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author | Anton Babushkin <anton.babushkin@me.com> | 2014-09-28 13:41:21 +0400 |
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committer | Anton Babushkin <anton.babushkin@me.com> | 2014-09-28 13:41:21 +0400 |
commit | 1cc5f3778dd6c18f3a14c64959d28f978b0305ef (patch) | |
tree | f2b8138e6f85b5f760fa22bbe3aecbce61539277 | |
parent | cf4604f5c3614bc5cd1b82dfee693cbac36181ab (diff) | |
parent | 8a18cfa3869555389e7e9ff8f104d83f9c54cb43 (diff) | |
download | px4-firmware-1cc5f3778dd6c18f3a14c64959d28f978b0305ef.tar.gz px4-firmware-1cc5f3778dd6c18f3a14c64959d28f978b0305ef.tar.bz2 px4-firmware-1cc5f3778dd6c18f3a14c64959d28f978b0305ef.zip |
Merge branch 'master' into takeoff_fix
115 files changed, 5023 insertions, 1294 deletions
diff --git a/LICENSE.md b/LICENSE.md new file mode 100644 index 000000000..2ad83eba4 --- /dev/null +++ b/LICENSE.md @@ -0,0 +1,41 @@ +The PX4 firmware is licensed generally under a permissive 3-clause BSD license. Contributions are required +to be made under the same license. Any exception to this general rule is listed below. + + /**************************************************************************** + * + * 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 + * 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 middleware: BSD 3-clause + - PX4 flight control stack: BSD 3-clause + - NuttX operating system: BSD 3-clause + - Exceptions: Currently only this [400 LOC file](https://github.com/PX4/Firmware/blob/master/src/lib/external_lgpl/tecs/tecs.cpp) remains LGPL, but will be replaced with a BSD implementation.
\ No newline at end of file diff --git a/NuttX b/NuttX -Subproject 088146b90eee5b614ea6386a64dae343a49a517 +Subproject 41fffa0df192e4a26d2325c7ac5d9b5d7ba0211 diff --git a/README.md b/README.md new file mode 100644 index 000000000..84fb02e3b --- /dev/null +++ b/README.md @@ -0,0 +1,10 @@ +## PX4 Aerial Middleware and Flight Control Stack ## + +* Official Website: http://px4.io +* License: BSD 3-clause (see LICENSE.md) +* Supported airframes: + * Multicopters + * Fixed wing +* Binaries (always up-to-date from master): + * [Downloads](https://pixhawk.org/downloads) +* Mailing list: [Google Groups](http://groups.google.com/group/px4users) diff --git a/ROMFS/px4fmu_common/init.d/3031_phantom b/ROMFS/px4fmu_common/init.d/3031_phantom index 31dfe7100..53c48d8aa 100644 --- a/ROMFS/px4fmu_common/init.d/3031_phantom +++ b/ROMFS/px4fmu_common/init.d/3031_phantom @@ -30,6 +30,9 @@ then param set FW_RR_P 0.08 param set FW_R_LIM 50 param set FW_R_RMAX 0 + # Bottom of bay and nominal zero-pitch attitude differ + # the payload bay is pitched up about 7 degrees + param set SENS_BOARD_Y_OFF 7.0 fi set MIXER phantom diff --git a/ROMFS/px4fmu_common/init.d/3035_viper b/ROMFS/px4fmu_common/init.d/3035_viper index a4c1e832d..3714b612f 100644 --- a/ROMFS/px4fmu_common/init.d/3035_viper +++ b/ROMFS/px4fmu_common/init.d/3035_viper @@ -8,3 +8,5 @@ sh /etc/init.d/rc.fw_defaults set MIXER Viper + +set FAILSAFE "-c567 -p 1000" diff --git a/ROMFS/px4fmu_common/init.d/rc.interface b/ROMFS/px4fmu_common/init.d/rc.interface index 1de0abb58..e44cd0953 100644 --- a/ROMFS/px4fmu_common/init.d/rc.interface +++ b/ROMFS/px4fmu_common/init.d/rc.interface @@ -77,4 +77,9 @@ then pwm max -c $PWM_OUTPUTS -p $PWM_MAX fi fi + + if [ $FAILSAFE != none ] + then + pwm failsafe -d $OUTPUT_DEV $FAILSAFE + fi fi diff --git a/ROMFS/px4fmu_common/init.d/rc.uavcan b/ROMFS/px4fmu_common/init.d/rc.uavcan new file mode 100644 index 000000000..9a470a6b8 --- /dev/null +++ b/ROMFS/px4fmu_common/init.d/rc.uavcan @@ -0,0 +1,18 @@ +#!nsh +# +# UAVCAN initialization script. +# + +if param compare UAVCAN_ENABLE 1 +then + if uavcan start + then + # First sensor publisher to initialize takes lowest instance ID + # This delay ensures that UAVCAN-interfaced sensors would be allocated on lowest instance IDs + sleep 1 + echo "[init] UAVCAN started" + else + echo "[init] ERROR: Could not start UAVCAN" + tone_alarm $TUNE_OUT_ERROR + fi +fi diff --git a/ROMFS/px4fmu_common/init.d/rcS b/ROMFS/px4fmu_common/init.d/rcS index c9e6a27ca..ea04ece34 100644 --- a/ROMFS/px4fmu_common/init.d/rcS +++ b/ROMFS/px4fmu_common/init.d/rcS @@ -66,6 +66,9 @@ then # sercon + # Try to get an USB console + nshterm /dev/ttyACM0 & + # # Start the ORB (first app to start) # @@ -96,11 +99,9 @@ then # if rgbled start then - echo "[init] RGB Led" else if blinkm start then - echo "[init] BlinkM" blinkm systemstate fi fi @@ -129,6 +130,7 @@ then set LOAD_DEFAULT_APPS yes set GPS yes set GPS_FAKE no + set FAILSAFE none # # Set DO_AUTOCONFIG flag to use it in AUTOSTART scripts @@ -279,9 +281,6 @@ then fi fi - # Try to get an USB console - nshterm /dev/ttyACM0 & - # # Start the datamanager (and do not abort boot if it fails) # @@ -304,11 +303,10 @@ then then if [ $OUTPUT_MODE == uavcan_esc ] then - if uavcan start 1 + if param compare UAVCAN_ENABLE 0 then - echo "CAN UP" - else - echo "CAN ERR" + echo "[init] OVERRIDING UAVCAN_ENABLE = 1" + param set UAVCAN_ENABLE 1 fi fi @@ -448,6 +446,11 @@ then mavlink start $MAVLINK_FLAGS # + # UAVCAN + # + sh /etc/init.d/rc.uavcan + + # # Sensors, Logging, GPS # sh /etc/init.d/rc.sensors diff --git a/ROMFS/px4fmu_common/mixers/FMU_AERT.mix b/ROMFS/px4fmu_common/mixers/FMU_AERT.mix index 0ec663e35..7fed488af 100644 --- a/ROMFS/px4fmu_common/mixers/FMU_AERT.mix +++ b/ROMFS/px4fmu_common/mixers/FMU_AERT.mix @@ -64,21 +64,22 @@ O: 10000 10000 0 -10000 10000 S: 0 3 0 20000 -10000 -10000 10000 -Gimbal / flaps / payload mixer for last four channels +Gimbal / flaps / payload mixer for last four channels, +using the payload control group ----------------------------------------------------- M: 1 O: 10000 10000 0 -10000 10000 -S: 0 4 10000 10000 0 -10000 10000 +S: 2 0 10000 10000 0 -10000 10000 M: 1 O: 10000 10000 0 -10000 10000 -S: 0 5 10000 10000 0 -10000 10000 +S: 2 1 10000 10000 0 -10000 10000 M: 1 O: 10000 10000 0 -10000 10000 -S: 0 6 10000 10000 0 -10000 10000 +S: 2 2 10000 10000 0 -10000 10000 M: 1 O: 10000 10000 0 -10000 10000 -S: 0 7 10000 10000 0 -10000 10000 +S: 2 3 10000 10000 0 -10000 10000 diff --git a/ROMFS/px4fmu_common/mixers/Viper.mix b/ROMFS/px4fmu_common/mixers/Viper.mix index 79c4447be..5a0381bd8 100755 --- a/ROMFS/px4fmu_common/mixers/Viper.mix +++ b/ROMFS/px4fmu_common/mixers/Viper.mix @@ -52,21 +52,20 @@ M: 1 O: 10000 10000 0 -10000 10000 S: 0 3 0 20000 -10000 -10000 10000 -Gimbal / flaps / payload mixer for last four channels +Inputs to the mixer come from channel group 2 (payload), channels 0 +(bay servo 1), 1 (bay servo 2) and 3 (drop release). ----------------------------------------------------- M: 1 O: 10000 10000 0 -10000 10000 -S: 0 4 10000 10000 0 -10000 10000 +S: 2 0 10000 10000 0 -10000 10000 M: 1 O: 10000 10000 0 -10000 10000 -S: 0 5 10000 10000 0 -10000 10000 +S: 2 1 10000 10000 0 -10000 10000 M: 1 O: 10000 10000 0 -10000 10000 -S: 0 6 10000 10000 0 -10000 10000 +S: 2 2 -10000 -10000 0 -10000 10000 + -M: 1 -O: 10000 10000 0 -10000 10000 -S: 0 7 10000 10000 0 -10000 10000 diff --git a/ROMFS/px4fmu_test/unit_test_data/mavlink_tests/empty_dir/.gitignore b/ROMFS/px4fmu_test/unit_test_data/mavlink_tests/empty_dir/.gitignore new file mode 100644 index 000000000..e69de29bb --- /dev/null +++ b/ROMFS/px4fmu_test/unit_test_data/mavlink_tests/empty_dir/.gitignore diff --git a/ROMFS/px4fmu_test/unit_test_data/mavlink_tests/test_238.data b/ROMFS/px4fmu_test/unit_test_data/mavlink_tests/test_238.data Binary files differnew file mode 100644 index 000000000..973de16e5 --- /dev/null +++ b/ROMFS/px4fmu_test/unit_test_data/mavlink_tests/test_238.data diff --git a/ROMFS/px4fmu_test/unit_test_data/mavlink_tests/test_239.data b/ROMFS/px4fmu_test/unit_test_data/mavlink_tests/test_239.data Binary files differnew file mode 100644 index 000000000..7e8764c03 --- /dev/null +++ b/ROMFS/px4fmu_test/unit_test_data/mavlink_tests/test_239.data diff --git a/ROMFS/px4fmu_test/unit_test_data/mavlink_tests/test_240.data b/ROMFS/px4fmu_test/unit_test_data/mavlink_tests/test_240.data Binary files differnew file mode 100644 index 000000000..f3fe31687 --- /dev/null +++ b/ROMFS/px4fmu_test/unit_test_data/mavlink_tests/test_240.data diff --git a/Tools/px_uploader.py b/Tools/px_uploader.py index d8f4884bc..b46db00b5 100755 --- a/Tools/px_uploader.py +++ b/Tools/px_uploader.py @@ -178,9 +178,9 @@ class uploader(object): MAVLINK_REBOOT_ID1 = bytearray(b'\xfe\x21\x72\xff\x00\x4c\x00\x00\x80\x3f\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\xf6\x00\x01\x00\x00\x48\xf0') MAVLINK_REBOOT_ID0 = bytearray(b'\xfe\x21\x45\xff\x00\x4c\x00\x00\x80\x3f\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\x00\xf6\x00\x00\x00\x00\xd7\xac') - def __init__(self, portname, baudrate): + def __init__(self, portname, baudrate, interCharTimeout=0.001, timeout=0.5): # open the port, keep the default timeout short so we can poll quickly - self.port = serial.Serial(portname, baudrate, timeout=2.0) + self.port = serial.Serial(portname, baudrate) self.otp = b'' self.sn = b'' @@ -195,7 +195,7 @@ class uploader(object): def __recv(self, count=1): c = self.port.read(count) if len(c) < 1: - raise RuntimeError("timeout waiting for data") + raise RuntimeError("timeout waiting for data (%u bytes)", count) # print("recv " + binascii.hexlify(c)) return c diff --git a/makefiles/config_px4fmu-v1_default.mk b/makefiles/config_px4fmu-v1_default.mk index a7c10f52f..6f39b56a1 100644 --- a/makefiles/config_px4fmu-v1_default.mk +++ b/makefiles/config_px4fmu-v1_default.mk @@ -25,11 +25,8 @@ MODULES += drivers/mpu6000 MODULES += drivers/hmc5883 MODULES += drivers/ms5611 MODULES += drivers/mb12xx -MODULES += drivers/ll40ls MODULES += drivers/gps MODULES += drivers/hil -MODULES += drivers/hott/hott_telemetry -MODULES += drivers/hott/hott_sensors MODULES += drivers/blinkm MODULES += drivers/rgbled MODULES += drivers/mkblctrl @@ -43,8 +40,6 @@ MODULES += modules/sensors # System commands # MODULES += systemcmds/mtd -MODULES += systemcmds/bl_update -MODULES += systemcmds/i2c MODULES += systemcmds/mixer MODULES += systemcmds/param MODULES += systemcmds/perf @@ -152,5 +147,4 @@ endef # command priority stack entrypoint BUILTIN_COMMANDS := \ $(call _B, sercon, , 2048, sercon_main ) \ - $(call _B, serdis, , 2048, serdis_main ) \ - $(call _B, sysinfo, , 2048, sysinfo_main ) + $(call _B, serdis, , 2048, serdis_main ) diff --git a/makefiles/config_px4fmu-v2_default.mk b/makefiles/config_px4fmu-v2_default.mk index d0a40445d..5f146686c 100644 --- a/makefiles/config_px4fmu-v2_default.mk +++ b/makefiles/config_px4fmu-v2_default.mk @@ -41,6 +41,7 @@ MODULES += drivers/frsky_telemetry MODULES += modules/sensors MODULES += drivers/mkblctrl MODULES += drivers/pca8574 +MODULES += drivers/px4flow # Needs to be burned to the ground and re-written; for now, diff --git a/makefiles/config_px4fmu-v2_test.mk b/makefiles/config_px4fmu-v2_test.mk index 932f92261..a41670a77 100644 --- a/makefiles/config_px4fmu-v2_test.mk +++ b/makefiles/config_px4fmu-v2_test.mk @@ -54,6 +54,9 @@ MODULES += lib/conversion # LIBRARIES += lib/mathlib/CMSIS +MODULES += modules/unit_test +MODULES += modules/mavlink/mavlink_tests + # # Transitional support - add commands from the NuttX export archive. # diff --git a/mavlink/include/mavlink/v1.0 b/mavlink/include/mavlink/v1.0 -Subproject 4d7487c2bc5f5ccf87bca82970fb2c08d6d8bd5 +Subproject 2423e47b4f9169e77f7194b36fa2118e018c94e diff --git a/nuttx-configs/aerocore/nsh/defconfig b/nuttx-configs/aerocore/nsh/defconfig index 8d0bae7b9..317194f68 100644 --- a/nuttx-configs/aerocore/nsh/defconfig +++ b/nuttx-configs/aerocore/nsh/defconfig @@ -314,7 +314,7 @@ CONFIG_STM32_I2CTIMEOTICKS=500 # CONFIG_ARCH_NOINTC is not set # CONFIG_ARCH_VECNOTIRQ is not set CONFIG_ARCH_DMA=y -CONFIG_ARCH_IRQPRIO=y +# CONFIG_ARCH_IRQPRIO is not set # CONFIG_CUSTOM_STACK is not set # CONFIG_ADDRENV is not set CONFIG_ARCH_HAVE_VFORK=y diff --git a/nuttx-configs/px4fmu-v1/nsh/defconfig b/nuttx-configs/px4fmu-v1/nsh/defconfig index a651faffa..cd9c05b13 100644 --- a/nuttx-configs/px4fmu-v1/nsh/defconfig +++ b/nuttx-configs/px4fmu-v1/nsh/defconfig @@ -287,8 +287,7 @@ CONFIG_STM32_USART_SINGLEWIRE=y # # CONFIG_STM32_I2C_DYNTIMEO is not set CONFIG_STM32_I2CTIMEOSEC=0 -CONFIG_STM32_I2CTIMEOMS=10 -CONFIG_STM32_I2CTIMEOTICKS=500 +CONFIG_STM32_I2CTIMEOMS=1 # CONFIG_STM32_I2C_DUTY16_9 is not set # @@ -309,7 +308,7 @@ CONFIG_STM32_I2CTIMEOTICKS=500 # CONFIG_ARCH_NOINTC is not set # CONFIG_ARCH_VECNOTIRQ is not set CONFIG_ARCH_DMA=y -CONFIG_ARCH_IRQPRIO=y +# CONFIG_ARCH_IRQPRIO is not set # CONFIG_CUSTOM_STACK is not set # CONFIG_ADDRENV is not set CONFIG_ARCH_HAVE_VFORK=y diff --git a/nuttx-configs/px4fmu-v2/nsh/defconfig b/nuttx-configs/px4fmu-v2/nsh/defconfig index a55c95a29..e31f40cd2 100644 --- a/nuttx-configs/px4fmu-v2/nsh/defconfig +++ b/nuttx-configs/px4fmu-v2/nsh/defconfig @@ -323,8 +323,7 @@ CONFIG_STM32_USART_SINGLEWIRE=y # # CONFIG_STM32_I2C_DYNTIMEO is not set CONFIG_STM32_I2CTIMEOSEC=0 -CONFIG_STM32_I2CTIMEOMS=10 -CONFIG_STM32_I2CTIMEOTICKS=500 +CONFIG_STM32_I2CTIMEOMS=1 # CONFIG_STM32_I2C_DUTY16_9 is not set # @@ -350,7 +349,7 @@ CONFIG_SDIO_PRI=128 # CONFIG_ARCH_NOINTC is not set # CONFIG_ARCH_VECNOTIRQ is not set CONFIG_ARCH_DMA=y -CONFIG_ARCH_IRQPRIO=y +# CONFIG_ARCH_IRQPRIO is not set # CONFIG_CUSTOM_STACK is not set # CONFIG_ADDRENV is not set CONFIG_ARCH_HAVE_VFORK=y diff --git a/nuttx-configs/px4io-v1/nsh/defconfig b/nuttx-configs/px4io-v1/nsh/defconfig index 3785e0367..7c76be7ec 100755 --- a/nuttx-configs/px4io-v1/nsh/defconfig +++ b/nuttx-configs/px4io-v1/nsh/defconfig @@ -83,7 +83,6 @@ CONFIG_ARCH_BOARD="px4io-v1" CONFIG_BOARD_LOOPSPERMSEC=2000 CONFIG_DRAM_SIZE=0x00002000 CONFIG_DRAM_START=0x20000000 -CONFIG_ARCH_IRQPRIO=y CONFIG_ARCH_INTERRUPTSTACK=n CONFIG_ARCH_STACKDUMP=y CONFIG_ARCH_BOOTLOADER=n @@ -134,6 +133,8 @@ CONFIG_STM32_USART2=y CONFIG_STM32_USART3=y CONFIG_STM32_I2C1=y CONFIG_STM32_I2C2=n +CONFIG_STM32_I2CTIMEOSEC=0 +CONFIG_STM32_I2CTIMEOMS=1 CONFIG_STM32_BKP=n CONFIG_STM32_PWR=n CONFIG_STM32_DAC=n diff --git a/nuttx-configs/px4io-v2/nsh/defconfig b/nuttx-configs/px4io-v2/nsh/defconfig index e6563e587..02b51e3d7 100755 --- a/nuttx-configs/px4io-v2/nsh/defconfig +++ b/nuttx-configs/px4io-v2/nsh/defconfig @@ -79,7 +79,6 @@ CONFIG_ARCH_BOARD_PX4IO_V2=y CONFIG_BOARD_LOOPSPERMSEC=2000 CONFIG_DRAM_SIZE=0x00002000 CONFIG_DRAM_START=0x20000000 -CONFIG_ARCH_IRQPRIO=y CONFIG_ARCH_INTERRUPTSTACK=n CONFIG_ARCH_STACKDUMP=y CONFIG_ARCH_BOOTLOADER=n diff --git a/src/drivers/airspeed/airspeed.cpp b/src/drivers/airspeed/airspeed.cpp index 41942aacd..293690d27 100644 --- a/src/drivers/airspeed/airspeed.cpp +++ b/src/drivers/airspeed/airspeed.cpp @@ -165,7 +165,7 @@ Airspeed::probe() */ _retries = 4; int ret = measure(); - _retries = 2; + _retries = 0; return ret; } @@ -381,7 +381,10 @@ Airspeed::cycle_trampoline(void *arg) Airspeed *dev = (Airspeed *)arg; dev->cycle(); - dev->update_status(); + // XXX we do not know if this is + // really helping - do not update the + // subsys state right now + //dev->update_status(); } void diff --git a/src/drivers/drv_pwm_output.h b/src/drivers/drv_pwm_output.h index 84815fdfb..bc586f395 100644 --- a/src/drivers/drv_pwm_output.h +++ b/src/drivers/drv_pwm_output.h @@ -95,6 +95,11 @@ __BEGIN_DECLS #define PWM_LOWEST_MAX 1700 /** + * Do not output a channel with this value + */ +#define PWM_IGNORE_THIS_CHANNEL UINT16_MAX + +/** * Servo output signal type, value is actual servo output pulse * width in microseconds. */ @@ -200,10 +205,13 @@ ORB_DECLARE(output_pwm); #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) +#define PWM_SERVO_SET_FORCE_SAFETY_OFF _IOC(_PWM_SERVO_BASE, 23) /** force failsafe mode (failsafe values are set immediately even if failsafe condition not met) */ -#define PWM_SERVO_SET_FORCE_FAILSAFE _IOC(_PWM_SERVO_BASE, 24) +#define PWM_SERVO_SET_FORCE_FAILSAFE _IOC(_PWM_SERVO_BASE, 24) + +/** make failsafe non-recoverable (termination) if it occurs */ +#define PWM_SERVO_SET_TERMINATION_FAILSAFE _IOC(_PWM_SERVO_BASE, 25) /* * diff --git a/src/drivers/drv_px4flow.h b/src/drivers/drv_px4flow.h index 76ec55c3e..ab640837b 100644 --- a/src/drivers/drv_px4flow.h +++ b/src/drivers/drv_px4flow.h @@ -46,37 +46,6 @@ #define PX4FLOW_DEVICE_PATH "/dev/px4flow" -/** - * @addtogroup topics - * @{ - */ - -/** - * Optical flow in NED body frame in SI units. - * - * @see http://en.wikipedia.org/wiki/International_System_of_Units - * - * @warning If possible the usage of the raw flow and performing rotation-compensation - * using the autopilot angular rate estimate is recommended. - */ -struct px4flow_report { - - uint64_t timestamp; /**< in microseconds since system start */ - - 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 per second, rotation-compensated */ - float flow_comp_y_m; /**< speed over ground in meters per second, rotation-compensated */ - float ground_distance_m; /**< Altitude / distance to ground in meters */ - uint8_t quality; /**< Quality of the measurement, 0: bad quality, 255: maximum quality */ - uint8_t sensor_id; /**< id of the sensor emitting the flow value */ - -}; - -/** - * @} - */ - /* * ObjDev tag for px4flow data. */ diff --git a/src/drivers/ets_airspeed/ets_airspeed.cpp b/src/drivers/ets_airspeed/ets_airspeed.cpp index f98d615a2..0f77bb805 100644 --- a/src/drivers/ets_airspeed/ets_airspeed.cpp +++ b/src/drivers/ets_airspeed/ets_airspeed.cpp @@ -155,7 +155,6 @@ ETSAirspeed::collect() } uint16_t diff_pres_pa_raw = val[1] << 8 | val[0]; - uint16_t diff_pres_pa; if (diff_pres_pa_raw == 0) { // a zero value means the pressure sensor cannot give us a // value. We need to return, and not report a value or the @@ -166,28 +165,21 @@ ETSAirspeed::collect() return -1; } - if (diff_pres_pa_raw < _diff_pres_offset + MIN_ACCURATE_DIFF_PRES_PA) { - diff_pres_pa = 0; - } else { - diff_pres_pa = diff_pres_pa_raw - _diff_pres_offset; - } - // The raw value still should be compensated for the known offset diff_pres_pa_raw -= _diff_pres_offset; // Track maximum differential pressure measured (so we can work out top speed). - if (diff_pres_pa > _max_differential_pressure_pa) { - _max_differential_pressure_pa = diff_pres_pa; + if (diff_pres_pa_raw > _max_differential_pressure_pa) { + _max_differential_pressure_pa = diff_pres_pa_raw; } 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.differential_pressure_raw_pa = (float)diff_pres_pa_raw; + report.differential_pressure_filtered_pa = diff_pres_pa_raw; + report.differential_pressure_raw_pa = diff_pres_pa_raw; report.temperature = -1000.0f; report.max_differential_pressure_pa = _max_differential_pressure_pa; @@ -369,7 +361,7 @@ test() err(1, "immediate read failed"); warnx("single read"); - warnx("diff pressure: %f pa", (double)report.differential_pressure_pa); + warnx("diff pressure: %f pa", (double)report.differential_pressure_filtered_pa); /* start the sensor polling at 2Hz */ if (OK != ioctl(fd, SENSORIOCSPOLLRATE, 2)) @@ -394,7 +386,7 @@ test() err(1, "periodic read failed"); warnx("periodic read %u", i); - warnx("diff pressure: %f pa", (double)report.differential_pressure_pa); + warnx("diff pressure: %f pa", (double)report.differential_pressure_filtered_pa); } /* reset the sensor polling to its default rate */ diff --git a/src/drivers/hmc5883/hmc5883.cpp b/src/drivers/hmc5883/hmc5883.cpp index 0e9a961ac..e4ecfa6b5 100644 --- a/src/drivers/hmc5883/hmc5883.cpp +++ b/src/drivers/hmc5883/hmc5883.cpp @@ -1283,14 +1283,13 @@ int HMC5883::set_excitement(unsigned enable) if (OK != ret) perf_count(_comms_errors); + _conf_reg &= ~0x03; // reset previous excitement mode if (((int)enable) < 0) { _conf_reg |= 0x01; } else if (enable > 0) { _conf_reg |= 0x02; - } else { - _conf_reg &= ~0x03; } // ::printf("set_excitement enable=%d regA=0x%x\n", (int)enable, (unsigned)_conf_reg); diff --git a/src/drivers/meas_airspeed/meas_airspeed.cpp b/src/drivers/meas_airspeed/meas_airspeed.cpp index 159706278..1d9a463ad 100644 --- a/src/drivers/meas_airspeed/meas_airspeed.cpp +++ b/src/drivers/meas_airspeed/meas_airspeed.cpp @@ -228,44 +228,23 @@ MEASAirspeed::collect() // the raw value still should be compensated for the known offset diff_press_pa_raw -= _diff_pres_offset; - float diff_press_pa = fabsf(diff_press_pa_raw); - /* - 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). */ - if (diff_press_pa > _max_differential_pressure_pa) { - _max_differential_pressure_pa = diff_press_pa; + if (diff_press_pa_raw > _max_differential_pressure_pa) { + _max_differential_pressure_pa = diff_press_pa_raw; } report.timestamp = hrt_absolute_time(); 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_filtered_pa = _filter.apply(diff_press_pa_raw); report.differential_pressure_raw_pa = diff_press_pa_raw; report.max_differential_pressure_pa = _max_differential_pressure_pa; @@ -345,7 +324,7 @@ 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 */ @@ -394,7 +373,7 @@ MEASAirspeed::voltage_correction(float &diff_press_pa, float &temperature) if (voltage_diff < -1.0f) { voltage_diff = -1.0f; } - temperature -= voltage_diff * temp_slope; + temperature -= voltage_diff * temp_slope; #endif // CONFIG_ARCH_BOARD_PX4FMU_V2 } @@ -523,7 +502,7 @@ test() } warnx("single read"); - warnx("diff pressure: %d pa", (int)report.differential_pressure_pa); + warnx("diff pressure: %d pa", (int)report.differential_pressure_filtered_pa); /* start the sensor polling at 2Hz */ if (OK != ioctl(fd, SENSORIOCSPOLLRATE, 2)) { @@ -551,7 +530,7 @@ test() } warnx("periodic read %u", i); - warnx("diff pressure: %d pa", (int)report.differential_pressure_pa); + warnx("diff pressure: %d pa", (int)report.differential_pressure_filtered_pa); warnx("temperature: %d C (0x%02x)", (int)report.temperature, (unsigned) report.temperature); } diff --git a/src/drivers/ms5611/ms5611.cpp b/src/drivers/ms5611/ms5611.cpp index 873fa62c4..889643d0d 100644 --- a/src/drivers/ms5611/ms5611.cpp +++ b/src/drivers/ms5611/ms5611.cpp @@ -130,7 +130,7 @@ protected: float _T; /* altitude conversion calibration */ - unsigned _msl_pressure; /* in kPa */ + unsigned _msl_pressure; /* in Pa */ orb_advert_t _baro_topic; @@ -466,7 +466,7 @@ MS5611::ioctl(struct file *filp, int cmd, unsigned long arg) irqrestore(flags); return -ENOMEM; } - irqrestore(flags); + irqrestore(flags); return OK; } diff --git a/src/drivers/pca9685/arduino_Adafruit_PWM_Servo_Driver_Library_license.txt b/src/drivers/pca9685/arduino_Adafruit_PWM_Servo_Driver_Library_license.txt new file mode 100644 index 000000000..9c5eb42eb --- /dev/null +++ b/src/drivers/pca9685/arduino_Adafruit_PWM_Servo_Driver_Library_license.txt @@ -0,0 +1,29 @@ +The following license agreement covers re-used code from the arduino driver +for the Adafruit I2C to PWM converter. + +Software License Agreement (BSD License) + +Copyright (c) 2012, Adafruit Industries +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 of the copyright holders 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 ''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 HOLDER 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. diff --git a/src/drivers/pca9685/module.mk b/src/drivers/pca9685/module.mk new file mode 100644 index 000000000..7a5c7996e --- /dev/null +++ b/src/drivers/pca9685/module.mk @@ -0,0 +1,42 @@ +############################################################################ +# +# 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 +# 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. +# +############################################################################ + +# +# Driver for the PCA9685 I2C PWM controller +# The chip is used on the adafruit I2C PWM converter, +# which allows to control servos via I2C. +# https://www.adafruit.com/product/815 + +MODULE_COMMAND = pca9685 + +SRCS = pca9685.cpp diff --git a/src/drivers/pca9685/pca9685.cpp b/src/drivers/pca9685/pca9685.cpp new file mode 100644 index 000000000..6f69ce8a1 --- /dev/null +++ b/src/drivers/pca9685/pca9685.cpp @@ -0,0 +1,651 @@ +/**************************************************************************** + * + * 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 + * 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 pca9685.cpp + * + * Driver for the PCA9685 I2C PWM module + * The chip is used on the Adafruit I2C/PWM converter https://www.adafruit.com/product/815 + * + * Parts of the code are adapted from the arduino library for the board + * https://github.com/adafruit/Adafruit-PWM-Servo-Driver-Library + * for the license of these parts see the + * arduino_Adafruit_PWM_Servo_Driver_Library_license.txt file + * see https://github.com/adafruit/Adafruit-PWM-Servo-Driver-Library for contributors + * + * @author Thomas Gubler <thomasgubler@gmail.com> + */ + +#include <nuttx/config.h> + +#include <drivers/device/i2c.h> + +#include <sys/types.h> +#include <stdint.h> +#include <string.h> +#include <stdlib.h> +#include <stdbool.h> +#include <fcntl.h> +#include <unistd.h> +#include <stdio.h> +#include <ctype.h> +#include <math.h> + +#include <nuttx/wqueue.h> +#include <nuttx/clock.h> + +#include <systemlib/perf_counter.h> +#include <systemlib/err.h> +#include <systemlib/systemlib.h> + +#include <uORB/uORB.h> +#include <uORB/topics/actuator_controls.h> + +#include <board_config.h> +#include <drivers/drv_io_expander.h> + +#define PCA9685_SUBADR1 0x2 +#define PCA9685_SUBADR2 0x3 +#define PCA9685_SUBADR3 0x4 + +#define PCA9685_MODE1 0x0 +#define PCA9685_PRESCALE 0xFE + +#define LED0_ON_L 0x6 +#define LED0_ON_H 0x7 +#define LED0_OFF_L 0x8 +#define LED0_OFF_H 0x9 + +#define ALLLED_ON_L 0xFA +#define ALLLED_ON_H 0xFB +#define ALLLED_OFF_L 0xFC +#define ALLLED_OF + +#define ADDR 0x40 // I2C adress + +#define PCA9685_DEVICE_PATH "/dev/pca9685" +#define PCA9685_BUS PX4_I2C_BUS_EXPANSION +#define PCA9685_PWMFREQ 60.0f +#define PCA9685_NCHANS 16 // total amount of pwm outputs + +#define PCA9685_PWMMIN 150 // this is the 'minimum' pulse length count (out of 4096) +#define PCA9685_PWMMAX 600 // this is the 'maximum' pulse length count (out of 4096)_PWMFREQ 60.0f + +#define PCA9685_PWMCENTER ((PCA9685_PWMMAX + PCA9685_PWMMIN)/2) +#define PCA9685_MAXSERVODEG 90.0f /* maximal servo deflection in degrees + PCA9685_PWMMIN <--> -PCA9685_MAXSERVODEG + PCA9685_PWMMAX <--> PCA9685_MAXSERVODEG + */ +#define PCA9685_SCALE ((PCA9685_PWMMAX - PCA9685_PWMCENTER)/(M_DEG_TO_RAD_F * PCA9685_MAXSERVODEG)) // scales from rad to PWM + +/* oddly, ERROR is not defined for c++ */ +#ifdef ERROR +# undef ERROR +#endif +static const int ERROR = -1; + +class PCA9685 : public device::I2C +{ +public: + PCA9685(int bus=PCA9685_BUS, uint8_t address=ADDR); + virtual ~PCA9685(); + + + virtual int init(); + virtual int ioctl(struct file *filp, int cmd, unsigned long arg); + virtual int info(); + virtual int reset(); + bool is_running() { return _running; } + +private: + work_s _work; + + + enum IOX_MODE _mode; + bool _running; + int _i2cpwm_interval; + bool _should_run; + perf_counter_t _comms_errors; + + uint8_t _msg[6]; + + int _actuator_controls_sub; + struct actuator_controls_s _actuator_controls; + uint16_t _current_values[NUM_ACTUATOR_CONTROLS]; /**< stores the current pwm output + values as sent to the setPin() */ + + bool _mode_on_initialized; /** Set to true after the first call of i2cpwm in mode IOX_MODE_ON */ + + static void i2cpwm_trampoline(void *arg); + void i2cpwm(); + + /** + * Helper function to set the pwm frequency + */ + int setPWMFreq(float freq); + + /** + * Helper function to set the demanded pwm value + * @param num pwm output number + */ + int setPWM(uint8_t num, uint16_t on, uint16_t off); + + /** + * Sets pin without having to deal with on/off tick placement and properly handles + * a zero value as completely off. Optional invert parameter supports inverting + * the pulse for sinking to ground. + * @param num pwm output number + * @param val should be a value from 0 to 4095 inclusive. + */ + int setPin(uint8_t num, uint16_t val, bool invert = false); + + + /* Wrapper to read a byte from addr */ + int read8(uint8_t addr, uint8_t &value); + + /* Wrapper to wite a byte to addr */ + int write8(uint8_t addr, uint8_t value); + +}; + +/* for now, we only support one board */ +namespace +{ +PCA9685 *g_pca9685; +} + +void pca9685_usage(); + +extern "C" __EXPORT int pca9685_main(int argc, char *argv[]); + +PCA9685::PCA9685(int bus, uint8_t address) : + I2C("pca9685", PCA9685_DEVICE_PATH, bus, address, 100000), + _mode(IOX_MODE_OFF), + _running(false), + _i2cpwm_interval(SEC2TICK(1.0f/60.0f)), + _should_run(false), + _comms_errors(perf_alloc(PC_COUNT, "actuator_controls_2_comms_errors")), + _actuator_controls_sub(-1), + _actuator_controls(), + _mode_on_initialized(false) +{ + memset(&_work, 0, sizeof(_work)); + memset(_msg, 0, sizeof(_msg)); + memset(_current_values, 0, sizeof(_current_values)); +} + +PCA9685::~PCA9685() +{ +} + +int +PCA9685::init() +{ + int ret; + ret = I2C::init(); + if (ret != OK) { + return ret; + } + + ret = reset(); + if (ret != OK) { + return ret; + } + + ret = setPWMFreq(PCA9685_PWMFREQ); + + return ret; +} + +int +PCA9685::ioctl(struct file *filp, int cmd, unsigned long arg) +{ + int ret = -EINVAL; + switch (cmd) { + + case IOX_SET_MODE: + + if (_mode != (IOX_MODE)arg) { + + switch ((IOX_MODE)arg) { + case IOX_MODE_OFF: + warnx("shutting down"); + break; + case IOX_MODE_ON: + warnx("starting"); + break; + case IOX_MODE_TEST_OUT: + warnx("test starting"); + break; + + default: + return -1; + } + + _mode = (IOX_MODE)arg; + } + + // if not active, kick it + if (!_running) { + _running = true; + work_queue(LPWORK, &_work, (worker_t)&PCA9685::i2cpwm_trampoline, this, 1); + } + + + return OK; + + default: + // see if the parent class can make any use of it + ret = CDev::ioctl(filp, cmd, arg); + break; + } + + return ret; +} + +int +PCA9685::info() +{ + int ret = OK; + + if (is_running()) { + warnx("Driver is running, mode: %u", _mode); + } else { + warnx("Driver started but not running"); + } + + return ret; +} + +void +PCA9685::i2cpwm_trampoline(void *arg) +{ + PCA9685 *i2cpwm = reinterpret_cast<PCA9685 *>(arg); + + i2cpwm->i2cpwm(); +} + +/** + * Main loop function + */ +void +PCA9685::i2cpwm() +{ + if (_mode == IOX_MODE_TEST_OUT) { + setPin(0, PCA9685_PWMCENTER); + _should_run = true; + } else if (_mode == IOX_MODE_OFF) { + _should_run = false; + } else { + if (!_mode_on_initialized) { + /* Subscribe to actuator control 2 (payload group for gimbal) */ + _actuator_controls_sub = orb_subscribe(ORB_ID(actuator_controls_2)); + /* set the uorb update interval lower than the driver pwm interval */ + orb_set_interval(_actuator_controls_sub, 1000.0f / PCA9685_PWMFREQ - 5); + + _mode_on_initialized = true; + } + + /* Read the servo setpoints from the actuator control topics (gimbal) */ + bool updated; + orb_check(_actuator_controls_sub, &updated); + if (updated) { + orb_copy(ORB_ID(actuator_controls_2), _actuator_controls_sub, &_actuator_controls); + for (int i = 0; i < NUM_ACTUATOR_CONTROLS; i++) { + /* Scale the controls to PWM, first multiply by pi to get rad, + * the control[i] values are on the range -1 ... 1 */ + uint16_t new_value = PCA9685_PWMCENTER + + (_actuator_controls.control[i] * M_PI_F * PCA9685_SCALE); + debug("%d: current: %u, new %u, control %.2f", i, _current_values[i], new_value, + (double)_actuator_controls.control[i]); + if (new_value != _current_values[i] && + isfinite(new_value) && + new_value >= PCA9685_PWMMIN && + new_value <= PCA9685_PWMMAX) { + /* This value was updated, send the command to adjust the PWM value */ + setPin(i, new_value); + _current_values[i] = new_value; + } + } + } + _should_run = true; + } + + // check if any activity remains, else stop + if (!