sensors::accel_init() /* set the driver to poll at 1000Hz */ ioctl(fd, SENSORIOCSPOLLRATE, 1000); -#elif CONFIG_ARCH_BOARD_PX4FMU_V2 +#elif CONFIG_ARCH_BOARD_PX4FMU_V2 || CONFIG_ARCH_BOARD_AEROCORE /* set the accel internal sampling rate up to at leat 800Hz */ ioctl(fd, ACCELIOCSSAMPLERATE, 800); @@ -792,7 +812,7 @@ Sensors::accel_init() ioctl(fd, SENSORIOCSPOLLRATE, 800); #else -#error Need a board configuration, either CONFIG_ARCH_BOARD_PX4FMU_V1 or CONFIG_ARCH_BOARD_PX4FMU_V2 +#error Need a board configuration, either CONFIG_ARCH_BOARD_PX4FMU_V1, CONFIG_ARCH_BOARD_PX4FMU_V2 or CONFIG_ARCH_BOARD_AEROCORE #endif @@ -818,12 +838,14 @@ Sensors::gyro_init() #ifdef CONFIG_ARCH_BOARD_PX4FMU_V1 /* set the gyro internal sampling rate up to at least 1000Hz */ - if (ioctl(fd, GYROIOCSSAMPLERATE, 1000) != OK) + if (ioctl(fd, GYROIOCSSAMPLERATE, 1000) != OK) { ioctl(fd, GYROIOCSSAMPLERATE, 800); + } /* set the driver to poll at 1000Hz */ - if (ioctl(fd, SENSORIOCSPOLLRATE, 1000) != OK) + if (ioctl(fd, SENSORIOCSPOLLRATE, 1000) != OK) { ioctl(fd, SENSORIOCSPOLLRATE, 800); + } #else @@ -878,12 +900,15 @@ Sensors::mag_init() ret = ioctl(fd, MAGIOCGEXTERNAL, 0); - if (ret < 0) + if (ret < 0) { errx(1, "FATAL: unknown if magnetometer is external or onboard"); - else if (ret == 1) + + } else if (ret == 1) { _mag_is_external = true; - else + + } else { _mag_is_external = false; + } close(fd); } @@ -983,10 +1008,12 @@ Sensors::mag_poll(struct sensor_combined_s &raw) math::Vector<3> vect(mag_report.x, mag_report.y, mag_report.z); - if (_mag_is_external) + if (_mag_is_external) { vect = _external_mag_rotation * vect; - else + + } else { vect = _board_rotation * vect; + } raw.magnetometer_ga[0] = vect(0); raw.magnetometer_ga[1] = vect(1); @@ -1029,11 +1056,15 @@ Sensors::diff_pres_poll(struct sensor_combined_s &raw) raw.differential_pressure_pa = _diff_pres.differential_pressure_pa; raw.differential_pressure_timestamp = _diff_pres.timestamp; + raw.differential_pressure_filtered_pa = _diff_pres.differential_pressure_filtered_pa; - _airspeed.timestamp = hrt_absolute_time(); - _airspeed.indicated_airspeed_m_s = calc_indicated_airspeed(_diff_pres.differential_pressure_pa); - _airspeed.true_airspeed_m_s = calc_true_airspeed(_diff_pres.differential_pressure_pa + raw.baro_pres_mbar * 1e2f, - raw.baro_pres_mbar * 1e2f, raw.baro_temp_celcius - PCB_TEMP_ESTIMATE_DEG); + float air_temperature_celsius = (_diff_pres.temperature > -300.0f) ? _diff_pres.temperature : (raw.baro_temp_celcius - PCB_TEMP_ESTIMATE_DEG); + + _airspeed.timestamp = _diff_pres.timestamp; + _airspeed.indicated_airspeed_m_s = calc_indicated_airspeed(_diff_pres.differential_pressure_filtered_pa); + _airspeed.true_airspeed_m_s = calc_true_airspeed(_diff_pres.differential_pressure_filtered_pa + raw.baro_pres_mbar * 1e2f, + raw.baro_pres_mbar * 1e2f, air_temperature_celsius); + _airspeed.air_temperature_celsius = air_temperature_celsius; /* announce the airspeed if needed, just publish else */ if (_airspeed_pub > 0) { @@ -1100,8 +1131,9 @@ Sensors::parameter_update_poll(bool forced) _parameters.gyro_scale[2], }; - if (OK != ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gscale)) + if (OK != ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gscale)) { warn("WARNING: failed to set scale / offsets for gyro"); + } close(fd); @@ -1115,8 +1147,9 @@ Sensors::parameter_update_poll(bool forced) _parameters.accel_scale[2], }; - if (OK != ioctl(fd, ACCELIOCSSCALE, (long unsigned int)&ascale)) + if (OK != ioctl(fd, ACCELIOCSSCALE, (long unsigned int)&ascale)) { warn("WARNING: failed to set scale / offsets for accel"); + } close(fd); @@ -1130,8 +1163,9 @@ Sensors::parameter_update_poll(bool forced) _parameters.mag_scale[2], }; - if (OK != ioctl(fd, MAGIOCSSCALE, (long unsigned int)&mscale)) + if (OK != ioctl(fd, MAGIOCSSCALE, (long unsigned int)&mscale)) { warn("WARNING: failed to set scale / offsets for mag"); + } close(fd); @@ -1145,8 +1179,10 @@ Sensors::parameter_update_poll(bool forced) 1.0f, }; - if (OK != ioctl(fd, AIRSPEEDIOCSSCALE, (long unsigned int)&airscale)) + if (OK != ioctl(fd, AIRSPEEDIOCSSCALE, (long unsigned int)&airscale)) { warn("WARNING: failed to set scale / offsets for airspeed sensor"); + } + close(fd); } @@ -1164,22 +1200,27 @@ void Sensors::adc_poll(struct sensor_combined_s &raw) { /* only read if publishing */ - if (!_publishing) + if (!_publishing) { return; + } hrt_abstime t = hrt_absolute_time(); + /* rate limit to 100 Hz */ if (t - _last_adc >= 10000) { - /* make space for a maximum of eight channels */ - struct adc_msg_s buf_adc[8]; + /* make space for a maximum of twelve channels (to ensure reading all channels at once) */ + struct adc_msg_s buf_adc[12]; /* read all channels available */ int ret = read(_fd_adc, &buf_adc, sizeof(buf_adc)); if (ret >= (int)sizeof(buf_adc[0])) { - for (unsigned i = 0; i < sizeof(buf_adc) / sizeof(buf_adc[0]); i++) { + + /* Read add channels we got */ + for (unsigned i = 0; i < ret / sizeof(buf_adc[0]); i++) { /* Save raw voltage values */ - if (i < (sizeof(raw.adc_voltage_v)) / sizeof(raw.adc_voltage_v[0])) { + if (i < (sizeof(raw.adc_voltage_v) / sizeof(raw.adc_voltage_v[0]))) { raw.adc_voltage_v[i] = buf_adc[i].am_data / (4096.0f / 3.3f); + raw.adc_mapping[i] = buf_adc[i].am_channel; } /* look for specific channels and process the raw voltage to measurement data */ @@ -1189,6 +1230,7 @@ Sensors::adc_poll(struct sensor_combined_s &raw) if (voltage > BATT_V_IGNORE_THRESHOLD) { _battery_status.voltage_v = voltage; + /* one-time initialization of low-pass value to avoid long init delays */ if (_battery_status.voltage_filtered_v < BATT_V_IGNORE_THRESHOLD) { _battery_status.voltage_filtered_v = voltage; @@ -1207,19 +1249,24 @@ Sensors::adc_poll(struct sensor_combined_s &raw) /* handle current only if voltage is valid */ if (_battery_status.voltage_v > 0.0f) { float current = (buf_adc[i].am_data * _parameters.battery_current_scaling); + /* check measured current value */ if (current >= 0.0f) { _battery_status.timestamp = t; _battery_status.current_a = current; + if (_battery_current_timestamp != 0) { /* initialize discharged value */ - if (_battery_status.discharged_mah < 0.0f) + if (_battery_status.discharged_mah < 0.0f) { _battery_status.discharged_mah = 0.0f; + } + _battery_discharged += current * (t - _battery_current_timestamp); _battery_status.discharged_mah = ((float) _battery_discharged) / 3600000.0f; } } } + _battery_current_timestamp = t; } else if (ADC_AIRSPEED_VOLTAGE_CHANNEL == buf_adc[i].am_channel) { @@ -1238,6 +1285,8 @@ Sensors::adc_poll(struct sensor_combined_s &raw) _diff_pres.timestamp = t; _diff_pres.differential_pressure_pa = diff_pres_pa; + _diff_pres.differential_pressure_filtered_pa = diff_pres_pa; + _diff_pres.temperature = -1000.0f; _diff_pres.voltage = voltage; /* announce the airspeed if needed, just publish else */ @@ -1250,8 +1299,10 @@ Sensors::adc_poll(struct sensor_combined_s &raw) } } } + _last_adc = t; - if (_battery_status.voltage_v > 0.0f) { + + if (_battery_status.voltage_filtered_v > BATT_V_IGNORE_THRESHOLD) { /* announce the battery status if needed, just publish else */ if (_battery_pub > 0) { orb_publish(ORB_ID(battery_status), _battery_pub, &_battery_status); @@ -1264,6 +1315,66 @@ Sensors::adc_poll(struct sensor_combined_s &raw) } } +float +Sensors::get_rc_value(enum RC_CHANNELS_FUNCTION func, float min_value, float max_value) +{ + if (_rc.function[func] >= 0) { + float value = _rc.chan[_rc.function[func]].scaled; + + if (value < min_value) { + return min_value; + + } else if (value > max_value) { + return max_value; + + } else { + return value; + } + + } else { + return 0.0f; + } +} + +switch_pos_t +Sensors::get_rc_sw3pos_position(enum RC_CHANNELS_FUNCTION func, float on_th, bool on_inv, float mid_th, bool mid_inv) +{ + if (_rc.function[func] >= 0) { + float value = 0.5f * _rc.chan[_rc.function[func]].scaled + 0.5f; + + if (on_inv ? value < on_th : value > on_th) { + return SWITCH_POS_ON; + + } else if (mid_inv ? value < mid_th : value > mid_th) { + return SWITCH_POS_MIDDLE; + + } else { + return SWITCH_POS_OFF; + } + + } else { + return SWITCH_POS_NONE; + } +} + +switch_pos_t +Sensors::get_rc_sw2pos_position(enum RC_CHANNELS_FUNCTION func, float on_th, bool on_inv) +{ + if (_rc.function[func] >= 0) { + float value = 0.5f * _rc.chan[_rc.function[func]].scaled + 0.5f; + + if (on_inv ? value < on_th : value > on_th) { + return SWITCH_POS_ON; + + } else { + return SWITCH_POS_OFF; + } + + } else { + return SWITCH_POS_NONE; + } +} + void Sensors::rc_poll() { @@ -1272,70 +1383,58 @@ Sensors::rc_poll() if (rc_updated) { /* read low-level values from FMU or IO RC inputs (PPM, Spektrum, S.Bus) */ - struct rc_input_values rc_input; + struct rc_input_values rc_input; orb_copy(ORB_ID(input_rc), _rc_sub, &rc_input); - if (rc_input.rc_lost) - return; - - struct manual_control_setpoint_s manual_control; - struct actuator_controls_s actuator_group_3; - - /* initialize to default values */ - manual_control.roll = NAN; - manual_control.pitch = NAN; - manual_control.yaw = NAN; - manual_control.throttle = NAN; - - manual_control.mode_switch = NAN; - manual_control.return_switch = NAN; - manual_control.assisted_switch = NAN; - manual_control.mission_switch = NAN; -// manual_control.auto_offboard_input_switch = NAN; - - manual_control.flaps = NAN; - manual_control.aux1 = NAN; - manual_control.aux2 = NAN; - manual_control.aux3 = NAN; - manual_control.aux4 = NAN; - manual_control.aux5 = NAN; - - /* require at least four channels to consider the signal valid */ - if (rc_input.channel_count < 4) - return; - - /* failsafe check */ - if (_parameters.rc_fs_ch != 0) { - if (_parameters.rc_fs_mode == 0) { - if (rc_input.values[_parameters.rc_fs_ch - 1] < _parameters.rc_fs_thr) - return; - - } else if (_parameters.rc_fs_mode == 1) { - if (rc_input.values[_parameters.rc_fs_ch - 1] > _parameters.rc_fs_thr) - return; + /* detect RC signal loss */ + bool signal_lost; + + /* check flags and require at least four channels to consider the signal valid */ + if (rc_input.rc_lost || rc_input.rc_failsafe || rc_input.channel_count < 4) { + /* signal is lost or no enough channels */ + signal_lost = true; + + } else { + /* signal looks good */ + signal_lost = false; + + /* check failsafe */ + int8_t fs_ch = _rc.function[_parameters.rc_map_failsafe]; // get channel mapped to throttle + + if (_parameters.rc_map_failsafe > 0) { // if not 0, use channel number instead of rc.function mapping + fs_ch = _parameters.rc_map_failsafe - 1; + } + + if (_parameters.rc_fails_thr > 0 && fs_ch >= 0) { + /* failsafe configured */ + if ((_parameters.rc_fails_thr < _parameters.min[fs_ch] && rc_input.values[fs_ch] < _parameters.rc_fails_thr) || + (_parameters.rc_fails_thr > _parameters.max[fs_ch] && rc_input.values[fs_ch] > _parameters.rc_fails_thr)) { + /* failsafe triggered, signal is lost by receiver */ + signal_lost = true; + } } } unsigned channel_limit = rc_input.channel_count; - if (channel_limit > _rc_max_chan_count) + if (channel_limit > _rc_max_chan_count) { channel_limit = _rc_max_chan_count; + } - /* we are accepting this message */ - _rc_last_valid = rc_input.timestamp_last_signal; - - /* Read out values from raw message */ + /* read out and scale values from raw message even if signal is invalid */ for (unsigned int i = 0; i < channel_limit; i++) { /* * 1) Constrain to min/max values, as later processing depends on bounds. */ - if (rc_input.values[i] < _parameters.min[i]) + if (rc_input.values[i] < _parameters.min[i]) { rc_input.values[i] = _parameters.min[i]; + } - if (rc_input.values[i] > _parameters.max[i]) + if (rc_input.values[i] > _parameters.max[i]) { rc_input.values[i] = _parameters.max[i]; + } /* * 2) Scale around the mid point differently for lower and upper range. @@ -1367,135 +1466,81 @@ Sensors::rc_poll() _rc.chan[i].scaled *= _parameters.rev[i]; /* handle any parameter-induced blowups */ - if (!isfinite(_rc.chan[i].scaled)) + if (!isfinite(_rc.chan[i].scaled)) { _rc.chan[i].scaled = 0.0f; + } } _rc.chan_count = rc_input.channel_count; + _rc.rssi = rc_input.rssi; + _rc.signal_lost = signal_lost; _rc.timestamp = rc_input.timestamp_last_signal; - manual_control.timestamp = rc_input.timestamp_last_signal; - - /* roll input - rolling right is stick-wise and rotation-wise positive */ - manual_control.roll = limit_minus_one_to_one(_rc.chan[_rc.function[ROLL]].scaled); - /* - * pitch input - stick down is negative, but stick down is pitching up (pos) in NED, - * so reverse sign. - */ - manual_control.pitch = limit_minus_one_to_one(-1.0f * _rc.chan[_rc.function[PITCH]].scaled); - /* yaw input - stick right is positive and positive rotation */ - manual_control.yaw = limit_minus_one_to_one(_rc.chan[_rc.function[YAW]].scaled); - /* throttle input */ - manual_control.throttle = _rc.chan[_rc.function[THROTTLE]].scaled; - - if (manual_control.throttle < 0.0f) manual_control.throttle = 0.0f; - - if (manual_control.throttle > 1.0f) manual_control.throttle = 1.0f; - - /* scale output */ - if (isfinite(_parameters.rc_scale_roll) && _parameters.rc_scale_roll > 0.0f) { - manual_control.roll *= _parameters.rc_scale_roll; - } - - if (isfinite(_parameters.rc_scale_pitch) && _parameters.rc_scale_pitch > 0.0f) { - manual_control.pitch *= _parameters.rc_scale_pitch; - } - - if (isfinite(_parameters.rc_scale_yaw) && _parameters.rc_scale_yaw > 0.0f) { - manual_control.yaw *= _parameters.rc_scale_yaw; - } - - /* flaps */ - if (_rc.function[FLAPS] >= 0) { - - manual_control.flaps = limit_minus_one_to_one(_rc.chan[_rc.function[FLAPS]].scaled); - - if (isfinite(_parameters.rc_scale_flaps) && _parameters.rc_scale_flaps > 0.0f) { - manual_control.flaps *= _parameters.rc_scale_flaps; - } - } - - /* mode switch input */ - if (_rc.function[MODE] >= 0) { - manual_control.mode_switch = limit_minus_one_to_one(_rc.chan[_rc.function[MODE]].scaled); - } - - /* assisted switch input */ - if (_rc.function[ASSISTED] >= 0) { - manual_control.assisted_switch = limit_minus_one_to_one(_rc.chan[_rc.function[ASSISTED]].scaled); - } - - /* mission switch input */ - if (_rc.function[MISSION] >= 0) { - manual_control.mission_switch = limit_minus_one_to_one(_rc.chan[_rc.function[MISSION]].scaled); - } - - /* return switch input */ - if (_rc.function[RETURN] >= 0) { - manual_control.return_switch = limit_minus_one_to_one(_rc.chan[_rc.function[RETURN]].scaled); - } - -// if (_rc.function[OFFBOARD_MODE] >= 0) { -// manual_control.auto_offboard_input_switch = limit_minus_one_to_one(_rc.chan[_rc.function[OFFBOARD_MODE]].scaled); -// } - - /* aux functions, only assign if valid mapping is present */ - if (_rc.function[AUX_1] >= 0) { - manual_control.aux1 = limit_minus_one_to_one(_rc.chan[_rc.function[AUX_1]].scaled); - } - - if (_rc.function[AUX_2] >= 0) { - manual_control.aux2 = limit_minus_one_to_one(_rc.chan[_rc.function[AUX_2]].scaled); - } - - if (_rc.function[AUX_3] >= 0) { - manual_control.aux3 = limit_minus_one_to_one(_rc.chan[_rc.function[AUX_3]].scaled); - } - - if (_rc.function[AUX_4] >= 0) { - manual_control.aux4 = limit_minus_one_to_one(_rc.chan[_rc.function[AUX_4]].scaled); - } - - if (_rc.function[AUX_5] >= 0) { - manual_control.aux5 = limit_minus_one_to_one(_rc.chan[_rc.function[AUX_5]].scaled); - } - - /* copy from mapped manual control to control group 3 */ - actuator_group_3.control[0] = manual_control.roll; - actuator_group_3.control[1] = manual_control.pitch; - actuator_group_3.control[2] = manual_control.yaw; - actuator_group_3.control[3] = manual_control.throttle; - actuator_group_3.control[4] = manual_control.flaps; - actuator_group_3.control[5] = manual_control.aux1; - actuator_group_3.control[6] = manual_control.aux2; - actuator_group_3.control[7] = manual_control.aux3; - - /* check if ready for publishing */ + /* publish rc_channels topic even if signal is invalid, for debug */ if (_rc_pub > 0) { orb_publish(ORB_ID(rc_channels), _rc_pub, &_rc); } else { - /* advertise the rc topic */ _rc_pub = orb_advertise(ORB_ID(rc_channels), &_rc); } - /* check if ready for publishing */ - if (_manual_control_pub > 0) { - orb_publish(ORB_ID(manual_control_setpoint), _manual_control_pub, &manual_control); + if (!signal_lost) { + struct manual_control_setpoint_s manual; + memset(&manual, 0 , sizeof(manual)); + + /* fill values in manual_control_setpoint topic only if signal is valid */ + manual.timestamp = rc_input.timestamp_last_signal; + + /* limit controls */ + manual.y = get_rc_value(ROLL, -1.0, 1.0); + manual.x = get_rc_value(PITCH, -1.0, 1.0); + manual.r = get_rc_value(YAW, -1.0, 1.0); + manual.z = get_rc_value(THROTTLE, 0.0, 1.0); + manual.flaps = get_rc_value(FLAPS, -1.0, 1.0); + manual.aux1 = get_rc_value(AUX_1, -1.0, 1.0); + manual.aux2 = get_rc_value(AUX_2, -1.0, 1.0); + manual.aux3 = get_rc_value(AUX_3, -1.0, 1.0); + manual.aux4 = get_rc_value(AUX_4, -1.0, 1.0); + manual.aux5 = get_rc_value(AUX_5, -1.0, 1.0); + + /* mode switches */ + manual.mode_switch = get_rc_sw3pos_position(MODE, _parameters.rc_auto_th, _parameters.rc_auto_inv, _parameters.rc_assist_th, _parameters.rc_assist_inv); + manual.posctl_switch = get_rc_sw2pos_position(POSCTL, _parameters.rc_posctl_th, _parameters.rc_posctl_inv); + manual.return_switch = get_rc_sw2pos_position(RETURN, _parameters.rc_return_th, _parameters.rc_return_inv); + manual.loiter_switch = get_rc_sw2pos_position(LOITER, _parameters.rc_loiter_th, _parameters.rc_loiter_inv); + + /* publish manual_control_setpoint topic */ + if (_manual_control_pub > 0) { + orb_publish(ORB_ID(manual_control_setpoint), _manual_control_pub, &manual); - } else { - _manual_control_pub = orb_advertise(ORB_ID(manual_control_setpoint), &manual_control); - } + } else { + _manual_control_pub = orb_advertise(ORB_ID(manual_control_setpoint), &manual); + } - /* check if ready for publishing */ - if (_actuator_group_3_pub > 0) { - orb_publish(ORB_ID(actuator_controls_3), _actuator_group_3_pub, &actuator_group_3); + /* copy from mapped manual control to control group 3 */ + struct actuator_controls_s actuator_group_3; + memset(&actuator_group_3, 0 , sizeof(actuator_group_3)); - } else { - _actuator_group_3_pub = orb_advertise(ORB_ID(actuator_controls_3), &actuator_group_3); + actuator_group_3.timestamp = rc_input.timestamp_last_signal; + + actuator_group_3.control[0] = manual.y; + actuator_group_3.control[1] = manual.x; + actuator_group_3.control[2] = manual.r; + actuator_group_3.control[3] = manual.z; + actuator_group_3.control[4] = manual.flaps; + actuator_group_3.control[5] = manual.aux1; + actuator_group_3.control[6] = manual.aux2; + actuator_group_3.control[7] = manual.aux3; + + /* publish actuator_controls_3 topic */ + if (_actuator_group_3_pub > 0) { + orb_publish(ORB_ID(actuator_controls_3), _actuator_group_3_pub, &actuator_group_3); + + } else { + _actuator_group_3_pub = orb_advertise(ORB_ID(actuator_controls_3), &actuator_group_3); + } } } - } void @@ -1572,12 +1617,10 @@ Sensors::task_main() while (!_task_should_exit) { - /* wait for up to 100ms for data */ - int pret = poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 100); + /* wait for up to 50ms for data */ + int pret = poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 50); - /* timed out - periodic check for _task_should_exit, etc. */ - if (pret == 0) - continue; + /* if pret == 0 it timed out - periodic check for _task_should_exit, etc. */ /* this is undesirable but not much we can do - might want to flag unhappy status */ if (pret < 0) { @@ -1607,8 +1650,9 @@ Sensors::task_main() diff_pres_poll(raw); /* Inform other processes that new data is available to copy */ - if (_publishing) + if (_publishing) { orb_publish(ORB_ID(sensor_combined), _sensor_pub, &raw); + } /* Look for new r/c input data */ rc_poll(); @@ -1616,7 +1660,7 @@ Sensors::task_main() perf_end(_loop_perf); } - printf("[sensors] exiting.\n"); + warnx("[sensors] exiting."); _sensors_task = -1; _exit(0); @@ -1631,7 +1675,7 @@ Sensors::start() _sensors_task = task_spawn_cmd("sensors_task", SCHED_DEFAULT, SCHED_PRIORITY_MAX - 5, - 2048, + 2000, (main_t)&Sensors::task_main_trampoline, nullptr); @@ -1645,18 +1689,21 @@ Sensors::start() int sensors_main(int argc, char *argv[]) { - if (argc < 1) + if (argc < 1) { errx(1, "usage: sensors {start|stop|status}"); + } if (!strcmp(argv[1], "start")) { - if (sensors::g_sensors != nullptr) + if (sensors::g_sensors != nullptr) { errx(0, "already running"); + } sensors::g_sensors = new Sensors; - if (sensors::g_sensors == nullptr) + if (sensors::g_sensors == nullptr) { errx(1, "alloc failed"); + } if (OK != sensors::g_sensors->start()) { delete sensors::g_sensors; @@ -1668,8 +1715,9 @@ int sensors_main(int argc, char *argv[]) } if (!strcmp(argv[1], "stop")) { - if (sensors::g_sensors == nullptr) + if (sensors::g_sensors == nullptr) { errx(1, "not running"); + } delete sensors::g_sensors; sensors::g_sensors = nullptr; @@ -1688,4 +1736,3 @@ int sensors_main(int argc, char *argv[]) warnx("unrecognized command"); return 1; } - diff --git a/src/modules/systemlib/mixer/mixer.h b/src/modules/systemlib/mixer/mixer.h index 1c889a811..fa9d28b74 100644 --- a/src/modules/systemlib/mixer/mixer.h +++ b/src/modules/systemlib/mixer/mixer.h @@ -516,7 +516,7 @@ private: float _roll_scale; float _pitch_scale; float _yaw_scale; - float _deadband; + float _idle_speed; unsigned _rotor_count; const Rotor *_rotors; diff --git a/src/modules/systemlib/mixer/mixer_load.c b/src/modules/systemlib/mixer/mixer_load.c index b05273c0d..bf3428a50 100644 --- a/src/modules/systemlib/mixer/mixer_load.c +++ b/src/modules/systemlib/mixer/mixer_load.c @@ -41,6 +41,7 @@ #include <string.h> #include <stdio.h> #include <ctype.h> +#include <systemlib/err.h> #include "mixer_load.h" diff --git a/src/modules/systemlib/mixer/mixer_multirotor.cpp b/src/modules/systemlib/mixer/mixer_multirotor.cpp index bf77795d5..1ca0a21e9 100644 --- a/src/modules/systemlib/mixer/mixer_multirotor.cpp +++ b/src/modules/systemlib/mixer/mixer_multirotor.cpp @@ -67,6 +67,11 @@ namespace { +float constrain(float val, float min, float max) +{ + return (val < min) ? min : ((val > max) ? max : val); +} + /* * These tables automatically generated by multi_tables - do not edit. */ @@ -171,12 +176,12 @@ MultirotorMixer::MultirotorMixer(ControlCallback control_cb, float roll_scale, float pitch_scale, float yaw_scale, - float deadband) : + float idle_speed) : Mixer(control_cb, cb_handle), _roll_scale(roll_scale), _pitch_scale(pitch_scale), _yaw_scale(yaw_scale), - _deadband(-1.0f + deadband), /* shift to output range here to avoid runtime calculation */ + _idle_speed(-1.0f + idle_speed * 2.0f), /* shift to output range here to avoid runtime calculation */ _rotor_count(_config_rotor_count[geometry]), _rotors(_config_index[geometry]) { @@ -276,67 +281,67 @@ MultirotorMixer::from_text(Mixer::ControlCallback control_cb, uintptr_t cb_handl unsigned MultirotorMixer::mix(float *outputs, unsigned space) { - float roll = get_control(0, 0) * _roll_scale; + float roll = constrain(get_control(0, 0) * _roll_scale, -1.0f, 1.0f); //lowsyslog("roll: %d, get_control0: %d, %d\n", (int)(roll), (int)(get_control(0, 0)), (int)(_roll_scale)); - float pitch = get_control(0, 1) * _pitch_scale; - float yaw = get_control(0, 2) * _yaw_scale; - float thrust = get_control(0, 3); + float pitch = constrain(get_control(0, 1) * _pitch_scale, -1.0f, 1.0f); + float yaw = constrain(get_control(0, 2) * _yaw_scale, -1.0f, 1.0f); + float thrust = constrain(get_control(0, 3), 0.0f, 1.0f); //lowsyslog("thrust: %d, get_control3: %d\n", (int)(thrust), (int)(get_control(0, 3))); - float max = 0.0f; - float fixup_scale; + float min_out = 0.0f; + float max_out = 0.0f; + float scale_yaw = 1.0f; - /* use an output factor to prevent too strong control signals at low throttle */ - float min_thrust = 0.05f; - float max_thrust = 1.0f; - float startpoint_full_control = 0.40f; - float output_factor; + /* perform initial mix pass yielding unbounded outputs, ignore yaw */ + for (unsigned i = 0; i < _rotor_count; i++) { + float out = roll * _rotors[i].roll_scale + + pitch * _rotors[i].pitch_scale + + thrust; - /* keep roll, pitch and yaw control to 0 below min thrust */ - if (thrust <= min_thrust) { - output_factor = 0.0f; - /* linearly increase the output factor from 0 to 1 between min_thrust and startpoint_full_control */ + /* limit yaw if it causes outputs clipping */ + if (out >= 0.0f && out < -yaw * _rotors[i].yaw_scale) { + yaw = -out / _rotors[i].yaw_scale; + } - } else if (thrust < startpoint_full_control && thrust > min_thrust) { - output_factor = (thrust / max_thrust) / (startpoint_full_control - min_thrust); - /* and then stay at full control */ + /* calculate min and max output values */ + if (out < min_out) { + min_out = out; + } + if (out > max_out) { + max_out = out; + } - } else { - output_factor = max_thrust; + outputs[i] = out; } - roll *= output_factor; - pitch *= output_factor; - yaw *= output_factor; - + /* scale down roll/pitch controls if some outputs are negative, don't add yaw, keep total thrust */ + if (min_out < 0.0) { + float scale_in = thrust / (thrust - min_out); - /* perform initial mix pass yielding un-bounded outputs */ - for (unsigned i = 0; i < _rotor_count; i++) { - float tmp = roll * _rotors[i].roll_scale + - pitch * _rotors[i].pitch_scale + - yaw * _rotors[i].yaw_scale + - thrust; - - if (tmp > max) - max = tmp; + /* mix again with adjusted controls */ + for (unsigned i = 0; i < _rotor_count; i++) { + outputs[i] = scale_in * (roll * _rotors[i].roll_scale + pitch * _rotors[i].pitch_scale) + thrust; + } - outputs[i] = tmp; + } else { + /* roll/pitch mixed without limiting, add yaw control */ + for (unsigned i = 0; i < _rotor_count; i++) { + outputs[i] += yaw * _rotors[i].yaw_scale; + } } - /* scale values into the -1.0 - 1.0 range */ - if (max > 1.0f) { - fixup_scale = 2.0f / max; + /* scale down all outputs if some outputs are too large, reduce total thrust */ + float scale_out; + if (max_out > 1.0f) { + scale_out = 1.0f / max_out; } else { - fixup_scale = 2.0f; + scale_out = 1.0f; } - for (unsigned i = 0; i < _rotor_count; i++) - outputs[i] = -1.0f + (outputs[i] * fixup_scale); - - /* ensure outputs are out of the deadband */ - for (unsigned i = 0; i < _rotor_count; i++) - if (outputs[i] < _deadband) - outputs[i] = _deadband; + /* scale outputs to range _idle_speed..1 */ + for (unsigned i = 0; i < _rotor_count; i++) { + outputs[i] = _idle_speed + (outputs[i] * (1.0f - _idle_speed) * scale_out); + } return _rotor_count; } diff --git a/src/modules/systemlib/param/param.c b/src/modules/systemlib/param/param.c index 2d773fd25..7a499ca72 100644 --- a/src/modules/systemlib/param/param.c +++ b/src/modules/systemlib/param/param.c @@ -521,73 +521,15 @@ param_save_default(void) return ERROR; } - if (res == OK) { - res = param_export(fd, false); + res = param_export(fd, false); - if (res != OK) { - warnx("failed to write parameters to file: %s", filename); - } + if (res != OK) { + warnx("failed to write parameters to file: %s", filename); } close(fd); return res; - -#if 0 - const char *filename_tmp = malloc(strlen(filename) + 5); - sprintf(filename_tmp, "%s.tmp", filename); - - /* delete temp file if exist */ - res = unlink(filename_tmp); - - if (res != OK && errno == ENOENT) - res = OK; - - if (res != OK) - warn("failed to delete temp file: %s", filename_tmp); - - if (res == OK) { - /* write parameters to temp file */ - fd = open(filename_tmp, O_WRONLY | O_CREAT | O_EXCL); - - if (fd < 0) { - warn("failed to open temp file: %s", filename_tmp); - res = ERROR; - } - - if (res == OK) { - res = param_export(fd, false); - - if (res != OK) - warnx("failed to write parameters to file: %s", filename_tmp); - } - - close(fd); - } - - if (res == OK) { - /* delete parameters file */ - res = unlink(filename); - - if (res != OK && errno == ENOENT) - res = OK; - - if (res != OK) - warn("failed to delete parameters file: %s", filename); - } - - if (res == OK) { - /* rename temp file to parameters */ - res = rename(filename_tmp, filename); - - if (res != OK) - warn("failed to rename %s to %s", filename_tmp, filename); - } - - free(filename_tmp); - - return res; -#endif } /** diff --git a/src/modules/systemlib/pid/pid.c b/src/modules/systemlib/pid/pid.c index 6a4e9392a..45f218a5b 100644 --- a/src/modules/systemlib/pid/pid.c +++ b/src/modules/systemlib/pid/pid.c @@ -53,7 +53,7 @@ #define SIGMA 0.000001f -__EXPORT void pid_init(PID_t *pid, uint8_t mode, float dt_min) +__EXPORT void pid_init(PID_t *pid, pid_mode_t mode, float dt_min) { pid->mode = mode; pid->dt_min = dt_min; diff --git a/src/modules/systemlib/rc_check.c b/src/modules/systemlib/rc_check.c index 21e15ec56..c0c1a5cb4 100644 --- a/src/modules/systemlib/rc_check.c +++ b/src/modules/systemlib/rc_check.c @@ -140,7 +140,7 @@ int rc_calibration_check(int mavlink_fd) { /* sanity checks pass, enable channel */ if (count) { mavlink_log_critical(mavlink_fd, "ERROR: %d config error(s) for RC channel %d.", count, (i + 1)); - warnx(mavlink_fd, "ERROR: %d config error(s) for RC channel %d.", count, (i + 1)); + warnx("ERROR: %d config error(s) for RC channel %d.", count, (i + 1)); usleep(100000); } diff --git a/src/modules/systemlib/system_params.c b/src/modules/systemlib/system_params.c index ec2bc3a9a..702e435ac 100644 --- a/src/modules/systemlib/system_params.c +++ b/src/modules/systemlib/system_params.c @@ -62,12 +62,23 @@ PARAM_DEFINE_INT32(SYS_AUTOSTART, 0); PARAM_DEFINE_INT32(SYS_AUTOCONFIG, 0); /** - * Set usage of IO board - * - * Can be used to use a standard startup script but with a FMU only set-up. Set to 0 to force the FMU only set-up. - * - * @min 0 - * @max 1 - * @group System - */ +* Set usage of IO board +* +* Can be used to use a standard startup script but with a FMU only set-up. Set to 0 to force the FMU only set-up. +* +* @min 0 +* @max 1 +* @group System +*/ PARAM_DEFINE_INT32(SYS_USE_IO, 1); + +/** +* Set restart type +* +* Set by px4io to indicate type of restart +* +* @min 0 +* @max 2 +* @group System +*/ +PARAM_DEFINE_INT32(SYS_RESTART_TYPE, 2); diff --git a/src/modules/uORB/objects_common.cpp b/src/modules/uORB/objects_common.cpp index fb24de8d1..90675bb2e 100644 --- a/src/modules/uORB/objects_common.cpp +++ b/src/modules/uORB/objects_common.cpp @@ -90,6 +90,9 @@ ORB_DEFINE(battery_status, struct battery_status_s); #include "topics/servorail_status.h" ORB_DEFINE(servorail_status, struct servorail_status_s); +#include "topics/system_power.h" +ORB_DEFINE(system_power, struct system_power_s); + #include "topics/vehicle_global_position.h" ORB_DEFINE(vehicle_global_position, struct vehicle_global_position_s); @@ -124,7 +127,7 @@ ORB_DEFINE(position_setpoint_triplet, struct position_setpoint_triplet_s); ORB_DEFINE(vehicle_global_velocity_setpoint, struct vehicle_global_velocity_setpoint_s); #include "topics/mission.h" -ORB_DEFINE(mission, struct mission_s); +ORB_DEFINE(offboard_mission, struct mission_s); ORB_DEFINE(onboard_mission, struct mission_s); #include "topics/mission_result.h" @@ -193,3 +196,6 @@ ORB_DEFINE(esc_status, struct esc_status_s); #include "topics/encoders.h" ORB_DEFINE(encoders, struct encoders_s); + +#include "topics/estimator_status.h" +ORB_DEFINE(estimator_status, struct estimator_status_report); diff --git a/src/modules/uORB/topics/airspeed.h b/src/modules/uORB/topics/airspeed.h index a3da3758f..d2ee754cd 100644 --- a/src/modules/uORB/topics/airspeed.h +++ b/src/modules/uORB/topics/airspeed.h @@ -52,9 +52,10 @@ * Airspeed */ struct airspeed_s { - uint64_t timestamp; /**< microseconds since system boot, needed to integrate */ + uint64_t timestamp; /**< microseconds since system boot, needed to integrate */ float indicated_airspeed_m_s; /**< indicated airspeed in meters per second, -1 if unknown */ - float true_airspeed_m_s; /**< true airspeed in meters per second, -1 if unknown */ + float true_airspeed_m_s; /**< true airspeed in meters per second, -1 if unknown */ + float air_temperature_celsius; /**< air temperature in degrees celsius, -1000 if unknown */ }; /** diff --git a/src/modules/uORB/topics/differential_pressure.h b/src/modules/uORB/topics/differential_pressure.h index 5d94d4288..01e14cda9 100644 --- a/src/modules/uORB/topics/differential_pressure.h +++ b/src/modules/uORB/topics/differential_pressure.h @@ -52,12 +52,14 @@ * Differential pressure. */ struct differential_pressure_s { - uint64_t timestamp; /**< microseconds since system boot, needed to integrate */ - uint64_t error_count; - float differential_pressure_pa; /**< Differential pressure reading */ - float max_differential_pressure_pa; /**< Maximum differential pressure reading */ - float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */ - float temperature; /**< Temperature provided by sensor */ + uint64_t timestamp; /**< Microseconds since system boot, needed to integrate */ + uint64_t error_count; /**< Number of errors detected by driver */ + float differential_pressure_pa; /**< Differential pressure reading */ + float differential_pressure_raw_pa; /**< Raw differential pressure reading (may be negative) */ + float differential_pressure_filtered_pa; /**< Low pass filtered differential pressure reading */ + float max_differential_pressure_pa; /**< Maximum differential pressure reading */ + float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */ + float temperature; /**< Temperature provided by sensor, -1000.0f if unknown */ }; diff --git a/src/modules/uORB/topics/esc_status.h b/src/modules/uORB/topics/esc_status.h index 11332d7a7..628824efa 100644 --- a/src/modules/uORB/topics/esc_status.h +++ b/src/modules/uORB/topics/esc_status.h @@ -60,7 +60,7 @@ enum ESC_VENDOR { ESC_VENDOR_GENERIC = 0, /**< generic ESC */ ESC_VENDOR_MIKROKOPTER, /**< Mikrokopter */ - ESC_VENDOR_GRAUPNER_HOTT /**< Graupner HoTT ESC */ + ESC_VENDOR_GRAUPNER_HOTT /**< Graupner HoTT ESC */ }; enum ESC_CONNECTION_TYPE { @@ -79,16 +79,15 @@ enum ESC_CONNECTION_TYPE { /** * Electronic speed controller status. */ -struct esc_status_s -{ +struct esc_status_s { /* use of a counter and timestamp recommended (but not necessary) */ uint16_t counter; /**< incremented by the writing thread everytime new data is stored */ uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */ - + uint8_t esc_count; /**< number of connected ESCs */ enum ESC_CONNECTION_TYPE esc_connectiontype; /**< how ESCs connected to the system */ - + struct { uint16_t esc_address; /**< Address of current ESC (in most cases 1-8 / must be set by driver) */ enum ESC_VENDOR esc_vendor; /**< Vendor of current ESC */ diff --git a/src/modules/uORB/topics/estimator_status.h b/src/modules/uORB/topics/estimator_status.h new file mode 100644 index 000000000..5530cdb21 --- /dev/null +++ b/src/modules/uORB/topics/estimator_status.h @@ -0,0 +1,80 @@ +/**************************************************************************** + * + * Copyright (c) 2014 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file estimator_status.h + * Definition of the estimator_status_report uORB topic. + * + * @author Lorenz Meier <lm@inf.ethz.ch> + */ + +#ifndef ESTIMATOR_STATUS_H_ +#define ESTIMATOR_STATUS_H_ + +#include <stdint.h> +#include <stdbool.h> +#include "../uORB.h" + +/** + * @addtogroup topics + * @{ + */ + +/** + * Estimator status report. + * + * This is a generic status report struct which allows any of the onboard estimators + * to write the internal state to the system log. + * + */ +struct estimator_status_report { + + /* NOTE: Ordering of fields optimized to align to 32 bit / 4 bytes - change with consideration only */ + + uint64_t timestamp; /**< Timestamp in microseconds since boot */ + float states[32]; /**< Internal filter states */ + float n_states; /**< Number of states effectively used */ + bool states_nan; /**< If set to true, one of the states is NaN */ + bool covariance_nan; /**< If set to true, the covariance matrix went NaN */ + bool kalman_gain_nan; /**< If set to true, the Kalman gain matrix went NaN */ + +}; + +/** + * @} + */ + +/* register this as object request broker structure */ +ORB_DECLARE(estimator_status); + +#endif diff --git a/src/modules/uORB/topics/filtered_bottom_flow.h b/src/modules/uORB/topics/filtered_bottom_flow.h index ab6de2613..c5d545542 100644 --- a/src/modules/uORB/topics/filtered_bottom_flow.h +++ b/src/modules/uORB/topics/filtered_bottom_flow.h @@ -53,8 +53,7 @@ /** * Filtered bottom flow in bodyframe. */ -struct filtered_bottom_flow_s -{ +struct filtered_bottom_flow_s { uint64_t timestamp; /**< time of this estimate, in microseconds since system start */ float sumx; /**< Integrated bodyframe x flow in meters */ diff --git a/src/modules/uORB/topics/manual_control_setpoint.h b/src/modules/uORB/topics/manual_control_setpoint.h index eac6d6e98..19a29635b 100644 --- a/src/modules/uORB/topics/manual_control_setpoint.h +++ b/src/modules/uORB/topics/manual_control_setpoint.h @@ -44,6 +44,16 @@ #include "../uORB.h" /** + * Switch position + */ +typedef enum { + SWITCH_POS_NONE = 0, /**< switch is not mapped */ + SWITCH_POS_ON, /**< switch activated (value = 1) */ + SWITCH_POS_MIDDLE, /**< middle position (value = 0) */ + SWITCH_POS_OFF /**< switch not activated (value = -1) */ +} switch_pos_t; + +/** * @addtogroup topics * @{ */ @@ -51,32 +61,42 @@ struct manual_control_setpoint_s { uint64_t timestamp; - float roll; /**< ailerons roll / roll rate input */ - float pitch; /**< elevator / pitch / pitch rate */ - float yaw; /**< rudder / yaw rate / yaw */ - float throttle; /**< throttle / collective thrust / altitude */ - - float mode_switch; /**< mode 3 position switch (mandatory): manual, assisted, auto */ - float return_switch; /**< land 2 position switch (mandatory): land, no effect */ - float assisted_switch; /**< assisted 2 position switch (optional): seatbelt, simple */ - float mission_switch; /**< mission 2 position switch (optional): mission, loiter */ - /** - * Any of the channels below may not be available and be set to NaN + * Any of the channels may not be available and be set to NaN * to indicate that it does not contain valid data. + * The variable names follow the definition of the + * MANUAL_CONTROL mavlink message. + * The default range is from -1 to 1 (mavlink message -1000 to 1000) + * The range for the z variable is defined from 0 to 1. (The z field of + * the MANUAL_CONTROL mavlink message is defined from -1000 to 1000) */ + float x; /**< stick position in x direction -1..1 + in general corresponds to forward/back motion or pitch of vehicle, + in general a positive value means forward or negative pitch and + a negative value means backward or positive pitch */ + float y; /**< stick position in y direction -1..1 + in general