_should_run) { + _running = false; + return; + } + + // re-queue ourselves to run again later + _running = true; + work_queue(LPWORK, &_work, (worker_t)&PCA9685::i2cpwm_trampoline, this, _i2cpwm_interval); +} + +int +PCA9685::setPWM(uint8_t num, uint16_t on, uint16_t off) +{ + int ret; + /* convert to correct message */ + _msg[0] = LED0_ON_L + 4 * num; + _msg[1] = on; + _msg[2] = on >> 8; + _msg[3] = off; + _msg[4] = off >> 8; + + /* try i2c transfer */ + ret = transfer(_msg, 5, nullptr, 0); + + if (OK != ret) { + perf_count(_comms_errors); + log("i2c::transfer returned %d", ret); + } + + return ret; +} + +int +PCA9685::setPin(uint8_t num, uint16_t val, bool invert) +{ + // Clamp value between 0 and 4095 inclusive. + if (val > 4095) { + val = 4095; + } + if (invert) { + if (val == 0) { + // Special value for signal fully on. + return setPWM(num, 4096, 0); + } else if (val == 4095) { + // Special value for signal fully off. + return setPWM(num, 0, 4096); + } else { + return setPWM(num, 0, 4095-val); + } + } else { + if (val == 4095) { + // Special value for signal fully on. + return setPWM(num, 4096, 0); + } else if (val == 0) { + // Special value for signal fully off. + return setPWM(num, 0, 4096); + } else { + return setPWM(num, 0, val); + } + } + + return ERROR; +} + +int +PCA9685::setPWMFreq(float freq) +{ + int ret = OK; + freq *= 0.9f; /* Correct for overshoot in the frequency setting (see issue + https://github.com/adafruit/Adafruit-PWM-Servo-Driver-Library/issues/11). */ + float prescaleval = 25000000; + prescaleval /= 4096; + prescaleval /= freq; + prescaleval -= 1; + uint8_t prescale = uint8_t(prescaleval + 0.5f); //implicit floor() + uint8_t oldmode; + ret = read8(PCA9685_MODE1, oldmode); + if (ret != OK) { + return ret; + } + uint8_t newmode = (oldmode&0x7F) | 0x10; // sleep + + ret = write8(PCA9685_MODE1, newmode); // go to sleep + if (ret != OK) { + return ret; + } + ret = write8(PCA9685_PRESCALE, prescale); // set the prescaler + if (ret != OK) { + return ret; + } + ret = write8(PCA9685_MODE1, oldmode); + if (ret != OK) { + return ret; + } + + usleep(5000); //5ms delay (from arduino driver) + + ret = write8(PCA9685_MODE1, oldmode | 0xa1); // This sets the MODE1 register to turn on auto increment. + if (ret != OK) { + return ret; + } + + return ret; +} + +/* Wrapper to read a byte from addr */ +int +PCA9685::read8(uint8_t addr, uint8_t &value) +{ + int ret = OK; + + /* send addr */ + ret = transfer(&addr, sizeof(addr), nullptr, 0); + if (ret != OK) { + goto fail_read; + } + + /* get value */ + ret = transfer(nullptr, 0, &value, 1); + if (ret != OK) { + goto fail_read; + } + + return ret; + +fail_read: + perf_count(_comms_errors); + log("i2c::transfer returned %d", ret); + + return ret; +} + +int PCA9685::reset(void) { + warnx("resetting"); + return write8(PCA9685_MODE1, 0x0); +} + +/* Wrapper to wite a byte to addr */ +int +PCA9685::write8(uint8_t addr, uint8_t value) { + int ret = OK; + _msg[0] = addr; + _msg[1] = value; + /* send addr and value */ + ret = transfer(_msg, 2, nullptr, 0); + if (ret != OK) { + perf_count(_comms_errors); + log("i2c::transfer returned %d", ret); + } + return ret; +} + +void +pca9685_usage() +{ + warnx("missing command: try 'start', 'test', 'stop', 'info'"); + warnx("options:"); + warnx(" -b i2cbus (%d)", PX4_I2C_BUS_EXPANSION); + warnx(" -a addr (0x%x)", ADDR); +} + +int +pca9685_main(int argc, char *argv[]) +{ + int i2cdevice = -1; + int i2caddr = ADDR; // 7bit + + int ch; + + // jump over start/off/etc and look at options first + while ((ch = getopt(argc, argv, "a:b:")) != EOF) { + switch (ch) { + case 'a': + i2caddr = strtol(optarg, NULL, 0); + break; + + case 'b': + i2cdevice = strtol(optarg, NULL, 0); + break; + + default: + pca9685_usage(); + exit(0); + } + } + + if (optind >= argc) { + pca9685_usage(); + exit(1); + } + + const char *verb = argv[optind]; + + int fd; + int ret; + + if (!strcmp(verb, "start")) { + if (g_pca9685 != nullptr) { + errx(1, "already started"); + } + + if (i2cdevice == -1) { + // try the external bus first + i2cdevice = PX4_I2C_BUS_EXPANSION; + g_pca9685 = new PCA9685(PX4_I2C_BUS_EXPANSION, i2caddr); + + if (g_pca9685 != nullptr && OK != g_pca9685->init()) { + delete g_pca9685; + g_pca9685 = nullptr; + } + + if (g_pca9685 == nullptr) { + errx(1, "init failed"); + } + } + + if (g_pca9685 == nullptr) { + g_pca9685 = new PCA9685(i2cdevice, i2caddr); + + if (g_pca9685 == nullptr) { + errx(1, "new failed"); + } + + if (OK != g_pca9685->init()) { + delete g_pca9685; + g_pca9685 = nullptr; + errx(1, "init failed"); + } + } + fd = open(PCA9685_DEVICE_PATH, 0); + if (fd == -1) { + errx(1, "Unable to open " PCA9685_DEVICE_PATH); + } + ret = ioctl(fd, IOX_SET_MODE, (unsigned long)IOX_MODE_ON); + close(fd); + + + exit(0); + } + + // need the driver past this point + if (g_pca9685 == nullptr) { + warnx("not started, run pca9685 start"); + exit(1); + } + + if (!strcmp(verb, "info")) { + g_pca9685->info(); + exit(0); + } + + if (!strcmp(verb, "reset")) { + g_pca9685->reset(); + exit(0); + } + + + if (!strcmp(verb, "test")) { + fd = open(PCA9685_DEVICE_PATH, 0); + + if (fd == -1) { + errx(1, "Unable to open " PCA9685_DEVICE_PATH); + } + + ret = ioctl(fd, IOX_SET_MODE, (unsigned long)IOX_MODE_TEST_OUT); + + close(fd); + exit(ret); + } + + if (!strcmp(verb, "stop")) { + fd = open(PCA9685_DEVICE_PATH, 0); + + if (fd == -1) { + errx(1, "Unable to open " PCA9685_DEVICE_PATH); + } + + ret = ioctl(fd, IOX_SET_MODE, (unsigned long)IOX_MODE_OFF); + close(fd); + + // wait until we're not running any more + for (unsigned i = 0; i < 15; i++) { + if (!g_pca9685->is_running()) { + break; + } + + usleep(50000); + printf("."); + fflush(stdout); + } + printf("\n"); + fflush(stdout); + + if (!g_pca9685->is_running()) { + delete g_pca9685; + g_pca9685= nullptr; + warnx("stopped, exiting"); + exit(0); + } else { + warnx("stop failed."); + exit(1); + } + } + + pca9685_usage(); + exit(0); +} diff --git a/src/drivers/px4flow/px4flow.cpp b/src/drivers/px4flow/px4flow.cpp index f214b5964..60ad3c1af 100644 --- a/src/drivers/px4flow/px4flow.cpp +++ b/src/drivers/px4flow/px4flow.cpp @@ -37,7 +37,7 @@ * * Driver for the PX4FLOW module connected via I2C. */ - + #include <nuttx/config.h> #include <drivers/device/i2c.h> @@ -68,7 +68,7 @@ #include <uORB/uORB.h> #include <uORB/topics/subsystem_info.h> -//#include <uORB/topics/optical_flow.h> +#include <uORB/topics/optical_flow.h> #include <board_config.h> @@ -80,7 +80,7 @@ /* PX4FLOW Registers addresses */ #define PX4FLOW_REG 0x00 /* Measure Register */ -#define PX4FLOW_CONVERSION_INTERVAL 8000 /* 8ms 125Hz +#define PX4FLOW_CONVERSION_INTERVAL 8000 /* 8ms 125Hz */ /* oddly, ERROR is not defined for c++ */ #ifdef ERROR @@ -115,17 +115,17 @@ class PX4FLOW : public device::I2C public: PX4FLOW(int bus = PX4FLOW_BUS, int address = I2C_FLOW_ADDRESS); virtual ~PX4FLOW(); - + virtual int init(); - + virtual ssize_t read(struct file *filp, char *buffer, size_t buflen); virtual int ioctl(struct file *filp, int cmd, unsigned long arg); - + /** * Diagnostics - print some basic information about the driver. */ void print_info(); - + protected: virtual int probe(); @@ -136,13 +136,13 @@ private: bool _sensor_ok; int _measure_ticks; bool _collect_phase; - + orb_advert_t _px4flow_topic; perf_counter_t _sample_perf; perf_counter_t _comms_errors; perf_counter_t _buffer_overflows; - + /** * Test whether the device supported by the driver is present at a * specific address. @@ -151,7 +151,7 @@ private: * @return True if the device is present. */ int probe_address(uint8_t address); - + /** * Initialise the automatic measurement state machine and start it. * @@ -159,12 +159,12 @@ private: * to make it more aggressive about resetting the bus in case of errors. */ void start(); - + /** * Stop the automatic measurement state machine. */ void stop(); - + /** * Perform a poll cycle; collect from the previous measurement * and start a new one. @@ -179,8 +179,8 @@ private: * @param arg Instance pointer for the driver that is polling. */ static void cycle_trampoline(void *arg); - - + + }; /* @@ -201,7 +201,7 @@ PX4FLOW::PX4FLOW(int bus, int address) : { // enable debug() calls _debug_enabled = true; - + // work_cancel in the dtor will explode if we don't do this... memset(&_work, 0, sizeof(_work)); } @@ -226,13 +226,13 @@ PX4FLOW::init() goto out; /* allocate basic report buffers */ - _reports = new RingBuffer(2, sizeof(px4flow_report)); + _reports = new RingBuffer(2, sizeof(struct optical_flow_s)); if (_reports == nullptr) goto out; /* get a publish handle on the px4flow topic */ - struct px4flow_report zero_report; + struct optical_flow_s zero_report; memset(&zero_report, 0, sizeof(zero_report)); _px4flow_topic = orb_advertise(ORB_ID(optical_flow), &zero_report); @@ -323,24 +323,24 @@ PX4FLOW::ioctl(struct file *filp, int cmd, unsigned long arg) /* lower bound is mandatory, upper bound is a sanity check */ if ((arg < 1) || (arg > 100)) return -EINVAL; - + irqstate_t flags = irqsave(); if (!_reports->resize(arg)) { irqrestore(flags); return -ENOMEM; } irqrestore(flags); - + return OK; } case SENSORIOCGQUEUEDEPTH: return _reports->size(); - + case SENSORIOCRESET: /* XXX implement this */ return -EINVAL; - + default: /* give it to the superclass */ return I2C::ioctl(filp, cmd, arg); @@ -350,8 +350,8 @@ PX4FLOW::ioctl(struct file *filp, int cmd, unsigned long arg) ssize_t PX4FLOW::read(struct file *filp, char *buffer, size_t buflen) { - unsigned count = buflen / sizeof(struct px4flow_report); - struct px4flow_report *rbuf = reinterpret_cast<struct px4flow_report *>(buffer); + unsigned count = buflen / sizeof(struct optical_flow_s); + struct optical_flow_s *rbuf = reinterpret_cast<struct optical_flow_s *>(buffer); int ret = 0; /* buffer must be large enough */ @@ -425,7 +425,7 @@ PX4FLOW::measure() return ret; } ret = OK; - + return ret; } @@ -433,14 +433,14 @@ int PX4FLOW::collect() { int ret = -EIO; - + /* read from the sensor */ uint8_t val[22] = {0, 0,0, 0,0, 0,0, 0,0, 0,0, 0,0, 0,0, 0,0, 0,0, 0,0, 0}; - + perf_begin(_sample_perf); - + ret = transfer(nullptr, 0, &val[0], 22); - + if (ret < 0) { log("error reading from sensor: %d", ret); @@ -448,7 +448,7 @@ PX4FLOW::collect() perf_end(_sample_perf); return ret; } - + // f.frame_count = val[1] << 8 | val[0]; // f.pixel_flow_x_sum= val[3] << 8 | val[2]; // f.pixel_flow_y_sum= val[5] << 8 | val[4]; @@ -466,7 +466,7 @@ PX4FLOW::collect() int16_t flowcy = val[9] << 8 | val[8]; int16_t gdist = val[21] << 8 | val[20]; - struct px4flow_report report; + struct optical_flow_s report; report.flow_comp_x_m = float(flowcx)/1000.0f; report.flow_comp_y_m = float(flowcy)/1000.0f; report.flow_raw_x= val[3] << 8 | val[2]; @@ -503,7 +503,7 @@ PX4FLOW::start() /* schedule a cycle to start things */ work_queue(HPWORK, &_work, (worker_t)&PX4FLOW::cycle_trampoline, this, 1); - + /* notify about state change */ struct subsystem_info_s info = { true, @@ -644,7 +644,7 @@ start() fail: - if (g_dev != nullptr) + if (g_dev != nullptr) { delete g_dev; g_dev = nullptr; @@ -678,7 +678,7 @@ void stop() void test() { - struct px4flow_report report; + struct optical_flow_s report; ssize_t sz; int ret; @@ -777,7 +777,7 @@ px4flow_main(int argc, char *argv[]) */ if (!strcmp(argv[1], "start")) px4flow::start(); - + /* * Stop the driver */ diff --git a/src/drivers/px4fmu/fmu.cpp b/src/drivers/px4fmu/fmu.cpp index 82977a032..122a3cd17 100644 --- a/src/drivers/px4fmu/fmu.cpp +++ b/src/drivers/px4fmu/fmu.cpp @@ -1272,7 +1272,9 @@ PX4FMU::write(file *filp, const char *buffer, size_t len) memcpy(values, buffer, count * 2); for (uint8_t i = 0; i < count; i++) { - up_pwm_servo_set(i, values[i]); + if (values[i] != PWM_IGNORE_THIS_CHANNEL) { + up_pwm_servo_set(i, values[i]); + } } return count * 2; diff --git a/src/drivers/px4io/px4io.cpp b/src/drivers/px4io/px4io.cpp index 32069cf09..3fdb1dd1f 100644 --- a/src/drivers/px4io/px4io.cpp +++ b/src/drivers/px4io/px4io.cpp @@ -1175,6 +1175,14 @@ PX4IO::io_set_arming_state() clear |= PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE; } + // XXX this is for future support in the commander + // but can be removed if unneeded + // if (armed.termination_failsafe) { + // set |= PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE; + // } else { + // clear |= PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE; + // } + if (armed.ready_to_arm) { set |= PX4IO_P_SETUP_ARMING_IO_ARM_OK; @@ -1968,7 +1976,7 @@ PX4IO::print_status(bool extended_status) printf("actuators"); for (unsigned i = 0; i < _max_actuators; i++) - printf(" %u", io_reg_get(PX4IO_PAGE_ACTUATORS, i)); + printf(" %hi", int16_t(io_reg_get(PX4IO_PAGE_ACTUATORS, i))); printf("\n"); printf("servos"); @@ -2038,7 +2046,8 @@ PX4IO::print_status(bool extended_status) ((arming & PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK) ? " INAIR_RESTART_OK" : ""), ((arming & PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE) ? " ALWAYS_PWM_ENABLE" : ""), ((arming & PX4IO_P_SETUP_ARMING_LOCKDOWN) ? " LOCKDOWN" : ""), - ((arming & PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE) ? " FORCE_FAILSAFE" : "") + ((arming & PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE) ? " FORCE_FAILSAFE" : ""), + ((arming & PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE) ? " TERM_FAILSAFE" : "") ); #ifdef CONFIG_ARCH_BOARD_PX4FMU_V1 printf("rates 0x%04x default %u alt %u relays 0x%04x\n", @@ -2262,6 +2271,17 @@ PX4IO::ioctl(file * filep, int cmd, unsigned long arg) } break; + case PWM_SERVO_SET_TERMINATION_FAILSAFE: + /* if failsafe occurs, do not allow the system to recover */ + if (arg == 0) { + /* clear termination failsafe flag */ + ret = io_reg_modify(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_ARMING, PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE, 0); + } else { + /* set termination failsafe flag */ + ret = io_reg_modify(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_ARMING, 0, PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE); + } + break; + case DSM_BIND_START: /* only allow DSM2, DSM-X and DSM-X with more than 7 channels */ diff --git a/src/drivers/sf0x/sf0x.cpp b/src/drivers/sf0x/sf0x.cpp index bca1715fa..d382d08d0 100644 --- a/src/drivers/sf0x/sf0x.cpp +++ b/src/drivers/sf0x/sf0x.cpp @@ -520,11 +520,9 @@ SF0X::collect() /* clear buffer if last read was too long ago */ uint64_t read_elapsed = hrt_elapsed_time(&_last_read); + /* timed out - retry */ 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 */ @@ -550,18 +548,19 @@ SF0X::collect() return -EAGAIN; } - /* we did increment the index to the next position already, so just add the additional fields */ - _linebuf_index += (ret - 1); + /* let the write pointer point to the next free entry */ + _linebuf_index += ret; _last_read = hrt_absolute_time(); - if (_linebuf_index < 1) { - /* we need at least the two end bytes to make sense of this string */ + /* require a reasonable amount of minimum bytes */ + if (_linebuf_index < 6) { + /* we need at this format: x.xx\r\n */ return -EAGAIN; - } else if (_linebuf[_linebuf_index - 1] != '\r' || _linebuf[_linebuf_index] != '\n') { + } else if (_linebuf[_linebuf_index - 2] != '\r' || _linebuf[_linebuf_index - 1] != '\n') { - if (_linebuf_index >= readlen - 1) { + if (_linebuf_index == readlen) { /* we have a full buffer, but no line ending - abort */ _linebuf_index = 0; perf_count(_comms_errors); @@ -577,9 +576,7 @@ SF0X::collect() bool valid; /* enforce line ending */ - unsigned lend = (_linebuf_index < (sizeof(_linebuf) - 1)) ? _linebuf_index : (sizeof(_linebuf) - 1); - - _linebuf[lend] = '\0'; + _linebuf[_linebuf_index] = '\0'; if (_linebuf[0] == '-' && _linebuf[1] == '-' && _linebuf[2] == '.') { si_units = -1.0f; @@ -591,14 +588,16 @@ SF0X::collect() valid = false; /* wipe out partially read content from last cycle(s), check for dot */ - for (unsigned i = 0; i < (lend - 2); i++) { + for (unsigned i = 0; i < (_linebuf_index - 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)); + /* wipe out any partial measurements */ + for (unsigned j = 0; j <= i; j++) { + _linebuf[j] = ' '; + } } - if (_linebuf[i] == '.') { + /* we need a digit before the dot and a dot for a valid number */ + if (i > 0 && ((_linebuf[i - 1] >= '0') && (_linebuf[i - 1] <= '9')) && (_linebuf[i] == '.')) { valid = true; } } @@ -606,7 +605,7 @@ SF0X::collect() if (valid) { si_units = strtod(_linebuf, &end); - /* we require at least 3 characters for a valid number */ + /* we require at least four characters for a valid number */ if (end > _linebuf + 3) { valid = true; } else { @@ -616,7 +615,7 @@ SF0X::collect() } } - debug("val (float): %8.4f, raw: %s, valid: %s\n", (double)si_units, _linebuf, ((valid) ? "OK" : "NO")); + debug("val (float): %8.4f, raw: %s, valid: %s", (double)si_units, _linebuf, ((valid) ? "OK" : "NO")); /* done with this chunk, resetting - even if invalid */ _linebuf_index = 0; @@ -708,12 +707,12 @@ SF0X::cycle() int collect_ret = collect(); if (collect_ret == -EAGAIN) { - /* reschedule to grab the missing bits, time to transmit 10 bytes @9600 bps */ + /* reschedule to grab the missing bits, time to transmit 8 bytes @ 9600 bps */ work_queue(HPWORK, &_work, (worker_t)&SF0X::cycle_trampoline, this, - USEC2TICK(1100)); + USEC2TICK(1042 * 8)); return; } diff --git a/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp b/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp index 46db788a6..926a8db2a 100644 --- a/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp +++ b/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp @@ -169,7 +169,7 @@ float ECL_PitchController::control_bodyrate(float roll, float pitch, if (!lock_integrator && _k_i > 0.0f && airspeed > 0.5f * airspeed_min) { - float id = _rate_error * dt; + float id = _rate_error * dt * scaler; /* * anti-windup: do not allow integrator to increase if actuator is at limit @@ -190,7 +190,9 @@ float ECL_PitchController::control_bodyrate(float roll, float pitch, float integrator_constrained = math::constrain(_integrator * _k_i, -_integrator_max, _integrator_max); /* Apply PI rate controller and store non-limited output */ - _last_output = (_bodyrate_setpoint * _k_ff +_rate_error * _k_p + integrator_constrained) * scaler * scaler; //scaler is proportional to 1/airspeed + _last_output = _bodyrate_setpoint * _k_ff * scaler + + _rate_error * _k_p * scaler * scaler + + integrator_constrained; //scaler is proportional to 1/airspeed // warnx("pitch: _integrator: %.4f, _integrator_max: %.4f, airspeed %.4f, _k_i %.4f, _k_p: %.4f", (double)_integrator, (double)_integrator_max, (double)airspeed, (double)_k_i, (double)_k_p); // warnx("roll: _last_output %.4f", (double)_last_output); return math::constrain(_last_output, -1.0f, 1.0f); diff --git a/src/lib/ecl/attitude_fw/ecl_roll_controller.cpp b/src/lib/ecl/attitude_fw/ecl_roll_controller.cpp index 9894a34d7..94bd26f03 100644 --- a/src/lib/ecl/attitude_fw/ecl_roll_controller.cpp +++ b/src/lib/ecl/attitude_fw/ecl_roll_controller.cpp @@ -135,7 +135,7 @@ float ECL_RollController::control_bodyrate(float pitch, if (!lock_integrator && _k_i > 0.0f && airspeed > 0.5f * airspeed_min) { - float id = _rate_error * dt; + float id = _rate_error * dt * scaler; /* * anti-windup: do not allow integrator to increase if actuator is at limit @@ -157,7 +157,9 @@ float ECL_RollController::control_bodyrate(float pitch, //warnx("roll: _integrator: %.4f, _integrator_max: %.4f", (double)_integrator, (double)_integrator_max); /* Apply PI rate controller and store non-limited output */ - _last_output = (_bodyrate_setpoint * _k_ff + _rate_error * _k_p + integrator_constrained) * scaler * scaler; //scaler is proportional to 1/airspeed + _last_output = _bodyrate_setpoint * _k_ff * scaler + + _rate_error * _k_p * scaler * scaler + + integrator_constrained; //scaler is proportional to 1/airspeed return math::constrain(_last_output, -1.0f, 1.0f); } diff --git a/src/lib/external_lgpl/tecs/tecs.cpp b/src/lib/external_lgpl/tecs/tecs.cpp index a57a0481a..023bd71bf 100644 --- a/src/lib/external_lgpl/tecs/tecs.cpp +++ b/src/lib/external_lgpl/tecs/tecs.cpp @@ -238,7 +238,7 @@ void TECS::_update_height_demand(float demand, float state) _hgt_dem_adj = demand;//0.025f * demand + 0.975f * _hgt_dem_adj_last; _hgt_dem_adj_last = _hgt_dem_adj; - _hgt_rate_dem = (_hgt_dem_adj-state)*_heightrate_p; + _hgt_rate_dem = (_hgt_dem_adj-state)*_heightrate_p + _heightrate_ff * (_hgt_dem_adj - _hgt_dem_adj_last)/_DT; // Limit height rate of change if (_hgt_rate_dem > _maxClimbRate) { _hgt_rate_dem = _maxClimbRate; @@ -252,6 +252,11 @@ void TECS::_update_height_demand(float demand, float state) void TECS::_detect_underspeed(void) { + if (!_detect_underspeed_enabled) { + _underspeed = false; + return; + } + if (((_integ5_state < _TASmin * 0.9f) && (_throttle_dem >= _THRmaxf * 0.95f)) || ((_integ3_state < _hgt_dem_adj) && _underspeed)) { _underspeed = true; diff --git a/src/lib/external_lgpl/tecs/tecs.h b/src/lib/external_lgpl/tecs/tecs.h index bcc2d90e5..8ac31de6f 100644 --- a/src/lib/external_lgpl/tecs/tecs.h +++ b/src/lib/external_lgpl/tecs/tecs.h @@ -47,6 +47,7 @@ public: _rollComp(0.0f), _spdWeight(0.5f), _heightrate_p(0.0f), + _heightrate_ff(0.0f), _speedrate_p(0.0f), _throttle_dem(0.0f), _pitch_dem(0.0f), @@ -66,6 +67,9 @@ public: _hgt_dem_prev(0.0f), _TAS_dem_adj(0.0f), _STEdotErrLast(0.0f), + _underspeed(false), + _detect_underspeed_enabled(true), + _badDescent(false), _climbOutDem(false), _SPE_dem(0.0f), _SKE_dem(0.0f), @@ -217,10 +221,18 @@ public: _heightrate_p = heightrate_p; } + void set_heightrate_ff(float heightrate_ff) { + _heightrate_ff = heightrate_ff; + } + void set_speedrate_p(float speedrate_p) { _speedrate_p = speedrate_p; } + void set_detect_underspeed_enabled(bool enabled) { + _detect_underspeed_enabled = enabled; + } + private: struct tecs_state _tecs_state; @@ -249,6 +261,7 @@ private: float _rollComp; float _spdWeight; float _heightrate_p; + float _heightrate_ff; float _speedrate_p; // throttle demand in the range from 0.0 to 1.0 @@ -323,6 +336,9 @@ private: // Underspeed condition bool _underspeed; + // Underspeed detection enabled + bool _detect_underspeed_enabled; + // Bad descent condition caused by unachievable airspeed demand bool _badDescent; diff --git a/src/lib/launchdetection/CatapultLaunchMethod.cpp b/src/lib/launchdetection/CatapultLaunchMethod.cpp index c555a0a69..2ea1c414b 100644 --- a/src/lib/launchdetection/CatapultLaunchMethod.cpp +++ b/src/lib/launchdetection/CatapultLaunchMethod.cpp @@ -49,9 +49,11 @@ CatapultLaunchMethod::CatapultLaunchMethod(SuperBlock *parent) : SuperBlock(parent, "CAT"), last_timestamp(hrt_absolute_time()), integrator(0.0f), - launchDetected(false), - threshold_accel(this, "A"), - threshold_time(this, "T") + state(LAUNCHDETECTION_RES_NONE), + thresholdAccel(this, "A"), + thresholdTime(this, "T"), + motorDelay(this, "MDEL"), + pitchMaxPreThrottle(this, "PMAX") { } @@ -65,34 +67,66 @@ void CatapultLaunchMethod::update(float accel_x) float dt = (float)hrt_elapsed_time(&last_timestamp) * 1e-6f; last_timestamp = hrt_absolute_time(); - if (accel_x > threshold_accel.get()) { - integrator += accel_x * dt; -// warnx("*** integrator %.3f, threshold_accel %.3f, threshold_time %.3f, accel_x %.3f, dt %.3f", -// (double)integrator, (double)threshold_accel.get(), (double)threshold_time.get(), (double)accel_x, (double)dt); - if (integrator > threshold_accel.get() * threshold_time.get()) { - launchDetected = true; + switch (state) { + case LAUNCHDETECTION_RES_NONE: + /* Detect a acceleration that is longer and stronger as the minimum given by the params */ + if (accel_x > thresholdAccel.get()) { + integrator += dt; + if (integrator > thresholdTime.get()) { + if (motorDelay.get() > 0.0f) { + state = LAUNCHDETECTION_RES_DETECTED_ENABLECONTROL; + warnx("Launch detected: state: enablecontrol, waiting %.2fs until using full" + " throttle", (double)motorDelay.get()); + } else { + /* No motor delay set: go directly to enablemotors state */ + state = LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS; + warnx("Launch detected: state: enablemotors (delay not activated)"); + } + } + } else { + /* reset */ + reset(); } + break; + + case LAUNCHDETECTION_RES_DETECTED_ENABLECONTROL: + /* Vehicle is currently controlling attitude but not with full throttle. Waiting undtil delay is + * over to allow full throttle */ + motorDelayCounter += dt; + if (motorDelayCounter > motorDelay.get()) { + warnx("Launch detected: state enablemotors"); + state = LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS; + } + break; + + default: + break; - } else { -// warnx("integrator %.3f, threshold_accel %.3f, threshold_time %.3f, accel_x %.3f, dt %.3f", -// (double)integrator, (double)threshold_accel.get(), (double)threshold_time.get(), (double)accel_x, (double)dt); - /* reset integrator */ - integrator = 0.0f; - launchDetected = false; } } -bool CatapultLaunchMethod::getLaunchDetected() +LaunchDetectionResult CatapultLaunchMethod::getLaunchDetected() const { - return launchDetected; + return state; } void CatapultLaunchMethod::reset() { integrator = 0.0f; - launchDetected = false; + motorDelayCounter = 0.0f; + state = LAUNCHDETECTION_RES_NONE; +} + +float CatapultLaunchMethod::getPitchMax(float pitchMaxDefault) { + /* If motor is turned on do not impose the extra limit on maximum pitch */ + if (state == LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS) { + return pitchMaxDefault; + } else { + return pitchMaxPreThrottle.get(); + } + } } diff --git a/src/lib/launchdetection/CatapultLaunchMethod.h b/src/lib/launchdetection/CatapultLaunchMethod.h index 23757f6f3..321dfb1de 100644 --- a/src/lib/launchdetection/CatapultLaunchMethod.h +++ b/src/lib/launchdetection/CatapultLaunchMethod.h @@ -57,16 +57,23 @@ public: ~CatapultLaunchMethod(); void update(float accel_x); - bool getLaunchDetected(); + LaunchDetectionResult getLaunchDetected() const; void reset(); + float getPitchMax(float pitchMaxDefault); private: hrt_abstime last_timestamp; float integrator; - bool launchDetected; + float motorDelayCounter; - control::BlockParamFloat threshold_accel; - control::BlockParamFloat threshold_time; + LaunchDetectionResult state; + + control::BlockParamFloat thresholdAccel; + control::BlockParamFloat thresholdTime; + control::BlockParamFloat motorDelay; + control::BlockParamFloat pitchMaxPreThrottle; /**< Upper pitch limit before throttle is turned on. + Can be used to make sure that the AC does not climb + too much while attached to a bungee */ }; diff --git a/src/lib/launchdetection/LaunchDetector.cpp b/src/lib/launchdetection/LaunchDetector.cpp index 3bf47bbb0..52f5c3257 100644 --- a/src/lib/launchdetection/LaunchDetector.cpp +++ b/src/lib/launchdetection/LaunchDetector.cpp @@ -46,6 +46,7 @@ namespace launchdetection LaunchDetector::LaunchDetector() : SuperBlock(NULL, "LAUN"), + activeLaunchDetectionMethodIndex(-1), launchdetection_on(this, "ALL_ON"), throttlePreTakeoff(this, "THR_PRE") { @@ -65,7 +66,14 @@ LaunchDetector::~LaunchDetector() void LaunchDetector::reset() { /* Reset all detectors */ - launchMethods[0]->reset(); + for (uint8_t i = 0; i < sizeof(launchMethods)/sizeof(LaunchMethod); i++) { + launchMethods[i]->reset(); + } + + /* Reset active launchdetector */ + activeLaunchDetectionMethodIndex = -1; + + } void LaunchDetector::update(float accel_x) @@ -77,17 +85,44 @@ void LaunchDetector::update(float accel_x) } } -bool LaunchDetector::getLaunchDetected() +LaunchDetectionResult LaunchDetector::getLaunchDetected() { if (launchdetection_on.get() == 1) { - for (uint8_t i = 0; i < sizeof(launchMethods)/sizeof(LaunchMethod); i++) { - if(launchMethods[i]->getLaunchDetected()) { - return true; + if (activeLaunchDetectionMethodIndex < 0) { + /* None of the active launchmethods has detected a launch, check all launchmethods */ + for (uint8_t i = 0; i < sizeof(launchMethods)/sizeof(LaunchMethod); i++) { + if(launchMethods[i]->getLaunchDetected() != LAUNCHDETECTION_RES_NONE) { + warnx("selecting launchmethod %d", i); + activeLaunchDetectionMethodIndex = i; // from now on only check this method + return launchMethods[i]->getLaunchDetected(); + } } + } else { + return launchMethods[activeLaunchDetectionMethodIndex]->getLaunchDetected(); } } - return false; + return LAUNCHDETECTION_RES_NONE; } +float LaunchDetector::getPitchMax(float pitchMaxDefault) { + if (!launchdetection_on.get()) { + return pitchMaxDefault; + } + + /* if a lauchdetectionmethod is active or only one exists return the pitch limit from this method, + * otherwise use the default limit */ + if (activeLaunchDetectionMethodIndex < 0) { + if (sizeof(launchMethods)/sizeof(LaunchMethod) > 1) { + return pitchMaxDefault; + } else { + return launchMethods[0]->getPitchMax(pitchMaxDefault); + } + } else { + return launchMethods[activeLaunchDetectionMethodIndex]->getPitchMax(pitchMaxDefault); + } + +} + + } diff --git a/src/lib/launchdetection/LaunchDetector.h b/src/lib/launchdetection/LaunchDetector.h index 1a214b66e..4215b49d2 100644 --- a/src/lib/launchdetection/LaunchDetector.h +++ b/src/lib/launchdetection/LaunchDetector.h @@ -59,14 +59,23 @@ public: void reset(); void update(float accel_x); - bool getLaunchDetected(); + LaunchDetectionResult getLaunchDetected(); bool launchDetectionEnabled() { return (bool)launchdetection_on.get(); }; float getThrottlePreTakeoff() {return throttlePreTakeoff.get(); } + /* Returns a maximum pitch in deg. Different launch methods may impose upper pitch limits during launch */ + float getPitchMax(float pitchMaxDefault); + // virtual bool getLaunchDetected(); protected: private: + int activeLaunchDetectionMethodIndex; /**< holds a index to the launchMethod in the array launchMethods + which detected a Launch. If no launchMethod has detected a launch yet the + value is -1. Once one launchMetthod has detected a launch only this + method is checked for further adavancing in the state machine (e.g. when + to power up the motors) */ + LaunchMethod* launchMethods[1]; control::BlockParamInt launchdetection_on; control::BlockParamFloat throttlePreTakeoff; diff --git a/src/lib/launchdetection/LaunchMethod.h b/src/lib/launchdetection/LaunchMethod.h index e04467f6a..8b5220cb3 100644 --- a/src/lib/launchdetection/LaunchMethod.h +++ b/src/lib/launchdetection/LaunchMethod.h @@ -44,13 +44,27 @@ namespace launchdetection { +enum LaunchDetectionResult { + LAUNCHDETECTION_RES_NONE = 0, /**< No launch has been detected */ + LAUNCHDETECTION_RES_DETECTED_ENABLECONTROL = 1, /**< Launch has been detected, the controller should + control the attitude. However any motors should not throttle + up and still be set to 'throttlePreTakeoff'. + For instance this is used to have a delay for the motor + when launching a fixed wing aircraft from a bungee */ + LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS = 2 /**< Launch has been detected, teh controller should control + attitude and also throttle up the motors. */ +}; + class LaunchMethod { public: virtual void update(float accel_x) = 0; - virtual bool getLaunchDetected() = 0; + virtual LaunchDetectionResult getLaunchDetected() const = 0; virtual void reset() = 0; + /* Returns a upper pitch limit if required, otherwise returns pitchMaxDefault */ + virtual float getPitchMax(float pitchMaxDefault) = 0; + protected: private: }; diff --git a/src/lib/launchdetection/launchdetection_params.c b/src/lib/launchdetection/launchdetection_params.c index 8df8c696c..e3aa7ab2d 100644 --- a/src/lib/launchdetection/launchdetection_params.c +++ b/src/lib/launchdetection/launchdetection_params.c @@ -78,6 +78,31 @@ PARAM_DEFINE_FLOAT(LAUN_CAT_A, 30.0f); PARAM_DEFINE_FLOAT(LAUN_CAT_T, 0.05f); /** + * Motor delay + * + * Delay between starting attitude control and powering up the throttle (giving throttle control to the controller) + * Before this timespan is up the throttle will be set to LAUN_THR_PRE, set to 0 to deactivate + * + * @unit seconds + * @min 0 + * @group Launch detection + */ +PARAM_DEFINE_FLOAT(LAUN_CAT_MDEL, 0.0f); + +/** + * Maximum pitch before the throttle is powered up (during motor delay phase) + * + * This is an extra limit for the maximum pitch which is imposed in the phase before the throttle turns on. + * This allows to limit the maximum pitch angle during a bungee launch (make the launch less steep). + * + * @unit deg + * @min 0 + * @max 45 + * @group Launch detection + */ +PARAM_DEFINE_FLOAT(LAUN_CAT_PMAX, 30.0f); + +/** * Throttle setting while detecting launch. * * The throttle is set to this value while the system is waiting for the take-off. diff --git a/src/modules/commander/airspeed_calibration.cpp b/src/modules/commander/airspeed_calibration.cpp index 0e58c68b6..339b11bbe 100644 --- a/src/modules/commander/airspeed_calibration.cpp +++ b/src/modules/commander/airspeed_calibration.cpp @@ -180,11 +180,13 @@ int do_airspeed_calibration(int mavlink_fd) return ERROR; } - mavlink_log_critical(mavlink_fd, "Offset of %d Pa, create airflow now!", (int)diff_pres_offset); + mavlink_log_critical(mavlink_fd, "Offset of %d Pascal", (int)diff_pres_offset); /* wait 500 ms to ensure parameter propagated through the system */ usleep(500 * 1000); + mavlink_log_critical(mavlink_fd, "Create airflow now"); + calibration_counter = 0; const unsigned maxcount = 3000; @@ -204,18 +206,18 @@ int do_airspeed_calibration(int mavlink_fd) calibration_counter++; if (fabsf(diff_pres.differential_pressure_raw_pa) < 50.0f) { - if (calibration_counter % 100 == 0) { - mavlink_log_critical(mavlink_fd, "Missing airflow! (%d, wanted: 50 Pa, #h101)", - (int)diff_pres.differential_pressure_raw_pa); + if (calibration_counter % 500 == 0) { + mavlink_log_info(mavlink_fd, "Create airflow! (%d, wanted: 50 Pa)", + (int)diff_pres.differential_pressure_raw_pa); } continue; } /* do not allow negative values */ if (diff_pres.differential_pressure_raw_pa < 0.0f) { - mavlink_log_info(mavlink_fd, "negative pressure: ERROR (%d Pa)", - (int)diff_pres.differential_pressure_raw_pa); - mavlink_log_critical(mavlink_fd, "%d Pa: swap static and dynamic ports!", (int)diff_pres.differential_pressure_raw_pa); + mavlink_log_critical(mavlink_fd, "Swap static and dynamic ports!"); + mavlink_log_info(mavlink_fd, "ERROR: Negative pressure difference detected! (%d Pa)", + (int)diff_pres.differential_pressure_raw_pa); close(diff_pres_sub); /* the user setup is wrong, wipe the calibration to force a proper re-calibration */ @@ -236,7 +238,7 @@ int do_airspeed_calibration(int mavlink_fd) mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name); return ERROR; } else { - mavlink_log_info(mavlink_fd, "positive pressure: OK (%d Pa)", + mavlink_log_info(mavlink_fd, "Positive pressure: OK (%d Pa)", (int)diff_pres.differential_pressure_raw_pa); break; } diff --git a/src/modules/commander/commander.cpp b/src/modules/commander/commander.cpp index 6c2c03070..a5a772825 100644 --- a/src/modules/commander/commander.cpp +++ b/src/modules/commander/commander.cpp @@ -129,7 +129,7 @@ extern struct system_load_s system_load; #define POSITION_TIMEOUT (2 * 1000 * 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 DL_TIMEOUT 5 * 1000* 1000 +#define DL_TIMEOUT (10 * 1000 * 1000) #define OFFBOARD_TIMEOUT 500000 #define DIFFPRESS_TIMEOUT 2000000 @@ -615,6 +615,11 @@ bool handle_command(struct vehicle_status_s *status_local, const struct safety_s case VEHICLE_CMD_PREFLIGHT_CALIBRATION: case VEHICLE_CMD_PREFLIGHT_SET_SENSOR_OFFSETS: case VEHICLE_CMD_PREFLIGHT_STORAGE: + case VEHICLE_CMD_CUSTOM_0: + case VEHICLE_CMD_CUSTOM_1: + case VEHICLE_CMD_CUSTOM_2: + case VEHICLE_CMD_PAYLOAD_PREPARE_DEPLOY: + case VEHICLE_CMD_PAYLOAD_CONTROL_DEPLOY: /* ignore commands that handled in low prio loop */ break; diff --git a/src/modules/commander/state_machine_helper.cpp b/src/modules/commander/state_machine_helper.cpp index f8589d24b..684c61a17 100644 --- a/src/modules/commander/state_machine_helper.cpp +++ b/src/modules/commander/state_machine_helper.cpp @@ -182,12 +182,19 @@ arming_state_transition(struct vehicle_status_s *status, ///< current vehicle s // Fail transition if power levels on the avionics rail // are measured but are insufficient - if (status->condition_power_input_valid && ((status->avionics_power_rail_voltage > 0.0f) && - (status->avionics_power_rail_voltage < 4.9f))) { - - mavlink_log_critical(mavlink_fd, "NOT ARMING: Avionics power low: %6.2f V.", (double)status->avionics_power_rail_voltage); - feedback_provided = true; - valid_transition = false; + if (status->condition_power_input_valid && (status->avionics_power_rail_voltage > 0.0f)) { + // Check avionics rail voltages + if (status->avionics_power_rail_voltage < 4.75f) { + mavlink_log_critical(mavlink_fd, "NOT ARMING: Avionics power low: %6.2f Volt", (double)status->avionics_power_rail_voltage); + feedback_provided = true; + valid_transition = false; + } else if (status->avionics_power_rail_voltage < 4.9f) { + mavlink_log_critical(mavlink_fd, "CAUTION: Avionics power low: %6.2f