corresponds to right/left motion or roll of vehicle, + in general a positive value means right or positive roll and + a negative value means left or negative roll */ + float z; /**< throttle stick position 0..1 + in general corresponds to up/down motion or thrust of vehicle, + in general the value corresponds to the demanded throttle by the user, + if the input is used for setting the setpoint of a vertical position + controller any value > 0.5 means up and any value < 0.5 means down */ + float r; /**< yaw stick/twist positon, -1..1 + in general corresponds to the righthand rotation around the vertical + (downwards) axis of the vehicle */ + float flaps; /**< flap position */ + float aux1; /**< default function: camera yaw / azimuth */ + float aux2; /**< default function: camera pitch / tilt */ + float aux3; /**< default function: camera trigger */ + float aux4; /**< default function: camera roll */ + float aux5; /**< default function: payload drop */ - // XXX needed or parameter? - //float auto_offboard_input_switch; /**< controller setpoint source (0 = onboard, 1 = offboard) */ - - float flaps; /**< flap position */ - - float aux1; /**< default function: camera yaw / azimuth */ - float aux2; /**< default function: camera pitch / tilt */ - float aux3; /**< default function: camera trigger */ - float aux4; /**< default function: camera roll */ - float aux5; /**< default function: payload drop */ - + switch_pos_t mode_switch; /**< main mode 3 position switch (mandatory): _MANUAL_, ASSIST, AUTO */ + switch_pos_t return_switch; /**< return to launch 2 position switch (mandatory): _NORMAL_, RTL */ + switch_pos_t posctl_switch; /**< position control 2 position switch (optional): _ALTCTL_, POSCTL */ + switch_pos_t loiter_switch; /**< loiter 2 position switch (optional): _MISSION_, LOITER */ }; /**< manual control inputs */ /** diff --git a/src/modules/uORB/topics/mission.h b/src/modules/uORB/topics/mission.h index 194e2ed0c..ef4bc1def 100644 --- a/src/modules/uORB/topics/mission.h +++ b/src/modules/uORB/topics/mission.h @@ -77,8 +77,7 @@ enum ORIGIN { * This is the position the MAV is heading towards. If it of type loiter, * the MAV is circling around it with the given loiter radius in meters. */ -struct mission_item_s -{ +struct mission_item_s { bool altitude_is_relative; /**< true if altitude is relative from start point */ double lat; /**< latitude in degrees */ double lon; /**< longitude in degrees */ @@ -106,7 +105,7 @@ struct mission_s */ /* register this as object request broker structure */ -ORB_DECLARE(mission); +ORB_DECLARE(offboard_mission); ORB_DECLARE(onboard_mission); #endif diff --git a/src/modules/uORB/topics/navigation_capabilities.h b/src/modules/uORB/topics/navigation_capabilities.h index 391756f99..7a5ae9891 100644 --- a/src/modules/uORB/topics/navigation_capabilities.h +++ b/src/modules/uORB/topics/navigation_capabilities.h @@ -52,12 +52,12 @@ * Airspeed */ struct navigation_capabilities_s { - float turn_distance; /**< the optimal distance to a waypoint to switch to the next */ + float turn_distance; /**< the optimal distance to a waypoint to switch to the next */ - /* Landing parameters: see fw_pos_control_l1/landingslope.h */ - float landing_horizontal_slope_displacement; - float landing_slope_angle_rad; - float landing_flare_length; + /* Landing parameters: see fw_pos_control_l1/landingslope.h */ + float landing_horizontal_slope_displacement; + float landing_slope_angle_rad; + float landing_flare_length; }; /** diff --git a/src/modules/uORB/topics/offboard_control_setpoint.h b/src/modules/uORB/topics/offboard_control_setpoint.h index 7901b930a..68d3e494b 100644 --- a/src/modules/uORB/topics/offboard_control_setpoint.h +++ b/src/modules/uORB/topics/offboard_control_setpoint.h @@ -45,12 +45,11 @@ /** * Off-board control inputs. - * + * * Typically sent by a ground control station / joystick or by * some off-board controller via C or SIMULINK. */ -enum OFFBOARD_CONTROL_MODE -{ +enum OFFBOARD_CONTROL_MODE { OFFBOARD_CONTROL_MODE_DIRECT = 0, OFFBOARD_CONTROL_MODE_DIRECT_RATES = 1, OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE = 2, diff --git a/src/modules/uORB/topics/optical_flow.h b/src/modules/uORB/topics/optical_flow.h index 98f0e3fa2..0196ae86b 100644 --- a/src/modules/uORB/topics/optical_flow.h +++ b/src/modules/uORB/topics/optical_flow.h @@ -57,6 +57,7 @@ struct optical_flow_s { uint64_t timestamp; /**< in microseconds since system start */ + uint64_t flow_timestamp; /**< timestamp from flow sensor */ int16_t flow_raw_x; /**< flow in pixels in X direction, not rotation-compensated */ int16_t flow_raw_y; /**< flow in pixels in Y direction, not rotation-compensated */ float flow_comp_x_m; /**< speed over ground in meters, rotation-compensated */ diff --git a/src/modules/uORB/topics/position_setpoint_triplet.h b/src/modules/uORB/topics/position_setpoint_triplet.h index cf1ddfc38..34aaa30dd 100644 --- a/src/modules/uORB/topics/position_setpoint_triplet.h +++ b/src/modules/uORB/topics/position_setpoint_triplet.h @@ -54,24 +54,24 @@ enum SETPOINT_TYPE { - SETPOINT_TYPE_NORMAL = 0, /**< normal setpoint */ - SETPOINT_TYPE_LOITER, /**< loiter setpoint */ - SETPOINT_TYPE_TAKEOFF, /**< takeoff setpoint */ + SETPOINT_TYPE_NORMAL = 0, /**< normal setpoint */ + SETPOINT_TYPE_LOITER, /**< loiter setpoint */ + SETPOINT_TYPE_TAKEOFF, /**< takeoff setpoint */ SETPOINT_TYPE_LAND, /**< land setpoint, altitude must be ignored, vehicle must descend until landing */ SETPOINT_TYPE_IDLE, /**< do nothing, switch off motors or keep at idle speed (MC) */ }; struct position_setpoint_s { - bool valid; /**< true if setpoint is valid */ + bool valid; /**< true if setpoint is valid */ enum SETPOINT_TYPE type; /**< setpoint type to adjust behavior of position controller */ - double lat; /**< latitude, in deg */ - double lon; /**< longitude, in deg */ - float alt; /**< altitude AMSL, in m */ - float yaw; /**< yaw (only for multirotors), in rad [-PI..PI), NaN = hold current yaw */ + double lat; /**< latitude, in deg */ + double lon; /**< longitude, in deg */ + float alt; /**< altitude AMSL, in m */ + float yaw; /**< yaw (only for multirotors), in rad [-PI..PI), NaN = hold current yaw */ float loiter_radius; /**< loiter radius (only for fixed wing), in m */ int8_t loiter_direction; /**< loiter direction: 1 = CW, -1 = CCW */ - float pitch_min; /**< minimal pitch angle for fixed wing takeoff waypoints */ + float pitch_min; /**< minimal pitch angle for fixed wing takeoff waypoints */ }; /** @@ -85,7 +85,7 @@ struct position_setpoint_triplet_s struct position_setpoint_s current; struct position_setpoint_s next; - nav_state_t nav_state; /**< navigation state */ + nav_state_t nav_state; /**< navigation state */ }; /** diff --git a/src/modules/uORB/topics/rc_channels.h b/src/modules/uORB/topics/rc_channels.h index 086b2ef15..b60402452 100644 --- a/src/modules/uORB/topics/rc_channels.h +++ b/src/modules/uORB/topics/rc_channels.h @@ -52,29 +52,28 @@ */ #define RC_CHANNELS_MAPPED_MAX 15 -/** +/** * This defines the mapping of the RC functions. * The value assigned to the specific function corresponds to the entry of * the channel array chan[]. */ -enum RC_CHANNELS_FUNCTION -{ - THROTTLE = 0, - ROLL = 1, - PITCH = 2, - YAW = 3, - MODE = 4, - RETURN = 5, - ASSISTED = 6, - MISSION = 7, - OFFBOARD_MODE = 8, - FLAPS = 9, - AUX_1 = 10, - AUX_2 = 11, - AUX_3 = 12, - AUX_4 = 13, - AUX_5 = 14, - RC_CHANNELS_FUNCTION_MAX /**< indicates the number of functions. There can be more functions than RC channels. */ +enum RC_CHANNELS_FUNCTION { + THROTTLE = 0, + ROLL = 1, + PITCH = 2, + YAW = 3, + MODE = 4, + RETURN = 5, + POSCTL = 6, + LOITER = 7, + OFFBOARD_MODE = 8, + FLAPS = 9, + AUX_1 = 10, + AUX_2 = 11, + AUX_3 = 12, + AUX_4 = 13, + AUX_5 = 14, + RC_CHANNELS_FUNCTION_MAX /**< indicates the number of functions. There can be more functions than RC channels. */ }; /** @@ -85,16 +84,17 @@ enum RC_CHANNELS_FUNCTION struct rc_channels_s { uint64_t timestamp; /**< In microseconds since boot time. */ - uint64_t timestamp_last_valid; /**< timestamp of last valid RC signal. */ - struct { - float scaled; /**< Scaled to -1..1 (throttle: 0..1) */ - } chan[RC_CHANNELS_MAPPED_MAX]; - uint8_t chan_count; /**< number of valid channels */ + uint64_t timestamp_last_valid; /**< timestamp of last valid RC signal. */ + struct { + float scaled; /**< Scaled to -1..1 (throttle: 0..1) */ + } chan[RC_CHANNELS_MAPPED_MAX]; + uint8_t chan_count; /**< number of valid channels */ - /*String array to store the names of the functions*/ - char function_name[RC_CHANNELS_FUNCTION_MAX][20]; - int8_t function[RC_CHANNELS_FUNCTION_MAX]; - uint8_t rssi; /**< Overall receive signal strength */ + /*String array to store the names of the functions*/ + char function_name[RC_CHANNELS_FUNCTION_MAX][20]; + int8_t function[RC_CHANNELS_FUNCTION_MAX]; + uint8_t rssi; /**< Overall receive signal strength */ + bool signal_lost; /**< control signal lost, should be checked together with topic timeout */ }; /**< radio control channels. */ /** diff --git a/src/modules/uORB/topics/sensor_combined.h b/src/modules/uORB/topics/sensor_combined.h index 92812efd4..fa3367de9 100644 --- a/src/modules/uORB/topics/sensor_combined.h +++ b/src/modules/uORB/topics/sensor_combined.h @@ -98,12 +98,15 @@ struct sensor_combined_s { float baro_pres_mbar; /**< Barometric pressure, already temp. comp. */ float baro_alt_meter; /**< Altitude, already temp. comp. */ float baro_temp_celcius; /**< Temperature in degrees celsius */ - float adc_voltage_v[4]; /**< ADC voltages of ADC Chan 10/11/12/13 or -1 */ + float adc_voltage_v[10]; /**< ADC voltages of ADC Chan 10/11/12/13 or -1 */ + unsigned adc_mapping[10]; /**< Channel indices of each of these values */ float mcu_temp_celcius; /**< Internal temperature measurement of MCU */ uint64_t baro_timestamp; /**< Barometer timestamp */ float differential_pressure_pa; /**< Airspeed sensor differential pressure */ uint64_t differential_pressure_timestamp; /**< Last measurement timestamp */ + float differential_pressure_filtered_pa; /**< Low pass filtered airspeed sensor differential pressure reading */ + }; /** diff --git a/src/modules/uORB/topics/subsystem_info.h b/src/modules/uORB/topics/subsystem_info.h index cfe0bf69e..d3a7ce10d 100644 --- a/src/modules/uORB/topics/subsystem_info.h +++ b/src/modules/uORB/topics/subsystem_info.h @@ -50,8 +50,7 @@ #include <stdbool.h> #include "../uORB.h" -enum SUBSYSTEM_TYPE -{ +enum SUBSYSTEM_TYPE { SUBSYSTEM_TYPE_GYRO = 1, SUBSYSTEM_TYPE_ACC = 2, SUBSYSTEM_TYPE_MAG = 4, diff --git a/src/modules/position_estimator_mc/position_estimator_mc_params.h b/src/modules/uORB/topics/system_power.h index c4c95f7b4..7763b6004 100755..100644 --- a/src/modules/position_estimator_mc/position_estimator_mc_params.h +++ b/src/modules/uORB/topics/system_power.h @@ -1,9 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: Damian Aregger <daregger@student.ethz.ch> - * Tobias Naegeli <naegelit@student.ethz.ch> - * Lorenz Meier <lm@inf.ethz.ch> + * Copyright (C) 2012-2013 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -34,36 +31,41 @@ * ****************************************************************************/ -/* - * @file position_estimator_mc_params.h - * - * Parameters for Position Estimator +/** + * @file system_power.h + * + * Definition of the system_power voltage and power status uORB topic. */ -#include <systemlib/param/param.h> +#ifndef SYSTEM_POWER_H_ +#define SYSTEM_POWER_H_ -struct position_estimator_mc_params { - float addNoise; - float sigma; - float R; - int baro; /* consider barometer */ -}; +#include "../uORB.h" +#include <stdint.h> -struct position_estimator_mc_param_handles { - param_t addNoise; - param_t sigma; - param_t r; - param_t baro_param_handle; -}; +/** + * @addtogroup topics + * @{ + */ /** - * Initialize all parameter handles and values - * + * voltage and power supply status */ -int parameters_init(struct position_estimator_mc_param_handles *h); +struct system_power_s { + uint64_t timestamp; /**< microseconds since system boot */ + float voltage5V_v; /**< peripheral 5V rail voltage */ + uint8_t usb_connected:1; /**< USB is connected when 1 */ + uint8_t brick_valid:1; /**< brick power is good when 1 */ + uint8_t servo_valid:1; /**< servo power is good when 1 */ + uint8_t periph_5V_OC:1; /**< peripheral overcurrent when 1 */ + uint8_t hipower_5V_OC:1; /**< hi power peripheral overcurrent when 1 */ +}; /** - * Update all parameters - * + * @} */ -int parameters_update(const struct position_estimator_mc_param_handles *h, struct position_estimator_mc_params *p); + +/* register this as object request broker structure */ +ORB_DECLARE(system_power); + +#endif diff --git a/src/modules/uORB/topics/telemetry_status.h b/src/modules/uORB/topics/telemetry_status.h index 5192d4d58..76693c46e 100644 --- a/src/modules/uORB/topics/telemetry_status.h +++ b/src/modules/uORB/topics/telemetry_status.h @@ -44,10 +44,10 @@ #include "../uORB.h" enum TELEMETRY_STATUS_RADIO_TYPE { - TELEMETRY_STATUS_RADIO_TYPE_GENERIC = 0, - TELEMETRY_STATUS_RADIO_TYPE_3DR_RADIO, - TELEMETRY_STATUS_RADIO_TYPE_UBIQUITY_BULLET, - TELEMETRY_STATUS_RADIO_TYPE_WIRE + TELEMETRY_STATUS_RADIO_TYPE_GENERIC = 0, + TELEMETRY_STATUS_RADIO_TYPE_3DR_RADIO, + TELEMETRY_STATUS_RADIO_TYPE_UBIQUITY_BULLET, + TELEMETRY_STATUS_RADIO_TYPE_WIRE }; /** @@ -57,14 +57,14 @@ enum TELEMETRY_STATUS_RADIO_TYPE { struct telemetry_status_s { uint64_t timestamp; - enum TELEMETRY_STATUS_RADIO_TYPE type; /**< type of the radio hardware */ - uint8_t rssi; /**< local signal strength */ - uint8_t remote_rssi; /**< remote signal strength */ - uint16_t rxerrors; /**< receive errors */ - uint16_t fixed; /**< count of error corrected packets */ - uint8_t noise; /**< background noise level */ - uint8_t remote_noise; /**< remote background noise level */ - uint8_t txbuf; /**< how full the tx buffer is as a percentage */ + enum TELEMETRY_STATUS_RADIO_TYPE type; /**< type of the radio hardware */ + uint8_t rssi; /**< local signal strength */ + uint8_t remote_rssi; /**< remote signal strength */ + uint16_t rxerrors; /**< receive errors */ + uint16_t fixed; /**< count of error corrected packets */ + uint8_t noise; /**< background noise level */ + uint8_t remote_noise; /**< remote background noise level */ + uint8_t txbuf; /**< how full the tx buffer is as a percentage */ }; /** diff --git a/src/modules/uORB/topics/vehicle_attitude_setpoint.h b/src/modules/uORB/topics/vehicle_attitude_setpoint.h index 7596f944f..d526a8ff2 100644 --- a/src/modules/uORB/topics/vehicle_attitude_setpoint.h +++ b/src/modules/uORB/topics/vehicle_attitude_setpoint.h @@ -52,8 +52,7 @@ /** * vehicle attitude setpoint. */ -struct vehicle_attitude_setpoint_s -{ +struct vehicle_attitude_setpoint_s { uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */ float roll_body; /**< body angle in NED frame */ diff --git a/src/modules/uORB/topics/vehicle_bodyframe_speed_setpoint.h b/src/modules/uORB/topics/vehicle_bodyframe_speed_setpoint.h index fbfab09f3..fd1ade671 100644 --- a/src/modules/uORB/topics/vehicle_bodyframe_speed_setpoint.h +++ b/src/modules/uORB/topics/vehicle_bodyframe_speed_setpoint.h @@ -48,8 +48,7 @@ * @{ */ -struct vehicle_bodyframe_speed_setpoint_s -{ +struct vehicle_bodyframe_speed_setpoint_s { uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */ float vx; /**< in m/s */ diff --git a/src/modules/uORB/topics/vehicle_command.h b/src/modules/uORB/topics/vehicle_command.h index e6e4743c6..c21a29b13 100644 --- a/src/modules/uORB/topics/vehicle_command.h +++ b/src/modules/uORB/topics/vehicle_command.h @@ -51,43 +51,42 @@ * Should contain all commands from MAVLink's VEHICLE_CMD ENUM, * but can contain additional ones. */ -enum VEHICLE_CMD -{ - VEHICLE_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing)| Latitude| Longitude| Altitude| */ - VEHICLE_CMD_NAV_LOITER_UNLIM=17, /* Loiter around this MISSION an unlimited amount of time |Empty| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */ - VEHICLE_CMD_NAV_LOITER_TURNS=18, /* Loiter around this MISSION for X turns |Turns| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */ - VEHICLE_CMD_NAV_LOITER_TIME=19, /* Loiter around this MISSION for X seconds |Seconds (decimal)| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */ - VEHICLE_CMD_NAV_RETURN_TO_LAUNCH=20, /* Return to launch location |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_NAV_LAND=21, /* Land at location |Empty| Empty| Empty| Desired yaw angle.| Latitude| Longitude| Altitude| */ - VEHICLE_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer| Latitude| Longitude| Altitude| */ - VEHICLE_CMD_NAV_ROI=80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */ - VEHICLE_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */ - VEHICLE_CMD_NAV_LAST=95, /* NOP - This command is only used to mark the upper limit of the NAV/ACTION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_CONDITION_DELAY=112, /* Delay mission state machine. |Delay in seconds (decimal)| Empty| Empty| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_CONDITION_CHANGE_ALT=113, /* Ascend/descend at rate. Delay mission state machine until desired altitude reached. |Descent / Ascend rate (m/s)| Empty| Empty| Empty| Empty| Empty| Finish Altitude| */ - VEHICLE_CMD_CONDITION_DISTANCE=114, /* Delay mission state machine until within desired distance of next NAV point. |Distance (meters)| Empty| Empty| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_CONDITION_YAW=115, /* Reach a certain target angle. |target angle: [0-360], 0 is north| speed during yaw change:[deg per second]| direction: negative: counter clockwise, positive: clockwise [-1,1]| relative offset or absolute angle: [ 1,0]| Empty| Empty| Empty| */ - VEHICLE_CMD_CONDITION_LAST=159, /* NOP - This command is only used to mark the upper limit of the CONDITION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_DO_SET_MODE=176, /* Set system mode. |Mode, as defined by ENUM MAV_MODE| Empty| Empty| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_DO_JUMP=177, /* Jump to the desired command in the mission list. Repeat this action only the specified number of times |Sequence number| Repeat count| Empty| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_DO_CHANGE_SPEED=178, /* Change speed and/or throttle set points. |Speed type (0=Airspeed, 1=Ground Speed)| Speed (m/s, -1 indicates no change)| Throttle ( Percent, -1 indicates no change)| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_DO_SET_HOME=179, /* Changes the home location either to the current location or a specified location. |Use current (1=use current location, 0=use specified location)| Empty| Empty| Empty| Latitude| Longitude| Altitude| */ - VEHICLE_CMD_DO_SET_PARAMETER=180, /* Set a system parameter. Caution! Use of this command requires knowledge of the numeric enumeration value of the parameter. |Parameter number| Parameter value| Empty| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_DO_SET_RELAY=181, /* Set a relay to a condition. |Relay number| Setting (1=on, 0=off, others possible depending on system hardware)| Empty| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_DO_REPEAT_RELAY=182, /* Cycle a relay on and off for a desired number of cyles with a desired period. |Relay number| Cycle count| Cycle time (seconds, decimal)| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_DO_SET_SERVO=183, /* Set a servo to a desired PWM value. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Empty| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_DO_REPEAT_SERVO=184, /* Cycle a between its nominal setting and a desired PWM for a desired number of cycles with a desired period. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Cycle count| Cycle time (seconds)| Empty| Empty| Empty| */ - VEHICLE_CMD_DO_CONTROL_VIDEO=200, /* Control onboard camera system. |Camera ID (-1 for all)| Transmission: 0: disabled, 1: enabled compressed, 2: enabled raw| Transmission mode: 0: video stream, >0: single images every n seconds (decimal)| Recording: 0: disabled, 1: enabled compressed, 2: enabled raw| Empty| Empty| Empty| */ - VEHICLE_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ - VEHICLE_CMD_PREFLIGHT_CALIBRATION=241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Empty| Empty| */ - VEHICLE_CMD_PREFLIGHT_SET_SENSOR_OFFSETS=242, /* Set sensor offsets. This command will be only accepted if in pre-flight mode. |Sensor to adjust the offsets for: 0: gyros, 1: accelerometer, 2: magnetometer, 3: barometer, 4: optical flow| X axis offset (or generic dimension 1), in the sensor's raw units| Y axis offset (or generic dimension 2), in the sensor's raw units| Z axis offset (or generic dimension 3), in the sensor's raw units| Generic dimension 4, in the sensor's raw units| Generic dimension 5, in the sensor's raw units| Generic dimension 6, in the sensor's raw units| */ - VEHICLE_CMD_PREFLIGHT_STORAGE=245, /* Request storage of different parameter values and logs. This command will be only accepted if in pre-flight mode. |Parameter storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Mission storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Reserved| Reserved| Empty| Empty| Empty| */ - VEHICLE_CMD_PREFLIGHT_REBOOT_SHUTDOWN=246, /* Request the reboot or shutdown of system components. |0: Do nothing for autopilot, 1: Reboot autopilot, 2: Shutdown autopilot.| 0: Do nothing for onboard computer, 1: Reboot onboard computer, 2: Shutdown onboard computer.| Reserved| Reserved| Empty| Empty| Empty| */ - VEHICLE_CMD_OVERRIDE_GOTO=252, /* Hold / continue the current action |MAV_GOTO_DO_HOLD: hold MAV_GOTO_DO_CONTINUE: continue with next item in mission plan| MAV_GOTO_HOLD_AT_CURRENT_POSITION: Hold at current position MAV_GOTO_HOLD_AT_SPECIFIED_POSITION: hold at specified position| MAV_FRAME coordinate frame of hold point| Desired yaw angle in degrees| Latitude / X position| Longitude / Y position| Altitude / Z position| */ - VEHICLE_CMD_MISSION_START=300, /* start running a mission |first_item: the first mission item to run| last_item: the last mission item to run (after this item is run, the mission ends)| */ - VEHICLE_CMD_COMPONENT_ARM_DISARM=400, /* Arms / Disarms a component |1 to arm, 0 to disarm| */ - VEHICLE_CMD_START_RX_PAIR=500, /* Starts receiver pairing |0:Spektrum| 0:Spektrum DSM2, 1:Spektrum DSMX| */ - VEHICLE_CMD_ENUM_END=501, /* | */ +enum VEHICLE_CMD { + VEHICLE_CMD_NAV_WAYPOINT = 16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing)| Latitude| Longitude| Altitude| */ + VEHICLE_CMD_NAV_LOITER_UNLIM = 17, /* Loiter around this MISSION an unlimited amount of time |Empty| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */ + VEHICLE_CMD_NAV_LOITER_TURNS = 18, /* Loiter around this MISSION for X turns |Turns| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */ + VEHICLE_CMD_NAV_LOITER_TIME = 19, /* Loiter around this MISSION for X seconds |Seconds (decimal)| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */ + VEHICLE_CMD_NAV_RETURN_TO_LAUNCH = 20, /* Return to launch location |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_NAV_LAND = 21, /* Land at location |Empty| Empty| Empty| Desired yaw angle.| Latitude| Longitude| Altitude| */ + VEHICLE_CMD_NAV_TAKEOFF = 22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer| Latitude| Longitude| Altitude| */ + VEHICLE_CMD_NAV_ROI = 80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */ + VEHICLE_CMD_NAV_PATHPLANNING = 81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */ + VEHICLE_CMD_NAV_LAST = 95, /* NOP - This command is only used to mark the upper limit of the NAV/ACTION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_CONDITION_DELAY = 112, /* Delay mission state machine. |Delay in seconds (decimal)| Empty| Empty| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_CONDITION_CHANGE_ALT = 113, /* Ascend/descend at rate. Delay mission state machine until desired altitude reached. |Descent / Ascend rate (m/s)| Empty| Empty| Empty| Empty| Empty| Finish Altitude| */ + VEHICLE_CMD_CONDITION_DISTANCE = 114, /* Delay mission state machine until within desired distance of next NAV point. |Distance (meters)| Empty| Empty| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_CONDITION_YAW = 115, /* Reach a certain target angle. |target angle: [0-360], 0 is north| speed during yaw change:[deg per second]| direction: negative: counter clockwise, positive: clockwise [-1,1]| relative offset or absolute angle: [ 1,0]| Empty| Empty| Empty| */ + VEHICLE_CMD_CONDITION_LAST = 159, /* NOP - This command is only used to mark the upper limit of the CONDITION commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_DO_SET_MODE = 176, /* Set system mode. |Mode, as defined by ENUM MAV_MODE| Empty| Empty| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_DO_JUMP = 177, /* Jump to the desired command in the mission list. Repeat this action only the specified number of times |Sequence number| Repeat count| Empty| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_DO_CHANGE_SPEED = 178, /* Change speed and/or throttle set points. |Speed type (0=Airspeed, 1=Ground Speed)| Speed (m/s, -1 indicates no change)| Throttle ( Percent, -1 indicates no change)| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_DO_SET_HOME = 179, /* Changes the home location either to the current location or a specified location. |Use current (1=use current location, 0=use specified location)| Empty| Empty| Empty| Latitude| Longitude| Altitude| */ + VEHICLE_CMD_DO_SET_PARAMETER = 180, /* Set a system parameter. Caution! Use of this command requires knowledge of the numeric enumeration value of the parameter. |Parameter number| Parameter value| Empty| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_DO_SET_RELAY = 181, /* Set a relay to a condition. |Relay number| Setting (1=on, 0=off, others possible depending on system hardware)| Empty| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_DO_REPEAT_RELAY = 182, /* Cycle a relay on and off for a desired number of cyles with a desired period. |Relay number| Cycle count| Cycle time (seconds, decimal)| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_DO_SET_SERVO = 183, /* Set a servo to a desired PWM value. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Empty| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_DO_REPEAT_SERVO = 184, /* Cycle a between its nominal setting and a desired PWM for a desired number of cycles with a desired period. |Servo number| PWM (microseconds, 1000 to 2000 typical)| Cycle count| Cycle time (seconds)| Empty| Empty| Empty| */ + VEHICLE_CMD_DO_CONTROL_VIDEO = 200, /* Control onboard camera system. |Camera ID (-1 for all)| Transmission: 0: disabled, 1: enabled compressed, 2: enabled raw| Transmission mode: 0: video stream, >0: single images every n seconds (decimal)| Recording: 0: disabled, 1: enabled compressed, 2: enabled raw| Empty| Empty| Empty| */ + VEHICLE_CMD_DO_LAST = 240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ + VEHICLE_CMD_PREFLIGHT_CALIBRATION = 241, /* Trigger calibration. This command will be only accepted if in pre-flight mode. |Gyro calibration: 0: no, 1: yes| Magnetometer calibration: 0: no, 1: yes| Ground pressure: 0: no, 1: yes| Radio calibration: 0: no, 1: yes| Accelerometer calibration: 0: no, 1: yes| Empty| Empty| */ + VEHICLE_CMD_PREFLIGHT_SET_SENSOR_OFFSETS = 242, /* Set sensor offsets. This command will be only accepted if in pre-flight mode. |Sensor to adjust the offsets for: 0: gyros, 1: accelerometer, 2: magnetometer, 3: barometer, 4: optical flow| X axis offset (or generic dimension 1), in the sensor's raw units| Y axis offset (or generic dimension 2), in the sensor's raw units| Z axis offset (or generic dimension 3), in the sensor's raw units| Generic dimension 4, in the sensor's raw units| Generic dimension 5, in the sensor's raw units| Generic dimension 6, in the sensor's raw units| */ + VEHICLE_CMD_PREFLIGHT_STORAGE = 245, /* Request storage of different parameter values and logs. This command will be only accepted if in pre-flight mode. |Parameter storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Mission storage: 0: READ FROM FLASH/EEPROM, 1: WRITE CURRENT TO FLASH/EEPROM| Reserved| Reserved| Empty| Empty| Empty| */ + VEHICLE_CMD_PREFLIGHT_REBOOT_SHUTDOWN = 246, /* Request the reboot or shutdown of system components. |0: Do nothing for autopilot, 1: Reboot autopilot, 2: Shutdown autopilot.| 0: Do nothing for onboard computer, 1: Reboot onboard computer, 2: Shutdown onboard computer.| Reserved| Reserved| Empty| Empty| Empty| */ + VEHICLE_CMD_OVERRIDE_GOTO = 252, /* Hold / continue the current action |MAV_GOTO_DO_HOLD: hold MAV_GOTO_DO_CONTINUE: continue with next item in mission plan| MAV_GOTO_HOLD_AT_CURRENT_POSITION: Hold at current position MAV_GOTO_HOLD_AT_SPECIFIED_POSITION: hold at specified position| MAV_FRAME coordinate frame of hold point| Desired yaw angle in degrees| Latitude / X position| Longitude / Y position| Altitude / Z position| */ + VEHICLE_CMD_MISSION_START = 300, /* start running a mission |first_item: the first mission item to run| last_item: the last mission item to run (after this item is run, the mission ends)| */ + VEHICLE_CMD_COMPONENT_ARM_DISARM = 400, /* Arms / Disarms a component |1 to arm, 0 to disarm| */ + VEHICLE_CMD_START_RX_PAIR = 500, /* Starts receiver pairing |0:Spektrum| 0:Spektrum DSM2, 1:Spektrum DSMX| */ + VEHICLE_CMD_ENUM_END = 501, /* | */ }; /** @@ -96,14 +95,13 @@ enum VEHICLE_CMD * Should contain all of MAVLink's VEHICLE_CMD_RESULT values * but can contain additional ones. */ -enum VEHICLE_CMD_RESULT -{ - VEHICLE_CMD_RESULT_ACCEPTED=0, /* Command ACCEPTED and EXECUTED | */ - VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED=1, /* Command TEMPORARY REJECTED/DENIED | */ - VEHICLE_CMD_RESULT_DENIED=2, /* Command PERMANENTLY DENIED | */ - VEHICLE_CMD_RESULT_UNSUPPORTED=3, /* Command UNKNOWN/UNSUPPORTED | */ - VEHICLE_CMD_RESULT_FAILED=4, /* Command executed, but failed | */ - VEHICLE_CMD_RESULT_ENUM_END=5, /* | */ +enum VEHICLE_CMD_RESULT { + VEHICLE_CMD_RESULT_ACCEPTED = 0, /* Command ACCEPTED and EXECUTED | */ + VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED = 1, /* Command TEMPORARY REJECTED/DENIED | */ + VEHICLE_CMD_RESULT_DENIED = 2, /* Command PERMANENTLY DENIED | */ + VEHICLE_CMD_RESULT_UNSUPPORTED = 3, /* Command UNKNOWN/UNSUPPORTED | */ + VEHICLE_CMD_RESULT_FAILED = 4, /* Command executed, but failed | */ + VEHICLE_CMD_RESULT_ENUM_END = 5, /* | */ }; /** @@ -111,8 +109,7 @@ enum VEHICLE_CMD_RESULT * @{ */ -struct vehicle_command_s -{ +struct vehicle_command_s { float param1; /**< Parameter 1, as defined by MAVLink VEHICLE_CMD enum. */ float param2; /**< Parameter 2, as defined by MAVLink VEHICLE_CMD enum. */ float param3; /**< Parameter 3, as defined by MAVLink VEHICLE_CMD enum. */ diff --git a/src/modules/uORB/topics/vehicle_control_debug.h b/src/modules/uORB/topics/vehicle_control_debug.h index 6184284a4..2a45eaccc 100644 --- a/src/modules/uORB/topics/vehicle_control_debug.h +++ b/src/modules/uORB/topics/vehicle_control_debug.h @@ -47,8 +47,7 @@ * @addtogroup topics * @{ */ -struct vehicle_control_debug_s -{ +struct vehicle_control_debug_s { uint64_t timestamp; /**< in microseconds since system start */ float roll_p; /**< roll P control part */ @@ -77,9 +76,9 @@ struct vehicle_control_debug_s }; /**< vehicle_control_debug */ - /** - * @} - */ +/** +* @} +*/ /* register this as object request broker structure */ ORB_DECLARE(vehicle_control_debug); diff --git a/src/modules/uORB/topics/vehicle_control_mode.h b/src/modules/uORB/topics/vehicle_control_mode.h index 7cbb37cd8..ea554006f 100644 --- a/src/modules/uORB/topics/vehicle_control_mode.h +++ b/src/modules/uORB/topics/vehicle_control_mode.h @@ -1,10 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: @author Lorenz Meier <lm@inf.ethz.ch> - * @author Petri Tanskanen <petri.tanskanen@inf.ethz.ch> - * @author Thomas Gubler <thomasgubler@student.ethz.ch> - * @author Julian Oes <joes@student.ethz.ch> + * Copyright (c) 2012-2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -38,8 +34,13 @@ /** * @file vehicle_control_mode.h * Definition of the vehicle_control_mode uORB topic. - * + * * All control apps should depend their actions based on the flags set here. + * + * @author Lorenz Meier <lm@inf.ethz.ch> + * @author Petri Tanskanen <petri.tanskanen@inf.ethz.ch> + * @author Thomas Gubler <thomasgubler@student.ethz.ch> + * @author Julian Oes <joes@student.ethz.ch> */ #ifndef VEHICLE_CONTROL_MODE @@ -61,8 +62,7 @@ * Encodes the complete system state and is set by the commander app. */ -struct vehicle_control_mode_s -{ +struct vehicle_control_mode_s { uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */ bool flag_armed; diff --git a/src/modules/uORB/topics/vehicle_global_position.h b/src/modules/uORB/topics/vehicle_global_position.h index ff9e98e1c..4897ca737 100644 --- a/src/modules/uORB/topics/vehicle_global_position.h +++ b/src/modules/uORB/topics/vehicle_global_position.h @@ -1,9 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: @author Thomas Gubler <thomasgubler@student.ethz.ch> - * @author Julian Oes <joes@student.ethz.ch> - * @author Lorenz Meier <lm@inf.ethz.ch> + * Copyright (c) 2012-2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -37,6 +34,10 @@ /** * @file vehicle_global_position.h * Definition of the global fused WGS84 position uORB topic. + * + * @author Thomas Gubler <thomasgubler@student.ethz.ch> + * @author Julian Oes <joes@student.ethz.ch> + * @author Lorenz Meier <lm@inf.ethz.ch> */ #ifndef VEHICLE_GLOBAL_POSITION_T_H_ @@ -59,13 +60,9 @@ * estimator, which will take more sources of information into account than just GPS, * e.g. control inputs of the vehicle in a Kalman-filter implementation. */ -struct vehicle_global_position_s -{ +struct vehicle_global_position_s { uint64_t timestamp; /**< Time of this estimate, in microseconds since system start */ - bool global_valid; /**< true if position satisfies validity criteria of estimator */ - bool baro_valid; /**< true if baro_alt is valid (vel_d is also valid in this case) */ - uint64_t time_gps_usec; /**< GPS timestamp in microseconds */ double lat; /**< Latitude in degrees */ double lon; /**< Longitude in degrees */ @@ -74,8 +71,8 @@ struct vehicle_global_position_s float vel_e; /**< Ground east velocity, m/s */ float vel_d; /**< Ground downside velocity, m/s */ float yaw; /**< Yaw in radians -PI..+PI. */ - - float baro_alt; /**< Barometric altitude (not raw baro but fused with accelerometer) */ + float eph; + float epv; }; /** diff --git a/src/modules/uORB/topics/vehicle_global_velocity_setpoint.h b/src/modules/uORB/topics/vehicle_global_velocity_setpoint.h index 73961cdfe..5dac877d0 100644 --- a/src/modules/uORB/topics/vehicle_global_velocity_setpoint.h +++ b/src/modules/uORB/topics/vehicle_global_velocity_setpoint.h @@ -47,8 +47,7 @@ * @{ */ -struct vehicle_global_velocity_setpoint_s -{ +struct vehicle_global_velocity_setpoint_s { float vx; /**< in m/s NED */ float vy; /**< in m/s NED */ float vz; /**< in m/s NED */ diff --git a/src/modules/uORB/topics/vehicle_gps_position.h b/src/modules/uORB/topics/vehicle_gps_position.h index 1639a08c2..794c3f8bc 100644 --- a/src/modules/uORB/topics/vehicle_gps_position.h +++ b/src/modules/uORB/topics/vehicle_gps_position.h @@ -53,13 +53,12 @@ /** * GPS position in WGS84 coordinates. */ -struct vehicle_gps_position_s -{ +struct vehicle_gps_position_s { uint64_t timestamp_position; /**< Timestamp for position information */ int32_t lat; /**< Latitude in 1E-7 degrees */ int32_t lon; /**< Longitude in 1E-7 degrees */ int32_t alt; /**< Altitude in 1E-3 meters (millimeters) above MSL */ - + uint64_t timestamp_variance; float s_variance_m_s; /**< speed accuracy estimate m/s */ float p_variance_m; /**< position accuracy estimate m */ diff --git a/src/modules/uORB/topics/vehicle_local_position.h b/src/modules/uORB/topics/vehicle_local_position.h index d567f2e02..a15303ea4 100644 --- a/src/modules/uORB/topics/vehicle_local_position.h +++ b/src/modules/uORB/topics/vehicle_local_position.h @@ -1,7 +1,6 @@ /**************************************************************************** * * Copyright (C) 2012 PX4 Development Team. All rights reserved. - * Author: @author Lorenz Meier <lm@inf.ethz.ch> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -35,6 +34,9 @@ /** * @file vehicle_local_position.h * Definition of the local fused NED position uORB topic. + * + * @author Lorenz Meier <lm@inf.ethz.ch> + * @author Anton Babushkin <anton.babushkin@me.com> */ #ifndef TOPIC_VEHICLE_LOCAL_POSITION_H_ @@ -52,8 +54,7 @@ /** * Fused local position in NED. */ -struct vehicle_local_position_s -{ +struct vehicle_local_position_s { uint64_t timestamp; /**< Time of this estimate, in microseconds since system start */ bool xy_valid; /**< true if x and y are valid */ bool z_valid; /**< true if z is valid */ @@ -73,8 +74,8 @@ struct vehicle_local_position_s bool xy_global; /**< true if position (x, y) is valid and has valid global reference (ref_lat, ref_lon) */ bool z_global; /**< true if z is valid and has valid global reference (ref_alt) */ uint64_t ref_timestamp; /**< Time when reference position was set */ - int32_t ref_lat; /**< Reference point latitude in 1E7 degrees */ - int32_t ref_lon; /**< Reference point longitude in 1E7 degrees */ + double ref_lat; /**< Reference point latitude in degrees */ + double ref_lon; /**< Reference point longitude in degrees */ float ref_alt; /**< Reference altitude AMSL in meters, MUST be set to current (not at reference point!) ground level */ bool landed; /**< true if vehicle is landed */ /* Distance to surface */ diff --git a/src/modules/uORB/topics/vehicle_local_position_setpoint.h b/src/modules/uORB/topics/vehicle_local_position_setpoint.h index d24d81e3a..8988a0330 100644 --- a/src/modules/uORB/topics/vehicle_local_position_setpoint.h +++ b/src/modules/uORB/topics/vehicle_local_position_setpoint.h @@ -49,8 +49,7 @@ * @{ */ -struct vehicle_local_position_setpoint_s -{ +struct vehicle_local_position_setpoint_s { float x; /**< in meters NED */ float y; /**< in meters NED */ float z; /**< in meters NED */ diff --git a/src/modules/uORB/topics/vehicle_rates_setpoint.h b/src/modules/uORB/topics/vehicle_rates_setpoint.h index 46e62c4b7..9f8b412a7 100644 --- a/src/modules/uORB/topics/vehicle_rates_setpoint.h +++ b/src/modules/uORB/topics/vehicle_rates_setpoint.h @@ -47,8 +47,7 @@ * @addtogroup topics * @{ */ -struct vehicle_rates_setpoint_s -{ +struct vehicle_rates_setpoint_s { uint64_t timestamp; /**< in microseconds since system