Volt", (double)status->avionics_power_rail_voltage); + feedback_provided = true; + } else if (status->avionics_power_rail_voltage > 5.4f) { + mavlink_log_critical(mavlink_fd, "CAUTION: Avionics power high: %6.2f Volt", (double)status->avionics_power_rail_voltage); + feedback_provided = true; + } } } diff --git a/src/modules/dataman/dataman.c b/src/modules/dataman/dataman.c index ca1fe9bbb..b2355d4d8 100644 --- a/src/modules/dataman/dataman.c +++ b/src/modules/dataman/dataman.c @@ -797,7 +797,7 @@ 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, 2000, task_main, NULL)) <= 0) { + if ((task = task_spawn_cmd("dataman", SCHED_DEFAULT, SCHED_PRIORITY_DEFAULT, 2000, task_main, NULL)) <= 0) { warn("task start failed"); return -1; } 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 index 91d17e787..97abb76a9 100644 --- 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 @@ -58,6 +58,7 @@ #include <drivers/drv_accel.h> #include <drivers/drv_mag.h> #include <drivers/drv_baro.h> +#include <drivers/drv_range_finder.h> #ifdef SENSOR_COMBINED_SUB #include <uORB/topics/sensor_combined.h> #endif @@ -96,7 +97,10 @@ extern "C" __EXPORT int ekf_att_pos_estimator_main(int argc, char *argv[]); __EXPORT uint32_t millis(); +__EXPORT uint64_t getMicros(); + static uint64_t IMUmsec = 0; +static uint64_t IMUusec = 0; static const uint64_t FILTER_INIT_DELAY = 1 * 1000 * 1000; uint32_t millis() @@ -104,6 +108,11 @@ uint32_t millis() return IMUmsec; } +uint64_t getMicros() +{ + return IMUusec; +} + class FixedwingEstimator { public: @@ -171,6 +180,7 @@ private: #else int _sensor_combined_sub; #endif + int _distance_sub; /**< distance measurement */ int _airspeed_sub; /**< airspeed subscription */ int _baro_sub; /**< barometer subscription */ int _gps_sub; /**< GPS subscription */ @@ -196,7 +206,8 @@ private: 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 wind_estimate_s _wind; /**< Wind estimate */ + struct wind_estimate_s _wind; /**< wind estimate */ + struct range_finder_report _distance; /**< distance estimate */ struct gyro_scale _gyro_offsets; struct accel_scale _accel_offsets; @@ -226,6 +237,7 @@ private: hrt_abstime _filter_start_time; hrt_abstime _last_sensor_timestamp; hrt_abstime _last_run; + hrt_abstime _distance_last_valid; bool _gyro_valid; bool _accel_valid; bool _mag_valid; @@ -342,6 +354,7 @@ FixedwingEstimator::FixedwingEstimator() : #else _sensor_combined_sub(-1), #endif + _distance_sub(-1), _airspeed_sub(-1), _baro_sub(-1), _gps_sub(-1), @@ -399,6 +412,7 @@ FixedwingEstimator::FixedwingEstimator() : _filter_start_time(0), _last_sensor_timestamp(0), _last_run(0), + _distance_last_valid(0), _gyro_valid(false), _accel_valid(false), _mag_valid(false), @@ -549,6 +563,7 @@ FixedwingEstimator::parameters_update() _ekf->gyroProcessNoise = _parameters.gyro_pnoise; _ekf->accelProcessNoise = _parameters.acc_pnoise; _ekf->airspeedMeasurementSigma = _parameters.eas_noise; + _ekf->rngFinderPitch = 0.0f; // XXX base on SENS_BOARD_Y_OFF } return OK; @@ -704,6 +719,7 @@ FixedwingEstimator::task_main() /* * do subscriptions */ + _distance_sub = orb_subscribe(ORB_ID(sensor_range_finder)); _baro_sub = orb_subscribe(ORB_ID(sensor_baro0)); _airspeed_sub = orb_subscribe(ORB_ID(airspeed)); _gps_sub = orb_subscribe(ORB_ID(vehicle_gps_position)); @@ -753,6 +769,7 @@ FixedwingEstimator::task_main() bool newHgtData = false; bool newAdsData = false; bool newDataMag = false; + bool newRangeData = false; float posNED[3] = {0.0f, 0.0f, 0.0f}; // North, East Down position (m) @@ -850,7 +867,8 @@ FixedwingEstimator::task_main() } _last_sensor_timestamp = _gyro.timestamp; - IMUmsec = _gyro.timestamp / 1e3f; + IMUmsec = _gyro.timestamp / 1e3; + IMUusec = _gyro.timestamp; float deltaT = (_gyro.timestamp - _last_run) / 1e6f; _last_run = _gyro.timestamp; @@ -914,7 +932,8 @@ FixedwingEstimator::task_main() // Copy gyro and accel _last_sensor_timestamp = _sensor_combined.timestamp; - IMUmsec = _sensor_combined.timestamp / 1e3f; + IMUmsec = _sensor_combined.timestamp / 1e3; + IMUusec = _sensor_combined.timestamp; float deltaT = (_sensor_combined.timestamp - _last_run) / 1e6f; @@ -994,8 +1013,6 @@ FixedwingEstimator::task_main() if (gps_updated) { - last_gps = _gps.timestamp_position; - orb_copy(ORB_ID(vehicle_gps_position), _gps_sub, &_gps); perf_count(_perf_gps); @@ -1008,11 +1025,17 @@ FixedwingEstimator::task_main() _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) { + float gps_elapsed = hrt_elapsed_time(&last_gps) / 1e6f; + + const float pos_reset_threshold = 5.0f; // seconds + + /* timeout of 5 seconds */ + if (gps_elapsed > pos_reset_threshold) { _ekf->ResetPosition(); _ekf->ResetVelocity(); _ekf->ResetStoredStates(); } + _ekf->updateDtGpsFilt(math::constrain((_gps.timestamp_position - last_gps) / 1e6f, 0.01f, pos_reset_threshold)); /* fuse GPS updates */ @@ -1044,6 +1067,8 @@ FixedwingEstimator::task_main() newDataGps = true; + last_gps = _gps.timestamp_position; + } } @@ -1052,8 +1077,15 @@ FixedwingEstimator::task_main() orb_check(_baro_sub, &baro_updated); if (baro_updated) { + + hrt_abstime baro_last = _baro.timestamp; + orb_copy(ORB_ID(sensor_baro0), _baro_sub, &_baro); + float baro_elapsed = (_baro.timestamp - baro_last) / 1e6f; + + _ekf->updateDtHgtFilt(math::constrain(baro_elapsed, 0.001f, 0.1)); + _ekf->baroHgt = _baro.altitude; if (!_baro_init) { @@ -1114,6 +1146,19 @@ FixedwingEstimator::task_main() newDataMag = false; } + orb_check(_distance_sub, &newRangeData); + + if (newRangeData) { + orb_copy(ORB_ID(sensor_range_finder), _distance_sub, &_distance); + + if (_distance.valid) { + _ekf->rngMea = _distance.distance; + _distance_last_valid = _distance.timestamp; + } else { + newRangeData = false; + } + } + /* * CHECK IF ITS THE RIGHT TIME TO RUN THINGS ALREADY */ @@ -1197,6 +1242,7 @@ FixedwingEstimator::task_main() } else if (_ekf->statesInitialised) { // We're apparently initialized in this case now + // check (and reset the filter as needed) int check = check_filter_state(); if (check) { @@ -1206,21 +1252,7 @@ FixedwingEstimator::task_main() // 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 @@ -1334,6 +1366,13 @@ FixedwingEstimator::task_main() _ekf->fuseVtasData = false; } + if (newRangeData) { + _ekf->fuseRngData = true; + _ekf->useRangeFinder = true; + _ekf->RecallStates(_ekf->statesAtRngTime, (IMUmsec - 500.0f)); + _ekf->GroundEKF(); + } + // Output results math::Quaternion q(_ekf->states[0], _ekf->states[1], _ekf->states[2], _ekf->states[3]); @@ -1447,6 +1486,10 @@ FixedwingEstimator::task_main() _global_pos.vel_d = _local_pos.vz; } + /* terrain altitude */ + _global_pos.terrain_alt = _ekf->hgtRef - _ekf->flowStates[1]; + _global_pos.terrain_alt_valid = (_distance_last_valid > 0) && + (hrt_elapsed_time(&_distance_last_valid) < 20 * 1000 * 1000); _global_pos.yaw = _local_pos.yaw; @@ -1467,8 +1510,10 @@ FixedwingEstimator::task_main() if (hrt_elapsed_time(&_wind.timestamp) > 99000) { _wind.timestamp = _global_pos.timestamp; - _wind.windspeed_north = _ekf->states[14]; - _wind.windspeed_east = _ekf->states[15]; + _wind.windspeed_north = _ekf->windSpdFiltNorth; + _wind.windspeed_east = _ekf->windSpdFiltEast; + // XXX we need to do something smart about the covariance here + // but we default to the estimate covariance for now _wind.covariance_north = _ekf->P[14][14]; _wind.covariance_east = _ekf->P[15][15]; diff --git a/src/modules/ekf_att_pos_estimator/estimator_23states.cpp b/src/modules/ekf_att_pos_estimator/estimator_23states.cpp index c7c7305b2..94a6d165f 100644 --- a/src/modules/ekf_att_pos_estimator/estimator_23states.cpp +++ b/src/modules/ekf_att_pos_estimator/estimator_23states.cpp @@ -2,6 +2,11 @@ #include <string.h> #include <stdio.h> #include <stdarg.h> +#include <math.h> + +#ifndef M_PI_F +#define M_PI_F ((float)M_PI) +#endif #define EKF_COVARIANCE_DIVERGED 1.0e8f @@ -38,13 +43,14 @@ AttPosEKF::AttPosEKF() : resetStates{}, storedStates{}, statetimeStamp{}, + lastVelPosFusion(millis()), statesAtVelTime{}, statesAtPosTime{}, statesAtHgtTime{}, statesAtMagMeasTime{}, statesAtVtasMeasTime{}, statesAtRngTime{}, - statesAtOptFlowTime{}, + statesAtFlowTime{}, correctedDelAng(), correctedDelVel(), summedDelAng(), @@ -59,7 +65,16 @@ AttPosEKF::AttPosEKF() : accel(), dVelIMU(), dAngIMU(), - dtIMU(0), + dtIMU(0.005f), + dtIMUfilt(0.005f), + dtVelPos(0.01f), + dtVelPosFilt(0.01f), + dtHgtFilt(0.01f), + dtGpsFilt(0.1f), + windSpdFiltNorth(0.0f), + windSpdFiltEast(0.0f), + windSpdFiltAltitude(0.0f), + windSpdFiltClimb(0.0f), fusionModeGPS(0), innovVelPos{}, varInnovVelPos{}, @@ -103,13 +118,13 @@ AttPosEKF::AttPosEKF() : inhibitWindStates(true), inhibitMagStates(true), - inhibitGndHgtState(true), + inhibitGndState(true), onGround(true), staticMode(true), useAirspeed(true), useCompass(true), - useRangeFinder(false), + useRangeFinder(true), useOpticalFlow(false), ekfDiverged(false), @@ -117,7 +132,24 @@ AttPosEKF::AttPosEKF() : current_ekf_state{}, last_ekf_error{}, numericalProtection(true), - storeIndex(0) + storeIndex(0), + storedOmega{}, + Popt{}, + flowStates{}, + prevPosN(0.0f), + prevPosE(0.0f), + auxFlowObsInnov{}, + auxFlowObsInnovVar{}, + fScaleFactorVar(0.0f), + Tnb_flow{}, + R_LOS(0.0f), + auxFlowTestRatio{}, + auxRngTestRatio(0.0f), + flowInnovGate(0.0f), + auxFlowInnovGate(0.0f), + rngInnovGate(0.0f), + minFlowRng(0.0f), + moCompR_LOS(0.0f) { memset(&last_ekf_error, 0, sizeof(last_ekf_error)); memset(¤t_ekf_state, 0, sizeof(current_ekf_state)); @@ -260,6 +292,9 @@ void AttPosEKF::UpdateStrapdownEquationsNED() // Constrain states (to protect against filter divergence) ConstrainStates(); + + // update filtered IMU time step length + dtIMUfilt = 0.99f * dtIMUfilt + 0.01f * dtIMU; } void AttPosEKF::CovariancePrediction(float dt) @@ -312,7 +347,7 @@ void AttPosEKF::CovariancePrediction(float dt) } else { for (uint8_t i=16; i<=21; i++) processNoise[i] = 0; } - if (!inhibitGndHgtState) { + if (!inhibitGndState) { processNoise[22] = dt * sqrtf(sq(states[4]) + sq(states[5])) * gndHgtSigma; } else { processNoise[22] = 0; @@ -962,6 +997,21 @@ void AttPosEKF::CovariancePrediction(float dt) ConstrainVariances(); } +void AttPosEKF::updateDtGpsFilt(float dt) +{ + dtGpsFilt = ConstrainFloat(dt, 0.001f, 2.0f) * 0.05f + dtGpsFilt * 0.95f; +} + +void AttPosEKF::updateDtHgtFilt(float dt) +{ + dtHgtFilt = ConstrainFloat(dt, 0.001f, 2.0f) * 0.05f + dtHgtFilt * 0.95f; +} + +void AttPosEKF::updateDtVelPosFilt(float dt) +{ + dtVelPosFilt = ConstrainFloat(dt, 0.0005f, 2.0f) * 0.05f + dtVelPosFilt * 0.95f; +} + void AttPosEKF::FuseVelposNED() { @@ -998,6 +1048,18 @@ void AttPosEKF::FuseVelposNED() // associated with sequential fusion if (fuseVelData || fusePosData || fuseHgtData) { + uint64_t tNow = getMicros(); + updateDtVelPosFilt((tNow - lastVelPosFusion) / 1e6f); + lastVelPosFusion = tNow; + + // scaler according to the number of repetitions of the + // same measurement in one fusion step + float gpsVarianceScaler = dtGpsFilt / dtVelPosFilt; + + // scaler according to the number of repetitions of the + // same measurement in one fusion step + float hgtVarianceScaler = dtHgtFilt / dtVelPosFilt; + // set the GPS data timeout depending on whether airspeed data is present if (useAirspeed) horizRetryTime = gpsRetryTime; else horizRetryTime = gpsRetryTimeNoTAS; @@ -1010,12 +1072,12 @@ void AttPosEKF::FuseVelposNED() // 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[0] = gpsVarianceScaler * 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[2] = gpsVarianceScaler * sq(vdSigma) + sq(velErr); + R_OBS[3] = gpsVarianceScaler * sq(posNeSigma) + sq(posErr); R_OBS[4] = R_OBS[3]; - R_OBS[5] = sq(posDSigma) + sq(posErr); + R_OBS[5] = hgtVarianceScaler * sq(posDSigma) + sq(posErr); // calculate innovations and check GPS data validity using an innovation consistency check if (fuseVelData) @@ -1173,7 +1235,7 @@ void AttPosEKF::FuseVelposNED() } } // Don't update terrain state if inhibited - if (inhibitGndHgtState) { + if (inhibitGndState) { Kfusion[22] = 0; } @@ -1356,7 +1418,7 @@ void AttPosEKF::FuseMagnetometer() Kfusion[i] = 0; } } - if (!inhibitGndHgtState) { + if (!inhibitGndState) { 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]); } else { Kfusion[22] = 0; @@ -1430,11 +1492,6 @@ void AttPosEKF::FuseMagnetometer() Kfusion[20] = 0; Kfusion[21] = 0; } - if (!inhibitGndHgtState) { - 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]); - } else { - Kfusion[22] = 0; - } varInnovMag[1] = 1.0f/SK_MY[0]; innovMag[1] = MagPred[1] - magData.y; } @@ -1505,11 +1562,6 @@ void AttPosEKF::FuseMagnetometer() Kfusion[20] = 0; Kfusion[21] = 0; } - if (!inhibitGndHgtState) { - 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]); - } else { - Kfusion[22] = 0; - } varInnovMag[2] = 1.0f/SK_MZ[0]; innovMag[2] = MagPred[2] - magData.z; @@ -1616,6 +1668,32 @@ void AttPosEKF::FuseAirspeed() // Perform fusion of True Airspeed measurement if (useAirspeed && fuseVtasData && (VtasPred > 1.0f) && (VtasMeas > 8.0f)) { + + float altDiff = fabsf(windSpdFiltAltitude - hgtMea); + + if (isfinite(windSpdFiltClimb)) { + windSpdFiltClimb = ((1.0f - 0.0002f) * windSpdFiltClimb) + (0.0002f * states[6]); + } else { + windSpdFiltClimb = states[6]; + } + + if (altDiff < 20.0f) { + // Lowpass the output of the wind estimate - we want a long-term + // stable estimate, but not start to load into the overall dynamics + // of the system (which adjusting covariances would do) + + // Change filter coefficient based on altitude change rate + float windFiltCoeff = ConstrainFloat(fabsf(windSpdFiltClimb) / 1000.0f, 0.00005f, 0.2f); + + windSpdFiltNorth = ((1.0f - windFiltCoeff) * windSpdFiltNorth) + (windFiltCoeff * vwn); + windSpdFiltEast = ((1.0f - windFiltCoeff) * windSpdFiltEast) + (windFiltCoeff * vwe); + } else { + windSpdFiltNorth = vwn; + windSpdFiltEast = vwe; + } + + windSpdFiltAltitude = hgtMea; + // 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; @@ -1675,11 +1753,6 @@ void AttPosEKF::FuseAirspeed() Kfusion[i] = 0; } } - if (!inhibitGndHgtState) { - 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]); - } else { - Kfusion[22] = 0; - } varInnovVtas = 1.0f/SK_TAS; // Calculate the measurement innovation @@ -1811,8 +1884,11 @@ void AttPosEKF::FuseRangeFinder() rngPred = (ptd - pd)/cosRngTilt; innovRng = rngPred - rngMea; - // Check the innovation for consistency and don't fuse if > 5Sigma - if ((innovRng*innovRng*SK_RNG[0]) < 25) + // calculate the innovation consistency test ratio + auxRngTestRatio = sq(innovRng) / (sq(rngInnovGate) * varInnovRng); + + // Check the innovation for consistency and don't fuse if out of bounds + if (auxRngTestRatio < 1.0f) { // correct the state vector states[22] = states[22] - Kfusion[22] * innovRng; @@ -1827,285 +1903,387 @@ void AttPosEKF::FuseRangeFinder() void AttPosEKF::FuseOptFlow() { - static uint8_t obsIndex; - static float SH_LOS[13]; - static float SKK_LOS[15]; - static float SK_LOS[2]; - static float q0 = 0.0f; - static float q1 = 0.0f; - static float q2 = 0.0f; - static float q3 = 1.0f; - static float vn = 0.0f; - static float ve = 0.0f; - static float vd = 0.0f; - static float pd = 0.0f; - static float ptd = 0.0f; - static float R_LOS = 0.01f; - static float losPred[2]; - - // Transformation matrix from nav to body axes - Mat3f Tnb_local; - // Transformation matrix from body to sensor axes - // assume camera is aligned with Z body axis plus a misalignment - // defined by 3 small angles about X, Y and Z body axis - Mat3f Tbs; - Tbs.x.y = a3; - Tbs.y.x = -a3; - Tbs.x.z = -a2; - Tbs.z.x = a2; - Tbs.y.z = a1; - Tbs.z.y = -a1; - // Transformation matrix from navigation to sensor axes - Mat3f Tns; - float H_LOS[n_states]; - for (uint8_t i = 0; i < n_states; i++) { - H_LOS[i] = 0.0f; - } - Vector3f velNED_local; - Vector3f relVelSensor; +// static uint8_t obsIndex; +// static float SH_LOS[13]; +// static float SKK_LOS[15]; +// static float SK_LOS[2]; +// static float q0 = 0.0f; +// static float q1 = 0.0f; +// static float q2 = 0.0f; +// static float q3 = 1.0f; +// static float vn = 0.0f; +// static float ve = 0.0f; +// static float vd = 0.0f; +// static float pd = 0.0f; +// static float ptd = 0.0f; +// static float R_LOS = 0.01f; +// static float losPred[2]; + +// // Transformation matrix from nav to body axes +// Mat3f Tnb_local; +// // Transformation matrix from body to sensor axes +// // assume camera is aligned with Z body axis plus a misalignment +// // defined by 3 small angles about X, Y and Z body axis +// Mat3f Tbs; +// Tbs.x.y = a3; +// Tbs.y.x = -a3; +// Tbs.x.z = -a2; +// Tbs.z.x = a2; +// Tbs.y.z = a1; +// Tbs.z.y = -a1; +// // Transformation matrix from navigation to sensor axes +// Mat3f Tns; +// float H_LOS[n_states]; +// for (uint8_t i = 0; i < n_states; i++) { +// H_LOS[i] = 0.0f; +// } +// Vector3f velNED_local; +// Vector3f relVelSensor; + +// // Perform sequential fusion of optical flow measurements only when in the air and tilt is less than 30 deg. +// if (useOpticalFlow && (fuseOptFlowData || obsIndex == 1) && !onGround && Tbs.z.z > 0.866f && rngMea > 5.0f && rngMea < 39.0f) +// { +// // Sequential fusion of XY components to spread processing load across +// // two prediction time steps. + +// // Calculate observation jacobians and Kalman gains +// if (fuseOptFlowData) +// { +// // Copy required states to local variable names +// q0 = statesAtOptFlowTime[0]; +// q1 = statesAtOptFlowTime[1]; +// q2 = statesAtOptFlowTime[2]; +// q3 = statesAtOptFlowTime[3]; +// vn = statesAtOptFlowTime[4]; +// ve = statesAtOptFlowTime[5]; +// vd = statesAtOptFlowTime[6]; +// pd = statesAtOptFlowTime[9]; +// ptd = statesAtOptFlowTime[22]; +// velNED_local.x = vn; +// velNED_local.y = ve; +// velNED_local.z = vd; + +// // calculate rotation from NED to body axes +// float q00 = sq(q0); +// float q11 = sq(q1); +// float q22 = sq(q2); +// float q33 = sq(q3); +// float q01 = q0 * q1; +// float q02 = q0 * q2; +// float q03 = q0 * q3; +// float q12 = q1 * q2; +// float q13 = q1 * q3; +// float q23 = q2 * q3; +// Tnb_local.x.x = q00 + q11 - q22 - q33; +// Tnb_local.y.y = q00 - q11 + q22 - q33; +// Tnb_local.z.z = q00 - q11 - q22 + q33; +// Tnb_local.y.x = 2*(q12 - q03); +// Tnb_local.z.x = 2*(q13 + q02); +// Tnb_local.x.y = 2*(q12 + q03); +// Tnb_local.z.y = 2*(q23 - q01); +// Tnb_local.x.z = 2*(q13 - q02); +// Tnb_local.y.z = 2*(q23 + q01); + +// // calculate transformation from NED to sensor axes +// Tns = Tbs*Tnb_local; + +// // calculate range from ground plain to centre of sensor fov assuming flat earth +// float range = ConstrainFloat(((ptd - pd)/Tns.z.z),0.5f,100.0f); + +// // calculate relative velocity in sensor frame +// relVelSensor = Tns*velNED_local; + +// // divide velocity by range and include angular rate effects to get predicted angular LOS rates relative to X and Y axes +// losPred[0] = relVelSensor.y/range; +// losPred[1] = -relVelSensor.x/range; + +// //printf("relVelSensor.x=%5.1f, relVelSensor.y=%5.1f\n", relVelSensor.x, relVelSensor.y); +// //printf("Xpred=%5.2f, Xmea=%5.2f, Ypred=%5.2f, Ymea=%5.2f, delAng.x=%4.4f, delAng.y=%4.4f\n", losPred[0], losData[0], losPred[1], losData[1], delAng.x, delAng.y); +// //printf("omegaX=%5.2f, omegaY=%5.2f, velY=%5.1f velX=%5.1f\n, range=%5.1f\n", delAngRel.x/dt, delAngRel.y/dt, relVelSensor.y, relVelSensor.x, range); + +// // Calculate observation jacobians +// SH_LOS[0] = a1*(2*q0*q1 + 2*q2*q3) + a2*(2*q0*q2 - 2*q1*q3) - sq(q0) + sq(q1) + sq(q2) - sq(q3); +// SH_LOS[1] = vd*(a2*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + 2*q0*q2 - 2*q1*q3 - a3*(2*q0*q1 + 2*q2*q3)) - ve*(a3*(sq(q0) - sq(q1) + sq(q2) - sq(q3)) + 2*q0*q3 + 2*q1*q2 + a2*(2*q0*q1 - 2*q2*q3)) + vn*(a2*(2*q0*q2 + 2*q1*q3) + a3*(2*q0*q3 - 2*q1*q2) - sq(q0) - sq(q1) + sq(q2) + sq(q3)); +// SH_LOS[2] = ve*(a1*(2*q0*q1 - 2*q2*q3) + a3*(2*q0*q3 + 2*q1*q2) - sq(q0) + sq(q1) - sq(q2) + sq(q3)) - vd*(a1*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + 2*q0*q1 + 2*q2*q3 + a3*(2*q0*q2 - 2*q1*q3)) + vn*(a3*(sq(q0) + sq(q1) - sq(q2) - sq(q3)) + 2*q0*q3 - 2*q1*q2 - a1*(2*q0*q2 + 2*q1*q3)); +// SH_LOS[3] = 1/(pd - ptd); +// SH_LOS[4] = 2*q1 - 2*a2*q3 + 2*a3*q2; +// SH_LOS[5] = 2*a2*q2 - 2*q0 + 2*a3*q3; +// SH_LOS[6] = 2*q2 + 2*a2*q0 - 2*a3*q1; +// SH_LOS[7] = 1/sq(pd - ptd); +// SH_LOS[8] = 2*q2 + 2*a1*q3 - 2*a3*q1; +// SH_LOS[9] = 2*q3 - 2*a1*q2 + 2*a3*q0; +// SH_LOS[10] = 2*a1*q1 - 2*q0 + 2*a3*q3; +// SH_LOS[11] = 2*q3 + 2*a2*q1 + 2*a3*q0; +// SH_LOS[12] = 2*q1 + 2*a1*q0 + 2*a3*q2; + +// for (uint8_t i = 0; i < n_states; i++) H_LOS[i] = 0; +// H_LOS[0] = - SH_LOS[2]*SH_LOS[3]*(2*a1*q1 - 2*q0 + 2*a2*q2) - SH_LOS[0]*SH_LOS[3]*(ve*SH_LOS[10] - vd*SH_LOS[12] + vn*SH_LOS[9]); +// H_LOS[1] = - SH_LOS[2]*SH_LOS[3]*(2*q1 + 2*a1*q0 - 2*a2*q3) - SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[10] + ve*SH_LOS[12] - vn*SH_LOS[8]); +// H_LOS[2] = SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[9] + ve*SH_LOS[8] + vn*SH_LOS[12]) - SH_LOS[2]*SH_LOS[3]*(2*q2 + 2*a2*q0 + 2*a1*q3); +// H_LOS[3] = SH_LOS[2]*SH_LOS[3]*(2*q3 - 2*a1*q2 + 2*a2*q1) + SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[8] - ve*SH_LOS[9] + vn*SH_LOS[10]); +// H_LOS[4] = -SH_LOS[0]*SH_LOS[3]*(a3*(sq(q0) + sq(q1) - sq(q2) - sq(q3)) + 2*q0*q3 - 2*q1*q2 - a1*(2*q0*q2 + 2*q1*q3)); +// H_LOS[5] = -SH_LOS[0]*SH_LOS[3]*(a1*(2*q0*q1 - 2*q2*q3) + a3*(2*q0*q3 + 2*q1*q2) - sq(q0) + sq(q1) - sq(q2) + sq(q3)); +// H_LOS[6] = SH_LOS[0]*SH_LOS[3]*(a1*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + 2*q0*q1 + 2*q2*q3 + a3*(2*q0*q2 - 2*q1*q3)); +// H_LOS[9] = SH_LOS[0]*SH_LOS[2]*SH_LOS[7]; +// H_LOS[22] = -SH_LOS[0]*SH_LOS[2]*SH_LOS[7]; + +// // Calculate Kalman gain +// SKK_LOS[0] = a2*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + 2*q0*q2 - 2*q1*q3 - a3*(2*q0*q1 + 2*q2*q3); +// SKK_LOS[1] = a3*(sq(q0) - sq(q1) + sq(q2) - sq(q3)) + 2*q0*q3 + 2*q1*q2 + a2*(2*q0*q1 - 2*q2*q3); +// SKK_LOS[2] = a2*(2*q0*q2 + 2*q1*q3) + a3*(2*q0*q3 - 2*q1*q2) - sq(q0) - sq(q1) + sq(q2) + sq(q3); +// SKK_LOS[3] = a1*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + 2*q0*q1 + 2*q2*q3 + a3*(2*q0*q2 - 2*q1*q3); +// SKK_LOS[4] = a1*(2*q0*q1 - 2*q2*q3) + a3*(2*q0*q3 + 2*q1*q2) - sq(q0) + sq(q1) - sq(q2) + sq(q3); +// SKK_LOS[5] = a3*(sq(q0) + sq(q1) - sq(q2) - sq(q3)) + 2*q0*q3 - 2*q1*q2 - a1*(2*q0*q2 + 2*q1*q3); +// SKK_LOS[6] = SH_LOS[2]*SH_LOS[3]*(2*q3 - 2*a1*q2 + 2*a2*q1) + SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[8] - ve*SH_LOS[9] + vn*SH_LOS[10]); +// SKK_LOS[7] = SH_LOS[2]*SH_LOS[3]*(2*q1 + 2*a1*q0 - 2*a2*q3) + SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[10] + ve*SH_LOS[12] - vn*SH_LOS[8]); +// SKK_LOS[8] = SH_LOS[2]*SH_LOS[3]*(2*a1*q1 - 2*q0 + 2*a2*q2) + SH_LOS[0]*SH_LOS[3]*(ve*SH_LOS[10] - vd*SH_LOS[12] + vn*SH_LOS[9]); +// SKK_LOS[9] = SH_LOS[2]*SH_LOS[3]*(2*q2 + 2*a2*q0 + 2*a1*q3) - SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[9] + ve*SH_LOS[8] + vn*SH_LOS[12]); +// SKK_LOS[10] = SH_LOS[1]*SH_LOS[3]*(2*a1*q1 - 2*q0 + 2*a2*q2) + SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[6] - ve*SH_LOS[11] + vn*SH_LOS[5]); +// SKK_LOS[11] = SH_LOS[1]*SH_LOS[3]*(2*q1 + 2*a1*q0 - 2*a2*q3) - SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[11] + ve*SH_LOS[6] + vn*SH_LOS[4]); +// SKK_LOS[12] = SH_LOS[1]*SH_LOS[3]*(2*q2 + 2*a2*q0 + 2*a1*q3) - SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[5] + ve*SH_LOS[4] - vn*SH_LOS[6]); +// SKK_LOS[13] = SH_LOS[1]*SH_LOS[3]*(2*q3 - 2*a1*q2 + 2*a2*q1) - SH_LOS[0]*SH_LOS[3]*(ve*SH_LOS[5] - vd*SH_LOS[4] + vn*SH_LOS[11]); +// SKK_LOS[14] = SH_LOS[0]; + +// SK_LOS[0] = 1/(R_LOS + SKK_LOS[8]*(P[0][0]*SKK_LOS[8] + P[1][0]*SKK_LOS[7] + P[2][0]*SKK_LOS[9] - P[3][0]*SKK_LOS[6] - P[9][0]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][0]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][0]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][0]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][0]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) + SKK_LOS[7]*(P[0][1]*SKK_LOS[8] + P[1][1]*SKK_LOS[7] + P[2][1]*SKK_LOS[9] - P[3][1]*SKK_LOS[6] - P[9][1]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][1]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][1]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][1]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][1]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) + SKK_LOS[9]*(P[0][2]*SKK_LOS[8] + P[1][2]*SKK_LOS[7] + P[2][2]*SKK_LOS[9] - P[3][2]*SKK_LOS[6] - P[9][2]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][2]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][2]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][2]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][2]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) - SKK_LOS[6]*(P[0][3]*SKK_LOS[8] + P[1][3]*SKK_LOS[7] + P[2][3]*SKK_LOS[9] - P[3][3]*SKK_LOS[6] - P[9][3]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][3]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][3]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][3]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][3]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) - SH_LOS[2]*SH_LOS[7]*SKK_LOS[14]*(P[0][9]*SKK_LOS[8] + P[1][9]*SKK_LOS[7] + P[2][9]*SKK_LOS[9] - P[3][9]*SKK_LOS[6] - P[9][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][9]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][9]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][9]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) + SH_LOS[2]*SH_LOS[7]*SKK_LOS[14]*(P[0][22]*SKK_LOS[8] + P[1][22]*SKK_LOS[7] + P[2][22]*SKK_LOS[9] - P[3][22]*SKK_LOS[6] - P[9][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][22]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][22]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][22]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) + SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14]*(P[0][4]*SKK_LOS[8] + P[1][4]*SKK_LOS[7] + P[2][4]*SKK_LOS[9] - P[3][4]*SKK_LOS[6] - P[9][4]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][4]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][4]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][4]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) + SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14]*(P[0][5]*SKK_LOS[8] + P[1][5]*SKK_LOS[7] + P[2][5]*SKK_LOS[9] - P[3][5]*SKK_LOS[6] - P[9][5]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][5]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][5]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][5]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) - SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]*(P[0][6]*SKK_LOS[8] + P[1][6]*SKK_LOS[7] + P[2][6]*SKK_LOS[9] - P[3][6]*SKK_LOS[6] - P[9][6]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][6]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][6]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][6]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14])); +// Kfusion[0] = -SK_LOS[0]*(P[0][0]*SKK_LOS[8] + P[0][1]*SKK_LOS[7] - P[0][3]*SKK_LOS[6] + P[0][2]*SKK_LOS[9] - P[0][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[0][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[0][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[0][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[0][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[1] = -SK_LOS[0]*(P[1][0]*SKK_LOS[8] + P[1][1]*SKK_LOS[7] - P[1][3]*SKK_LOS[6] + P[1][2]*SKK_LOS[9] - P[1][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[1][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[1][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[1][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[1][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[2] = -SK_LOS[0]*(P[2][0]*SKK_LOS[8] + P[2][1]*SKK_LOS[7] - P[2][3]*SKK_LOS[6] + P[2][2]*SKK_LOS[9] - P[2][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[2][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[2][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[2][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[2][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[3] = -SK_LOS[0]*(P[3][0]*SKK_LOS[8] + P[3][1]*SKK_LOS[7] - P[3][3]*SKK_LOS[6] + P[3][2]*SKK_LOS[9] - P[3][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[3][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[3][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[3][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[3][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[4] = -SK_LOS[0]*(P[4][0]*SKK_LOS[8] + P[4][1]*SKK_LOS[7] - P[4][3]*SKK_LOS[6] + P[4][2]*SKK_LOS[9] - P[4][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[4][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[4][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[5] = -SK_LOS[0]*(P[5][0]*SKK_LOS[8] + P[5][1]*SKK_LOS[7] - P[5][3]*SKK_LOS[6] + P[5][2]*SKK_LOS[9] - P[5][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[5][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[5][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[5][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[6] = -SK_LOS[0]*(P[6][0]*SKK_LOS[8] + P[6][1]*SKK_LOS[7] - P[6][3]*SKK_LOS[6] + P[6][2]*SKK_LOS[9] - P[6][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[6][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[6][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[6][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[7] = -SK_LOS[0]*(P[7][0]*SKK_LOS[8] + P[7][1]*SKK_LOS[7] - P[7][3]*SKK_LOS[6] + P[7][2]*SKK_LOS[9] - P[7][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[7][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[7][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[7][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[7][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[8] = -SK_LOS[0]*(P[8][0]*SKK_LOS[8] + P[8][1]*SKK_LOS[7] - P[8][3]*SKK_LOS[6] + P[8][2]*SKK_LOS[9] - P[8][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[8][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[8][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[8][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[8][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[9] = -SK_LOS[0]*(P[9][0]*SKK_LOS[8] + P[9][1]*SKK_LOS[7] - P[9][3]*SKK_LOS[6] + P[9][2]*SKK_LOS[9] - P[9][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[9][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[9][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[9][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[9][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[10] = -SK_LOS[0]*(P[10][0]*SKK_LOS[8] + P[10][1]*SKK_LOS[7] - P[10][3]*SKK_LOS[6] + P[10][2]*SKK_LOS[9] - P[10][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[10][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[10][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[10][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[10][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[11] = -SK_LOS[0]*(P[11][0]*SKK_LOS[8] + P[11][1]*SKK_LOS[7] - P[11][3]*SKK_LOS[6] + P[11][2]*SKK_LOS[9] - P[11][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[11][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[11][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[11][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[11][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[12] = -SK_LOS[0]*(P[12][0]*SKK_LOS[8] + P[12][1]*SKK_LOS[7] - P[12][3]*SKK_LOS[6] + P[12][2]*SKK_LOS[9] - P[12][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[12][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[12][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[12][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[12][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[13] = 0.0f;//-SK_LOS[0]*(P[13][0]*SKK_LOS[8] + P[13][1]*SKK_LOS[7] - P[13][3]*SKK_LOS[6] + P[13][2]*SKK_LOS[9] - P[13][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[13][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[13][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[13][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[13][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[14] = -SK_LOS[0]*(P[14][0]*SKK_LOS[8] + P[14][1]*SKK_LOS[7] - P[14][3]*SKK_LOS[6] + P[14][2]*SKK_LOS[9] - P[14][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[14][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[14][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[14][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[14][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[15] = -SK_LOS[0]*(P[15][0]*SKK_LOS[8] + P[15][1]*SKK_LOS[7] - P[15][3]*SKK_LOS[6] + P[15][2]*SKK_LOS[9] - P[15][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[15][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[15][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[15][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[15][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[16] = -SK_LOS[0]*(P[16][0]*SKK_LOS[8] + P[16][1]*SKK_LOS[7] - P[16][3]*SKK_LOS[6] + P[16][2]*SKK_LOS[9] - P[16][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[16][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[16][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[16][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[16][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[17] = -SK_LOS[0]*(P[17][0]*SKK_LOS[8] + P[17][1]*SKK_LOS[7] - P[17][3]*SKK_LOS[6] + P[17][2]*SKK_LOS[9] - P[17][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[17][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[17][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[17][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[17][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[18] = -SK_LOS[0]*(P[18][0]*SKK_LOS[8] + P[18][1]*SKK_LOS[7] - P[18][3]*SKK_LOS[6] + P[18][2]*SKK_LOS[9] - P[18][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[18][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[18][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[18][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[18][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[19] = -SK_LOS[0]*(P[19][0]*SKK_LOS[8] + P[19][1]*SKK_LOS[7] - P[19][3]*SKK_LOS[6] + P[19][2]*SKK_LOS[9] - P[19][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[19][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[19][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[19][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[19][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[20] = -SK_LOS[0]*(P[20][0]*SKK_LOS[8] + P[20][1]*SKK_LOS[7] - P[20][3]*SKK_LOS[6] + P[20][2]*SKK_LOS[9] - P[20][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[20][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[20][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[20][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[20][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[21] = -SK_LOS[0]*(P[21][0]*SKK_LOS[8] + P[21][1]*SKK_LOS[7] - P[21][3]*SKK_LOS[6] + P[21][2]*SKK_LOS[9] - P[21][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[21][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[21][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[21][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[21][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// Kfusion[22] = -SK_LOS[0]*(P[22][0]*SKK_LOS[8] + P[22][1]*SKK_LOS[7] - P[22][3]*SKK_LOS[6] + P[22][2]*SKK_LOS[9] - P[22][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[22][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[22][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); +// varInnovOptFlow[0] = 1.0f/SK_LOS[0]; +// innovOptFlow[0] = losPred[0] - losData[0]; + +// // set the observation index to 1 to fuse the y component next time round and reset the commence fusion flag +// obsIndex = 1; +// fuseOptFlowData = false; +// } +// else if (obsIndex == 1) // we are now fusing the Y measurement +// { +// // Calculate observation jacobians +// for (uint8_t i = 0; i < n_states; i++) H_LOS[i] = 0; +// H_LOS[0] = SH_LOS[1]*SH_LOS[3]*(2*a1*q1 - 2*q0 + 2*a2*q2) + SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[6] - ve*SH_LOS[11] + vn*SH_LOS[5]); +// H_LOS[1] = SH_LOS[1]*SH_LOS[3]*(2*q1 + 2*a1*q0 - 2*a2*q3) - SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[11] + ve*SH_LOS[6] + vn*SH_LOS[4]); +// H_LOS[2] = SH_LOS[1]*SH_LOS[3]*(2*q2 + 2*a2*q0 + 2*a1*q3) - SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[5] + ve*SH_LOS[4] - vn*SH_LOS[6]); +// H_LOS[3] = SH_LOS[0]*SH_LOS[3]*(ve*SH_LOS[5] - vd*SH_LOS[4] + vn*SH_LOS[11]) - SH_LOS[1]*SH_LOS[3]*(2*q3 - 2*a1*q2 + 2*a2*q1); +// H_LOS[4] = SH_LOS[0]*SH_LOS[3]*(a2*(2*q0*q2 + 2*q1*q3) + a3*(2*q0*q3 - 2*q1*q2) - sq(q0) - sq(q1) + sq(q2) + sq(q3)); +// H_LOS[5] = -SH_LOS[0]*SH_LOS[3]*(a3*(sq(q0) - sq(q1) + sq(q2) - sq(q3)) + 2*q0*q3 + 2*q1*q2 + a2*(2*q0*q1 - 2*q2*q3)); +// H_LOS[6] = SH_LOS[0]*SH_LOS[3]*(a2*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + 2*q0*q2 - 2*q1*q3 - a3*(2*q0*q1 + 2*q2*q3)); +// H_LOS[9] = -SH_LOS[0]*SH_LOS[1]*SH_LOS[7]; +// H_LOS[22] = SH_LOS[0]*SH_LOS[1]*SH_LOS[7]; + +// // Calculate Kalman gains +// SK_LOS[1] = 1/(R_LOS + SKK_LOS[12]*(P[0][2]*SKK_LOS[10] + P[1][2]*SKK_LOS[11] + P[2][2]*SKK_LOS[12] - P[3][2]*SKK_LOS[13] - P[9][2]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][2]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][2]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][2]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][2]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) - SKK_LOS[13]*(P[0][3]*SKK_LOS[10] + P[1][3]*SKK_LOS[11] + P[2][3]*SKK_LOS[12] - P[3][3]*SKK_LOS[13] - P[9][3]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][3]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][3]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][3]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][3]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) + SKK_LOS[10]*(P[0][0]*SKK_LOS[10] + P[1][0]*SKK_LOS[11] + P[2][0]*(SH_LOS[1]*SH_LOS[3]*(2*q2 + 2*a2*q0 + 2*a1*q3) - SH_LOS[3]*SKK_LOS[14]*(vd*SH_LOS[5] + ve*SH_LOS[4] - vn*SH_LOS[6])) - P[3][0]*(SH_LOS[1]*SH_LOS[3]*(2*q3 - 2*a1*q2 + 2*a2*q1) - SH_LOS[3]*SKK_LOS[14]*(ve*SH_LOS[5] - vd*SH_LOS[4] + vn*SH_LOS[11])) - P[9][0]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][0]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][0]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][0]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][0]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) + SKK_LOS[11]*(P[0][1]*SKK_LOS[10] + P[1][1]*SKK_LOS[11] + P[2][1]*(SH_LOS[1]*SH_LOS[3]*(2*q2 + 2*a2*q0 + 2*a1*q3) - SH_LOS[3]*SKK_LOS[14]*(vd*SH_LOS[5] + ve*SH_LOS[4] - vn*SH_LOS[6])) - P[3][1]*(SH_LOS[1]*SH_LOS[3]*(2*q3 - 2*a1*q2 + 2*a2*q1) - SH_LOS[3]*SKK_LOS[14]*(ve*SH_LOS[5] - vd*SH_LOS[4] + vn*SH_LOS[11])) - P[9][1]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][1]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][1]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][1]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][1]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) - SH_LOS[1]*SH_LOS[7]*SKK_LOS[14]*(P[0][9]*SKK_LOS[10] + P[1][9]*SKK_LOS[11] + P[2][9]*SKK_LOS[12] - P[3][9]*SKK_LOS[13] - P[9][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][9]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][9]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][9]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) + SH_LOS[1]*SH_LOS[7]*SKK_LOS[14]*(P[0][22]*SKK_LOS[10] + P[1][22]*SKK_LOS[11] + P[2][22]*SKK_LOS[12] - P[3][22]*SKK_LOS[13] - P[9][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][22]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][22]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][22]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) + SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14]*(P[0][4]*SKK_LOS[10] + P[1][4]*SKK_LOS[11] + P[2][4]*SKK_LOS[12] - P[3][4]*SKK_LOS[13] - P[9][4]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][4]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][4]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][4]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) - SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]*(P[0][5]*SKK_LOS[10] + P[1][5]*SKK_LOS[11] + P[2][5]*SKK_LOS[12] - P[3][5]*SKK_LOS[13] - P[9][5]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][5]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][5]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][5]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) + SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]*(P[0][6]*SKK_LOS[10] + P[1][6]*SKK_LOS[11] + P[2][6]*SKK_LOS[12] - P[3][6]*SKK_LOS[13] - P[9][6]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][6]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][6]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][6]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14])); +// Kfusion[0] = SK_LOS[1]*(P[0][0]*SKK_LOS[10] - P[0][3]*SKK_LOS[13] + P[0][1]*SKK_LOS[11] + P[0][2]*SKK_LOS[12] - P[0][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[0][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[0][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[0][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[0][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[1] = SK_LOS[1]*(P[1][0]*SKK_LOS[10] - P[1][3]*SKK_LOS[13] + P[1][1]*SKK_LOS[11] + P[1][2]*SKK_LOS[12] - P[1][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[1][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[1][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[1][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[1][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[2] = SK_LOS[1]*(P[2][0]*SKK_LOS[10] - P[2][3]*SKK_LOS[13] + P[2][1]*SKK_LOS[11] + P[2][2]*SKK_LOS[12] - P[2][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[2][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[2][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[2][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[2][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[3] = SK_LOS[1]*(P[3][0]*SKK_LOS[10] - P[3][3]*SKK_LOS[13] + P[3][1]*SKK_LOS[11] + P[3][2]*SKK_LOS[12] - P[3][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[3][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[3][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[3][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[3][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[4] = SK_LOS[1]*(P[4][0]*SKK_LOS[10] - P[4][3]*SKK_LOS[13] + P[4][1]*SKK_LOS[11] + P[4][2]*SKK_LOS[12] - P[4][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[4][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[4][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[5] = SK_LOS[1]*(P[5][0]*SKK_LOS[10] - P[5][3]*SKK_LOS[13] + P[5][1]*SKK_LOS[11] + P[5][2]*SKK_LOS[12] - P[5][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[5][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[5][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[5][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[6] = SK_LOS[1]*(P[6][0]*SKK_LOS[10] - P[6][3]*SKK_LOS[13] + P[6][1]*SKK_LOS[11] + P[6][2]*SKK_LOS[12] - P[6][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[6][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[6][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[6][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[6][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[7] = SK_LOS[1]*(P[7][0]*SKK_LOS[10] - P[7][3]*SKK_LOS[13] + P[7][1]*SKK_LOS[11] + P[7][2]*SKK_LOS[12] - P[7][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[7][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[7][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[7][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[7][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[8] = SK_LOS[1]*(P[8][0]*SKK_LOS[10] - P[8][3]*SKK_LOS[13] + P[8][1]*SKK_LOS[11] + P[8][2]*SKK_LOS[12] - P[8][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[8][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[8][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[8][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[8][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[9] = SK_LOS[1]*(P[9][0]*SKK_LOS[10] - P[9][3]*SKK_LOS[13] + P[9][1]*SKK_LOS[11] + P[9][2]*SKK_LOS[12] - P[9][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[9][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[9][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[9][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[9][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[10] = SK_LOS[1]*(P[10][0]*SKK_LOS[10] - P[10][3]*SKK_LOS[13] + P[10][1]*SKK_LOS[11] + P[10][2]*SKK_LOS[12] - P[10][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[10][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[10][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[10][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[10][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[11] = SK_LOS[1]*(P[11][0]*SKK_LOS[10] - P[11][3]*SKK_LOS[13] + P[11][1]*SKK_LOS[11] + P[11][2]*SKK_LOS[12] - P[11][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[11][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[11][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[11][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[11][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[12] = SK_LOS[1]*(P[12][0]*SKK_LOS[10] - P[12][3]*SKK_LOS[13] + P[12][1]*SKK_LOS[11] + P[12][2]*SKK_LOS[12] - P[12][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[12][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[12][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[12][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[12][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[13] = 0.0f;//SK_LOS[1]*(P[13][0]*SKK_LOS[10] - P[13][3]*SKK_LOS[13] + P[13][1]*SKK_LOS[11] + P[13][2]*SKK_LOS[12] - P[13][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[13][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[13][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[13][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[13][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[14] = SK_LOS[1]*(P[14][0]*SKK_LOS[10] - P[14][3]*SKK_LOS[13] + P[14][1]*SKK_LOS[11] + P[14][2]*SKK_LOS[12] - P[14][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[14][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[14][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[14][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[14][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[15] = SK_LOS[1]*(P[15][0]*SKK_LOS[10] - P[15][3]*SKK_LOS[13] + P[15][1]*SKK_LOS[11] + P[15][2]*SKK_LOS[12] - P[15][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[15][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[15][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[15][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[15][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[16] = SK_LOS[1]*(P[16][0]*SKK_LOS[10] - P[16][3]*SKK_LOS[13] + P[16][1]*SKK_LOS[11] + P[16][2]*SKK_LOS[12] - P[16][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[16][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[16][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[16][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[16][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[17] = SK_LOS[1]*(P[17][0]*SKK_LOS[10] - P[17][3]*SKK_LOS[13] + P[17][1]*SKK_LOS[11] + P[17][2]*SKK_LOS[12] - P[17][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[17][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[17][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[17][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[17][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[18] = SK_LOS[1]*(P[18][0]*SKK_LOS[10] - P[18][3]*SKK_LOS[13] + P[18][1]*SKK_LOS[11] + P[18][2]*SKK_LOS[12] - P[18][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[18][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[18][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[18][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[18][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[19] = SK_LOS[1]*(P[19][0]*SKK_LOS[10] - P[19][3]*SKK_LOS[13] + P[19][1]*SKK_LOS[11] + P[19][2]*SKK_LOS[12] - P[19][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[19][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[19][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[19][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[19][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[20] = SK_LOS[1]*(P[20][0]*SKK_LOS[10] - P[20][3]*SKK_LOS[13] + P[20][1]*SKK_LOS[11] + P[20][2]*SKK_LOS[12] - P[20][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[20][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[20][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[20][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[20][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[21] = SK_LOS[1]*(P[21][0]*SKK_LOS[10] - P[21][3]*SKK_LOS[13] + P[21][1]*SKK_LOS[11] + P[21][2]*SKK_LOS[12] - P[21][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[21][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[21][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[21][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[21][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// Kfusion[22] = SK_LOS[1]*(P[22][0]*SKK_LOS[10] - P[22][3]*SKK_LOS[13] + P[22][1]*SKK_LOS[11] + P[22][2]*SKK_LOS[12] - P[22][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[22][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[22][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); +// varInnovOptFlow[1] = 1.0f/SK_LOS[1]; +// innovOptFlow[1] = losPred[1] - losData[1]; + +// // reset the observation index +// obsIndex = 0; +// fuseOptFlowData = false; +// } + +// // Check the innovation for consistency and don't fuse if > 3Sigma +// if ((innovOptFlow[obsIndex]*innovOptFlow[obsIndex]/varInnovOptFlow[obsIndex]) < 9.0f) +// { +// // correct the state vector +// for (uint8_t j = 0; j < n_states; j++) +// { +// states[j] = states[j] - Kfusion[j] * innovOptFlow[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-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 KH to reduce the +// // number of operations +// for (uint8_t i = 0; i < n_states; i++) +// { +// for (uint8_t j = 0; j <= 6; j++) +// { +// KH[i][j] = Kfusion[i] * H_LOS[j]; +// } +// for (uint8_t j = 7; j <= 8; j++) +// { +// KH[i][j] = 0.0f; +// } +// KH[i][9] = Kfusion[i] * H_LOS[9]; +// for (uint8_t j = 10; j <= 21; j++) +// { +// KH[i][j] = 0.0f; +// } +// KH[i][22] = Kfusion[i] * H_LOS[22]; +// } +// for (uint8_t i = 0; i < n_states; i++) +// { +// for (uint8_t j = 0; j < n_states; j++) +// { +// KHP[i][j] = 0.0f; +// for (uint8_t k = 0; k <= 6; k++) +// { +// KHP[i][j] = KHP[i][j] + KH[i][k] * P[k][j]; +// } +// KHP[i][j] = KHP[i][j] + KH[i][9] * P[9][j]; +// KHP[i][j] = KHP[i][j] + KH[i][22] * P[2][j]; +// } +// } +// } +// for (uint8_t i = 0; i < n_states; i++) +// { +// for (uint8_t j = 0; j < n_states; j++) +// { +// P[i][j] = P[i][j] - KHP[i][j]; +// } +// } +// ForceSymmetry(); +// ConstrainVariances(); +// } +} -// Perform sequential fusion of optical flow measurements only when in the air and tilt is less than 30 deg. - if (useOpticalFlow && (fuseOptFlowData || obsIndex == 1) && !onGround && Tbs.z.z > 0.866f && rngMea > 5.0f && rngMea < 39.0f) - { - // Sequential fusion of XY components to spread processing load across - // two prediction time steps. +/* +Estimation of optical flow sensor focal length scale factor and terrain height using a two state EKF +This fiter requires optical flow rates that are not motion compensated +Range to ground measurement is assumed to be via a narrow beam type sensor - eg laser +*/ +void AttPosEKF::GroundEKF() +{ + // propagate ground position state noise each time this is called using the difference in position since the last observations and an RMS gradient assumption + // limit distance to prevent intialisation afer bad gps causing bad numerical conditioning + if (!inhibitGndState) { + float distanceTravelledSq; + distanceTravelledSq = sq(statesAtRngTime[7] - prevPosN) + sq(statesAtRngTime[8] - prevPosE); + prevPosN = statesAtRngTime[7]; + prevPosE = statesAtRngTime[8]; + distanceTravelledSq = min(distanceTravelledSq, 100.0f); + Popt[1][1] += (distanceTravelledSq * sq(gndHgtSigma)); + } + // we aren't using optical flow measurements in this hacked implementation so set the covariances for this state to zero to avoid numerical problems + Popt[0][0] = 0.0f; + Popt[0][1] = 0.0f; + Popt[1][0] = 0.0f; + + // Fuse range finder data + // Need to check that our range finder tilt angle is less than 30 degrees + float cosRngTilt = - Tbn.z.x * sinf(rngFinderPitch) + Tbn.z.z * cosf(rngFinderPitch); + if (useRangeFinder && fuseRngData && cosRngTilt > 0.87f) { + float range; // range from camera to centre of image + float q0; // quaternion at optical flow measurement time + float q1; // quaternion at optical flow measurement time + float q2; // quaternion at optical flow measurement time + float q3; // quaternion at optical flow measurement time + float R_RNG = 0.5; // range measurement variance (m^2) TODO make this a function of range and tilt to allow for sensor, alignment and AHRS errors + + // Copy required states to local variable names + q0 = statesAtRngTime[0]; + q1 = statesAtRngTime[1]; + q2 = statesAtRngTime[2]; + q3 = statesAtRngTime[3]; + + // calculate Kalman gains + float SK_RNG[3]; + SK_RNG[0] = sq(q0) - sq(q1) - sq(q2) + sq(q3); + SK_RNG[1] = 1/(R_RNG + Popt[1][1]/sq(SK_RNG[0])); + SK_RNG[2] = 1/SK_RNG[0]; + float K_RNG[2]; + if (!inhibitScaleState) { + K_RNG[0] = Popt[0][1]*SK_RNG[1]*SK_RNG[2]; + } else { + K_RNG[0] = 0.0f; + } + if (!inhibitGndState) { + K_RNG[1] = Popt[1][1]*SK_RNG[1]*SK_RNG[2]; + } else { + K_RNG[1] = 0.0f; + } - // Calculate observation jacobians and Kalman gains - if (fuseOptFlowData) - { - // Copy required states to local variable names - q0 = statesAtOptFlowTime[0]; - q1 = statesAtOptFlowTime[1]; - q2 = statesAtOptFlowTime[2]; - q3 = statesAtOptFlowTime[3]; - vn = statesAtOptFlowTime[4]; - ve = statesAtOptFlowTime[5]; - vd = statesAtOptFlowTime[6]; - pd = statesAtOptFlowTime[9]; - ptd = statesAtOptFlowTime[22]; - velNED_local.x = vn; - velNED_local.y = ve; - velNED_local.z = vd; - - // calculate rotation from NED to body axes - float q00 = sq(q0); - float q11 = sq(q1); - float q22 = sq(q2); - float q33 = sq(q3); - float q01 = q0 * q1; - float q02 = q0 * q2; - float q03 = q0 * q3; - float q12 = q1 * q2; - float q13 = q1 * q3; - float q23 = q2 * q3; - Tnb_local.x.x = q00 + q11 - q22 - q33; - Tnb_local.y.y = q00 - q11 + q22 - q33; - Tnb_local.z.z = q00 - q11 - q22 + q33; - Tnb_local.y.x = 2*(q12 - q03); - Tnb_local.z.x = 2*(q13 + q02); - Tnb_local.x.y = 2*(q12 + q03); - Tnb_local.z.y = 2*(q23 - q01); - Tnb_local.x.z = 2*(q13 - q02); - Tnb_local.y.z = 2*(q23 + q01); - - // calculate transformation from NED to sensor axes - Tns = Tbs*Tnb_local; - - // calculate range from ground plain to centre of sensor fov assuming flat earth - float range = ConstrainFloat(((ptd - pd)/Tns.z.z),0.5f,100.0f); - - // calculate relative velocity in sensor frame - relVelSensor = Tns*velNED_local; - - // divide velocity by range and include angular rate effects to get predicted angular LOS rates relative to X and Y axes - losPred[0] = relVelSensor.y/range; - losPred[1] = -relVelSensor.x/range; - - //printf("relVelSensor.x=%5.1f, relVelSensor.y=%5.1f\n", relVelSensor.x, relVelSensor.y); - //printf("Xpred=%5.2f, Xmea=%5.2f, Ypred=%5.2f, Ymea=%5.2f, delAng.x=%4.4f, delAng.y=%4.4f\n", losPred[0], losData[0], losPred[1], losData[1], delAng.x, delAng.y); - //printf("omegaX=%5.2f, omegaY=%5.2f, velY=%5.1f velX=%5.1f\n, range=%5.1f\n", delAngRel.x/dt, delAngRel.y/dt, relVelSensor.y, relVelSensor.x, range); + // Calculate the innovation variance for data logging + varInnovRng = 1.0f/SK_RNG[1]; - // Calculate observation jacobians - SH_LOS[0] = a1*(2*q0*q1 + 2*q2*q3) + a2*(2*q0*q2 - 2*q1*q3) - sq(q0) + sq(q1) + sq(q2) - sq(q3); - SH_LOS[1] = vd*(a2*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + 2*q0*q2 - 2*q1*q3 - a3*(2*q0*q1 + 2*q2*q3)) - ve*(a3*(sq(q0) - sq(q1) + sq(q2) - sq(q3)) + 2*q0*q3 + 2*q1*q2 + a2*(2*q0*q1 - 2*q2*q3)) + vn*(a2*(2*q0*q2 + 2*q1*q3) + a3*(2*q0*q3 - 2*q1*q2) - sq(q0) - sq(q1) + sq(q2) + sq(q3)); - SH_LOS[2] = ve*(a1*(2*q0*q1 - 2*q2*q3) + a3*(2*q0*q3 + 2*q1*q2) - sq(q0) + sq(q1) - sq(q2) + sq(q3)) - vd*(a1*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + 2*q0*q1 + 2*q2*q3 + a3*(2*q0*q2 - 2*q1*q3)) + vn*(a3*(sq(q0) + sq(q1) - sq(q2) - sq(q3)) + 2*q0*q3 - 2*q1*q2 - a1*(2*q0*q2 + 2*q1*q3)); - SH_LOS[3] = 1/(pd - ptd); - SH_LOS[4] = 2*q1 - 2*a2*q3 + 2*a3*q2; - SH_LOS[5] = 2*a2*q2 - 2*q0 + 2*a3*q3; - SH_LOS[6] = 2*q2 + 2*a2*q0 - 2*a3*q1; - SH_LOS[7] = 1/sq(pd - ptd); - SH_LOS[8] = 2*q2 + 2*a1*q3 - 2*a3*q1; - SH_LOS[9] = 2*q3 - 2*a1*q2 + 2*a3*q0; - SH_LOS[10] = 2*a1*q1 - 2*q0 + 2*a3*q3; - SH_LOS[11] = 2*q3 + 2*a2*q1 + 2*a3*q0; - SH_LOS[12] = 2*q1 + 2*a1*q0 + 2*a3*q2; - - for (uint8_t i = 0; i < n_states; i++) H_LOS[i] = 0; - H_LOS[0] = - SH_LOS[2]*SH_LOS[3]*(2*a1*q1 - 2*q0 + 2*a2*q2) - SH_LOS[0]*SH_LOS[3]*(ve*SH_LOS[10] - vd*SH_LOS[12] + vn*SH_LOS[9]); - H_LOS[1] = - SH_LOS[2]*SH_LOS[3]*(2*q1 + 2*a1*q0 - 2*a2*q3) - SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[10] + ve*SH_LOS[12] - vn*SH_LOS[8]); - H_LOS[2] = SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[9] + ve*SH_LOS[8] + vn*SH_LOS[12]) - SH_LOS[2]*SH_LOS[3]*(2*q2 + 2*a2*q0 + 2*a1*q3); - H_LOS[3] = SH_LOS[2]*SH_LOS[3]*(2*q3 - 2*a1*q2 + 2*a2*q1) + SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[8] - ve*SH_LOS[9] + vn*SH_LOS[10]); - H_LOS[4] = -SH_LOS[0]*SH_LOS[3]*(a3*(sq(q0) + sq(q1) - sq(q2) - sq(q3)) + 2*q0*q3 - 2*q1*q2 - a1*(2*q0*q2 + 2*q1*q3)); - H_LOS[5] = -SH_LOS[0]*SH_LOS[3]*(a1*(2*q0*q1 - 2*q2*q3) + a3*(2*q0*q3 + 2*q1*q2) - sq(q0) + sq(q1) - sq(q2) + sq(q3)); - H_LOS[6] = SH_LOS[0]*SH_LOS[3]*(a1*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + 2*q0*q1 + 2*q2*q3 + a3*(2*q0*q2 - 2*q1*q3)); - H_LOS[9] = SH_LOS[0]*SH_LOS[2]*SH_LOS[7]; - H_LOS[22] = -SH_LOS[0]*SH_LOS[2]*SH_LOS[7]; + // constrain terrain height to be below the vehicle + flowStates[1] = maxf(flowStates[1], statesAtRngTime[9] + minFlowRng); - // Calculate Kalman gain - SKK_LOS[0] = a2*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + 2*q0*q2 - 2*q1*q3 - a3*(2*q0*q1 + 2*q2*q3); - SKK_LOS[1] = a3*(sq(q0) - sq(q1) + sq(q2) - sq(q3)) + 2*q0*q3 + 2*q1*q2 + a2*(2*q0*q1 - 2*q2*q3); - SKK_LOS[2] = a2*(2*q0*q2 + 2*q1*q3) + a3*(2*q0*q3 - 2*q1*q2) - sq(q0) - sq(q1) + sq(q2) + sq(q3); - SKK_LOS[3] = a1*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + 2*q0*q1 + 2*q2*q3 + a3*(2*q0*q2 - 2*q1*q3); - SKK_LOS[4] = a1*(2*q0*q1 - 2*q2*q3) + a3*(2*q0*q3 + 2*q1*q2) - sq(q0) + sq(q1) - sq(q2) + sq(q3); - SKK_LOS[5] = a3*(sq(q0) + sq(q1) - sq(q2) - sq(q3)) + 2*q0*q3 - 2*q1*q2 - a1*(2*q0*q2 + 2*q1*q3); - SKK_LOS[6] = SH_LOS[2]*SH_LOS[3]*(2*q3 - 2*a1*q2 + 2*a2*q1) + SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[8] - ve*SH_LOS[9] + vn*SH_LOS[10]); - SKK_LOS[7] = SH_LOS[2]*SH_LOS[3]*(2*q1 + 2*a1*q0 - 2*a2*q3) + SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[10] + ve*SH_LOS[12] - vn*SH_LOS[8]); - SKK_LOS[8] = SH_LOS[2]*SH_LOS[3]*(2*a1*q1 - 2*q0 + 2*a2*q2) + SH_LOS[0]*SH_LOS[3]*(ve*SH_LOS[10] - vd*SH_LOS[12] + vn*SH_LOS[9]); - SKK_LOS[9] = SH_LOS[2]*SH_LOS[3]*(2*q2 + 2*a2*q0 + 2*a1*q3) - SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[9] + ve*SH_LOS[8] + vn*SH_LOS[12]); - SKK_LOS[10] = SH_LOS[1]*SH_LOS[3]*(2*a1*q1 - 2*q0 + 2*a2*q2) + SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[6] - ve*SH_LOS[11] + vn*SH_LOS[5]); - SKK_LOS[11] = SH_LOS[1]*SH_LOS[3]*(2*q1 + 2*a1*q0 - 2*a2*q3) - SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[11] + ve*SH_LOS[6] + vn*SH_LOS[4]); - SKK_LOS[12] = SH_LOS[1]*SH_LOS[3]*(2*q2 + 2*a2*q0 + 2*a1*q3) - SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[5] + ve*SH_LOS[4] - vn*SH_LOS[6]); - SKK_LOS[13] = SH_LOS[1]*SH_LOS[3]*(2*q3 - 2*a1*q2 + 2*a2*q1) - SH_LOS[0]*SH_LOS[3]*(ve*SH_LOS[5] - vd*SH_LOS[4] + vn*SH_LOS[11]); - SKK_LOS[14] = SH_LOS[0]; - - SK_LOS[0] = 1/(R_LOS + SKK_LOS[8]*(P[0][0]*SKK_LOS[8] + P[1][0]*SKK_LOS[7] + P[2][0]*SKK_LOS[9] - P[3][0]*SKK_LOS[6] - P[9][0]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][0]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][0]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][0]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][0]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) + SKK_LOS[7]*(P[0][1]*SKK_LOS[8] + P[1][1]*SKK_LOS[7] + P[2][1]*SKK_LOS[9] - P[3][1]*SKK_LOS[6] - P[9][1]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][1]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][1]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][1]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][1]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) + SKK_LOS[9]*(P[0][2]*SKK_LOS[8] + P[1][2]*SKK_LOS[7] + P[2][2]*SKK_LOS[9] - P[3][2]*SKK_LOS[6] - P[9][2]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][2]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][2]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][2]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][2]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) - SKK_LOS[6]*(P[0][3]*SKK_LOS[8] + P[1][3]*SKK_LOS[7] + P[2][3]*SKK_LOS[9] - P[3][3]*SKK_LOS[6] - P[9][3]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][3]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][3]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][3]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][3]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) - SH_LOS[2]*SH_LOS[7]*SKK_LOS[14]*(P[0][9]*SKK_LOS[8] + P[1][9]*SKK_LOS[7] + P[2][9]*SKK_LOS[9] - P[3][9]*SKK_LOS[6] - P[9][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][9]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][9]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][9]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) + SH_LOS[2]*SH_LOS[7]*SKK_LOS[14]*(P[0][22]*SKK_LOS[8] + P[1][22]*SKK_LOS[7] + P[2][22]*SKK_LOS[9] - P[3][22]*SKK_LOS[6] - P[9][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][22]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][22]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][22]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) + SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14]*(P[0][4]*SKK_LOS[8] + P[1][4]*SKK_LOS[7] + P[2][4]*SKK_LOS[9] - P[3][4]*SKK_LOS[6] - P[9][4]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][4]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][4]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][4]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) + SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14]*(P[0][5]*SKK_LOS[8] + P[1][5]*SKK_LOS[7] + P[2][5]*SKK_LOS[9] - P[3][5]*SKK_LOS[6] - P[9][5]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][5]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][5]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][5]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]) - SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]*(P[0][6]*SKK_LOS[8] + P[1][6]*SKK_LOS[7] + P[2][6]*SKK_LOS[9] - P[3][6]*SKK_LOS[6] - P[9][6]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][6]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][6]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][6]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14])); - Kfusion[0] = -SK_LOS[0]*(P[0][0]*SKK_LOS[8] + P[0][1]*SKK_LOS[7] - P[0][3]*SKK_LOS[6] + P[0][2]*SKK_LOS[9] - P[0][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[0][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[0][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[0][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[0][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[1] = -SK_LOS[0]*(P[1][0]*SKK_LOS[8] + P[1][1]*SKK_LOS[7] - P[1][3]*SKK_LOS[6] + P[1][2]*SKK_LOS[9] - P[1][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[1][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[1][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[1][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[1][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[2] = -SK_LOS[0]*(P[2][0]*SKK_LOS[8] + P[2][1]*SKK_LOS[7] - P[2][3]*SKK_LOS[6] + P[2][2]*SKK_LOS[9] - P[2][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[2][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[2][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[2][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[2][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[3] = -SK_LOS[0]*(P[3][0]*SKK_LOS[8] + P[3][1]*SKK_LOS[7] - P[3][3]*SKK_LOS[6] + P[3][2]*SKK_LOS[9] - P[3][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[3][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[3][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[3][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[3][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[4] = -SK_LOS[0]*(P[4][0]*SKK_LOS[8] + P[4][1]*SKK_LOS[7] - P[4][3]*SKK_LOS[6] + P[4][2]*SKK_LOS[9] - P[4][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[4][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[4][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[4][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[5] = -SK_LOS[0]*(P[5][0]*SKK_LOS[8] + P[5][1]*SKK_LOS[7] - P[5][3]*SKK_LOS[6] + P[5][2]*SKK_LOS[9] - P[5][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[5][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[5][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[5][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[5][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[6] = -SK_LOS[0]*(P[6][0]*SKK_LOS[8] + P[6][1]*SKK_LOS[7] - P[6][3]*SKK_LOS[6] + P[6][2]*SKK_LOS[9] - P[6][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[6][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[6][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[6][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[6][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[7] = -SK_LOS[0]*(P[7][0]*SKK_LOS[8] + P[7][1]*SKK_LOS[7] - P[7][3]*SKK_LOS[6] + P[7][2]*SKK_LOS[9] - P[7][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[7][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[7][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[7][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[7][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[8] = -SK_LOS[0]*(P[8][0]*SKK_LOS[8] + P[8][1]*SKK_LOS[7] - P[8][3]*SKK_LOS[6] + P[8][2]*SKK_LOS[9] - P[8][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[8][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[8][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[8][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[8][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[9] = -SK_LOS[0]*(P[9][0]*SKK_LOS[8] + P[9][1]*SKK_LOS[7] - P[9][3]*SKK_LOS[6] + P[9][2]*SKK_LOS[9] - P[9][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[9][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[9][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[9][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[9][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[10] = -SK_LOS[0]*(P[10][0]*SKK_LOS[8] + P[10][1]*SKK_LOS[7] - P[10][3]*SKK_LOS[6] + P[10][2]*SKK_LOS[9] - P[10][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[10][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[10][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[10][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[10][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[11] = -SK_LOS[0]*(P[11][0]*SKK_LOS[8] + P[11][1]*SKK_LOS[7] - P[11][3]*SKK_LOS[6] + P[11][2]*SKK_LOS[9] - P[11][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[11][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[11][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[11][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[11][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[12] = -SK_LOS[0]*(P[12][0]*SKK_LOS[8] + P[12][1]*SKK_LOS[7] - P[12][3]*SKK_LOS[6] + P[12][2]*SKK_LOS[9] - P[12][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[12][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[12][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[12][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[12][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[13] = 