start */ float roll; /**< body angular rates in NED frame */ @@ -58,9 +57,9 @@ struct vehicle_rates_setpoint_s }; /**< vehicle_rates_setpoint */ - /** - * @} - */ +/** +* @} +*/ /* register this as object request broker structure */ ORB_DECLARE(vehicle_rates_setpoint); diff --git a/src/modules/uORB/topics/vehicle_status.h b/src/modules/uORB/topics/vehicle_status.h index 5d40554fd..f56355246 100644 --- a/src/modules/uORB/topics/vehicle_status.h +++ b/src/modules/uORB/topics/vehicle_status.h @@ -63,12 +63,14 @@ /* main state machine */ typedef enum { MAIN_STATE_MANUAL = 0, - MAIN_STATE_SEATBELT, - MAIN_STATE_EASY, + MAIN_STATE_ALTCTL, + MAIN_STATE_POSCTL, MAIN_STATE_AUTO, MAIN_STATE_MAX } main_state_t; +// If you change the order, add or remove arming_state_t states make sure to update the arrays +// in state_machine_helper.cpp as well. typedef enum { ARMING_STATE_INIT = 0, ARMING_STATE_STANDBY, @@ -93,29 +95,6 @@ typedef enum { FAILSAFE_STATE_MAX } failsafe_state_t; -typedef enum { - MODE_SWITCH_MANUAL = 0, - MODE_SWITCH_ASSISTED, - MODE_SWITCH_AUTO -} mode_switch_pos_t; - -typedef enum { - ASSISTED_SWITCH_SEATBELT = 0, - ASSISTED_SWITCH_EASY -} assisted_switch_pos_t; - -typedef enum { - RETURN_SWITCH_NONE = 0, - RETURN_SWITCH_NORMAL, - RETURN_SWITCH_RETURN -} return_switch_pos_t; - -typedef enum { - MISSION_SWITCH_NONE = 0, - MISSION_SWITCH_LOITER, - MISSION_SWITCH_MISSION -} mission_switch_pos_t; - enum VEHICLE_MODE_FLAG { VEHICLE_MODE_FLAG_SAFETY_ARMED = 128, VEHICLE_MODE_FLAG_MANUAL_INPUT_ENABLED = 64, @@ -131,31 +110,31 @@ enum VEHICLE_MODE_FLAG { * Should match 1:1 MAVLink's MAV_TYPE ENUM */ enum VEHICLE_TYPE { - VEHICLE_TYPE_GENERIC=0, /* Generic micro air vehicle. | */ - VEHICLE_TYPE_FIXED_WING=1, /* Fixed wing aircraft. | */ - VEHICLE_TYPE_QUADROTOR=2, /* Quadrotor | */ - VEHICLE_TYPE_COAXIAL=3, /* Coaxial helicopter | */ - VEHICLE_TYPE_HELICOPTER=4, /* Normal helicopter with tail rotor. | */ - VEHICLE_TYPE_ANTENNA_TRACKER=5, /* Ground installation | */ - VEHICLE_TYPE_GCS=6, /* Operator control unit / ground control station | */ - VEHICLE_TYPE_AIRSHIP=7, /* Airship, controlled | */ - VEHICLE_TYPE_FREE_BALLOON=8, /* Free balloon, uncontrolled | */ - VEHICLE_TYPE_ROCKET=9, /* Rocket | */ - VEHICLE_TYPE_GROUND_ROVER=10, /* Ground rover | */ - VEHICLE_TYPE_SURFACE_BOAT=11, /* Surface vessel, boat, ship | */ - VEHICLE_TYPE_SUBMARINE=12, /* Submarine | */ - VEHICLE_TYPE_HEXAROTOR=13, /* Hexarotor | */ - VEHICLE_TYPE_OCTOROTOR=14, /* Octorotor | */ - VEHICLE_TYPE_TRICOPTER=15, /* Octorotor | */ - VEHICLE_TYPE_FLAPPING_WING=16, /* Flapping wing | */ - VEHICLE_TYPE_KITE=17, /* Kite | */ - VEHICLE_TYPE_ENUM_END=18, /* | */ + VEHICLE_TYPE_GENERIC = 0, /* Generic micro air vehicle. | */ + VEHICLE_TYPE_FIXED_WING = 1, /* Fixed wing aircraft. | */ + VEHICLE_TYPE_QUADROTOR = 2, /* Quadrotor | */ + VEHICLE_TYPE_COAXIAL = 3, /* Coaxial helicopter | */ + VEHICLE_TYPE_HELICOPTER = 4, /* Normal helicopter with tail rotor. | */ + VEHICLE_TYPE_ANTENNA_TRACKER = 5, /* Ground installation | */ + VEHICLE_TYPE_GCS = 6, /* Operator control unit / ground control station | */ + VEHICLE_TYPE_AIRSHIP = 7, /* Airship, controlled | */ + VEHICLE_TYPE_FREE_BALLOON = 8, /* Free balloon, uncontrolled | */ + VEHICLE_TYPE_ROCKET = 9, /* Rocket | */ + VEHICLE_TYPE_GROUND_ROVER = 10, /* Ground rover | */ + VEHICLE_TYPE_SURFACE_BOAT = 11, /* Surface vessel, boat, ship | */ + VEHICLE_TYPE_SUBMARINE = 12, /* Submarine | */ + VEHICLE_TYPE_HEXAROTOR = 13, /* Hexarotor | */ + VEHICLE_TYPE_OCTOROTOR = 14, /* Octorotor | */ + VEHICLE_TYPE_TRICOPTER = 15, /* Octorotor | */ + VEHICLE_TYPE_FLAPPING_WING = 16, /* Flapping wing | */ + VEHICLE_TYPE_KITE = 17, /* Kite | */ + VEHICLE_TYPE_ENUM_END = 18, /* | */ }; enum VEHICLE_BATTERY_WARNING { - VEHICLE_BATTERY_WARNING_NONE = 0, /**< no battery low voltage warning active */ - VEHICLE_BATTERY_WARNING_LOW, /**< warning of low voltage */ - VEHICLE_BATTERY_WARNING_CRITICAL /**< alerting of critical voltage */ + VEHICLE_BATTERY_WARNING_NONE = 0, /**< no battery low voltage warning active */ + VEHICLE_BATTERY_WARNING_LOW, /**< warning of low voltage */ + VEHICLE_BATTERY_WARNING_CRITICAL /**< alerting of critical voltage */ }; /** @@ -168,8 +147,7 @@ enum VEHICLE_BATTERY_WARNING { * * Encodes the complete system state and is set by the commander app. */ -struct vehicle_status_s -{ +struct vehicle_status_s { /* use of a counter and timestamp recommended (but not necessary) */ uint16_t counter; /**< incremented by the writing thread everytime new data is stored */ @@ -188,11 +166,6 @@ struct vehicle_status_s bool is_rotary_wing; - mode_switch_pos_t mode_switch; - return_switch_pos_t return_switch; - assisted_switch_pos_t assisted_switch; - mission_switch_pos_t mission_switch; - bool condition_battery_voltage_valid; bool condition_system_in_air_restore; /**< true if we can restore in mid air */ bool condition_system_sensors_initialized; @@ -219,7 +192,7 @@ struct vehicle_status_s uint32_t onboard_control_sensors_present; uint32_t onboard_control_sensors_enabled; uint32_t onboard_control_sensors_health; - + float load; /**< processor load from 0 to 1 */ float battery_voltage; float battery_current; diff --git a/src/modules/uORB/topics/vehicle_vicon_position.h b/src/modules/uORB/topics/vehicle_vicon_position.h index 0822fa89a..e19a34a5d 100644 --- a/src/modules/uORB/topics/vehicle_vicon_position.h +++ b/src/modules/uORB/topics/vehicle_vicon_position.h @@ -52,8 +52,7 @@ /** * Fused local position in NED. */ -struct vehicle_vicon_position_s -{ +struct vehicle_vicon_position_s { uint64_t timestamp; /**< time of this estimate, in microseconds since system start */ bool valid; /**< true if position satisfies validity criteria of estimator */ diff --git a/src/modules/unit_test/unit_test.cpp b/src/modules/unit_test/unit_test.cpp index 64ee544a2..02d1af481 100644 --- a/src/modules/unit_test/unit_test.cpp +++ b/src/modules/unit_test/unit_test.cpp @@ -32,17 +32,10 @@ * ****************************************************************************/ -/** - * @file unit_test.cpp - * A unit test library. - * - */ - #include "unit_test.h" #include <systemlib/err.h> - UnitTest::UnitTest() { } @@ -51,15 +44,15 @@ UnitTest::~UnitTest() { } -void -UnitTest::print_results(const char* result) +void UnitTest::printResults(void) +{ + warnx(mu_tests_failed() ? "SOME TESTS FAILED" : "ALL TESTS PASSED"); + warnx(" Tests passed : %d", mu_tests_passed()); + warnx(" Tests failed : %d", mu_tests_failed()); + warnx(" Assertions : %d", mu_assertion()); +} + +void UnitTest::printAssert(const char* msg, const char* test, const char* file, int line) { - if (result != 0) { - warnx("Failed: %s:%d", mu_last_test(), mu_line()); - warnx("%s", result); - } else { - warnx("ALL TESTS PASSED"); - warnx(" Tests run : %d", mu_tests_run()); - warnx(" Assertion : %d", mu_assertion()); - } + warnx("Assertion failed: %s - %s (%s:%d)", msg, test, file, line); } diff --git a/src/modules/unit_test/unit_test.h b/src/modules/unit_test/unit_test.h index 3020734f4..32eb8c308 100644 --- a/src/modules/unit_test/unit_test.h +++ b/src/modules/unit_test/unit_test.h @@ -32,62 +32,55 @@ * ****************************************************************************/ -/** - * @file unit_test.h - * A unit test library based on MinUnit (http://www.jera.com/techinfo/jtns/jtn002.html). - * - */ - #ifndef UNIT_TEST_H_ -#define UNIT_TEST_ +#define UNIT_TEST_H_ #include <systemlib/err.h> - class __EXPORT UnitTest { public: -#define xstr(s) str(s) -#define str(s) #s #define INLINE_GLOBAL(type,func) inline type& func() { static type x; return x; } INLINE_GLOBAL(int, mu_tests_run) +INLINE_GLOBAL(int, mu_tests_failed) +INLINE_GLOBAL(int, mu_tests_passed) INLINE_GLOBAL(int, mu_assertion) INLINE_GLOBAL(int, mu_line) INLINE_GLOBAL(const char*, mu_last_test) -#define mu_assert(message, test) \ - do \ - { \ - if (!(test)) \ - return __FILE__ ":" xstr(__LINE__) " " message " (" #test ")"; \ - else \ - mu_assertion()++; \ - } while (0) - - -#define mu_run_test(test) \ -do \ -{ \ - const char *message; \ - mu_last_test() = #test; \ - mu_line() = __LINE__; \ - message = test(); \ - mu_tests_run()++; \ - if (message) \ - return message; \ -} while (0) - - -public: UnitTest(); virtual ~UnitTest(); - virtual const char* run_tests() = 0; - virtual void print_results(const char* result); -}; - + virtual void runTests(void) = 0; + void printResults(void); + + void printAssert(const char* msg, const char* test, const char* file, int line); + +#define ut_assert(message, test) \ + do { \ + if (!(test)) { \ + printAssert(message, #test, __FILE__, __LINE__); \ + return false; \ + } else { \ + mu_assertion()++; \ + } \ + } while (0) + +#define ut_run_test(test) \ + do { \ + warnx("RUNNING TEST: %s", #test); \ + mu_tests_run()++; \ + if (!test()) { \ + warnx("TEST FAILED: %s", #test); \ + mu_tests_failed()++; \ + } else { \ + warnx("TEST PASSED: %s", #test); \ + mu_tests_passed()++; \ + } \ + } while (0) +}; #endif /* UNIT_TEST_H_ */ diff --git a/src/systemcmds/config/config.c b/src/systemcmds/config/config.c index 476015f3e..e6d4b763b 100644 --- a/src/systemcmds/config/config.c +++ b/src/systemcmds/config/config.c @@ -121,7 +121,7 @@ do_device(int argc, char *argv[]) errx(ret,"uORB publications could not be unblocked"); } else { - errx("no valid command: %s", argv[1]); + errx(1, "no valid command: %s", argv[1]); } } diff --git a/src/systemcmds/esc_calib/esc_calib.c b/src/systemcmds/esc_calib/esc_calib.c index ad1996694..7d80af307 100644 --- a/src/systemcmds/esc_calib/esc_calib.c +++ b/src/systemcmds/esc_calib/esc_calib.c @@ -182,7 +182,7 @@ esc_calib_main(int argc, char *argv[]) if (orb_updated) { errx(1, "ABORTING! Attitude control still active. Please ensure to shut down all controllers:\n" - "\tmultirotor_att_control stop\n" + "\tmc_att_control stop\n" "\tfw_att_control stop\n"); } diff --git a/src/systemcmds/mtd/24xxxx_mtd.c b/src/systemcmds/mtd/24xxxx_mtd.c index e34be44e3..a3f9dffff 100644 --- a/src/systemcmds/mtd/24xxxx_mtd.c +++ b/src/systemcmds/mtd/24xxxx_mtd.c @@ -142,12 +142,9 @@ struct at24c_dev_s { uint16_t pagesize; /* 32, 63 */ uint16_t npages; /* 128, 256, 512, 1024 */ - perf_counter_t perf_reads; - perf_counter_t perf_writes; - perf_counter_t perf_resets; - perf_counter_t perf_read_retries; - perf_counter_t perf_read_errors; - perf_counter_t perf_write_errors; + perf_counter_t perf_transfers; + perf_counter_t perf_resets_retries; + perf_counter_t perf_errors; }; /************************************************************************************ @@ -298,9 +295,9 @@ static ssize_t at24c_bread(FAR struct mtd_dev_s *dev, off_t startblock, for (;;) { - perf_begin(priv->perf_reads); + perf_begin(priv->perf_transfers); ret = I2C_TRANSFER(priv->dev, &msgv[0], 2); - perf_end(priv->perf_reads); + perf_end(priv->perf_transfers); if (ret >= 0) break; @@ -314,10 +311,10 @@ static ssize_t at24c_bread(FAR struct mtd_dev_s *dev, off_t startblock, * XXX maybe do special first-read handling with optional * bus reset as well? */ - perf_count(priv->perf_read_retries); + perf_count(priv->perf_resets_retries); if (--tries == 0) { - perf_count(priv->perf_read_errors); + perf_count(priv->perf_errors); return ERROR; } } @@ -383,9 +380,9 @@ static ssize_t at24c_bwrite(FAR struct mtd_dev_s *dev, off_t startblock, size_t for (;;) { - perf_begin(priv->perf_writes); + perf_begin(priv->perf_transfers); ret = I2C_TRANSFER(priv->dev, &msgv[0], 1); - perf_end(priv->perf_writes); + perf_end(priv->perf_transfers); if (ret >= 0) break; @@ -397,7 +394,7 @@ static ssize_t at24c_bwrite(FAR struct mtd_dev_s *dev, off_t startblock, size_t * poll for write completion. */ if (--tries == 0) { - perf_count(priv->perf_write_errors); + perf_count(priv->perf_errors); return ERROR; } } @@ -521,12 +518,9 @@ FAR struct mtd_dev_s *at24c_initialize(FAR struct i2c_dev_s *dev) { priv->mtd.ioctl = at24c_ioctl; priv->dev = dev; - priv->perf_reads = perf_alloc(PC_ELAPSED, "EEPROM read"); - priv->perf_writes = perf_alloc(PC_ELAPSED, "EEPROM write"); - priv->perf_resets = perf_alloc(PC_COUNT, "EEPROM reset"); - priv->perf_read_retries = perf_alloc(PC_COUNT, "EEPROM read retries"); - priv->perf_read_errors = perf_alloc(PC_COUNT, "EEPROM read errors"); - priv->perf_write_errors = perf_alloc(PC_COUNT, "EEPROM write errors"); + priv->perf_transfers = perf_alloc(PC_ELAPSED, "eeprom_trans"); + priv->perf_resets_retries = perf_alloc(PC_COUNT, "eeprom_rst"); + priv->perf_errors = perf_alloc(PC_COUNT, "eeprom_errs"); } /* attempt to read to validate device is present */ @@ -548,9 +542,9 @@ FAR struct mtd_dev_s *at24c_initialize(FAR struct i2c_dev_s *dev) { } }; - perf_begin(priv->perf_reads); + perf_begin(priv->perf_transfers); int ret = I2C_TRANSFER(priv->dev, &msgv[0], 2); - perf_end(priv->perf_reads); + perf_end(priv->perf_transfers); if (ret < 0) { return NULL; diff --git