0.0f;//-SK_LOS[0]*(P[13][0]*SKK_LOS[8] + P[13][1]*SKK_LOS[7] - P[13][3]*SKK_LOS[6] + P[13][2]*SKK_LOS[9] - P[13][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[13][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[13][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[13][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[13][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[14] = -SK_LOS[0]*(P[14][0]*SKK_LOS[8] + P[14][1]*SKK_LOS[7] - P[14][3]*SKK_LOS[6] + P[14][2]*SKK_LOS[9] - P[14][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[14][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[14][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[14][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[14][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[15] = -SK_LOS[0]*(P[15][0]*SKK_LOS[8] + P[15][1]*SKK_LOS[7] - P[15][3]*SKK_LOS[6] + P[15][2]*SKK_LOS[9] - P[15][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[15][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[15][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[15][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[15][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[16] = -SK_LOS[0]*(P[16][0]*SKK_LOS[8] + P[16][1]*SKK_LOS[7] - P[16][3]*SKK_LOS[6] + P[16][2]*SKK_LOS[9] - P[16][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[16][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[16][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[16][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[16][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[17] = -SK_LOS[0]*(P[17][0]*SKK_LOS[8] + P[17][1]*SKK_LOS[7] - P[17][3]*SKK_LOS[6] + P[17][2]*SKK_LOS[9] - P[17][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[17][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[17][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[17][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[17][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[18] = -SK_LOS[0]*(P[18][0]*SKK_LOS[8] + P[18][1]*SKK_LOS[7] - P[18][3]*SKK_LOS[6] + P[18][2]*SKK_LOS[9] - P[18][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[18][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[18][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[18][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[18][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[19] = -SK_LOS[0]*(P[19][0]*SKK_LOS[8] + P[19][1]*SKK_LOS[7] - P[19][3]*SKK_LOS[6] + P[19][2]*SKK_LOS[9] - P[19][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[19][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[19][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[19][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[19][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[20] = -SK_LOS[0]*(P[20][0]*SKK_LOS[8] + P[20][1]*SKK_LOS[7] - P[20][3]*SKK_LOS[6] + P[20][2]*SKK_LOS[9] - P[20][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[20][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[20][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[20][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[20][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[21] = -SK_LOS[0]*(P[21][0]*SKK_LOS[8] + P[21][1]*SKK_LOS[7] - P[21][3]*SKK_LOS[6] + P[21][2]*SKK_LOS[9] - P[21][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[21][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[21][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[21][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[21][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - Kfusion[22] = -SK_LOS[0]*(P[22][0]*SKK_LOS[8] + P[22][1]*SKK_LOS[7] - P[22][3]*SKK_LOS[6] + P[22][2]*SKK_LOS[9] - P[22][9]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][22]*SH_LOS[2]*SH_LOS[7]*SKK_LOS[14] + P[22][4]*SH_LOS[3]*SKK_LOS[5]*SKK_LOS[14] + P[22][5]*SH_LOS[3]*SKK_LOS[4]*SKK_LOS[14] - P[22][6]*SH_LOS[3]*SKK_LOS[3]*SKK_LOS[14]); - varInnovOptFlow[0] = 1.0f/SK_LOS[0]; - innovOptFlow[0] = losPred[0] - losData[0]; - - // reset the observation index to 0 (we start by fusing the X - // measurement) - obsIndex = 0; - fuseOptFlowData = false; - } - else if (obsIndex == 1) // we are now fusing the Y measurement - { - // Calculate observation jacobians - for (uint8_t i = 0; i < n_states; i++) H_LOS[i] = 0; - H_LOS[0] = SH_LOS[1]*SH_LOS[3]*(2*a1*q1 - 2*q0 + 2*a2*q2) + SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[6] - ve*SH_LOS[11] + vn*SH_LOS[5]); - H_LOS[1] = SH_LOS[1]*SH_LOS[3]*(2*q1 + 2*a1*q0 - 2*a2*q3) - SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[11] + ve*SH_LOS[6] + vn*SH_LOS[4]); - H_LOS[2] = SH_LOS[1]*SH_LOS[3]*(2*q2 + 2*a2*q0 + 2*a1*q3) - SH_LOS[0]*SH_LOS[3]*(vd*SH_LOS[5] + ve*SH_LOS[4] - vn*SH_LOS[6]); - H_LOS[3] = SH_LOS[0]*SH_LOS[3]*(ve*SH_LOS[5] - vd*SH_LOS[4] + vn*SH_LOS[11]) - SH_LOS[1]*SH_LOS[3]*(2*q3 - 2*a1*q2 + 2*a2*q1); - H_LOS[4] = SH_LOS[0]*SH_LOS[3]*(a2*(2*q0*q2 + 2*q1*q3) + a3*(2*q0*q3 - 2*q1*q2) - sq(q0) - sq(q1) + sq(q2) + sq(q3)); - H_LOS[5] = -SH_LOS[0]*SH_LOS[3]*(a3*(sq(q0) - sq(q1) + sq(q2) - sq(q3)) + 2*q0*q3 + 2*q1*q2 + a2*(2*q0*q1 - 2*q2*q3)); - H_LOS[6] = SH_LOS[0]*SH_LOS[3]*(a2*(sq(q0) - sq(q1) - sq(q2) + sq(q3)) + 2*q0*q2 - 2*q1*q3 - a3*(2*q0*q1 + 2*q2*q3)); - H_LOS[9] = -SH_LOS[0]*SH_LOS[1]*SH_LOS[7]; - H_LOS[22] = SH_LOS[0]*SH_LOS[1]*SH_LOS[7]; - - // Calculate Kalman gains - SK_LOS[1] = 1/(R_LOS + SKK_LOS[12]*(P[0][2]*SKK_LOS[10] + P[1][2]*SKK_LOS[11] + P[2][2]*SKK_LOS[12] - P[3][2]*SKK_LOS[13] - P[9][2]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][2]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][2]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][2]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][2]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) - SKK_LOS[13]*(P[0][3]*SKK_LOS[10] + P[1][3]*SKK_LOS[11] + P[2][3]*SKK_LOS[12] - P[3][3]*SKK_LOS[13] - P[9][3]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][3]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][3]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][3]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][3]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) + SKK_LOS[10]*(P[0][0]*SKK_LOS[10] + P[1][0]*SKK_LOS[11] + P[2][0]*(SH_LOS[1]*SH_LOS[3]*(2*q2 + 2*a2*q0 + 2*a1*q3) - SH_LOS[3]*SKK_LOS[14]*(vd*SH_LOS[5] + ve*SH_LOS[4] - vn*SH_LOS[6])) - P[3][0]*(SH_LOS[1]*SH_LOS[3]*(2*q3 - 2*a1*q2 + 2*a2*q1) - SH_LOS[3]*SKK_LOS[14]*(ve*SH_LOS[5] - vd*SH_LOS[4] + vn*SH_LOS[11])) - P[9][0]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][0]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][0]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][0]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][0]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) + SKK_LOS[11]*(P[0][1]*SKK_LOS[10] + P[1][1]*SKK_LOS[11] + P[2][1]*(SH_LOS[1]*SH_LOS[3]*(2*q2 + 2*a2*q0 + 2*a1*q3) - SH_LOS[3]*SKK_LOS[14]*(vd*SH_LOS[5] + ve*SH_LOS[4] - vn*SH_LOS[6])) - P[3][1]*(SH_LOS[1]*SH_LOS[3]*(2*q3 - 2*a1*q2 + 2*a2*q1) - SH_LOS[3]*SKK_LOS[14]*(ve*SH_LOS[5] - vd*SH_LOS[4] + vn*SH_LOS[11])) - P[9][1]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][1]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][1]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][1]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][1]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) - SH_LOS[1]*SH_LOS[7]*SKK_LOS[14]*(P[0][9]*SKK_LOS[10] + P[1][9]*SKK_LOS[11] + P[2][9]*SKK_LOS[12] - P[3][9]*SKK_LOS[13] - P[9][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][9]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][9]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][9]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) + SH_LOS[1]*SH_LOS[7]*SKK_LOS[14]*(P[0][22]*SKK_LOS[10] + P[1][22]*SKK_LOS[11] + P[2][22]*SKK_LOS[12] - P[3][22]*SKK_LOS[13] - P[9][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][22]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][22]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][22]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) + SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14]*(P[0][4]*SKK_LOS[10] + P[1][4]*SKK_LOS[11] + P[2][4]*SKK_LOS[12] - P[3][4]*SKK_LOS[13] - P[9][4]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][4]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][4]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][4]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) - SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]*(P[0][5]*SKK_LOS[10] + P[1][5]*SKK_LOS[11] + P[2][5]*SKK_LOS[12] - P[3][5]*SKK_LOS[13] - P[9][5]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][5]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][5]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][5]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]) + SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14]*(P[0][6]*SKK_LOS[10] + P[1][6]*SKK_LOS[11] + P[2][6]*SKK_LOS[12] - P[3][6]*SKK_LOS[13] - P[9][6]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][6]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][6]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][6]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14] + P[6][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14])); - Kfusion[0] = SK_LOS[1]*(P[0][0]*SKK_LOS[10] - P[0][3]*SKK_LOS[13] + P[0][1]*SKK_LOS[11] + P[0][2]*SKK_LOS[12] - P[0][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[0][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[0][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[0][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[0][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[1] = SK_LOS[1]*(P[1][0]*SKK_LOS[10] - P[1][3]*SKK_LOS[13] + P[1][1]*SKK_LOS[11] + P[1][2]*SKK_LOS[12] - P[1][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[1][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[1][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[1][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[1][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[2] = SK_LOS[1]*(P[2][0]*SKK_LOS[10] - P[2][3]*SKK_LOS[13] + P[2][1]*SKK_LOS[11] + P[2][2]*SKK_LOS[12] - P[2][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[2][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[2][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[2][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[2][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[3] = SK_LOS[1]*(P[3][0]*SKK_LOS[10] - P[3][3]*SKK_LOS[13] + P[3][1]*SKK_LOS[11] + P[3][2]*SKK_LOS[12] - P[3][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[3][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[3][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[3][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[3][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[4] = SK_LOS[1]*(P[4][0]*SKK_LOS[10] - P[4][3]*SKK_LOS[13] + P[4][1]*SKK_LOS[11] + P[4][2]*SKK_LOS[12] - P[4][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[4][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[4][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[4][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[5] = SK_LOS[1]*(P[5][0]*SKK_LOS[10] - P[5][3]*SKK_LOS[13] + P[5][1]*SKK_LOS[11] + P[5][2]*SKK_LOS[12] - P[5][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[5][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[5][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[5][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[5][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[6] = SK_LOS[1]*(P[6][0]*SKK_LOS[10] - P[6][3]*SKK_LOS[13] + P[6][1]*SKK_LOS[11] + P[6][2]*SKK_LOS[12] - P[6][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[6][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[6][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[6][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[6][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[7] = SK_LOS[1]*(P[7][0]*SKK_LOS[10] - P[7][3]*SKK_LOS[13] + P[7][1]*SKK_LOS[11] + P[7][2]*SKK_LOS[12] - P[7][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[7][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[7][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[7][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[7][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[8] = SK_LOS[1]*(P[8][0]*SKK_LOS[10] - P[8][3]*SKK_LOS[13] + P[8][1]*SKK_LOS[11] + P[8][2]*SKK_LOS[12] - P[8][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[8][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[8][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[8][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[8][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[9] = SK_LOS[1]*(P[9][0]*SKK_LOS[10] - P[9][3]*SKK_LOS[13] + P[9][1]*SKK_LOS[11] + P[9][2]*SKK_LOS[12] - P[9][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[9][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[9][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[9][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[9][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[10] = SK_LOS[1]*(P[10][0]*SKK_LOS[10] - P[10][3]*SKK_LOS[13] + P[10][1]*SKK_LOS[11] + P[10][2]*SKK_LOS[12] - P[10][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[10][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[10][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[10][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[10][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[11] = SK_LOS[1]*(P[11][0]*SKK_LOS[10] - P[11][3]*SKK_LOS[13] + P[11][1]*SKK_LOS[11] + P[11][2]*SKK_LOS[12] - P[11][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[11][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[11][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[11][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[11][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[12] = SK_LOS[1]*(P[12][0]*SKK_LOS[10] - P[12][3]*SKK_LOS[13] + P[12][1]*SKK_LOS[11] + P[12][2]*SKK_LOS[12] - P[12][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[12][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[12][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[12][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[12][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[13] = 0.0f;//SK_LOS[1]*(P[13][0]*SKK_LOS[10] - P[13][3]*SKK_LOS[13] + P[13][1]*SKK_LOS[11] + P[13][2]*SKK_LOS[12] - P[13][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[13][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[13][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[13][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[13][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[14] = SK_LOS[1]*(P[14][0]*SKK_LOS[10] - P[14][3]*SKK_LOS[13] + P[14][1]*SKK_LOS[11] + P[14][2]*SKK_LOS[12] - P[14][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[14][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[14][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[14][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[14][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[15] = SK_LOS[1]*(P[15][0]*SKK_LOS[10] - P[15][3]*SKK_LOS[13] + P[15][1]*SKK_LOS[11] + P[15][2]*SKK_LOS[12] - P[15][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[15][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[15][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[15][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[15][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[16] = SK_LOS[1]*(P[16][0]*SKK_LOS[10] - P[16][3]*SKK_LOS[13] + P[16][1]*SKK_LOS[11] + P[16][2]*SKK_LOS[12] - P[16][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[16][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[16][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[16][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[16][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[17] = SK_LOS[1]*(P[17][0]*SKK_LOS[10] - P[17][3]*SKK_LOS[13] + P[17][1]*SKK_LOS[11] + P[17][2]*SKK_LOS[12] - P[17][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[17][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[17][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[17][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[17][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[18] = SK_LOS[1]*(P[18][0]*SKK_LOS[10] - P[18][3]*SKK_LOS[13] + P[18][1]*SKK_LOS[11] + P[18][2]*SKK_LOS[12] - P[18][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[18][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[18][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[18][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[18][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[19] = SK_LOS[1]*(P[19][0]*SKK_LOS[10] - P[19][3]*SKK_LOS[13] + P[19][1]*SKK_LOS[11] + P[19][2]*SKK_LOS[12] - P[19][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[19][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[19][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[19][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[19][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[20] = SK_LOS[1]*(P[20][0]*SKK_LOS[10] - P[20][3]*SKK_LOS[13] + P[20][1]*SKK_LOS[11] + P[20][2]*SKK_LOS[12] - P[20][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[20][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[20][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[20][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[20][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[21] = SK_LOS[1]*(P[21][0]*SKK_LOS[10] - P[21][3]*SKK_LOS[13] + P[21][1]*SKK_LOS[11] + P[21][2]*SKK_LOS[12] - P[21][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[21][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[21][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[21][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[21][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - Kfusion[22] = SK_LOS[1]*(P[22][0]*SKK_LOS[10] - P[22][3]*SKK_LOS[13] + P[22][1]*SKK_LOS[11] + P[22][2]*SKK_LOS[12] - P[22][9]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][22]*SH_LOS[1]*SH_LOS[7]*SKK_LOS[14] + P[22][6]*SH_LOS[3]*SKK_LOS[0]*SKK_LOS[14] + P[22][4]*SH_LOS[3]*SKK_LOS[2]*SKK_LOS[14] - P[22][5]*SH_LOS[3]*SKK_LOS[1]*SKK_LOS[14]); - varInnovOptFlow[1] = 1.0f/SK_LOS[1]; - innovOptFlow[1] = losPred[1] - losData[1]; - } + // estimate range to centre of image + range = (flowStates[1] - statesAtRngTime[9]) * SK_RNG[2]; - // Check the innovation for consistency and don't fuse if > 3Sigma - if ((innovOptFlow[obsIndex]*innovOptFlow[obsIndex]/varInnovOptFlow[obsIndex]) < 9.0f) - { - // correct the state vector - for (uint8_t j = 0; j < n_states; j++) - { - states[j] = states[j] - Kfusion[j] * innovOptFlow[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-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 KH to reduce the - // number of operations - for (uint8_t i = 0; i < n_states; i++) - { - for (uint8_t j = 0; j <= 6; j++) - { - KH[i][j] = Kfusion[i] * H_LOS[j]; - } - for (uint8_t j = 7; j <= 8; j++) - { - KH[i][j] = 0.0f; - } - KH[i][9] = Kfusion[i] * H_LOS[9]; - for (uint8_t j = 10; j <= 21; j++) - { - KH[i][j] = 0.0f; - } - KH[i][22] = Kfusion[i] * H_LOS[22]; - } - for (uint8_t i = 0; i < n_states; i++) - { - for (uint8_t j = 0; j < n_states; j++) - { - KHP[i][j] = 0.0f; - for (uint8_t k = 0; k <= 6; k++) - { - KHP[i][j] = KHP[i][j] + KH[i][k] * P[k][j]; - } - KHP[i][j] = KHP[i][j] + KH[i][9] * P[9][j]; - KHP[i][j] = KHP[i][j] + KH[i][22] * P[2][j]; - } - } - } - for (uint8_t i = 0; i < n_states; i++) + // Calculate the measurement innovation + innovRng = range - rngMea; + + // calculate the innovation consistency test ratio + auxRngTestRatio = sq(innovRng) / (sq(rngInnovGate) * varInnovRng); + + // Check the innovation for consistency and don't fuse if out of bounds + if (auxRngTestRatio < 1.0f) { - for (uint8_t j = 0; j < n_states; j++) - { - P[i][j] = P[i][j] - KHP[i][j]; + // correct the state + for (uint8_t i = 0; i < 2 ; i++) { + flowStates[i] -= K_RNG[i] * innovRng; } + // constrain the states + + // constrain focal length to 0.1 to 10 mm + flowStates[0] = ConstrainFloat(flowStates[0], 0.1f, 10.0f); + // constrain altitude + flowStates[1] = maxf(flowStates[1], statesAtRngTime[9] + minFlowRng); + + // correct the covariance matrix + float nextPopt[2][2]; + nextPopt[0][0] = Popt[0][0] - (Popt[0][1]*Popt[1][0]*SK_RNG[1]*SK_RNG[2]) * SK_RNG[2]; + nextPopt[0][1] = Popt[0][1] - (Popt[0][1]*Popt[1][1]*SK_RNG[1]*SK_RNG[2]) * SK_RNG[2]; + nextPopt[1][0] = -Popt[1][0]*((Popt[1][1]*SK_RNG[1]*SK_RNG[2]) * SK_RNG[2] - 1.0f); + nextPopt[1][1] = -Popt[1][1]*((Popt[1][1]*SK_RNG[1]*SK_RNG[2]) * SK_RNG[2] - 1.0f); + // prevent the state variances from becoming negative and maintain symmetry + Popt[0][0] = maxf(nextPopt[0][0],0.0f); + Popt[1][1] = maxf(nextPopt[1][1],0.0f); + Popt[0][1] = 0.5f * (nextPopt[0][1] + nextPopt[1][0]); + Popt[1][0] = Popt[0][1]; } } - obsIndex = obsIndex + 1; - ForceSymmetry(); - ConstrainVariances(); } void AttPosEKF::zeroCols(float (&covMat)[n_states][n_states], uint8_t first, uint8_t last) @@ -2126,6 +2304,24 @@ float AttPosEKF::sq(float valIn) return valIn*valIn; } +float AttPosEKF::maxf(float valIn1, float valIn2) +{ + if (valIn1 >= valIn2) { + return valIn1; + } else { + return valIn2; + } +} + +float AttPosEKF::min(float valIn1, float valIn2) +{ + if (valIn1 <= valIn2) { + return valIn1; + } else { + return valIn2; + } +} + // Store states in a history array along with time stamp void AttPosEKF::StoreStates(uint64_t timestamp_ms) { @@ -2322,9 +2518,9 @@ void AttPosEKF::OnGroundCheck() } // don't update terrain offset state if on ground if (onGround) { - inhibitGndHgtState = true; + inhibitGndState = true; } else { - inhibitGndHgtState = false; + inhibitGndState = false; } } @@ -3006,9 +3202,14 @@ void AttPosEKF::ZeroVariables() { // Initialize on-init initialized variables - + dtIMUfilt = ConstrainFloat(dtIMU, 0.001f, 0.02f); + dtVelPosFilt = ConstrainFloat(dtVelPos, 0.04f, 0.5f); + dtGpsFilt = 1.0f / 5.0f; + dtHgtFilt = 1.0f / 100.0f; storeIndex = 0; + lastVelPosFusion = millis(); + // Do the data structure init for (unsigned i = 0; i < n_states; i++) { for (unsigned j = 0; j < n_states; j++) { @@ -3028,6 +3229,13 @@ void AttPosEKF::ZeroVariables() dVelIMU.zero(); lastGyroOffset.zero(); + windSpdFiltNorth = 0.0f; + windSpdFiltEast = 0.0f; + // setting the altitude to zero will give us a higher + // gain to adjust faster in the first step + windSpdFiltAltitude = 0.0f; + windSpdFiltClimb = 0.0f; + for (unsigned i = 0; i < data_buffer_size; i++) { for (unsigned j = 0; j < n_states; j++) { diff --git a/src/modules/ekf_att_pos_estimator/estimator_23states.h b/src/modules/ekf_att_pos_estimator/estimator_23states.h index faa6735ca..a607955a8 100644 --- a/src/modules/ekf_att_pos_estimator/estimator_23states.h +++ b/src/modules/ekf_att_pos_estimator/estimator_23states.h @@ -80,6 +80,14 @@ public: airspeedMeasurementSigma = 1.4f; gyroProcessNoise = 1.4544411e-2f; accelProcessNoise = 0.5f; + + gndHgtSigma = 0.1f; // terrain gradient 1-sigma + R_LOS = 0.03f; // optical flow measurement noise variance (rad/sec)^2 + flowInnovGate = 3.0f; // number of standard deviations applied to the optical flow innovation consistency check + auxFlowInnovGate = 10.0f; // number of standard deviations applied to the optical flow innovation consistency check used by the auxiliary filter + rngInnovGate = 10.0f; // number of standard deviations applied to the rnage finder innovation consistency check + minFlowRng = 0.01f; //minimum range between ground and flow sensor + moCompR_LOS = 0.2; // scaler from sensor gyro rate to uncertainty in LOS rate } struct mag_state_struct { @@ -116,13 +124,16 @@ public: 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 + // Times + uint64_t lastVelPosFusion; // the time of the last velocity fusion, in the standard time unit of the filter + 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 - float statesAtOptFlowTime[n_states]; // States at the effective optical flow measurement time + float statesAtFlowTime[n_states]; // States at the effective optical flow 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) @@ -140,7 +151,16 @@ public: 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) + float dtIMU; // time lapsed since the last IMU measurement or covariance update (sec), this may have significant jitter + float dtIMUfilt; // average time between IMU measurements (sec) + float dtVelPos; // time lapsed since the last position / velocity fusion (seconds), this may have significant jitter + float dtVelPosFilt; // average time between position / velocity fusion steps + float dtHgtFilt; // average time between height measurement updates + float dtGpsFilt; // average time between gps measurement updates + float windSpdFiltNorth; // average wind speed north component + float windSpdFiltEast; // average wind speed east component + float windSpdFiltAltitude; // the last altitude used to filter wind speed + float windSpdFiltClimb; // filtered climb rate 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 @@ -192,7 +212,8 @@ public: bool inhibitWindStates; // true when wind states and covariances are to remain constant bool inhibitMagStates; // true when magnetic field states and covariances are to remain constant - bool inhibitGndHgtState; // true when the terrain ground height offset state and covariances are to remain constant + bool inhibitGndState; // true when the terrain ground height offset state and covariances are to remain constant + bool inhibitScaleState; // true when the focal length scale factor state and covariances are to remain constant bool onGround; ///< boolean true when the flight vehicle is on the ground (not flying) bool staticMode; ///< boolean true if no position feedback is fused @@ -211,6 +232,30 @@ public: unsigned storeIndex; + // Optical Flow error estimation + float storedOmega[3][data_buffer_size]; // angular rate vector stored for the last 50 time steps used by optical flow eror estimators + + // Two state EKF used to estimate focal length scale factor and terrain position + float Popt[2][2]; // state covariance matrix + float flowStates[2]; // flow states [scale factor, terrain position] + float prevPosN; // north position at last measurement + float prevPosE; // east position at last measurement + float auxFlowObsInnov[2]; // optical flow observation innovations from focal length scale factor estimator + float auxFlowObsInnovVar[2]; // innovation variance for optical flow observations from focal length scale factor estimator + float fScaleFactorVar; // optical flow sensor focal length scale factor variance + Mat3f Tnb_flow; // Transformation matrix from nav to body at the time fo the optical flow measurement + float R_LOS; // Optical flow observation noise variance (rad/sec)^2 + float auxFlowTestRatio[2]; // ratio of X and Y flow observation innovations to fault threshold + float auxRngTestRatio; // ratio of range observation innovations to fault threshold + float flowInnovGate; // number of standard deviations used for the innovation consistency check + float auxFlowInnovGate; // number of standard deviations applied to the optical flow innovation consistency check + float rngInnovGate; // number of standard deviations used for the innovation consistency check + float minFlowRng; // minimum range over which to fuse optical flow measurements + float moCompR_LOS; // scaler from sensor gyro rate to uncertainty in LOS rate + +void updateDtGpsFilt(float dt); + +void updateDtHgtFilt(float dt); void UpdateStrapdownEquationsNED(); @@ -226,6 +271,8 @@ void FuseRangeFinder(); void FuseOptFlow(); +void GroundEKF(); + 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); @@ -268,6 +315,10 @@ static void quat2Tnb(Mat3f &Tnb, const float (&quat)[4]); static float sq(float valIn); +static float maxf(float valIn1, float valIn2); + +static float min(float valIn1, float valIn2); + void OnGroundCheck(); void CovarianceInit(); @@ -300,6 +351,8 @@ void InitializeDynamic(float (&initvelNED)[3], float declination); protected: +void updateDtVelPosFilt(float dt); + bool FilterHealthy(); bool GyroOffsetsDiverged(); @@ -314,3 +367,5 @@ void AttitudeInit(float ax, float ay, float az, float mx, float my, float mz, fl uint32_t millis(); +uint64_t getMicros(); + 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 0cea13cc4..c60d8d348 100644 --- a/src/modules/fw_att_control/fw_att_control_main.cpp +++ b/src/modules/fw_att_control/fw_att_control_main.cpp @@ -63,6 +63,7 @@ #include <uORB/topics/vehicle_control_mode.h> #include <uORB/topics/parameter_update.h> #include <uORB/topics/vehicle_global_position.h> +#include <uORB/topics/vehicle_status.h> #include <systemlib/param/param.h> #include <systemlib/err.h> #include <systemlib/pid/pid.h> @@ -124,6 +125,7 @@ private: int _params_sub; /**< notification of parameter updates */ int _manual_sub; /**< notification of manual control updates */ int _global_pos_sub; /**< global position subscription */ + int _vehicle_status_sub; /**< vehicle status subscription */ orb_advert_t _rate_sp_pub; /**< rate setpoint publication */ orb_advert_t _attitude_sp_pub; /**< attitude setpoint point */ @@ -139,12 +141,14 @@ private: struct actuator_controls_s _actuators; /**< actuator control inputs */ struct actuator_controls_s _actuators_airframe; /**< actuator control inputs */ struct vehicle_global_position_s _global_pos; /**< global position */ + struct vehicle_status_s _vehicle_status; /**< vehicle status */ perf_counter_t _loop_perf; /**< loop performance counter */ perf_counter_t _nonfinite_input_perf; /**< performance counter for non finite input */ perf_counter_t _nonfinite_output_perf; /**< performance counter for non finite output */ bool _setpoint_valid; /**< flag if the position control setpoint is valid */ + bool _debug; /**< if set to true, print debug output */ struct { float tconst; @@ -275,6 +279,11 @@ private: void global_pos_poll(); /** + * Check for vehicle status updates. + */ + void vehicle_status_poll(); + + /** * Shim for calling task_main from task_create. */ static void task_main_trampoline(int argc, char *argv[]); @@ -312,6 +321,7 @@ FixedwingAttitudeControl::FixedwingAttitudeControl() : _params_sub(-1), _manual_sub(-1), _global_pos_sub(-1), + _vehicle_status_sub(-1), /* publications */ _rate_sp_pub(-1), @@ -324,7 +334,8 @@ FixedwingAttitudeControl::FixedwingAttitudeControl() : _nonfinite_input_perf(perf_alloc(PC_COUNT, "fw att control nonfinite input")), _nonfinite_output_perf(perf_alloc(PC_COUNT, "fw att control nonfinite output")), /* states */ - _setpoint_valid(false) + _setpoint_valid(false), + _debug(false) { /* safely initialize structs */ _att = {}; @@ -336,6 +347,7 @@ FixedwingAttitudeControl::FixedwingAttitudeControl() : _actuators = {}; _actuators_airframe = {}; _global_pos = {}; + _vehicle_status = {}; _parameter_handles.tconst = param_find("FW_ATT_TC"); @@ -559,6 +571,18 @@ FixedwingAttitudeControl::global_pos_poll() } void +FixedwingAttitudeControl::vehicle_status_poll() +{ + /* check if there is new status information */ + bool vehicle_status_updated; + orb_check(_vehicle_status_sub, &vehicle_status_updated); + + if (vehicle_status_updated) { + orb_copy(ORB_ID(vehicle_status), _vehicle_status_sub, &_vehicle_status); + } +} + +void FixedwingAttitudeControl::task_main_trampoline(int argc, char *argv[]) { att_control::g_control->task_main(); @@ -583,6 +607,7 @@ FixedwingAttitudeControl::task_main() _params_sub = orb_subscribe(ORB_ID(parameter_update)); _manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); _global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position)); + _vehicle_status_sub = orb_subscribe(ORB_ID(vehicle_status)); /* rate limit vehicle status updates to 5Hz */ orb_set_interval(_vcontrol_mode_sub, 200); @@ -597,6 +622,7 @@ FixedwingAttitudeControl::task_main() vehicle_accel_poll(); vehicle_control_mode_poll(); vehicle_manual_poll(); + vehicle_status_poll(); /* wakeup source(s) */ struct pollfd fds[2]; @@ -665,6 +691,8 @@ FixedwingAttitudeControl::task_main() global_pos_poll(); + vehicle_status_poll(); + /* lock integrator until control is started */ bool lock_integrator; @@ -700,7 +728,8 @@ FixedwingAttitudeControl::task_main() perf_count(_nonfinite_input_perf); } } else { - airspeed = _airspeed.true_airspeed_m_s; + /* prevent numerical drama by requiring 0.5 m/s minimal speed */ + airspeed = math::max(0.5f, _airspeed.true_airspeed_m_s); } /* @@ -776,6 +805,13 @@ FixedwingAttitudeControl::task_main() } } + /* If the aircraft is on ground reset the integrators */ + if (_vehicle_status.condition_landed) { + _roll_ctrl.reset_integrator(); + _pitch_ctrl.reset_integrator(); + _yaw_ctrl.reset_integrator(); + } + /* Prepare speed_body_u and speed_body_w */ float speed_body_u = 0.0f; float speed_body_v = 0.0f; @@ -785,7 +821,7 @@ FixedwingAttitudeControl::task_main() speed_body_v = _att.R[0][1] * _global_pos.vel_n + _att.R[1][1] * _global_pos.vel_e + _att.R[2][1] * _global_pos.vel_d; speed_body_w = _att.R[0][2] * _global_pos.vel_n + _att.R[1][2] * _global_pos.vel_e + _att.R[2][2] * _global_pos.vel_d; } else { - if (loop_counter % 10 == 0) { + if (_debug && loop_counter % 10 == 0) { warnx("Did not get a valid R\n"); } } @@ -808,7 +844,7 @@ FixedwingAttitudeControl::task_main() _roll_ctrl.reset_integrator(); perf_count(_nonfinite_output_perf); - if (loop_counter % 10 == 0) { + if (_debug && loop_counter % 10 == 0) { warnx("roll_u %.4f", (double)roll_u); } } @@ -821,7 +857,7 @@ FixedwingAttitudeControl::task_main() if (!isfinite(pitch_u)) { _pitch_ctrl.reset_integrator(); perf_count(_nonfinite_output_perf); - if (loop_counter % 10 == 0) { + if (_debug && loop_counter % 10 == 0) { warnx("pitch_u %.4f, _yaw_ctrl.get_desired_rate() %.4f," " airspeed %.4f, airspeed_scaling %.4f," " roll_sp %.4f, pitch_sp %.4f," @@ -845,7 +881,7 @@ FixedwingAttitudeControl::task_main() if (!isfinite(yaw_u)) { _yaw_ctrl.reset_integrator(); perf_count(_nonfinite_output_perf); - if (loop_counter % 10 == 0) { + if (_debug && loop_counter % 10 == 0) { warnx("yaw_u %.4f", (double)yaw_u); } } @@ -853,13 +889,13 @@ FixedwingAttitudeControl::task_main() /* throttle passed through */ _actuators.control[3] = (isfinite(throttle_sp)) ? throttle_sp : 0.0f; if (!isfinite(throttle_sp)) { - if (loop_counter % 10 == 0) { + if (_debug && loop_counter % 10 == 0) { warnx("throttle_sp %.4f", (double)throttle_sp); } } } else { perf_count(_nonfinite_input_perf); - if (loop_counter % 10 == 0) { + if (_debug && loop_counter % 10 == 0) { warnx("Non-finite setpoint roll_sp: %.4f, pitch_sp %.4f", (double)roll_sp, (double)pitch_sp); } } 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 350ce6dec..23167eef4 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 @@ -102,6 +102,8 @@ static int _control_task = -1; /**< task handle for sensor task */ */ extern "C" __EXPORT int fw_pos_control_l1_main(int argc, char *argv[]); +using namespace launchdetection; + class FixedwingPositionControl { public: @@ -171,8 +173,7 @@ private: bool land_onslope; /* takeoff/launch states */ - bool launch_detected; - bool usePreTakeoffThrust; + LaunchDetectionResult launch_detection_state; bool last_manual; ///< true if the last iteration was in manual mode (used to determine when a reset is needed) @@ -210,6 +211,7 @@ private: float max_climb_rate; float climbout_diff; float heightrate_p; + float heightrate_ff; float speedrate_p; float throttle_damp; float integrator_gain; @@ -255,6 +257,7 @@ private: param_t max_climb_rate; param_t climbout_diff; param_t heightrate_p; + param_t heightrate_ff; param_t speedrate_p; param_t throttle_damp; param_t integrator_gain; @@ -380,7 +383,8 @@ private: bool climbout_mode, float climbout_pitch_min_rad, float altitude, const math::Vector<3> &ground_speed, - tecs_mode mode = TECS_MODE_NORMAL); + tecs_mode mode = TECS_MODE_NORMAL, + bool pitch_max_special = false); }; @@ -438,8 +442,7 @@ FixedwingPositionControl::FixedwingPositionControl() : land_stayonground(false), land_motor_lim(false), land_onslope(false), - launch_detected(false), - usePreTakeoffThrust(false), + launch_detection_state(LAUNCHDETECTION_RES_NONE), last_manual(false), landingslope(), flare_curve_alt_rel_last(0.0f), @@ -494,6 +497,7 @@ FixedwingPositionControl::FixedwingPositionControl() : _parameter_handles.speed_weight = param_find("FW_T_SPDWEIGHT"); _parameter_handles.pitch_damping = param_find("FW_T_PTCH_DAMP"); _parameter_handles.heightrate_p = param_find("FW_T_HRATE_P"); + _parameter_handles.heightrate_ff = param_find("FW_T_HRATE_FF"); _parameter_handles.speedrate_p = param_find("FW_T_SRATE_P"); /* fetch initial parameter values */ @@ -563,12 +567,19 @@ FixedwingPositionControl::parameters_update() param_get(_parameter_handles.climbout_diff, &(_parameters.climbout_diff)); param_get(_parameter_handles.heightrate_p, &(_parameters.heightrate_p)); + param_get(_parameter_handles.heightrate_ff, &(_parameters.heightrate_ff)); param_get(_parameter_handles.speedrate_p, &(_parameters.speedrate_p)); param_get(_parameter_handles.land_slope_angle, &(_parameters.land_slope_angle)); param_get(_parameter_handles.land_H1_virt, &(_parameters.land_H1_virt)); param_get(_parameter_handles.land_flare_alt_relative, &(_parameters.land_flare_alt_relative)); param_get(_parameter_handles.land_thrust_lim_alt_relative, &(_parameters.land_thrust_lim_alt_relative)); + + /* check if negative value for 2/3 of flare altitude is set for throttle cut */ + if (_parameters.land_thrust_lim_alt_relative < 0.0f) { + _parameters.land_thrust_lim_alt_relative = 0.66f * _parameters.land_flare_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)); @@ -594,6 +605,7 @@ FixedwingPositionControl::parameters_update() _tecs.set_indicated_airspeed_max(_parameters.airspeed_max); _tecs.set_max_climb_rate(_parameters.max_climb_rate); _tecs.set_heightrate_p(_parameters.heightrate_p); + _tecs.set_heightrate_ff(_parameters.heightrate_ff); _tecs.set_speedrate_p(_parameters.speedrate_p); /* sanity check parameters */ @@ -823,7 +835,7 @@ float FixedwingPositionControl::get_relative_landingalt(float land_setpoint_alt, * 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 ) { + if (range_finder_use_relative_alt < 0 || !range_finder.valid || range_finder.distance > range_finder_use_relative_alt ) { return rel_alt_estimated; } @@ -1076,41 +1088,46 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi } else if (pos_sp_triplet.current.type == SETPOINT_TYPE_TAKEOFF) { /* Perform launch detection */ - if(!launch_detected) { //do not do further checks once a launch was detected - if (launchDetector.launchDetectionEnabled()) { - static hrt_abstime last_sent = 0; - if(hrt_absolute_time() - last_sent > 4e6) { - mavlink_log_info(_mavlink_fd, "#audio: Launchdetection running"); - last_sent = hrt_absolute_time(); - } - - /* Tell the attitude controller to stop integrating while we are waiting - * for the launch */ - _att_sp.roll_reset_integral = true; - _att_sp.pitch_reset_integral = true; - _att_sp.yaw_reset_integral = true; - - /* Detect launch */ - launchDetector.update(_sensor_combined.accelerometer_m_s2[0]); - if (launchDetector.getLaunchDetected()) { - launch_detected = true; - mavlink_log_info(_mavlink_fd, "#audio: Takeoff"); - } - } else { - /* no takeoff detection --> fly */ - launch_detected = true; - warnx("launchdetection off"); + if (launchDetector.launchDetectionEnabled() && + launch_detection_state != LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS) { + /* Inform user that launchdetection is running */ + static hrt_abstime last_sent = 0; + if(hrt_absolute_time() - last_sent > 4e6) { + mavlink_log_info(_mavlink_fd, "#audio: Launchdetection running"); + last_sent = hrt_absolute_time(); } - } - _l1_control.navigate_waypoints(prev_wp, curr_wp, current_position, ground_speed_2d); - _att_sp.roll_body = _l1_control.nav_roll(); - _att_sp.yaw_body = _l1_control.nav_bearing(); + /* Detect launch */ + launchDetector.update(_sensor_combined.accelerometer_m_s2[0]); - if (launch_detected) { - usePreTakeoffThrust = false; + /* update our copy of the laucn detection state */ + launch_detection_state = launchDetector.getLaunchDetected(); + } else { + /* no takeoff detection --> fly */ + launch_detection_state = LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS; + } + + /* Set control values depending on the detection state */ + if (launch_detection_state != LAUNCHDETECTION_RES_NONE) { + /* Launch has been detected, hence we have to control the plane. */ - /* apply minimum pitch and limit roll if target altitude is not within 10 meters */ + _l1_control.navigate_waypoints(prev_wp, curr_wp, current_position, ground_speed_2d); + _att_sp.roll_body = _l1_control.nav_roll(); + _att_sp.yaw_body = _l1_control.nav_bearing(); + + /* Select throttle: only in LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS we want to use + * full throttle, otherwise we use the preTakeOff Throttle */ + float takeoff_throttle = launch_detection_state != + LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS ? + launchDetector.getThrottlePreTakeoff() : _parameters.throttle_max; + + /* select maximum pitch: the launchdetector may impose another limit for the pitch + * depending on the state of the launch */ + float takeoff_pitch_max_deg = launchDetector.getPitchMax(_parameters.pitch_limit_max); + float takeoff_pitch_max_rad = math::radians(takeoff_pitch_max_deg); + + /* apply minimum pitch and limit roll if target altitude is not within climbout_diff + * meters */ if (_parameters.climbout_diff > 0.001f && altitude_error > _parameters.climbout_diff) { /* enforce a minimum of 10 degrees pitch up on takeoff, or take parameter */ @@ -1118,18 +1135,20 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi calculate_target_airspeed(1.3f * _parameters.airspeed_min), eas2tas, math::radians(_parameters.pitch_limit_min), - math::radians(_parameters.pitch_limit_max), - _parameters.throttle_min, _parameters.throttle_max, + takeoff_pitch_max_rad, + _parameters.throttle_min, takeoff_throttle, _parameters.throttle_cruise, true, math::max(math::radians(pos_sp_triplet.current.pitch_min), math::radians(10.0f)), _global_pos.alt, ground_speed, - TECS_MODE_TAKEOFF); + TECS_MODE_TAKEOFF, + takeoff_pitch_max_deg != _parameters.pitch_limit_max); /* limit roll motion to ensure enough lift */ - _att_sp.roll_body = math::constrain(_att_sp.roll_body, math::radians(-15.0f), math::radians(15.0f)); + _att_sp.roll_body = math::constrain(_att_sp.roll_body, math::radians(-15.0f), + math::radians(15.0f)); } else { tecs_update_pitch_throttle(_pos_sp_triplet.current.alt, @@ -1138,17 +1157,26 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi math::radians(_parameters.pitch_limit_min), math::radians(_parameters.pitch_limit_max), _parameters.throttle_min, - _parameters.throttle_max, + takeoff_throttle, _parameters.throttle_cruise, false, math::radians(_parameters.pitch_limit_min), _global_pos.alt, ground_speed); } - } else { - usePreTakeoffThrust = true; + /* Tell the attitude controller to stop integrating while we are waiting + * for the launch */ + _att_sp.roll_reset_integral = true; + _att_sp.pitch_reset_integral = true; + _att_sp.yaw_reset_integral = true; + + /* Set default roll and pitch setpoints during detection phase */ + _att_sp.roll_body = 0.0f; + _att_sp.pitch_body = math::max(math::radians(pos_sp_triplet.current.pitch_min), + math::radians(10.0f)); } + } /* reset landing state */ @@ -1182,13 +1210,22 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi } } - if (usePreTakeoffThrust) { + /* Copy thrust and pitch values from tecs + * making sure again that the correct thrust is used, + * without depending on library calls for safety reasons */ + if (pos_sp_triplet.current.type == SETPOINT_TYPE_TAKEOFF && + launch_detection_state != LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS) { _att_sp.thrust = launchDetector.getThrottlePreTakeoff(); } else { _att_sp.thrust = math::min(_mTecs.getEnabled() ? _mTecs.getThrottleSetpoint() : _tecs.get_throttle_demand(), throttle_max); } - _att_sp.pitch_body = _mTecs.getEnabled() ? _mTecs.getPitchSetpoint() : _tecs.get_pitch_demand(); + /* During a takeoff waypoint while waiting for launch the pitch sp is set + * already (not by tecs) */ + if (!(pos_sp_triplet.current.type == SETPOINT_TYPE_TAKEOFF && + launch_detection_state == LAUNCHDETECTION_RES_NONE)) { + _att_sp.pitch_body = _mTecs.getEnabled() ? _mTecs.getPitchSetpoint() : _tecs.get_pitch_demand(); + } if (_control_mode.flag_control_position_enabled) { last_manual = false; @@ -1342,8 +1379,7 @@ FixedwingPositionControl::task_main() void FixedwingPositionControl::reset_takeoff_state() { - launch_detected = false; - usePreTakeoffThrust = false; + launch_detection_state = LAUNCHDETECTION_RES_NONE; launchDetector.reset(); } @@ -1362,7 +1398,7 @@ void FixedwingPositionControl::tecs_update_pitch_throttle(float alt_sp, float v_ bool climbout_mode, float climbout_pitch_min_rad, float altitude, const math::Vector<3> &ground_speed, - tecs_mode mode) + tecs_mode mode, bool pitch_max_special) { if (_mTecs.getEnabled()) { /* Using mtecs library: prepare arguments for mtecs call */ @@ -1377,9 +1413,20 @@ void FixedwingPositionControl::tecs_update_pitch_throttle(float alt_sp, float v_ } else { limitOverride.disablePitchMinOverride(); } + + if (pitch_max_special) { + /* Use the maximum pitch from the argument */ + limitOverride.enablePitchMaxOverride(M_RAD_TO_DEG_F * pitch_max_rad); + } else { + /* use pitch max set by MT param */ + limitOverride.disablePitchMaxOverride(); + } _mTecs.updateAltitudeSpeed(flightPathAngle, altitude, alt_sp, _airspeed.true_airspeed_m_s, v_sp, mode, limitOverride); } else { + /* No underspeed protection in landing mode */ + _tecs.set_detect_underspeed_enabled(!(mode == TECS_MODE_LAND || mode == TECS_MODE_LAND_THROTTLELIM)); + /* Using tecs library */ _tecs.update_pitch_throttle(_R_nb, _att.pitch, altitude, alt_sp, v_sp, _airspeed.indicated_airspeed_m_s, eas2tas, 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 41c374407..847ecbb5c 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 @@ -131,8 +131,8 @@ PARAM_DEFINE_FLOAT(FW_R_LIM, 45.0f); /** * Throttle limit max * - * This is the maximum throttle % that can be used by the controller. - * For overpowered aircraft, this should be reduced to a value that + * This is the maximum throttle % that can be used by the controller. + * For overpowered aircraft, this should be reduced to a value that * provides sufficient thrust to climb at the maximum pitch angle PTCH_MAX. * * @group L1 Control @@ -142,10 +142,10 @@ PARAM_DEFINE_FLOAT(FW_THR_MAX, 1.0f); /** * Throttle limit min * - * This is the minimum throttle % that can be used by the controller. - * For electric aircraft this will normally be set to zero, but can be set - * to a small non-zero value if a folding prop is fitted to prevent the - * prop from folding and unfolding repeatedly in-flight or to provide + * This is the minimum throttle % that can be used by the controller. + * For electric aircraft this will normally be set to zero, but can be set + * to a small non-zero value if a folding prop is fitted to prevent the + * prop from folding and unfolding repeatedly in-flight or to provide * some aerodynamic drag from a turning prop to improve the descent rate. * * For aircraft with internal combustion engine this parameter should be set @@ -158,7 +158,7 @@ PARAM_DEFINE_FLOAT(FW_THR_MIN, 0.0f); /** * Throttle limit value before flare * - * This throttle value will be set as throttle limit at FW_LND_TLALT, + * This throttle value will be set as throttle limit at FW_LND_TLALT, * before arcraft will flare. * * @group L1 Control @@ -180,17 +180,17 @@ PARAM_DEFINE_FLOAT(FW_CLMBOUT_DIFF, 25.0f); /** * Maximum climb rate * - * This is the best climb rate that the aircraft can achieve with - * the throttle set to THR_MAX and the airspeed set to the - * default value. For electric aircraft make sure this number can be - * achieved towards the end of flight when the battery voltage has reduced. - * The setting of this parameter can be checked by commanding a positive - * altitude change of 100m in loiter, RTL or guided mode. If the throttle - * required to climb is close to THR_MAX and the aircraft is maintaining - * airspeed, then this parameter is set correctly. If the airspeed starts - * to reduce, then the parameter is set to high, and if the throttle - * demand required to climb and maintain speed is noticeably less than - * FW_THR_MAX, then either FW_T_CLMB_MAX should be increased or + * This is the best climb rate that the aircraft can achieve with + * the throttle set to THR_MAX and the airspeed set to the + * default value. For electric aircraft make sure this number can be + * achieved towards the end of flight when the battery voltage has reduced. + * The setting of this parameter can be checked by commanding a positive + * altitude change of 100m in loiter, RTL or guided mode. If the throttle + * required to climb is close to THR_MAX and the aircraft is maintaining + * airspeed, then this parameter is set correctly. If the airspeed starts + * to reduce, then the parameter is set to high, and if the throttle + * demand required to climb and maintain speed is noticeably less than + * FW_THR_MAX, then either FW_T_CLMB_MAX should be increased or * FW_THR_MAX reduced. * * @group L1 Control @@ -200,8 +200,8 @@ PARAM_DEFINE_FLOAT(FW_T_CLMB_MAX, 5.0f); /** * Minimum descent rate * - * This is the sink rate of the aircraft with the throttle - * set to THR_MIN and flown at the same airspeed as used + * This is the sink rate of the aircraft with the throttle + * set to THR_MIN and flown at the same airspeed as used * to measure FW_T_CLMB_MAX. * * @group Fixed Wing TECS @@ -211,10 +211,10 @@ PARAM_DEFINE_FLOAT(FW_T_SINK_MIN, 2.0f); /** * Maximum descent rate * - * This sets the maximum descent rate that the controller will use. - * If this value is too large, the aircraft can over-speed on descent. - * This should be set to a value that can be achieved without - * exceeding the lower pitch angle limit and without over-speeding + * This sets the maximum descent rate that the controller will use. + * If this value is too large, the aircraft can over-speed on descent. + * This should be set to a value that can be achieved without + * exceeding the lower pitch angle limit and without over-speeding * the aircraft. * * @group Fixed Wing TECS @@ -224,7 +224,7 @@ PARAM_DEFINE_FLOAT(FW_T_SINK_MAX, 5.0f); /** * TECS time constant * - * This is the time constant of the TECS control algorithm (in seconds). + * This is the time constant of the TECS control algorithm (in seconds). * Smaller values make it faster to respond, larger values make it slower * to respond. * @@ -235,7 +235,7 @@ PARAM_DEFINE_FLOAT(FW_T_TIME_CONST, 5.0f); /** * TECS Throttle time constant * - * This is the time constant of the TECS throttle control algorithm (in seconds). + * This is the time constant of the TECS throttle control algorithm (in seconds). * Smaller values make it faster to respond, larger values make it slower * to respond. * @@ -246,7 +246,7 @@ PARAM_DEFINE_FLOAT(FW_T_THRO_CONST, 8.0f); /** * Throttle damping factor * - * This is the damping gain for the throttle demand loop. + * This is the damping gain for the throttle demand loop. * Increase to add damping to correct for oscillations in speed and height. * * @group Fixed Wing TECS @@ -256,9 +256,9 @@ PARAM_DEFINE_FLOAT(FW_T_THR_DAMP, 0.5f); /** * Integrator gain * - * This is the integrator gain on the control loop. - * Increasing this gain increases the speed at which speed - * and height offsets are trimmed out, but reduces damping and + * This is the integrator gain on the control loop. + * Increasing this gain increases the speed at which speed + * and height offsets are trimmed out, but reduces damping and * increases overshoot. * * @group Fixed Wing TECS @@ -269,9 +269,9 @@ PARAM_DEFINE_FLOAT(FW_T_INTEG_GAIN, 0.1f); * Maximum vertical acceleration * * 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 + * 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 * from under-speed conditions. * * @group Fixed Wing TECS @@ -281,10 +281,10 @@ PARAM_DEFINE_FLOAT(FW_T_VERT_ACC, 7.0f); /** * Complementary filter "omega" parameter for height * - * This is the cross-over frequency (in radians/second) of the complementary - * filter used to fuse vertical acceleration and barometric height to obtain - * an estimate of height rate and height. Increasing this frequency weights - * the solution more towards use of the barometer, whilst reducing it weights + * This is the cross-over frequency (in radians/second) of the complementary + * filter used to fuse vertical acceleration and barometric height to obtain + * an estimate of height rate and height. Increasing this frequency weights + * the solution more towards use of the barometer, whilst reducing it weights * the solution more towards use of the accelerometer data. * * @group Fixed Wing TECS @@ -294,10 +294,10 @@ PARAM_DEFINE_FLOAT(FW_T_HGT_OMEGA, 3.0f); /** * Complementary filter "omega" parameter for speed * - * This is the cross-over frequency (in radians/second) of the complementary - * filter used to fuse longitudinal acceleration and airspeed to obtain an + * This is the cross-over frequency (in radians/second) of the complementary + * filter used to fuse longitudinal acceleration and airspeed to obtain an * improved airspeed estimate. Increasing this frequency weights the solution - * more towards use of the arispeed sensor, whilst reducing it weights the + * more towards use of the arispeed sensor, whilst reducing it weights the * solution more towards use of the accelerometer data. * * @group Fixed Wing TECS @@ -307,13 +307,13 @@ PARAM_DEFINE_FLOAT(FW_T_SPD_OMEGA, 2.0f); /** * Roll -> Throttle feedforward * - * Increasing this gain turn increases the amount of throttle that will - * be used to compensate for the additional drag created by turning. - * Ideally this should be set to approximately 10 x the extra sink rate - * in m/s created by a 45 degree bank turn. Increase this gain if - * the aircraft initially loses energy in turns and reduce if the - * aircraft initially gains energy in turns. Efficient high aspect-ratio - * aircraft (eg powered sailplanes) can use a lower value, whereas + * Increasing this gain turn increases the amount of throttle that will + * be used to compensate for the additional drag created by turning. + * Ideally this should be set to approximately 10 x the extra sink rate + * in m/s created by a 45 degree bank turn. Increase this gain if + * the aircraft initially loses energy in turns and reduce if the + * aircraft initially gains energy in turns. Efficient high aspect-ratio + * aircraft (eg powered sailplanes) can use a lower value, whereas * inefficient low aspect-ratio models (eg delta wings) can use a higher value. * * @group Fixed Wing TECS @@ -323,15 +323,15 @@ PARAM_DEFINE_FLOAT(FW_T_RLL2THR, 10.0f); /** * Speed <--> Altitude priority * - * This parameter adjusts the amount of weighting that the pitch control - * applies to speed vs height errors. Setting it to 0.0 will cause the - * pitch control to control height and ignore speed errors. This will - * normally improve height accuracy but give larger airspeed errors. - * Setting it to 2.0 will cause the pitch control loop to control speed - * and ignore height errors. This will normally reduce airspeed errors, - * but give larger height errors. The default value of 1.0 allows the pitch - * control to simultaneously control height and speed. - * Note to Glider Pilots - set this parameter to 2.0 (The glider will + * This parameter adjusts the amount of weighting that the pitch control + * applies to speed vs height errors. Setting it to 0.0 will cause the + * pitch control to control height and ignore speed errors. This will + * normally improve height accuracy but give larger airspeed errors. + * Setting it to 2.0 will cause the pitch control loop to control speed + * and ignore height errors. This will normally reduce airspeed errors, + * but give larger height errors. The default value of 1.0 allows the pitch + * control to simultaneously control height and speed. + * Note to Glider Pilots - set this parameter to 2.0 (The glider will * adjust its pitch angle to maintain airspeed, ignoring changes in height). * * @group Fixed Wing TECS @@ -341,9 +341,9 @@ PARAM_DEFINE_FLOAT(FW_T_SPDWEIGHT, 1.0f); /** * Pitch damping factor * - * This is the damping gain for the pitch demand loop. Increase to add - * damping to correct for oscillations in height. The default value of 0.0 - * will work well provided the pitch to servo controller has been tuned + * This is the damping gain for the pitch demand loop. Increase to add + * damping to correct for oscillations in height. The default value of 0.0 + * will work well provided the pitch to servo controller has been tuned * properly. * * @group Fixed Wing TECS @@ -358,6 +358,13 @@ PARAM_DEFINE_FLOAT(FW_T_PTCH_DAMP, 0.0f); PARAM_DEFINE_FLOAT(FW_T_HRATE_P, 0.05f); /** + * Height rate FF factor + * + * @group Fixed Wing TECS + */ +PARAM_DEFINE_FLOAT(FW_T_HRATE_FF, 0.0f); + +/** * Speed rate P factor * * @group Fixed Wing TECS @@ -379,18 +386,23 @@ PARAM_DEFINE_FLOAT(FW_LND_ANG, 5.0f); PARAM_DEFINE_FLOAT(FW_LND_HVIRT, 10.0f); /** - * Landing flare altitude (relative) + * Landing flare altitude (relative to landing altitude) * + * @unit meter * @group L1 Control */ -PARAM_DEFINE_FLOAT(FW_LND_FLALT, 15.0f); +PARAM_DEFINE_FLOAT(FW_LND_FLALT, 8.0f); /** - * Landing throttle limit altitude (relative) + * Landing throttle limit altitude (relative landing altitude) + * + * Default of -1.0f lets the system default to applying throttle + * limiting at 2/3 of the flare altitude. * + * @unit meter * @group L1 Control */ -PARAM_DEFINE_FLOAT(FW_LND_TLALT, 5.0f); +PARAM_DEFINE_FLOAT(FW_LND_TLALT, -1.0f); /** * Landing heading hold horizontal distance diff --git a/src/modules/mavlink/mavlink_ftp.cpp b/src/modules/mavlink/mavlink_ftp.cpp index 00c8df18c..2a85c3702 100644 --- a/src/modules/mavlink/mavlink_ftp.cpp +++ b/src/modules/mavlink/mavlink_ftp.cpp @@ -31,38 +31,38 @@ * ****************************************************************************/ -#include <crc32.h> +/// @file mavlink_ftp.cpp +/// @author px4dev, Don Gagne <don@thegagnes.com> + #include <unistd.h> #include <stdio.h> #include <fcntl.h> #include <sys/stat.h> +#include <errno.h> #include "mavlink_ftp.h" +#include "mavlink_tests/mavlink_ftp_test.h" // Uncomment the line below to get better debug output. Never commit with this left on. //#define MAVLINK_FTP_DEBUG -MavlinkFTP *MavlinkFTP::_server; - MavlinkFTP * -MavlinkFTP::getServer() +MavlinkFTP::get_server(void) { - // XXX this really cries out for some locking... - if (_server == nullptr) { - _server = new MavlinkFTP; - } - return _server; + static MavlinkFTP server; + return &server; } MavlinkFTP::MavlinkFTP() : - _session_fds{}, - _workBufs{}, - _workFree{}, - _lock{} + _request_bufs{}, + _request_queue{}, + _request_queue_sem{}, + _utRcvMsgFunc{}, + _ftp_test{} { // initialise the request freelist - dq_init(&_workFree); - sem_init(&_lock, 0, 1); + dq_init(&_request_queue); + sem_init(&_request_queue_sem, 0, 1); // initialize session list for (size_t i=0; i<kMaxSession; i++) { @@ -71,161 +71,240 @@ MavlinkFTP::MavlinkFTP() : // drop work entries onto the free list for (unsigned i = 0; i < kRequestQueueSize; i++) { - _qFree(&_workBufs[i]); + _return_request(&_request_bufs[i]); } } +#ifdef MAVLINK_FTP_UNIT_TEST +void +MavlinkFTP::set_unittest_worker(ReceiveMessageFunc_t rcvMsgFunc, MavlinkFtpTest *ftp_test) +{ + _utRcvMsgFunc = rcvMsgFunc; + _ftp_test = ftp_test; +} +#endif + void MavlinkFTP::handle_message(Mavlink* mavlink, mavlink_message_t *msg) { // get a free request - auto req = _dqFree(); + struct Request* req = _get_request(); // if we couldn't get a request slot, just drop it - if (req != nullptr) { - - // decode the request - if (req->decode(mavlink, msg)) { + if (req == nullptr) { + warnx("Dropping FTP request: queue full\n"); + return; + } - // and queue it for the worker - work_queue(LPWORK, &req->work, &MavlinkFTP::_workerTrampoline, req, 0); - } else { - _qFree(req); + if (msg->msgid == MAVLINK_MSG_ID_FILE_TRANSFER_PROTOCOL) { + mavlink_msg_file_transfer_protocol_decode(msg, &req->message); + +#ifdef MAVLINK_FTP_UNIT_TEST + if (!_utRcvMsgFunc) { + warnx("Incorrectly written unit test\n"); + return; + } + // We use fake ids when unit testing + req->serverSystemId = MavlinkFtpTest::serverSystemId; + req->serverComponentId = MavlinkFtpTest::serverComponentId; + req->serverChannel = MavlinkFtpTest::serverChannel; +#else + // Not unit testing, use the real thing + req->serverSystemId = mavlink->get_system_id(); + req->serverComponentId = mavlink->get_component_id(); + req->serverChannel = mavlink->get_channel(); +#endif + + // This is the system id we want to target when sending + req->targetSystemId = msg->sysid; + + if (req->message.target_system == req->serverSystemId) { + req->mavlink = mavlink; +#ifdef MAVLINK_FTP_UNIT_TEST + // We are running in Unit Test mode. Don't queue, just call _worket directly. + _process_request(req); +#else + // We are running in normal mode. Queue the request to the worker + work_queue(LPWORK, &req->work, &MavlinkFTP::_worker_trampoline, req, 0); +#endif + return; } } + + _return_request(req); } +/// @brief Queued static work queue routine to handle mavlink messages void -MavlinkFTP::_workerTrampoline(void *arg) +MavlinkFTP::_worker_trampoline(void *arg) { - auto req = reinterpret_cast<Request *>(arg); - auto server = MavlinkFTP::getServer(); + Request* req = reinterpret_cast<Request *>(arg); + MavlinkFTP* server = MavlinkFTP::get_server(); // call the server worker with the work item - server->_worker(req); + server->_process_request(req); } +/// @brief Processes an FTP message void -MavlinkFTP::_worker(Request *req) +MavlinkFTP::_process_request(Request *req) { - auto hdr = req->header(); + PayloadHeader *payload = reinterpret_cast<PayloadHeader *>(&req->message.payload[0]); + ErrorCode errorCode = kErrNone; - uint32_t messageCRC; // basic sanity checks; must validate length before use - if ((hdr->magic != kProtocolMagic) || (hdr->size > kMaxDataLength)) { - errorCode = kErrNoRequest; + if (payload->size > kMaxDataLength) { + errorCode = kErrInvalidDataSize; goto out; } - // check request CRC to make sure this is one of ours - messageCRC = hdr->crc32; - hdr->crc32 = 0; - if (crc32(req->rawData(), req->dataSize()) != messageCRC) { - errorCode = kErrNoRequest; - goto out; - warnx("ftp: bad crc"); - } - #ifdef MAVLINK_FTP_DEBUG - printf("ftp: channel %u opc %u size %u offset %u\n", req->channel(), hdr->opcode, hdr->size, hdr->offset); + printf("ftp: channel %u opc %u size %u offset %u\n", req->serverChannel, payload->opcode, payload->size, payload->offset); #endif - switch (hdr->opcode) { + switch (payload->opcode) { case kCmdNone: break; - case kCmdTerminate: - errorCode = _workTerminate(req); + case kCmdTerminateSession: + errorCode = _workTerminate(payload); break; - case kCmdReset: - errorCode = _workReset(); + case kCmdResetSessions: + errorCode = _workReset(payload); break; - case kCmdList: - errorCode = _workList(req); + case kCmdListDirectory: + errorCode = _workList(payload); break; - case kCmdOpen: - errorCode = _workOpen(req, false); + case kCmdOpenFile: + errorCode = _workOpen(payload, false); break; - case kCmdCreate: - errorCode = _workOpen(req, true); + case kCmdCreateFile: + errorCode = _workOpen(payload, true); break; - case kCmdRead: - errorCode = _workRead(req); + case kCmdReadFile: + errorCode = _workRead(payload); break; - case kCmdWrite: - errorCode = _workWrite(req); + case kCmdWriteFile: + errorCode = _workWrite(payload); break; - case kCmdRemove: - errorCode = _workRemove(req); + case kCmdRemoveFile: + errorCode = _workRemoveFile(payload); break; + case kCmdCreateDirectory: + errorCode = _workCreateDirectory(payload); + break; + + case kCmdRemoveDirectory: + errorCode = _workRemoveDirectory(payload); + break; + default: - errorCode = kErrNoRequest; + errorCode = kErrUnknownCommand; break; } out: // handle success vs. error if (errorCode == kErrNone) { - hdr->opcode = kRspAck; + payload->req_opcode = payload->opcode; + payload->opcode = kRspAck; #ifdef MAVLINK_FTP_DEBUG warnx("FTP: ack\n"); #endif } else { warnx("FTP: nak %u", errorCode); - hdr->opcode = kRspNak; - hdr->size = 1; - hdr->data[0] = errorCode; + payload->req_opcode = payload->opcode; + payload->opcode = kRspNak; + payload->size = 1; + payload->data[0] = errorCode; + if (errorCode == kErrFailErrno) { + payload->size = 2; + payload->data[1] = errno; + } } + // respond to the request _reply(req); - // free the request buffer back to the freelist - _qFree(req); + _return_request(req); } +/// @brief Sends the specified FTP reponse message out through mavlink void MavlinkFTP::_reply(Request *req) { - auto hdr = req->header(); + PayloadHeader *payload = reinterpret_cast<PayloadHeader *>(&req->message.payload[0]); - hdr->magic = kProtocolMagic; + payload->seqNumber = payload->seqNumber + 1; - // message is assumed to be already constructed in the request buffer, so generate the CRC - hdr->crc32 = 0; - hdr->crc32 = crc32(req->rawData(), req->dataSize()); + mavlink_message_t msg; + msg.checksum = 0; +#ifndef MAVLINK_FTP_UNIT_TEST + uint16_t len = +#endif + mavlink_msg_file_transfer_protocol_pack_chan(req->serverSystemId, // Sender system id + req->serverComponentId, // Sender component id + req->serverChannel, // Channel to send on + &msg, // Message to pack payload into + 0, // Target network + req->targetSystemId, // Target system id + 0, // Target component id + (const uint8_t*)payload); // Payload to pack into message + + bool success = true; +#ifdef MAVLINK_FTP_UNIT_TEST + // Unit test hook is set, call that instead + _utRcvMsgFunc(&msg, _ftp_test); +#else + Mavlink *mavlink = req->mavlink; + + mavlink->lockMessageBufferMutex(); + success = mavlink->message_buffer_write(&msg, len); + mavlink->unlockMessageBufferMutex(); + +#endif - // then pack and send the reply back to the request source - req->reply(); + if (!success) { + warnx("FTP TX ERR"); + } +#ifdef MAVLINK_FTP_DEBUG + else { + warnx("wrote: sys: %d, comp: %d, chan: %d, checksum: %d", + req->serverSystemId, + req->serverComponentId, + req->serverChannel, + msg.checksum); + } +#endif } +/// @brief Responds to a List command MavlinkFTP::ErrorCode -MavlinkFTP::_workList(Request *req) +MavlinkFTP::_workList(PayloadHeader* payload) { - auto hdr = req->header(); - char dirPath[kMaxDataLength]; - strncpy(dirPath, req->dataAsCString(), kMaxDataLength); + strncpy(dirPath, _data_as_cstring(payload), kMaxDataLength); DIR *dp = opendir(dirPath); if (dp == nullptr) { warnx("FTP: can't open path '%s'", dirPath); - return kErrNotDir; + return kErrFailErrno; } #ifdef MAVLINK_FTP_DEBUG - warnx("FTP: list %s offset %d", dirPath, hdr->offset); + warnx("FTP: list %s offset %d", dirPath, payload->offset); #endif ErrorCode errorCode = kErrNone; @@ -233,19 +312,19 @@ MavlinkFTP::_workList(Request *req) unsigned offset = 0; // move to the requested offset - seekdir(dp, hdr->offset); + seekdir(dp, payload->offset); for (;;) { // read the directory entry if (readdir_r(dp, &entry, &result)) { warnx("FTP: list %s readdir_r failure\n", dirPath); - errorCode = kErrIO; + errorCode = kErrFailErrno; break; } // no more entries? if (result == nullptr) { - if (hdr->offset != 0 && offset == 0) { + if (payload->offset != 0 && offset == 0) { // User is requesting subsequent dir entries but there were none. This means the user asked // to seek past EOF. errorCode = kErrEOF; @@ -270,14 +349,22 @@ MavlinkFTP::_workList(Request *req) } break; case DTYPE_DIRECTORY: - direntType = kDirentDir; + if (strcmp(entry.d_name, ".") == 0 || strcmp(entry.d_name, "..") == 0) { + // Don't bother sending these back + direntType = kDirentSkip; + } else { + direntType = kDirentDir; + } break; default: - direntType = kDirentUnknown; - break; + // We only send back file and diretory entries, skip everything else + direntType = kDirentSkip; } - if (entry.d_type == DTYPE_FILE) { + if (direntType == kDirentSkip) { + // Skip send only dirent identifier + buf[0] = '\0'; + } else if (direntType == kDirentFile) { // Files send filename and file length snprintf(buf, sizeof(buf), "%s\t%d", entry.d_name, fileSize); } else { @@ -293,94 +380,95 @@ MavlinkFTP::_workList(Request *req) } // Move the data into the buffer - hdr->data[offset++] = direntType; - strcpy((char *)&hdr->data[offset], buf); + payload->data[offset++] = direntType; + strcpy((char *)&payload->data[offset], buf); #ifdef MAVLINK_FTP_DEBUG - printf("FTP: list %s %s\n", dirPath, (char *)&hdr->data[offset-1]); + printf("FTP: list %s %s\n", dirPath, (char *)&payload->data[offset-1]); #endif offset += nameLen + 1; } closedir(dp); - hdr->size = offset; + payload->size = offset; return errorCode; } +/// @brief Responds to an Open command MavlinkFTP::ErrorCode -MavlinkFTP::_workOpen(Request *req, bool create) +MavlinkFTP::_workOpen(PayloadHeader* payload, bool create) { - auto hdr = req->header(); - - int session_index = _findUnusedSession(); + int session_index = _find_unused_session(); if (session_index < 0) { - return kErrNoSession; + warnx("FTP: Open failed - out of sessions\n"); + return kErrNoSessionsAvailable; } - + + char *filename = _data_as_cstring(payload); uint32_t fileSize = 0; if (!create) { struct stat st; - if (stat(req->dataAsCString(), &st) != 0) { - return kErrNotFile; + if (stat(filename, &st) != 0) { + return kErrFailErrno; } fileSize = st.st_size; } int oflag = create ? (O_CREAT | O_EXCL | O_APPEND) : O_RDONLY; - int fd = ::open(req->dataAsCString(), oflag); + int fd = ::open(filename, oflag); if (fd < 0) { - return create ? kErrPerm : kErrNotFile; + return kErrFailErrno; } _session_fds[session_index] = fd; - hdr->session = session_index; + payload->session = session_index; if (create) { - hdr->size = 0; + payload->size = 0; } else { - hdr->size = sizeof(uint32_t); - *((uint32_t*)hdr->data) = fileSize; + payload->size = sizeof(uint32_t); + *((uint32_t*)payload->data) = fileSize; } return kErrNone; } +/// @brief Responds to a Read command MavlinkFTP::ErrorCode -MavlinkFTP::_workRead(Request *req) +MavlinkFTP::_workRead(PayloadHeader* payload) { - auto hdr = req->header(); - - int session_index = hdr->session; + int session_index = payload->session; - if (!_validSession(session_index)) { - return kErrNoSession; + if (!_valid_session(session_index)) { + return kErrInvalidSession; } // Seek to the specified position #ifdef MAVLINK_FTP_DEBUG - warnx("seek %d", hdr->offset); + warnx("seek %d", payload->offset); #endif - if (lseek(_session_fds[session_index], hdr->offset, SEEK_SET) < 0) { + if (lseek(_session_fds[session_index], payload->offset, SEEK_SET) < 0) { // Unable to see to the specified location warnx("seek fail"); return kErrEOF; } - int bytes_read = ::read(_session_fds[session_index], &hdr->data[0], kMaxDataLength); + int bytes_read = ::read(_session_fds[session_index], &payload->data[0], kMaxDataLength); if (bytes_read < 0) { // Negative return indicates error other than eof warnx("read fail %d", bytes_read); - return kErrIO; + return kErrFailErrno; } - hdr->size = bytes_read; + payload->size = bytes_read; return kErrNone; } +/// @brief Responds to a Write command MavlinkFTP::ErrorCode -MavlinkFTP::_workWrite(Request *req) +MavlinkFTP::_workWrite(PayloadHeader* payload) { #if 0 // NYI: Coming soon @@ -403,35 +491,44 @@ MavlinkFTP::_workWrite(Request *req) hdr->size = result; return kErrNone; #else - return kErrPerm; + return kErrUnknownCommand; #endif } +/// @brief Responds to a RemoveFile command MavlinkFTP::ErrorCode -MavlinkFTP::_workRemove(Request *req) +MavlinkFTP::_workRemoveFile(PayloadHeader* payload) { - //auto hdr = req->header(); - - // for now, send error reply - return kErrPerm; + char file[kMaxDataLength]; + strncpy(file, _data_as_cstring(payload), kMaxDataLength); + + if (unlink(file) == 0) { + payload->size = 0; + return kErrNone; + } else { + return kErrFailErrno; + } } +/// @brief Responds to a Terminate command MavlinkFTP::ErrorCode -MavlinkFTP::_workTerminate(Request *req) +MavlinkFTP::_workTerminate(PayloadHeader* payload) { - auto hdr = req->header(); - - if (!_validSession(hdr->session)) { - return kErrNoSession; + if (!_valid_session(payload->session)) { + return kErrInvalidSession; } - ::close(_session_fds[hdr->session]); + ::close(_session_fds[payload->session]); + _session_fds[payload->session] = -1; + + payload->size = 0; return kErrNone; } +/// @brief Responds to a Reset command MavlinkFTP::ErrorCode -MavlinkFTP::_workReset(void) +MavlinkFTP::_workReset(PayloadHeader* payload) { for (size_t i=0; i<kMaxSession; i++) { if (_session_fds[i] != -1) { @@ -440,11 +537,44 @@ MavlinkFTP::_workReset(void) } } + payload->size = 0; + return kErrNone; } +/// @brief Responds to a RemoveDirectory command +MavlinkFTP::ErrorCode +MavlinkFTP::_workRemoveDirectory(PayloadHeader* payload) +{ + char dir[kMaxDataLength]; + strncpy(dir, _data_as_cstring(payload), kMaxDataLength); + + if (rmdir(dir) == 0) { + payload->size = 0; + return kErrNone; + } else { + return kErrFailErrno; + } +} + +/// @brief Responds to a CreateDirectory command +MavlinkFTP::ErrorCode +MavlinkFTP::_workCreateDirectory(PayloadHeader* payload) +{ + char dir[kMaxDataLength]; + strncpy(dir, _data_as_cstring(payload), kMaxDataLength); + + if (mkdir(dir, S_IRWXU | S_IRWXG | S_IRWXO) == 0) { + payload->size = 0; + return kErrNone; + } else { + return kErrFailErrno; + } +} + +/// @brief Returns true if the specified session is a valid open session bool -MavlinkFTP::_validSession(unsigned index) +MavlinkFTP::_valid_session(unsigned index) { if ((index >= kMaxSession) || (_session_fds[index] < 0)) { return false; @@ -452,8 +582,9 @@ MavlinkFTP::_validSession(unsigned index) return true; } +/// @brief Returns an unused session index int -MavlinkFTP::_findUnusedSession(void) +MavlinkFTP::_find_unused_session(void) { for (size_t i=0; i<kMaxSession; i++) { if (_session_fds[i] == -1) { @@ -464,16 +595,53 @@ MavlinkFTP::_findUnusedSession(void) return -1; } +/// @brief Guarantees that the payload data is null terminated. +/// @return Returns a pointer to the payload data as a char * char * -MavlinkFTP::Request::dataAsCString() +MavlinkFTP::_data_as_cstring(PayloadHeader* payload) { // guarantee nul termination - if (header()->size < kMaxDataLength) { - requestData()[header()->size] = '\0'; + if (payload->size < kMaxDataLength) { + payload->data[payload->size] = '\0'; } else { - requestData()[kMaxDataLength - 1] = '\0'; + payload->data[kMaxDataLength - 1] = '\0'; } // and return data - return (char *)&(header()->data[0]); + return (char *)&(payload->data[0]); +} + +/// @brief Returns a unused Request entry. NULL if none available. +MavlinkFTP::Request * +MavlinkFTP::_get_request(void) +{ + _lock_request_queue(); + Request* req = reinterpret_cast<Request *>(dq_remfirst(&_request_queue)); + _unlock_request_queue(); + return req; +} + +/// @brief Locks a semaphore to provide exclusive access to the request queue +void +MavlinkFTP::_lock_request_queue(void) +{ + do {} + while (sem_wait(&_request_queue_sem) != 0); +} + +/// @brief Unlocks the semaphore providing exclusive access to the request queue +void +MavlinkFTP::_unlock_request_queue(void) +{ + sem_post(&_request_queue_sem); } + +/// @brief Returns a no longer needed request to the queue +void +MavlinkFTP::_return_request(Request *req) +{ + _lock_request_queue(); + dq_addlast(&req->work.dq, &_request_queue); + _unlock_request_queue(); +} + diff --git a/src/modules/mavlink/mavlink_ftp.h b/src/modules/mavlink/mavlink_ftp.h index 43de89de9..657e2f855 100644 --- a/src/modules/mavlink/mavlink_ftp.h +++ b/src/modules/mavlink/mavlink_ftp.h @@ -33,20 +33,8 @@ #pragma once -/** - * @file mavlink_ftp.h - * - * MAVLink remote file server. - * - * Messages are wrapped in ENCAPSULATED_DATA messages. Every message includes - * a session ID and sequence number. - * - * A limited number of requests (currently 2) may be outstanding at a time. - * Additional messages will be discarded. - * - * Messages consist of a fixed header, followed by a data area. - * - */ +/// @file mavlink_ftp.h +/// @author px4dev, Don Gagne <don@thegagnes.com> #include <dirent.h> #include <queue.h> @@ -57,174 +45,128 @@ #include "mavlink_messages.h" #include "mavlink_main.h" +class MavlinkFtpTest; + +/// @brief MAVLink remote file server. Support FTP like commands using MAVLINK_MSG_ID_FILE_TRANSFER_PROTOCOL message. +/// A limited number of requests (kRequestQueueSize) may be outstanding at a time. Additional messages will be discarded. class MavlinkFTP { public: + /// @brief Returns the one Mavlink FTP server in the system. + static MavlinkFTP* get_server(void); + + /// @brief Contructor is only public so unit test code can new objects. MavlinkFTP(); - - static MavlinkFTP *getServer(); - - // static interface - void handle_message(Mavlink* mavlink, - mavlink_message_t *msg); - -private: - - static const unsigned kRequestQueueSize = 2; - - static MavlinkFTP *_server; - - struct RequestHeader - { - uint8_t magic; - uint8_t session; - uint8_t opcode; - uint8_t size; - uint32_t crc32; - uint32_t offset; - uint8_t data[]; - }; - + + /// @brief Adds the specified message to the work queue. + void handle_message(Mavlink* mavlink, mavlink_message_t *msg); + + typedef void (*ReceiveMessageFunc_t)(const mavlink_message_t *msg, MavlinkFtpTest* ftpTest); + + /// @brief Sets up the server to run in unit test mode. + /// @param rcvmsgFunc Function which will be called to handle outgoing mavlink messages. + /// @param ftp_test MavlinkFtpTest object which the function is associated with + void set_unittest_worker(ReceiveMessageFunc_t rcvMsgFunc, MavlinkFtpTest *ftp_test); + + /// @brief This is the payload which is in mavlink_file_transfer_protocol_t.payload. We pad the structure ourselves to + /// 32 bit alignment to avoid usage of any pack pragmas. + struct PayloadHeader + { + uint16_t seqNumber; ///< sequence number for message + uint8_t session; ///< Session id for read and write commands + uint8_t opcode; ///< Command opcode + uint8_t size; ///< Size of data + uint8_t req_opcode; ///< Request opcode returned in kRspAck, kRspNak message + uint8_t padding[2]; ///< 32 bit aligment padding + uint32_t offset; ///< Offsets for List and Read commands + uint8_t data[]; ///< command data, varies by Opcode + }; + + /// @brief Command opcodes enum Opcode : uint8_t { - kCmdNone, // ignored, always acked - kCmdTerminate, // releases sessionID, closes file - kCmdReset, // terminates all sessions - kCmdList, // list files in <path> from <offset> - kCmdOpen, // opens <path> for reading, returns <session> - kCmdRead, // reads <size> bytes from <offset> in <session> - kCmdCreate, // creates <path> for writing, returns <session> - kCmdWrite, // appends <size> bytes at <offset> in <session> - kCmdRemove, // remove file (only if created by server?) - - kRspAck, - kRspNak + kCmdNone, ///< ignored, always acked + kCmdTerminateSession, ///< Terminates open Read session + kCmdResetSessions, ///< Terminates all open Read sessions + kCmdListDirectory, ///< List files in <path> from <offset> + kCmdOpenFile, ///< Opens file at <path> for reading, returns <session> + kCmdReadFile, ///< Reads <size> bytes from <offset> in <session> + kCmdCreateFile, ///< Creates file at <path> for writing, returns <session> + kCmdWriteFile, ///< Appends <size> bytes to file in <session> + kCmdRemoveFile, ///< Remove file at <path> + kCmdCreateDirectory, ///< Creates directory at <path> + kCmdRemoveDirectory, ///< Removes Directory at <path>, must be empty + + kRspAck = 128, ///< Ack response + kRspNak ///< Nak response }; - + + /// @brief Error codes returned in Nak response PayloadHeader.data[0]. enum ErrorCode : uint8_t - { + { kErrNone, - kErrNoRequest, - kErrNoSession, - kErrSequence, - kErrNotDir, - kErrNotFile, - kErrEOF, - kErrNotAppend, - kErrTooBig, - kErrIO, - kErrPerm - }; - - int _findUnusedSession(void); - bool _validSession(unsigned index); - - static const unsigned kMaxSession = 2; - int _session_fds[kMaxSession]; - - class Request + kErrFail, ///< Unknown failure + kErrFailErrno, ///< Command failed, errno sent back in PayloadHeader.data[1] + kErrInvalidDataSize, ///< PayloadHeader.size is invalid + kErrInvalidSession, ///< Session is not currently open + kErrNoSessionsAvailable, ///< All available Sessions in use + kErrEOF, ///< Offset past end of file for List and Read commands + kErrUnknownCommand ///< Unknown command opcode + }; + +private: + /// @brief Unit of work which is queued to work_queue + struct Request { - public: - union { - dq_entry_t entry; - work_s work; - }; - - bool decode(Mavlink *mavlink, mavlink_message_t *fromMessage) { - if (fromMessage->msgid == MAVLINK_MSG_ID_ENCAPSULATED_DATA) { - _mavlink = mavlink; - mavlink_msg_encapsulated_data_decode(fromMessage, &_message); - return true; - } - return false; - } - - void reply() { - - // XXX the proper way would be an IOCTL / uORB call, rather than exploiting the - // flat memory architecture, as we're operating between threads here. - mavlink_message_t msg; - msg.checksum = 0; - unsigned len = mavlink_msg_encapsulated_data_pack_chan(_mavlink->get_system_id(), _mavlink->get_component_id(), - _mavlink->get_channel(), &msg, sequence()+1, rawData()); - - _mavlink->lockMessageBufferMutex(); - bool success = _mavlink->message_buffer_write(&msg, len); - _mavlink->unlockMessageBufferMutex(); - - if (!success) { - warnx("FTP TX ERR"); - } -#ifdef MAVLINK_FTP_DEBUG - else { - warnx("wrote: sys: %d, comp: %d, chan: %d, len: %d, checksum: %d", - _mavlink->get_system_id(), - _mavlink->get_component_id(), - _mavlink->get_channel(), - len, - msg.checksum); - } -#endif - } - - uint8_t *rawData() { return &_message.data[0]; } - RequestHeader *header() { return reinterpret_cast<RequestHeader *>(&_message.data[0]); } - uint8_t *requestData() { return &(header()->data[0]); } - unsigned dataSize() { return header()->size + sizeof(RequestHeader); } - uint16_t sequence() const { return _message.seqnr; } - mavlink_channel_t channel() { return _mavlink->get_channel(); } - - char *dataAsCString(); - - private: - Mavlink *_mavlink; - mavlink_encapsulated_data_t _message; - + work_s work; ///< work queue entry + Mavlink *mavlink; ///< Mavlink to reply to + uint8_t serverSystemId; ///< System ID to send from + uint8_t serverComponentId; ///< Component ID to send from + uint8_t serverChannel; ///< Channel to send to + uint8_t targetSystemId; ///< System ID to target reply to + + mavlink_file_transfer_protocol_t message; ///< Protocol message }; - - static const uint8_t kProtocolMagic = 'f'; - static const char kDirentFile = 'F'; - static const char kDirentDir = 'D'; - static const char kDirentUnknown = 'U'; - static const uint8_t kMaxDataLength = MAVLINK_MSG_ENCAPSULATED_DATA_FIELD_DATA_LEN - sizeof(RequestHeader); - - /// Request worker; runs on the low-priority work queue to service - /// remote requests. - /// - static void _workerTrampoline(void *arg); - void _worker(Request *req); - - /// Reply to a request (XXX should be a Request method) - /// - void _reply(Request *req); - - ErrorCode _workList(Request *req); - ErrorCode _workOpen(Request *req, bool create); - ErrorCode _workRead(Request *req); - ErrorCode _workWrite(Request *req); - ErrorCode _workRemove(Request *req); - ErrorCode _workTerminate(Request *req); - ErrorCode _workReset(); - - // work freelist - Request _workBufs[kRequestQueueSize]; - dq_queue_t _workFree; - sem_t _lock; - - void _qLock() { do {} while (sem_wait(&_lock) != 0); } - void _qUnlock() { sem_post(&_lock); } - - void _qFree(Request *req) { - _qLock(); - dq_addlast(&req->entry, &_workFree); - _qUnlock(); - } - - Request *_dqFree() { - _qLock(); - auto req = reinterpret_cast<Request *>(dq_remfirst(&_workFree)); - _qUnlock(); - return req; - } - + + Request *_get_request(void); + void _return_request(Request *req); + void _lock_request_queue(void); + void _unlock_request_queue(void); + + char *_data_as_cstring(PayloadHeader* payload); + + static void _worker_trampoline(void *arg); + void _process_request(Request *req); + void _reply(Request *req); + + ErrorCode _workList(PayloadHeader *payload); + ErrorCode _workOpen(PayloadHeader *payload, bool create); + ErrorCode _workRead(PayloadHeader *payload); + ErrorCode _workWrite(PayloadHeader *payload); + ErrorCode _workTerminate(PayloadHeader *payload); + ErrorCode _workReset(PayloadHeader* payload); + ErrorCode _workRemoveDirectory(PayloadHeader *payload); + ErrorCode _workCreateDirectory(PayloadHeader *payload); + ErrorCode _workRemoveFile(PayloadHeader *payload); + + static const unsigned kRequestQueueSize = 2; ///< Max number of queued requests + Request _request_bufs[kRequestQueueSize]; ///< Request buffers which hold work + dq_queue_t _request_queue; ///< Queue of available Request buffers + sem_t _request_queue_sem; ///< Semaphore for locking access to _request_queue + + int _find_unused_session(void); + bool _valid_session(unsigned index); + + static const char kDirentFile = 'F'; ///< Identifies File returned from List command + static const char kDirentDir = 'D'; ///< Identifies Directory returned from List command + static const char kDirentSkip = 'S'; ///< Identifies Skipped entry from List command + + /// @brief Maximum data size in RequestHeader::data + static const uint8_t kMaxDataLength = MAVLINK_MSG_FILE_TRANSFER_PROTOCOL_FIELD_PAYLOAD_LEN - sizeof(PayloadHeader); + + static const unsigned kMaxSession = 2; ///< Max number of active sessions + int _session_fds[kMaxSession]; ///< Session file descriptors, 0 for empty slot + + ReceiveMessageFunc_t _utRcvMsgFunc; ///< Unit test override for mavlink message sending + MavlinkFtpTest *_ftp_test; ///< Additional parameter to _utRcvMsgFunc; }; diff --git a/src/modules/mavlink/mavlink_main.cpp b/src/modules/mavlink/mavlink_main.cpp index 408605939..940e64144 100644 --- a/src/modules/mavlink/mavlink_main.cpp +++ b/src/modules/mavlink/mavlink_main.cpp @@ -134,44 +134,44 @@ Mavlink::Mavlink() : _mode(MAVLINK_MODE_NORMAL), _channel(MAVLINK_COMM_0), _logbuffer {}, - _total_counter(0), - _receive_thread {}, - _verbose(false), - _forwarding_on(false), - _passing_on(false), - _ftp_on(false), - _uart_fd(-1), - _baudrate(57600), - _datarate(1000), - _datarate_events(500), - _rate_mult(1.0f), - _mavlink_param_queue_index(0), - mavlink_link_termination_allowed(false), - _subscribe_to_stream(nullptr), - _subscribe_to_stream_rate(0.0f), - _flow_control_enabled(true), - _last_write_success_time(0), - _last_write_try_time(0), - _bytes_tx(0), - _bytes_txerr(0), - _bytes_rx(0), - _bytes_timestamp(0), - _rate_tx(0.0f), - _rate_txerr(0.0f), - _rate_rx(0.0f), - _rstatus {}, - _message_buffer {}, - _message_buffer_mutex {}, - _send_mutex {}, - _param_initialized(false), - _param_system_id(0), - _param_component_id(0), - _param_system_type(0), - _param_use_hil_gps(0), - - /* performance counters */ - _loop_perf(perf_alloc(PC_ELAPSED, "mavlink_el")), - _txerr_perf(perf_alloc(PC_COUNT, "mavlink_txe")) + _total_counter(0), + _receive_thread {}, + _verbose(false), + _forwarding_on(false), + _passing_on(false), + _ftp_on(false), + _uart_fd(-1), + _baudrate(57600), + _datarate(1000), + _datarate_events(500), + _rate_mult(1.0f), + _mavlink_param_queue_index(0), + mavlink_link_termination_allowed(false), + _subscribe_to_stream(nullptr), + _subscribe_to_stream_rate(0.0f), + _flow_control_enabled(true), + _last_write_success_time(0), + _last_write_try_time(0), + _bytes_tx(0), + _bytes_txerr(0), + _bytes_rx(0), + _bytes_timestamp(0), + _rate_tx(0.0f), + _rate_txerr(0.0f), + _rate_rx(0.0f), + _rstatus {}, + _message_buffer {}, + _message_buffer_mutex {}, + _send_mutex {}, + _param_initialized(false), + _param_system_id(0), + _param_component_id(0), + _param_system_type(0), + _param_use_hil_gps(0), + + /* performance counters */ + _loop_perf(perf_alloc(PC_ELAPSED, "mavlink_el")), + _txerr_perf(perf_alloc(PC_COUNT, "mavlink_txe")) { fops.ioctl = (int (*)(file *, int, long unsigned int))&mavlink_dev_ioctl; @@ -217,6 +217,8 @@ Mavlink::Mavlink() : errx(1, "instance ID is out of range"); break; } + + _rstatus.type = TELEMETRY_STATUS_RADIO_TYPE_GENERIC; } Mavlink::~Mavlink() @@ -1227,7 +1229,10 @@ Mavlink::task_main(int argc, char *argv[]) _mode = MAVLINK_MODE_CUSTOM; } else if (strcmp(optarg, "camera") == 0) { - _mode = MAVLINK_MODE_CAMERA; + // left in here for compatibility + _mode = MAVLINK_MODE_ONBOARD; + } else if (strcmp(optarg, "onboard") == 0) { + _mode = MAVLINK_MODE_ONBOARD; } break; @@ -1287,8 +1292,8 @@ Mavlink::task_main(int argc, char *argv[]) warnx("mode: CUSTOM"); break; - case MAVLINK_MODE_CAMERA: - warnx("mode: CAMERA"); + case MAVLINK_MODE_ONBOARD: + warnx("mode: ONBOARD"); break; default: @@ -1391,13 +1396,14 @@ Mavlink::task_main(int argc, char *argv[]) configure_stream("POSITION_TARGET_GLOBAL_INT", 3.0f); configure_stream("ATTITUDE_TARGET", 3.0f); configure_stream("DISTANCE_SENSOR", 0.5f); + configure_stream("OPTICAL_FLOW", 20.0f); break; - case MAVLINK_MODE_CAMERA: + case MAVLINK_MODE_ONBOARD: configure_stream("SYS_STATUS", 1.0f); - configure_stream("ATTITUDE", 15.0f); - configure_stream("GLOBAL_POSITION_INT", 15.0f); - configure_stream("CAMERA_CAPTURE", 1.0f); + configure_stream("ATTITUDE", 50.0f); + configure_stream("GLOBAL_POSITION_INT", 50.0f); + configure_stream("CAMERA_CAPTURE", 2.0f); break; default: @@ -1653,6 +1659,8 @@ Mavlink::display_status() printf("\tGCS heartbeat:\t%llu us ago\n", hrt_elapsed_time(&_rstatus.heartbeat_time)); } + printf("\tmavlink chan: #%u\n", _channel); + if (_rstatus.timestamp > 0) { printf("\ttype:\t\t"); diff --git a/src/modules/mavlink/mavlink_main.h b/src/modules/mavlink/mavlink_main.h index 1e2e94cef..7f9d225bb 100644 --- a/src/modules/mavlink/mavlink_main.h +++ b/src/modules/mavlink/mavlink_main.h @@ -127,7 +127,7 @@ public: enum MAVLINK_MODE { MAVLINK_MODE_NORMAL = 0, MAVLINK_MODE_CUSTOM, - MAVLINK_MODE_CAMERA + MAVLINK_MODE_ONBOARD }; void set_mode(enum MAVLINK_MODE); diff --git a/src/modules/mavlink/mavlink_messages.cpp b/src/modules/mavlink/mavlink_messages.cpp index af4d46a36..a2f3828ff 100644 --- a/src/modules/mavlink/mavlink_messages.cpp +++ b/src/modules/mavlink/mavlink_messages.cpp @@ -774,6 +774,9 @@ private: MavlinkOrbSubscription *_airspeed_sub; uint64_t _airspeed_time; + MavlinkOrbSubscription *_sensor_combined_sub; + uint64_t _sensor_combined_time; + /* do not allow top copying this class */ MavlinkStreamVFRHUD(MavlinkStreamVFRHUD &); MavlinkStreamVFRHUD& operator = (const MavlinkStreamVFRHUD &); @@ -789,7 +792,9 @@ protected: _act_sub(_mavlink->add_orb_subscription(ORB_ID(actuator_controls_0))), _act_time(0), _airspeed_sub(_mavlink->add_orb_subscription(ORB_ID(airspeed))), - _airspeed_time(0) + _airspeed_time(0), + _sensor_combined_sub(_mavlink->add_orb_subscription(ORB_ID(sensor_combined))), + _sensor_combined_time(0) {} void send(const hrt_abstime t) @@ -799,12 +804,14 @@ protected: struct actuator_armed_s armed; struct actuator_controls_s act; struct airspeed_s airspeed; + struct sensor_combined_s sensor_combined; bool updated = _att_sub->update(&_att_time, &att); updated |= _pos_sub->update(&_pos_time, &pos); updated |= _armed_sub->update(&_armed_time, &armed); updated |= _act_sub->update(&_act_time, &act); updated |= _airspeed_sub->update(&_airspeed_time, &airspeed); + updated |= _sensor_combined_sub->update(&_sensor_combined_time, &sensor_combined); if (updated) { mavlink_vfr_hud_t msg; @@ -813,7 +820,7 @@ protected: msg.groundspeed = sqrtf(pos.vel_n * pos.vel_n + pos.vel_e * pos.vel_e); msg.heading = _wrap_2pi(att.yaw) * M_RAD_TO_DEG_F; msg.throttle = armed.armed ? act.control[3] * 100.0f : 0.0f; - msg.alt = pos.alt; + msg.alt = sensor_combined.baro_alt_meter; msg.climb = -pos.vel_d; _mavlink->send_message(MAVLINK_MSG_ID_VFR_HUD, &msg); @@ -879,8 +886,8 @@ protected: msg.eph = cm_uint16_from_m_float(gps.eph); msg.epv = cm_uint16_from_m_float(gps.epv); msg.vel = cm_uint16_from_m_float(gps.vel_m_s), - msg.cog = _wrap_2pi(gps.cog_rad) * M_RAD_TO_DEG_F * 1e2f, - msg.satellites_visible = gps.satellites_used; + msg.cog = _wrap_2pi(gps.cog_rad) * M_RAD_TO_DEG_F * 1e2f, + msg.satellites_visible = gps.satellites_used; _mavlink->send_message(MAVLINK_MSG_ID_GPS_RAW_INT, &msg); } @@ -950,11 +957,11 @@ protected: msg.lat = pos.lat * 1e7; msg.lon = pos.lon * 1e7; msg.alt = pos.alt * 1000.0f; - msg.relative_alt = (pos.alt - home.alt) * 1000.0f; - msg.vx = pos.vel_n * 100.0f; - msg.vy = pos.vel_e * 100.0f; - msg.vz = pos.vel_d * 100.0f; - msg.hdg = _wrap_2pi(pos.yaw) * M_RAD_TO_DEG_F * 100.0f; + msg.relative_alt = (pos.alt - home.alt) * 1000.0f; + msg.vx = pos.vel_n * 100.0f; + msg.vy = pos.vel_e * 100.0f; + msg.vz = pos.vel_d * 100.0f; + msg.hdg = _wrap_2pi(pos.yaw) * M_RAD_TO_DEG_F * 100.0f; _mavlink->send_message(MAVLINK_MSG_ID_GLOBAL_POSITION_INT, &msg); } @@ -1015,9 +1022,9 @@ protected: msg.x = pos.x; msg.y = pos.y; msg.z = pos.z; - msg.vx = pos.vx; - msg.vy = pos.vy; - msg.vz = pos.vz; + msg.vx = pos.vx; + msg.vy = pos.vy; + msg.vz = pos.vz; _mavlink->send_message(MAVLINK_MSG_ID_LOCAL_POSITION_NED, &msg); } @@ -1078,9 +1085,9 @@ protected: msg.x = pos.x; msg.y = pos.y; msg.z = pos.z; - msg.roll = pos.roll; - msg.pitch = pos.pitch; - msg.yaw = pos.yaw; + msg.roll = pos.roll; + msg.pitch = pos.pitch; + msg.yaw = pos.yaw; _mavlink->send_message(MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE, &msg); } diff --git a/src/modules/mavlink/mavlink_mission.cpp b/src/modules/mavlink/mavlink_mission.cpp index 7a761588a..a3c127cdc 100644 --- a/src/modules/mavlink/mavlink_mission.cpp +++ b/src/modules/mavlink/mavlink_mission.cpp @@ -58,6 +58,10 @@ #endif static const int ERROR = -1; +#define CHECK_SYSID_COMPID_MISSION(_msg) (_msg.target_system == mavlink_system.sysid && \ + ((_msg.target_component == mavlink_system.compid) || \ + (_msg.target_component == MAV_COMP_ID_MISSIONPLANNER) || \ + (_msg.target_component == MAV_COMP_ID_ALL))) MavlinkMissionManager::MavlinkMissionManager(Mavlink *mavlink) : MavlinkStream(mavlink), _state(MAVLINK_WPM_STATE_IDLE), @@ -79,8 +83,7 @@ MavlinkMissionManager::MavlinkMissionManager(Mavlink *mavlink) : MavlinkStream(m _mission_result_sub(-1), _offboard_mission_pub(-1), _slow_rate_limiter(_interval / 10.0f), - _verbose(false), - _comp_id(MAV_COMP_ID_MISSIONPLANNER) + _verbose(false) { _offboard_mission_sub = orb_subscribe(ORB_ID(offboard_mission)); _mission_result_sub = orb_subscribe(ORB_ID(mission_result)); @@ -384,7 +387,7 @@ MavlinkMissionManager::handle_mission_ack(const mavlink_message_t *msg) mavlink_mission_ack_t wpa; mavlink_msg_mission_ack_decode(msg, &wpa); - if (wpa.target_system == mavlink_system.sysid /*&& wpa.target_component == mavlink_wpm_comp_id*/) { + if (CHECK_SYSID_COMPID_MISSION(wpa)) { if ((msg->sysid == _transfer_partner_sysid && msg->compid == _transfer_partner_compid)) { if (_state == MAVLINK_WPM_STATE_SENDLIST) { _time_last_recv = hrt_absolute_time(); @@ -416,7 +419,7 @@ MavlinkMissionManager::handle_mission_set_current(const mavlink_message_t *msg) mavlink_mission_set_current_t wpc; mavlink_msg_mission_set_current_decode(msg, &wpc); - if (wpc.target_system == mavlink_system.sysid /*&& wpc.target_component == mavlink_wpm_comp_id*/) { + if (CHECK_SYSID_COMPID_MISSION(wpc)) { if (_state == MAVLINK_WPM_STATE_IDLE) { _time_last_recv = hrt_absolute_time(); @@ -451,7 +454,7 @@ MavlinkMissionManager::handle_mission_request_list(const mavlink_message_t *msg) mavlink_mission_request_list_t wprl; mavlink_msg_mission_request_list_decode(msg, &wprl); - if (wprl.target_system == mavlink_system.sysid /*&& wprl.target_component == mavlink_wpm_comp_id*/) { + if (CHECK_SYSID_COMPID_MISSION(wprl)) { if (_state == MAVLINK_WPM_STATE_IDLE || _state == MAVLINK_WPM_STATE_SENDLIST) { _time_last_recv = hrt_absolute_time(); @@ -487,7 +490,7 @@ MavlinkMissionManager::handle_mission_request(const mavlink_message_t *msg) mavlink_mission_request_t wpr; mavlink_msg_mission_request_decode(msg, &wpr); - if (wpr.target_system == mavlink_system.sysid /*&& wpr.target_component == mavlink_wpm_comp_id*/) { + if (CHECK_SYSID_COMPID_MISSION(wpr)) { if (msg->sysid == _transfer_partner_sysid && msg->compid == _transfer_partner_compid) { if (_state == MAVLINK_WPM_STATE_SENDLIST) { _time_last_recv = hrt_absolute_time(); @@ -558,7 +561,7 @@ MavlinkMissionManager::handle_mission_count(const mavlink_message_t *msg) mavlink_mission_count_t wpc; mavlink_msg_mission_count_decode(msg, &wpc); - if (wpc.target_system == mavlink_system.sysid/* && wpc.target_component == mavlink_wpm_comp_id*/) { + if (CHECK_SYSID_COMPID_MISSION(wpc)) { if (_state == MAVLINK_WPM_STATE_IDLE) { _time_last_recv = hrt_absolute_time(); @@ -624,7 +627,7 @@ MavlinkMissionManager::handle_mission_item(const mavlink_message_t *msg) mavlink_mission_item_t wp; mavlink_msg_mission_item_decode(msg, &wp); - if (wp.target_system == mavlink_system.sysid && wp.target_component == _comp_id) { + if (CHECK_SYSID_COMPID_MISSION(wp)) { if (_state == MAVLINK_WPM_STATE_GETLIST) { _time_last_recv = hrt_absolute_time(); @@ -710,7 +713,7 @@ MavlinkMissionManager::handle_mission_clear_all(const mavlink_message_t *msg) mavlink_mission_clear_all_t wpca; mavlink_msg_mission_clear_all_decode(msg, &wpca); - if (wpca.target_system == mavlink_system.sysid /*&& wpca.target_component == mavlink_wpm_comp_id */) { + if (CHECK_SYSID_COMPID_MISSION(wpca)) { if (_state == MAVLINK_WPM_STATE_IDLE) { /* don't touch mission items storage itself, but only items count in mission state */ @@ -795,10 +798,10 @@ int MavlinkMissionManager::format_mavlink_mission_item(const struct mission_item_s *mission_item, mavlink_mission_item_t *mavlink_mission_item) { if (mission_item->altitude_is_relative) { - mavlink_mission_item->frame = MAV_FRAME_GLOBAL; + mavlink_mission_item->frame = MAV_FRAME_GLOBAL_RELATIVE_ALT; } else { - mavlink_mission_item->frame = MAV_FRAME_GLOBAL_RELATIVE_ALT; + mavlink_mission_item->frame = MAV_FRAME_GLOBAL; } switch (mission_item->nav_cmd) { diff --git a/src/modules/mavlink/mavlink_mission.h b/src/modules/mavlink/mavlink_mission.h index 8ff27f87d..a7bb94c22 100644 --- a/src/modules/mavlink/mavlink_mission.h +++ b/src/modules/mavlink/mavlink_mission.h @@ -126,8 +126,6 @@ private: bool _verbose; - uint8_t _comp_id; - /* do not allow top copying this class */ MavlinkMissionManager(MavlinkMissionManager &); MavlinkMissionManager& operator = (const MavlinkMissionManager &); diff --git a/src/modules/mavlink/mavlink_receiver.cpp b/src/modules/mavlink/mavlink_receiver.cpp index c0fae0a2f..373d06d4d 100644 --- a/src/modules/mavlink/mavlink_receiver.cpp +++ b/src/modules/mavlink/mavlink_receiver.cpp @@ -54,6 +54,7 @@ #include <drivers/drv_gyro.h> #include <drivers/drv_mag.h> #include <drivers/drv_baro.h> +#include <drivers/drv_range_finder.h> #include <time.h> #include <float.h> #include <unistd.h> @@ -102,6 +103,7 @@ MavlinkReceiver::MavlinkReceiver(Mavlink *parent) : _battery_pub(-1), _cmd_pub(-1), _flow_pub(-1), + _range_pub(-1), _offboard_control_sp_pub(-1), _local_pos_sp_pub(-1), _global_vel_sp_pub(-1), @@ -112,7 +114,6 @@ MavlinkReceiver::MavlinkReceiver(Mavlink *parent) : _telemetry_status_pub(-1), _rc_pub(-1), _manual_pub(-1), - _radio_status_available(false), _control_mode_sub(orb_subscribe(ORB_ID(vehicle_control_mode))), _hil_frames(0), _old_timestamp(0), @@ -122,7 +123,7 @@ MavlinkReceiver::MavlinkReceiver(Mavlink *parent) : { // make sure the FTP server is started - (void)MavlinkFTP::getServer(); + (void)MavlinkFTP::get_server(); } MavlinkReceiver::~MavlinkReceiver() @@ -137,6 +138,10 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg) handle_message_command_long(msg); break; + case MAVLINK_MSG_ID_COMMAND_INT: + handle_message_command_int(msg); + break; + case MAVLINK_MSG_ID_OPTICAL_FLOW: handle_message_optical_flow(msg); break; @@ -169,8 +174,8 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg) handle_message_request_data_stream(msg); break; - case MAVLINK_MSG_ID_ENCAPSULATED_DATA: - MavlinkFTP::getServer()->handle_message(_mavlink, msg); + case MAVLINK_MSG_ID_FILE_TRANSFER_PROTOCOL: + MavlinkFTP::get_server()->handle_message(_mavlink, msg); break; default: @@ -197,6 +202,10 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg) handle_message_hil_state_quaternion(msg); break; + case MAVLINK_MSG_ID_HIL_OPTICAL_FLOW: + handle_message_hil_optical_flow(msg); + break; + default: break; } @@ -277,6 +286,62 @@ MavlinkReceiver::handle_message_command_long(mavlink_message_t *msg) } void +MavlinkReceiver::handle_message_command_int(mavlink_message_t *msg) +{ + /* command */ + mavlink_command_int_t cmd_mavlink; + mavlink_msg_command_int_decode(msg, &cmd_mavlink); + + if (cmd_mavlink.target_system == mavlink_system.sysid && ((cmd_mavlink.target_component == mavlink_system.compid) + || (cmd_mavlink.target_component == MAV_COMP_ID_ALL))) { + //check for MAVLINK terminate command + if (cmd_mavlink.command == MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN && ((int)cmd_mavlink.param1) == 3) { + /* This is the link shutdown command, terminate mavlink */ + warnx("terminated by remote command"); + fflush(stdout); + usleep(50000); + + /* terminate other threads and this thread */ + _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 (%d/%d) ID", + mavlink_system.sysid, mavlink_system.compid); + return; + } + + struct vehicle_command_s vcmd; + memset(&vcmd, 0, sizeof(vcmd)); + + /* Copy the content of mavlink_command_int_t cmd_mavlink into command_t cmd */ + vcmd.param1 = cmd_mavlink.param1; + vcmd.param2 = cmd_mavlink.param2; + vcmd.param3 = cmd_mavlink.param3; + vcmd.param4 = cmd_mavlink.param4; + /* these are coordinates as 1e7 scaled integers to work around the 32 bit floating point limits */ + vcmd.param5 = ((double)cmd_mavlink.x) / 1e7; + vcmd.param6 = ((double)cmd_mavlink.y) / 1e7; + vcmd.param7 = cmd_mavlink.z; + // XXX do proper translation + vcmd.command = (enum VEHICLE_CMD)cmd_mavlink.command; + vcmd.target_system = cmd_mavlink.target_system; + vcmd.target_component = cmd_mavlink.target_component; + vcmd.source_system = msg->sysid; + vcmd.source_component = msg->compid; + + if (_cmd_pub < 0) { + _cmd_pub = orb_advertise(ORB_ID(vehicle_command), &vcmd); + + } else { + orb_publish(ORB_ID(vehicle_command), _cmd_pub, &vcmd); + } + } + } +} + +void MavlinkReceiver::handle_message_optical_flow(mavlink_message_t *msg) { /* optical flow */ @@ -305,6 +370,52 @@ MavlinkReceiver::handle_message_optical_flow(mavlink_message_t *msg) } void +MavlinkReceiver::handle_message_hil_optical_flow(mavlink_message_t *msg) +{ + /* optical flow */ + mavlink_hil_optical_flow_t flow; + mavlink_msg_hil_optical_flow_decode(msg, &flow); + + struct optical_flow_s f; + 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; + f.flow_comp_y_m = flow.flow_comp_m_y; + f.ground_distance_m = flow.ground_distance; + f.quality = flow.quality; + f.sensor_id = flow.sensor_id; + + if (_flow_pub < 0) { + _flow_pub = orb_advertise(ORB_ID(optical_flow), &f); + + } else { + orb_publish(ORB_ID(optical_flow), _flow_pub, &f); + } + + /* Use distance value for range finder report */ + struct range_finder_report r; + memset(&r, 0, sizeof(f)); + + r.timestamp = hrt_absolute_time(); + r.error_count = 0; + r.type = RANGE_FINDER_TYPE_LASER; + r.distance = flow.ground_distance; + r.minimum_distance = 0.0f; + r.maximum_distance = 40.0f; // this is set to match the typical range of real sensors, could be made configurable + r.valid = (r.distance > r.minimum_distance) && (r.distance < r.maximum_distance); + + if (_range_pub < 0) { + _range_pub = orb_advertise(ORB_ID(sensor_range_finder), &r); + } else { + orb_publish(ORB_ID(sensor_range_finder), _range_pub, &r); + } +} + +void MavlinkReceiver::handle_message_set_mode(mavlink_message_t *msg) { mavlink_set_mode_t new_mode; @@ -385,7 +496,7 @@ MavlinkReceiver::handle_message_vision_position_estimate(mavlink_message_t *msg) vision_position.vx = 0.0f; vision_position.vy = 0.0f; vision_position.vz = 0.0f; - + math::Quaternion q; q.from_euler(pos.roll, pos.pitch, pos.yaw); @@ -430,9 +541,6 @@ MavlinkReceiver::handle_message_radio_status(mavlink_message_t *msg) } else { orb_publish(telemetry_status_orb_id[_mavlink->get_channel()], _telemetry_status_pub, &tstatus); } - - /* this means that heartbeats alone won't be published to the radio status no more */ - _radio_status_available = true; } } @@ -474,25 +582,17 @@ MavlinkReceiver::handle_message_heartbeat(mavlink_message_t *msg) struct telemetry_status_s &tstatus = _mavlink->get_rx_status(); - hrt_abstime tnow = hrt_absolute_time(); + /* set heartbeat time and topic time and publish - + * the telem status also gets updated on telemetry events + */ + tstatus.timestamp = hrt_absolute_time(); + tstatus.heartbeat_time = tstatus.timestamp; - /* always set heartbeat, publish only if telemetry link not up */ - tstatus.heartbeat_time = tnow; + if (_telemetry_status_pub < 0) { + _telemetry_status_pub = orb_advertise(telemetry_status_orb_id[_mavlink->get_channel()], &tstatus); - /* if no radio status messages arrive, lets at least publish that heartbeats were received */ - if (!