a/src/systemcmds/mtd/mtd.c b/src/systemcmds/mtd/mtd.c index 0a88d40f3..a57eaafe7 100644 --- a/src/systemcmds/mtd/mtd.c +++ b/src/systemcmds/mtd/mtd.c @@ -160,7 +160,11 @@ static void ramtron_attach(void) { /* find the right spi */ +#ifdef CONFIG_ARCH_BOARD_AEROCORE + struct spi_dev_s *spi = up_spiinitialize(4); +#else struct spi_dev_s *spi = up_spiinitialize(2); +#endif /* this resets the spi bus, set correct bus speed again */ SPI_SETFREQUENCY(spi, 10 * 1000 * 1000); SPI_SETBITS(spi, 8); diff --git a/src/systemcmds/nshterm/module.mk b/src/systemcmds/nshterm/module.mk index a48588535..b22b446da 100644 --- a/src/systemcmds/nshterm/module.mk +++ b/src/systemcmds/nshterm/module.mk @@ -38,4 +38,4 @@ MODULE_COMMAND = nshterm SRCS = nshterm.c -MODULE_STACKSIZE = 3000 +MODULE_STACKSIZE = 1200 diff --git a/src/systemcmds/param/module.mk b/src/systemcmds/param/module.mk index 63f15ad28..f716eb71e 100644 --- a/src/systemcmds/param/module.mk +++ b/src/systemcmds/param/module.mk @@ -38,7 +38,8 @@ MODULE_COMMAND = param SRCS = param.c -MODULE_STACKSIZE = 4096 +# Note: measurements yielded a max of 900 bytes used. +MODULE_STACKSIZE = 1800 MAXOPTIMIZATION = -Os diff --git a/src/systemcmds/param/param.c b/src/systemcmds/param/param.c index 0cbba0a37..d92ee88ef 100644 --- a/src/systemcmds/param/param.c +++ b/src/systemcmds/param/param.c @@ -61,8 +61,9 @@ static void do_load(const char* param_file_name); static void do_import(const char* param_file_name); static void do_show(const char* search_string); static void do_show_print(void *arg, param_t param); -static void do_set(const char* name, const char* val); +static void do_set(const char* name, const char* val, bool fail_on_not_found); static void do_compare(const char* name, const char* vals[], unsigned comparisons); +static void do_reset(); int param_main(int argc, char *argv[]) @@ -116,10 +117,17 @@ param_main(int argc, char *argv[]) } if (!strcmp(argv[1], "set")) { - if (argc >= 4) { - do_set(argv[2], argv[3]); + if (argc >= 5) { + + /* if the fail switch is provided, fails the command if not found */ + bool fail = !strcmp(argv[4], "fail"); + + do_set(argv[2], argv[3], fail); + + } else if (argc >= 4) { + do_set(argv[2], argv[3], false); } else { - errx(1, "not enough arguments.\nTry 'param set PARAM_NAME 3'"); + errx(1, "not enough arguments.\nTry 'param set PARAM_NAME 3 [fail]'"); } } @@ -130,6 +138,10 @@ param_main(int argc, char *argv[]) errx(1, "not enough arguments.\nTry 'param compare PARAM_NAME 3'"); } } + + if (!strcmp(argv[1], "reset")) { + do_reset(); + } } errx(1, "expected a command, try 'load', 'import', 'show', 'set', 'compare', 'select' or 'save'"); @@ -277,7 +289,7 @@ do_show_print(void *arg, param_t param) } static void -do_set(const char* name, const char* val) +do_set(const char* name, const char* val, bool fail_on_not_found) { int32_t i; float f; @@ -285,8 +297,8 @@ do_set(const char* name, const char* val) /* set nothing if parameter cannot be found */ if (param == PARAM_INVALID) { - /* param not found */ - errx(1, "Error: Parameter %s not found.", name); + /* param not found - fail silenty in scripts as it prevents booting */ + errx(((fail_on_not_found) ? 1 : 0), "Error: Parameter %s not found.", name); } printf("%c %s: ", @@ -402,3 +414,16 @@ do_compare(const char* name, const char* vals[], unsigned comparisons) exit(ret); } + +static void +do_reset() +{ + param_reset_all(); + + if (param_save_default()) { + warnx("Param export failed."); + exit(1); + } else { + exit(0); + } +} diff --git a/src/systemcmds/perf/module.mk b/src/systemcmds/perf/module.mk index 77952842b..ec39a7a85 100644 --- a/src/systemcmds/perf/module.mk +++ b/src/systemcmds/perf/module.mk @@ -39,3 +39,5 @@ MODULE_COMMAND = perf SRCS = perf.c MAXOPTIMIZATION = -Os + +MODULE_STACKSIZE = 1800 diff --git a/src/systemcmds/preflight_check/module.mk b/src/systemcmds/preflight_check/module.mk index 7c3c88783..0cb2a4cd0 100644 --- a/src/systemcmds/preflight_check/module.mk +++ b/src/systemcmds/preflight_check/module.mk @@ -40,3 +40,5 @@ MODULE_COMMAND = preflight_check SRCS = preflight_check.c MAXOPTIMIZATION = -Os + +MODULE_STACKSIZE = 1800 diff --git a/src/systemcmds/pwm/module.mk b/src/systemcmds/pwm/module.mk index 4a23bba90..13a24150f 100644 --- a/src/systemcmds/pwm/module.mk +++ b/src/systemcmds/pwm/module.mk @@ -38,4 +38,4 @@ MODULE_COMMAND = pwm SRCS = pwm.c -MODULE_STACKSIZE = 4096 +MODULE_STACKSIZE = 1800 diff --git a/src/systemcmds/pwm/pwm.c b/src/systemcmds/pwm/pwm.c index 7c23f38c2..1828c660f 100644 --- a/src/systemcmds/pwm/pwm.c +++ b/src/systemcmds/pwm/pwm.c @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -443,6 +443,110 @@ pwm_main(int argc, char *argv[]) exit(0); } } + usleep(2000); + } + exit(0); + + + } else if (!strcmp(argv[1], "steps")) { + + if (set_mask == 0) { + usage("no channels set"); + } + + /* get current servo values */ + struct pwm_output_values last_spos; + + for (unsigned i = 0; i < servo_count; i++) { + + ret = ioctl(fd, PWM_SERVO_GET(i), (unsigned long)&last_spos.values[i]); + if (ret != OK) + err(1, "PWM_SERVO_GET(%d)", i); + } + + /* perform PWM output */ + + /* Open console directly to grab CTRL-C signal */ + struct pollfd fds; + fds.fd = 0; /* stdin */ + fds.events = POLLIN; + + warnx("Running 5 steps. WARNING! Motors will be live in 5 seconds\nPress any key to abort now."); + sleep(5); + + unsigned off = 900; + unsigned idle = 1300; + unsigned full = 2000; + unsigned steps_timings_us[] = {2000, 5000, 20000, 50000}; + + unsigned phase = 0; + unsigned phase_counter = 0; + unsigned const phase_maxcount = 20; + + for ( unsigned steps_timing_index = 0; + steps_timing_index < sizeof(steps_timings_us) / sizeof(steps_timings_us[0]); + steps_timing_index++ ) { + + warnx("Sending step input with 0 to 100%% over a %u microseconds ramp", steps_timings_us[steps_timing_index]); + + while (1) { + for (unsigned i = 0; i < servo_count; i++) { + if (set_mask & 1<<i) { + + unsigned val; + + if (phase == 0) { + val = idle; + } else if (phase == 1) { + /* ramp - depending how steep it is this ramp will look instantaneous on the output */ + val = idle + (full - idle) * (phase_maxcount / (float)phase_counter); + } else { + val = off; + } + + ret = ioctl(fd, PWM_SERVO_SET(i), val); + if (ret != OK) + err(1, "PWM_SERVO_SET(%d)", i); + } + } + + /* abort on user request */ + char c; + ret = poll(&fds, 1, 0); + if (ret > 0) { + + int ret = read(0, &c, 1); + if (ret > 0) { + /* reset output to the last value */ + for (unsigned i = 0; i < servo_count; i++) { + if (set_mask & 1<<i) { + ret = ioctl(fd, PWM_SERVO_SET(i), last_spos.values[i]); + if (ret != OK) + err(1, "PWM_SERVO_SET(%d)", i); + } + } + warnx("Key pressed, user abort\n"); + exit(0); + } + } + if (phase == 1) { + usleep(steps_timings_us[steps_timing_index] / phase_maxcount); + + } else if (phase == 0) { + usleep(50000); + } else if (phase == 2) { + usleep(50000); + } else { + break; + } + + phase_counter++; + + if (phase_counter > phase_maxcount) { + phase++; + phase_counter = 0; + } + } } exit(0); diff --git a/src/systemcmds/reboot/module.mk b/src/systemcmds/reboot/module.mk index 19f64af54..edf9d8b37 100644 --- a/src/systemcmds/reboot/module.mk +++ b/src/systemcmds/reboot/module.mk @@ -39,3 +39,5 @@ MODULE_COMMAND = reboot SRCS = reboot.c MAXOPTIMIZATION = -Os + +MODULE_STACKSIZE = 800 diff --git a/src/systemcmds/tests/test_adc.c b/src/systemcmds/tests/test_adc.c index 030ac6e23..03391b851 100644 --- a/src/systemcmds/tests/test_adc.c +++ b/src/systemcmds/tests/test_adc.c @@ -66,8 +66,8 @@ int test_adc(int argc, char *argv[]) } for (unsigned i = 0; i < 5; i++) { - /* make space for a maximum of eight channels */ - struct adc_msg_s data[8]; + /* make space for a maximum of twelve channels */ + struct adc_msg_s data[12]; /* read all channels available */ ssize_t count = read(fd, data, sizeof(data)); diff --git a/src/systemcmds/top/module.mk b/src/systemcmds/top/module.mk index 9239aafc3..548a09f85 100644 --- a/src/systemcmds/top/module.mk +++ b/src/systemcmds/top/module.mk @@ -38,7 +38,7 @@ MODULE_COMMAND = top SRCS = top.c -MODULE_STACKSIZE = 3000 +MODULE_STACKSIZE = 1700 MAXOPTIMIZATION = -Os diff --git a/src/systemcmds/hw_ver/module.mk b/src/systemcmds/ver/module.mk index 3cc08b6a1..2eeb80b61 100644 --- a/src/systemcmds/hw_ver/module.mk +++ b/src/systemcmds/ver/module.mk @@ -32,12 +32,13 @@ ############################################################################ # -# Show and test hardware version +# "version" nsh-command displays version infromation for hw,sw, gcc,build etc +# can be also included and used in own code via "ver.h" # -MODULE_COMMAND = hw_ver -SRCS = hw_ver.c +MODULE_COMMAND = ver +SRCS = ver.c -MODULE_STACKSIZE = 1024 +MODULE_STACKSIZE = 1024 -MAXOPTIMIZATION = -Os +MAXOPTIMIZATION = -Os diff --git a/src/systemcmds/ver/ver.c b/src/systemcmds/ver/ver.c new file mode 100644 index 000000000..9ae080ee2 --- /dev/null +++ b/src/systemcmds/ver/ver.c @@ -0,0 +1,123 @@ +/**************************************************************************** +* +* Copyright (c) 2014 PX4 Development Team. All rights reserved. +* +* Redistribution and use in source and binary forms, with or without +* modification, are permitted provided that the following conditions +* are met: +* +* 1. Redistributions of source code must retain the above copyright +* notice, this list of conditions and the following disclaimer. +* 2. Redistributions in binary form must reproduce the above copyright +* notice, this list of conditions and the following disclaimer in +* the documentation and/or other materials provided with the +* distribution. +* 3. Neither the name PX4 nor the names of its contributors may be +* used to endorse or promote products derived from this software +* without specific prior written permission. +* +* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS +* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT +* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS +* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE +* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, +* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, +* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS +* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED +* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT +* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN +* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE +* POSSIBILITY OF SUCH DAMAGE. +* +****************************************************************************/ + +/** +* @file ver.c +* +* Version command, unifies way of showing versions of HW, SW, Build, GCC +* In case you want to add new version just extend version_main function +* +* @author Vladimir Kulla <ufon@kullaonline.net> +*/ + +#include <stdio.h> +#include <string.h> +#include <version/version.h> +#include <systemlib/err.h> + +// string constants for version commands +static const char sz_ver_hw_str[] = "hw"; +static const char sz_ver_hwcmp_str[] = "hwcmp"; +static const char sz_ver_git_str[] = "git"; +static const char sz_ver_bdate_str[] = "bdate"; +static const char sz_ver_gcc_str[] = "gcc"; +static const char sz_ver_all_str[] = "all"; + +static void usage(const char *reason) +{ + if (reason != NULL) { + printf("%s\n", reason); + } + + printf("usage: ver {hw|hwcmp|git|bdate|gcc|all}\n\n"); +} + +__EXPORT int ver_main(int argc, char *argv[]); + +int ver_main(int argc, char *argv[]) +{ + int ret = 1; //defaults to an error + + // first check if there are at least 2 params + if (argc >= 2) { + if (argv[1] != NULL) { + if (!strncmp(argv[1], sz_ver_hw_str, sizeof(sz_ver_hw_str))) { + printf("%s\n", HW_ARCH); + ret = 0; + + } else if (!strncmp(argv[1], sz_ver_hwcmp_str, sizeof(sz_ver_hwcmp_str))) { + if (argc >= 3 && argv[2] != NULL) { + // compare 3rd parameter with HW_ARCH string, in case of match, return 0 + ret = strncmp(HW_ARCH, argv[2], strlen(HW_ARCH)); + + if (ret == 0) { + printf("ver hwcmp match: %s\n", HW_ARCH); + } + + } else { + errx(1, "Not enough arguments, try 'ver hwcmp PX4FMU_V2'"); + } + + } else if (!strncmp(argv[1], sz_ver_git_str, sizeof(sz_ver_git_str))) { + printf("%s\n", FW_GIT); + ret = 0; + + } else if (!strncmp(argv[1], sz_ver_bdate_str, sizeof(sz_ver_bdate_str))) { + printf("%s %s\n", __DATE__, __TIME__); + ret = 0; + + } else if (!strncmp(argv[1], sz_ver_gcc_str, sizeof(sz_ver_gcc_str))) { + printf("%s\n", __VERSION__); + ret = 0; + + } else if (!strncmp(argv[1], sz_ver_all_str, sizeof(sz_ver_all_str))) { + printf("HW arch: %s\n", HW_ARCH); + printf("Build datetime: %s %s\n", __DATE__, __TIME__); + printf("FW git-hash: %s\n", FW_GIT); + printf("GCC toolchain: %s\n", __VERSION__); + ret = 0; + + } else { + errx(1, "unknown command.\n"); + } + + } else { + usage("Error, input parameter NULL.\n"); + } + + } else { + usage("Error, not enough parameters."); + } + + return ret; +} |