_radio_status_available) { - - tstatus.timestamp = tnow; - /* telem_time indicates the timestamp of a telemetry status packet and we got none */ - tstatus.telem_time = 0; - tstatus.type = TELEMETRY_STATUS_RADIO_TYPE_GENERIC; - - if (_telemetry_status_pub < 0) { - _telemetry_status_pub = orb_advertise(telemetry_status_orb_id[_mavlink->get_channel()], &tstatus); - - } else { - orb_publish(telemetry_status_orb_id[_mavlink->get_channel()], _telemetry_status_pub, &tstatus); - } + } else { + orb_publish(telemetry_status_orb_id[_mavlink->get_channel()], _telemetry_status_pub, &tstatus); } } } diff --git a/src/modules/mavlink/mavlink_receiver.h b/src/modules/mavlink/mavlink_receiver.h index 014193100..c4e12d8d8 100644 --- a/src/modules/mavlink/mavlink_receiver.h +++ b/src/modules/mavlink/mavlink_receiver.h @@ -110,7 +110,9 @@ private: void handle_message(mavlink_message_t *msg); void handle_message_command_long(mavlink_message_t *msg); + void handle_message_command_int(mavlink_message_t *msg); void handle_message_optical_flow(mavlink_message_t *msg); + void handle_message_hil_optical_flow(mavlink_message_t *msg); void handle_message_set_mode(mavlink_message_t *msg); void handle_message_vicon_position_estimate(mavlink_message_t *msg); void handle_message_vision_position_estimate(mavlink_message_t *msg); @@ -141,6 +143,7 @@ private: orb_advert_t _battery_pub; orb_advert_t _cmd_pub; orb_advert_t _flow_pub; + orb_advert_t _range_pub; orb_advert_t _offboard_control_sp_pub; orb_advert_t _local_pos_sp_pub; orb_advert_t _global_vel_sp_pub; @@ -151,7 +154,6 @@ private: orb_advert_t _telemetry_status_pub; orb_advert_t _rc_pub; orb_advert_t _manual_pub; - bool _radio_status_available; int _control_mode_sub; int _hil_frames; uint64_t _old_timestamp; diff --git a/src/modules/mavlink/mavlink_tests/mavlink_ftp_test.cpp b/src/modules/mavlink/mavlink_tests/mavlink_ftp_test.cpp new file mode 100644 index 000000000..022041c74 --- /dev/null +++ b/src/modules/mavlink/mavlink_tests/mavlink_ftp_test.cpp @@ -0,0 +1,757 @@ +/**************************************************************************** + * + * 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 mavlink_ftp_test.cpp +/// @author Don Gagne <don@thegagnes.com> + +#include <sys/stat.h> +#include <crc32.h> +#include <stdio.h> +#include <fcntl.h> + +#include "mavlink_ftp_test.h" +#include "../mavlink_ftp.h" + +/// @brief Test case file name for Read command. File are generated using mavlink_ftp_test_data.py +const MavlinkFtpTest::ReadTestCase MavlinkFtpTest::_rgReadTestCases[] = { + { "/etc/unit_test_data/mavlink_tests/test_238.data", MAVLINK_MSG_FILE_TRANSFER_PROTOCOL_FIELD_PAYLOAD_LEN - sizeof(MavlinkFTP::PayloadHeader) - 1}, // Read takes less than single packet + { "/etc/unit_test_data/mavlink_tests/test_239.data", MAVLINK_MSG_FILE_TRANSFER_PROTOCOL_FIELD_PAYLOAD_LEN - sizeof(MavlinkFTP::PayloadHeader) }, // Read completely fills single packet + { "/etc/unit_test_data/mavlink_tests/test_240.data", MAVLINK_MSG_FILE_TRANSFER_PROTOCOL_FIELD_PAYLOAD_LEN - sizeof(MavlinkFTP::PayloadHeader) + 1 }, // Read take two packets +}; + +const char MavlinkFtpTest::_unittest_microsd_dir[] = "/fs/microsd/ftp_unit_test_dir"; +const char MavlinkFtpTest::_unittest_microsd_file[] = "/fs/microsd/ftp_unit_test_dir/file"; + +MavlinkFtpTest::MavlinkFtpTest() : + _ftp_server{}, + _reply_msg{}, + _lastOutgoingSeqNumber{} +{ +} + +MavlinkFtpTest::~MavlinkFtpTest() +{ + +} + +/// @brief Called before every test to initialize the FTP Server. +void MavlinkFtpTest::init(void) +{ + _ftp_server = new MavlinkFTP;; + _ftp_server->set_unittest_worker(MavlinkFtpTest::receive_message, this); + + _cleanup_microsd(); +} + +/// @brief Called after every test to take down the FTP Server. +void MavlinkFtpTest::cleanup(void) +{ + delete _ftp_server; + + _cleanup_microsd(); +} + +/// @brief Tests for correct behavior of an Ack response. +bool MavlinkFtpTest::_ack_test(void) +{ + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + + payload.opcode = MavlinkFTP::kCmdNone; + + bool success = _send_receive_msg(&payload, // FTP payload header + 0, // size in bytes of data + nullptr, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("Didn't get Ack back", reply->opcode, MavlinkFTP::kRspAck); + ut_compare("Incorrect payload size", reply->size, 0); + + return true; +} + +/// @brief Tests for correct response to an invalid opcpde. +bool MavlinkFtpTest::_bad_opcode_test(void) +{ + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + + payload.opcode = 0xFF; // bogus opcode + + bool success = _send_receive_msg(&payload, // FTP payload header + 0, // size in bytes of data + nullptr, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("Didn't get Nak back", reply->opcode, MavlinkFTP::kRspNak); + ut_compare("Incorrect payload size", reply->size, 1); + ut_compare("Incorrect error code", reply->data[0], MavlinkFTP::kErrUnknownCommand); + + return true; +} + +/// @brief Tests for correct reponse to a payload which an invalid data size field. +bool MavlinkFtpTest::_bad_datasize_test(void) +{ + mavlink_message_t msg; + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + + payload.opcode = MavlinkFTP::kCmdListDirectory; + + _setup_ftp_msg(&payload, 0, nullptr, &msg); + + // Set the data size to be one larger than is legal + ((MavlinkFTP::PayloadHeader*)((mavlink_file_transfer_protocol_t*)msg.payload64)->payload)->size = MAVLINK_MSG_FILE_TRANSFER_PROTOCOL_FIELD_PAYLOAD_LEN + 1; + + _ftp_server->handle_message(nullptr /* mavlink */, &msg); + + if (!_decode_message(&_reply_msg, &ftp_msg, &reply)) { + return false; + } + + ut_compare("Didn't get Nak back", reply->opcode, MavlinkFTP::kRspNak); + ut_compare("Incorrect payload size", reply->size, 1); + ut_compare("Incorrect error code", reply->data[0], MavlinkFTP::kErrInvalidDataSize); + + return true; +} + +bool MavlinkFtpTest::_list_test(void) +{ + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + + char response1[] = "Dempty_dir|Ftest_238.data\t238|Ftest_239.data\t239|Ftest_240.data\t240"; + char response2[] = "Ddev|Detc|Dfs|Dobj"; + + struct _testCase { + const char *dir; ///< Directory to run List command on + char *response; ///< Expected response entries from List command + int response_count; ///< Number of directories that should be returned + bool success; ///< true: List command should succeed, false: List command should fail + }; + struct _testCase rgTestCases[] = { + { "/bogus", nullptr, 0, false }, + { "/etc/unit_test_data/mavlink_tests", response1, 4, true }, + { "/", response2, 4, true }, + }; + + for (size_t i=0; i<sizeof(rgTestCases)/sizeof(rgTestCases[0]); i++) { + const struct _testCase *test = &rgTestCases[i]; + + payload.opcode = MavlinkFTP::kCmdListDirectory; + payload.offset = 0; + + bool success = _send_receive_msg(&payload, // FTP payload header + strlen(test->dir)+1, // size in bytes of data + (uint8_t*)test->dir, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + if (test->success) { + ut_compare("Didn't get Ack back", reply->opcode, MavlinkFTP::kRspAck); + ut_compare("Incorrect payload size", reply->size, strlen(test->response) + 1); + + // The return order of directories from the List command is not repeatable. So we can't do a direct comparison + // to a hardcoded return result string. + + // Convert null terminators to seperator char so we can use strok to parse returned data + for (uint8_t j=0; j<reply->size-1; j++) { + if (reply->data[j] == 0) { + reply->data[j] = '|'; + } + } + + // Loop over returned directory entries trying to find then in the response list + char *dir; + int response_count = 0; + dir = strtok((char *)&reply->data[0], "|"); + while (dir != nullptr) { + ut_assert("Returned directory not found in expected response", strstr(test->response, dir)); + response_count++; + dir = strtok(nullptr, "|"); + } + + ut_compare("Incorrect number of directory entires returned", test->response_count, response_count); + } else { + ut_compare("Didn't get Nak back", reply->opcode, MavlinkFTP::kRspNak); + ut_compare("Incorrect payload size", reply->size, 2); + ut_compare("Incorrect error code", reply->data[0], MavlinkFTP::kErrFailErrno); + } + } + + return true; +} + +/// @brief Tests for correct reponse to a List command on a valid directory, but with an offset that +/// is beyond the last directory entry. +bool MavlinkFtpTest::_list_eof_test(void) +{ + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + const char *dir = "/"; + + payload.opcode = MavlinkFTP::kCmdListDirectory; + payload.offset = 4; // offset past top level dirs + + bool success = _send_receive_msg(&payload, // FTP payload header + strlen(dir)+1, // size in bytes of data + (uint8_t*)dir, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("Didn't get Nak back", reply->opcode, MavlinkFTP::kRspNak); + ut_compare("Incorrect payload size", reply->size, 1); + ut_compare("Incorrect error code", reply->data[0], MavlinkFTP::kErrEOF); + + return true; +} + +/// @brief Tests for correct reponse to an Open command on a file which does not exist. +bool MavlinkFtpTest::_open_badfile_test(void) +{ + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + const char *dir = "/foo"; // non-existent file + + payload.opcode = MavlinkFTP::kCmdOpenFile; + payload.offset = 0; + + bool success = _send_receive_msg(&payload, // FTP payload header + strlen(dir)+1, // size in bytes of data + (uint8_t*)dir, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("Didn't get Nak back", reply->opcode, MavlinkFTP::kRspNak); + ut_compare("Incorrect payload size", reply->size, 2); + ut_compare("Incorrect error code", reply->data[0], MavlinkFTP::kErrFailErrno); + + return true; +} + +/// @brief Tests for correct reponse to an Open command on a file, followed by Terminate +bool MavlinkFtpTest::_open_terminate_test(void) +{ + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + + for (size_t i=0; i<sizeof(_rgReadTestCases)/sizeof(_rgReadTestCases[0]); i++) { + struct stat st; + const ReadTestCase *test = &_rgReadTestCases[i]; + + payload.opcode = MavlinkFTP::kCmdOpenFile; + payload.offset = 0; + + bool success = _send_receive_msg(&payload, // FTP payload header + strlen(test->file)+1, // size in bytes of data + (uint8_t*)test->file, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("stat failed", stat(test->file, &st), 0); + + + ut_compare("Didn't get Ack back", reply->opcode, MavlinkFTP::kRspAck); + ut_compare("Incorrect payload size", reply->size, sizeof(uint32_t)); + ut_compare("File size incorrect", *((uint32_t*)&reply->data[0]), (uint32_t)st.st_size); + + payload.opcode = MavlinkFTP::kCmdTerminateSession; + payload.session = reply->session; + payload.size = 0; + + success = _send_receive_msg(&payload, // FTP payload header + 0, // size in bytes of data + nullptr, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("Didn't get Ack back", reply->opcode, MavlinkFTP::kRspAck); + ut_compare("Incorrect payload size", reply->size, 0); + } + + return true; +} + +/// @brief Tests for correct reponse to a Terminate command on an invalid session. +bool MavlinkFtpTest::_terminate_badsession_test(void) +{ + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + const char *file = _rgReadTestCases[0].file; + + payload.opcode = MavlinkFTP::kCmdOpenFile; + payload.offset = 0; + + bool success = _send_receive_msg(&payload, // FTP payload header + strlen(file)+1, // size in bytes of data + (uint8_t*)file, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("Didn't get Ack back", reply->opcode, MavlinkFTP::kRspAck); + + payload.opcode = MavlinkFTP::kCmdTerminateSession; + payload.session = reply->session + 1; + payload.size = 0; + + success = _send_receive_msg(&payload, // FTP payload header + 0, // size in bytes of data + nullptr, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("Didn't get Nak back", reply->opcode, MavlinkFTP::kRspNak); + ut_compare("Incorrect payload size", reply->size, 1); + ut_compare("Incorrect error code", reply->data[0], MavlinkFTP::kErrInvalidSession); + + return true; +} + +/// @brief Tests for correct reponse to a Read command on an open session. +bool MavlinkFtpTest::_read_test(void) +{ + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + + for (size_t i=0; i<sizeof(_rgReadTestCases)/sizeof(_rgReadTestCases[0]); i++) { + struct stat st; + const ReadTestCase *test = &_rgReadTestCases[i]; + + // Read in the file so we can compare it to what we get back + ut_compare("stat failed", stat(test->file, &st), 0); + uint8_t *bytes = new uint8_t[st.st_size]; + ut_assert("new failed", bytes != nullptr); + int fd = ::open(test->file, O_RDONLY); + ut_assert("open failed", fd != -1); + int bytes_read = ::read(fd, bytes, st.st_size); + ut_compare("read failed", bytes_read, st.st_size); + ::close(fd); + + // Test case data files are created for specific boundary conditions + ut_compare("Test case data files are out of date", test->length, st.st_size); + + payload.opcode = MavlinkFTP::kCmdOpenFile; + payload.offset = 0; + + bool success = _send_receive_msg(&payload, // FTP payload header + strlen(test->file)+1, // size in bytes of data + (uint8_t*)test->file, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("Didn't get Ack back", reply->opcode, MavlinkFTP::kRspAck); + + payload.opcode = MavlinkFTP::kCmdReadFile; + payload.session = reply->session; + payload.offset = 0; + + success = _send_receive_msg(&payload, // FTP payload header + 0, // size in bytes of data + nullptr, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("Didn't get Ack back", reply->opcode, MavlinkFTP::kRspAck); + ut_compare("Offset incorrect", reply->offset, 0); + + if (test->length <= MAVLINK_MSG_FILE_TRANSFER_PROTOCOL_FIELD_PAYLOAD_LEN - sizeof(MavlinkFTP::PayloadHeader)) { + ut_compare("Payload size incorrect", reply->size, (uint32_t)st.st_size); + ut_compare("File contents differ", memcmp(reply->data, bytes, st.st_size), 0); + } + + payload.opcode = MavlinkFTP::kCmdTerminateSession; + payload.session = reply->session; + payload.size = 0; + + success = _send_receive_msg(&payload, // FTP payload header + 0, // size in bytes of data + nullptr, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("Didn't get Ack back", reply->opcode, MavlinkFTP::kRspAck); + ut_compare("Incorrect payload size", reply->size, 0); + } + + return true; +} + +/// @brief Tests for correct reponse to a Read command on an invalid session. +bool MavlinkFtpTest::_read_badsession_test(void) +{ + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + const char *file = _rgReadTestCases[0].file; + + payload.opcode = MavlinkFTP::kCmdOpenFile; + payload.offset = 0; + + bool success = _send_receive_msg(&payload, // FTP payload header + strlen(file)+1, // size in bytes of data + (uint8_t*)file, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("Didn't get Ack back", reply->opcode, MavlinkFTP::kRspAck); + + payload.opcode = MavlinkFTP::kCmdReadFile; + payload.session = reply->session + 1; // Invalid session + payload.offset = 0; + + success = _send_receive_msg(&payload, // FTP payload header + 0, // size in bytes of data + nullptr, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + ut_compare("Didn't get Nak back", reply->opcode, MavlinkFTP::kRspNak); + ut_compare("Incorrect payload size", reply->size, 1); + ut_compare("Incorrect error code", reply->data[0], MavlinkFTP::kErrInvalidSession); + + return true; +} + +bool MavlinkFtpTest::_removedirectory_test(void) +{ + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + int fd; + + struct _testCase { + const char *dir; + bool success; + bool deleteFile; + }; + static const struct _testCase rgTestCases[] = { + { "/bogus", false, false }, + { "/etc/unit_test_data/mavlink_tests/empty_dir", false, false }, + { _unittest_microsd_dir, false, false }, + { _unittest_microsd_file, false, false }, + { _unittest_microsd_dir, true, true }, + }; + + ut_compare("mkdir failed", ::mkdir(_unittest_microsd_dir, S_IRWXU | S_IRWXG | S_IRWXO), 0); + ut_assert("open failed", (fd = ::open(_unittest_microsd_file, O_CREAT | O_EXCL)) != -1); + ::close(fd); + + for (size_t i=0; i<sizeof(rgTestCases)/sizeof(rgTestCases[0]); i++) { + const struct _testCase *test = &rgTestCases[i]; + + if (test->deleteFile) { + ut_compare("unlink failed", ::unlink(_unittest_microsd_file), 0); + } + + payload.opcode = MavlinkFTP::kCmdRemoveDirectory; + payload.offset = 0; + + bool success = _send_receive_msg(&payload, // FTP payload header + strlen(test->dir)+1, // size in bytes of data + (uint8_t*)test->dir, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + if (test->success) { + ut_compare("Didn't get Ack back", reply->opcode, MavlinkFTP::kRspAck); + ut_compare("Incorrect payload size", reply->size, 0); + } else { + ut_compare("Didn't get Nak back", reply->opcode, MavlinkFTP::kRspNak); + ut_compare("Incorrect payload size", reply->size, 2); + ut_compare("Incorrect error code", reply->data[0], MavlinkFTP::kErrFailErrno); + } + } + + return true; +} + +bool MavlinkFtpTest::_createdirectory_test(void) +{ + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + + struct _testCase { + const char *dir; + bool success; + }; + static const struct _testCase rgTestCases[] = { + { "/etc/bogus", false }, + { _unittest_microsd_dir, true }, + { _unittest_microsd_dir, false }, + { "/fs/microsd/bogus/bogus", false }, + }; + + for (size_t i=0; i<sizeof(rgTestCases)/sizeof(rgTestCases[0]); i++) { + const struct _testCase *test = &rgTestCases[i]; + + payload.opcode = MavlinkFTP::kCmdCreateDirectory; + payload.offset = 0; + + bool success = _send_receive_msg(&payload, // FTP payload header + strlen(test->dir)+1, // size in bytes of data + (uint8_t*)test->dir, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + if (test->success) { + ut_compare("Didn't get Ack back", reply->opcode, MavlinkFTP::kRspAck); + ut_compare("Incorrect payload size", reply->size, 0); + } else { + ut_compare("Didn't get Nak back", reply->opcode, MavlinkFTP::kRspNak); + ut_compare("Incorrect payload size", reply->size, 2); + ut_compare("Incorrect error code", reply->data[0], MavlinkFTP::kErrFailErrno); + } + } + + return true; +} + +bool MavlinkFtpTest::_removefile_test(void) +{ + MavlinkFTP::PayloadHeader payload; + mavlink_file_transfer_protocol_t ftp_msg; + MavlinkFTP::PayloadHeader *reply; + int fd; + + struct _testCase { + const char *file; + bool success; + }; + static const struct _testCase rgTestCases[] = { + { "/bogus", false }, + { _rgReadTestCases[0].file, false }, + { _unittest_microsd_dir, false }, + { _unittest_microsd_file, true }, + { _unittest_microsd_file, false }, + }; + + ut_compare("mkdir failed", ::mkdir(_unittest_microsd_dir, S_IRWXU | S_IRWXG | S_IRWXO), 0); + ut_assert("open failed", (fd = ::open(_unittest_microsd_file, O_CREAT | O_EXCL)) != -1); + ::close(fd); + + for (size_t i=0; i<sizeof(rgTestCases)/sizeof(rgTestCases[0]); i++) { + const struct _testCase *test = &rgTestCases[i]; + + payload.opcode = MavlinkFTP::kCmdRemoveFile; + payload.offset = 0; + + bool success = _send_receive_msg(&payload, // FTP payload header + strlen(test->file)+1, // size in bytes of data + (uint8_t*)test->file, // Data to start into FTP message payload + &ftp_msg, // Response from server + &reply); // Payload inside FTP message response + if (!success) { + return false; + } + + if (test->success) { + ut_compare("Didn't get Ack back", reply->opcode, MavlinkFTP::kRspAck); + ut_compare("Incorrect payload size", reply->size, 0); + } else { + ut_compare("Didn't get Nak back", reply->opcode, MavlinkFTP::kRspNak); + ut_compare("Incorrect payload size", reply->size, 2); + ut_compare("Incorrect error code", reply->data[0], MavlinkFTP::kErrFailErrno); + } + } + + return true; +} + +/// @brief Static method used as callback from MavlinkFTP. This method will be called by MavlinkFTP when +/// it needs to send a message out on Mavlink. +void MavlinkFtpTest::receive_message(const mavlink_message_t *msg, MavlinkFtpTest *ftp_test) +{ + ftp_test->_receive_message(msg); +} + +/// @brief Non-Static version of receive_message +void MavlinkFtpTest::_receive_message(const mavlink_message_t *msg) +{ + // Move the message into our own member variable + memcpy(&_reply_msg, msg, sizeof(mavlink_message_t)); +} + +/// @brief Decode and validate the incoming message +bool MavlinkFtpTest::_decode_message(const mavlink_message_t *msg, ///< Mavlink message to decode + mavlink_file_transfer_protocol_t *ftp_msg, ///< Decoded FTP message + MavlinkFTP::PayloadHeader **payload) ///< Payload inside FTP message response +{ + mavlink_msg_file_transfer_protocol_decode(msg, ftp_msg); + + // Make sure the targets are correct + ut_compare("Target network non-zero", ftp_msg->target_network, 0); + ut_compare("Target system id mismatch", ftp_msg->target_system, clientSystemId); + ut_compare("Target component id mismatch", ftp_msg->target_component, clientComponentId); + + *payload = reinterpret_cast<MavlinkFTP::PayloadHeader *>(ftp_msg->payload); + + // Make sure we have a good sequence number + ut_compare("Sequence number mismatch", (*payload)->seqNumber, _lastOutgoingSeqNumber + 1); + + // Bump sequence number for next outgoing message + _lastOutgoingSeqNumber++; + + return true; +} + +/// @brief Initializes an FTP message into a mavlink message +void MavlinkFtpTest::_setup_ftp_msg(MavlinkFTP::PayloadHeader *payload_header, ///< FTP payload header + uint8_t size, ///< size in bytes of data + const uint8_t *data, ///< Data to start into FTP message payload + mavlink_message_t *msg) ///< Returned mavlink message +{ + uint8_t payload_bytes[MAVLINK_MSG_FILE_TRANSFER_PROTOCOL_FIELD_PAYLOAD_LEN]; + MavlinkFTP::PayloadHeader *payload = reinterpret_cast<MavlinkFTP::PayloadHeader *>(payload_bytes); + + memcpy(payload, payload_header, sizeof(MavlinkFTP::PayloadHeader)); + + payload->seqNumber = _lastOutgoingSeqNumber; + payload->size = size; + if (size != 0) { + memcpy(payload->data, data, size); + } + + payload->padding[0] = 0; + payload->padding[1] = 0; + + msg->checksum = 0; + mavlink_msg_file_transfer_protocol_pack(clientSystemId, // Sender system id + clientComponentId, // Sender component id + msg, // Message to pack payload into + 0, // Target network + serverSystemId, // Target system id + serverComponentId, // Target component id + payload_bytes); // Payload to pack into message +} + +/// @brief Sends the specified FTP message to the server and returns response +bool MavlinkFtpTest::_send_receive_msg(MavlinkFTP::PayloadHeader *payload_header, ///< FTP payload header + uint8_t size, ///< size in bytes of data + const uint8_t *data, ///< Data to start into FTP message payload + mavlink_file_transfer_protocol_t *ftp_msg_reply, ///< Response from server + MavlinkFTP::PayloadHeader **payload_reply) ///< Payload inside FTP message response +{ + mavlink_message_t msg; + + _setup_ftp_msg(payload_header, size, data, &msg); + _ftp_server->handle_message(nullptr /* mavlink */, &msg); + return _decode_message(&_reply_msg, ftp_msg_reply, payload_reply); +} + +/// @brief Cleans up an files created on microsd during testing +void MavlinkFtpTest::_cleanup_microsd(void) +{ + ::unlink(_unittest_microsd_file); + ::rmdir(_unittest_microsd_dir); +} + +/// @brief Runs all the unit tests +void MavlinkFtpTest::runTests(void) +{ + ut_run_test(_ack_test); + ut_run_test(_bad_opcode_test); + ut_run_test(_bad_datasize_test); + ut_run_test(_list_test); + ut_run_test(_list_eof_test); + ut_run_test(_open_badfile_test); + ut_run_test(_open_terminate_test); + ut_run_test(_terminate_badsession_test); + ut_run_test(_read_test); + ut_run_test(_read_badsession_test); + ut_run_test(_removedirectory_test); + ut_run_test(_createdirectory_test); + ut_run_test(_removefile_test); +} + diff --git a/src/modules/mavlink/mavlink_tests/mavlink_ftp_test.h b/src/modules/mavlink/mavlink_tests/mavlink_ftp_test.h new file mode 100644 index 000000000..babd909da --- /dev/null +++ b/src/modules/mavlink/mavlink_tests/mavlink_ftp_test.h @@ -0,0 +1,107 @@ +/**************************************************************************** + * + * 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 mavlink_ftp_test.h +/// @author Don Gagne <don@thegagnes.com> + +#pragma once + +#include <unit_test/unit_test.h> +#include "../mavlink_bridge_header.h" +#include "../mavlink_ftp.h" + +class MavlinkFtpTest : public UnitTest +{ +public: + MavlinkFtpTest(); + virtual ~MavlinkFtpTest(); + + virtual void init(void); + virtual void cleanup(void); + + virtual void runTests(void); + + static void receive_message(const mavlink_message_t *msg, MavlinkFtpTest* ftpTest); + + static const uint8_t serverSystemId = 50; ///< System ID for server + static const uint8_t serverComponentId = 1; ///< Component ID for server + static const uint8_t serverChannel = 0; ///< Channel to send to + + static const uint8_t clientSystemId = 1; ///< System ID for client + static const uint8_t clientComponentId = 0; ///< Component ID for client + + // We don't want any of these + MavlinkFtpTest(const MavlinkFtpTest&); + MavlinkFtpTest& operator=(const MavlinkFtpTest&); + +private: + bool _ack_test(void); + bool _bad_opcode_test(void); + bool _bad_datasize_test(void); + bool _list_test(void); + bool _list_eof_test(void); + bool _open_badfile_test(void); + bool _open_terminate_test(void); + bool _terminate_badsession_test(void); + bool _read_test(void); + bool _read_badsession_test(void); + bool _removedirectory_test(void); + bool _createdirectory_test(void); + bool _removefile_test(void); + + void _receive_message(const mavlink_message_t *msg); + void _setup_ftp_msg(MavlinkFTP::PayloadHeader *payload_header, uint8_t size, const uint8_t *data, mavlink_message_t *msg); + bool _decode_message(const mavlink_message_t *msg, mavlink_file_transfer_protocol_t *ftp_msg, MavlinkFTP::PayloadHeader **payload); + bool _send_receive_msg(MavlinkFTP::PayloadHeader *payload_header, + uint8_t size, + const uint8_t *data, + mavlink_file_transfer_protocol_t *ftp_msg_reply, + MavlinkFTP::PayloadHeader **payload_reply); + void _cleanup_microsd(void); + + MavlinkFTP *_ftp_server; + + mavlink_message_t _reply_msg; + + uint16_t _lastOutgoingSeqNumber; + + struct ReadTestCase { + const char *file; + const uint16_t length; + }; + static const ReadTestCase _rgReadTestCases[]; + + static const char _unittest_microsd_dir[]; + static const char _unittest_microsd_file[]; +}; + diff --git a/src/modules/mavlink/mavlink_tests/mavlink_ftp_test_data.py b/src/modules/mavlink/mavlink_tests/mavlink_ftp_test_data.py new file mode 100644 index 000000000..a7e68f2a3 --- /dev/null +++ b/src/modules/mavlink/mavlink_tests/mavlink_ftp_test_data.py @@ -0,0 +1,7 @@ +import sys +print 'Arguments: file - ' + sys.argv[1] + ', length - ' + sys.argv[2] +file = open(sys.argv[1], 'w') +for i in range(int(sys.argv[2])): + b = bytearray([i & 0xFF]) + file.write(b) +file.close()
\ No newline at end of file diff --git a/src/modules/mavlink/mavlink_tests/mavlink_tests.cpp b/src/modules/mavlink/mavlink_tests/mavlink_tests.cpp new file mode 100644 index 000000000..d9c1e413a --- /dev/null +++ b/src/modules/mavlink/mavlink_tests/mavlink_tests.cpp @@ -0,0 +1,52 @@ +/**************************************************************************** + * + * 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 mavlink_ftp_tests.cpp + */ + +#include <systemlib/err.h> + +#include "mavlink_ftp_test.h" + +extern "C" __EXPORT int mavlink_tests_main(int argc, char *argv[]); + +int mavlink_tests_main(int argc, char *argv[]) +{ + MavlinkFtpTest* test = new MavlinkFtpTest; + + test->runTests(); + test->printResults(); + + return 0; +} diff --git a/src/modules/mavlink/mavlink_tests/module.mk b/src/modules/mavlink/mavlink_tests/module.mk new file mode 100644 index 000000000..07cfce1dc --- /dev/null +++ b/src/modules/mavlink/mavlink_tests/module.mk @@ -0,0 +1,48 @@ +############################################################################ +# +# 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. +# +############################################################################ + +# +# System state machine tests. +# + +MODULE_COMMAND = mavlink_tests +SRCS = mavlink_tests.cpp \ + mavlink_ftp_test.cpp \ + ../mavlink_ftp.cpp \ + ../mavlink.c + +INCLUDE_DIRS += $(MAVLINK_SRC)/include/mavlink + +MODULE_STACKSIZE = 5000 + +EXTRACXXFLAGS = -Weffc++ -DMAVLINK_FTP_UNIT_TEST diff --git a/src/modules/navigator/geofence.cpp b/src/modules/navigator/geofence.cpp index 266215308..49aec21e0 100644 --- a/src/modules/navigator/geofence.cpp +++ b/src/modules/navigator/geofence.cpp @@ -76,11 +76,7 @@ Geofence::~Geofence() bool Geofence::inside(const struct vehicle_global_position_s *vehicle) { - double lat = vehicle->lat / 1e7d; - double lon = vehicle->lon / 1e7d; - //float alt = vehicle->alt; - - return inside(lat, lon, vehicle->alt); + return inside(vehicle->lat, vehicle->lon, vehicle->alt); } bool Geofence::inside(double lat, double lon, float altitude) diff --git a/src/modules/navigator/mission.cpp b/src/modules/navigator/mission.cpp index 719301a0a..104065132 100644 --- a/src/modules/navigator/mission.cpp +++ b/src/modules/navigator/mission.cpp @@ -36,12 +36,14 @@ * Helper class to access missions * * @author Julian Oes <julian@oes.ch> + * @author Thomas Gubler <thomasgubler@gmail.com> */ #include <sys/types.h> #include <string.h> #include <stdlib.h> #include <unistd.h> +#include <float.h> #include <drivers/drv_hrt.h> @@ -49,6 +51,7 @@ #include <mavlink/mavlink_log.h> #include <systemlib/err.h> #include <geo/geo.h> +#include <lib/mathlib/mathlib.h> #include <uORB/uORB.h> #include <uORB/topics/mission.h> @@ -62,6 +65,7 @@ Mission::Mission(Navigator *navigator, const char *name) : _param_onboard_enabled(this, "ONBOARD_EN"), _param_takeoff_alt(this, "TAKEOFF_ALT"), _param_dist_1wp(this, "DIST_1WP"), + _param_altmode(this, "ALTMODE"), _onboard_mission({0}), _offboard_mission({0}), _current_onboard_mission_index(-1), @@ -72,7 +76,11 @@ Mission::Mission(Navigator *navigator, const char *name) : _mission_result({0}), _mission_type(MISSION_TYPE_NONE), _inited(false), - _dist_1wp_ok(false) + _dist_1wp_ok(false), + _missionFeasiblityChecker(), + _min_current_sp_distance_xy(FLT_MAX), + _mission_item_previous_alt(NAN), + _distance_current_previous(0.0f) { /* load initial params */ updateParams(); @@ -145,6 +153,8 @@ Mission::on_active() advance_mission(); set_mission_items(); + } else if (_mission_type != MISSION_TYPE_NONE &&_param_altmode.get() == MISSION_ALTMODE_FOH) { + altitude_sp_foh_update(); } else { /* if waypoint position reached allow loiter on the setpoint */ if (_waypoint_position_reached && _mission_item.nav_cmd != NAV_CMD_IDLE) { @@ -203,7 +213,7 @@ Mission::update_offboard_mission() * however warnings are issued to the gcs via mavlink from inside the MissionFeasiblityChecker */ dm_item_t dm_current = DM_KEY_WAYPOINTS_OFFBOARD(_offboard_mission.dataman_id); - missionFeasiblityChecker.checkMissionFeasible(_navigator->get_vstatus()->is_rotary_wing, + _missionFeasiblityChecker.checkMissionFeasible(_navigator->get_vstatus()->is_rotary_wing, dm_current, (size_t) _offboard_mission.count, _navigator->get_geofence(), _navigator->get_home_position()->alt); @@ -314,11 +324,19 @@ Mission::set_mission_items() /* make sure param is up to date */ updateParams(); + /* reset the altitude foh logic, if altitude foh is enabled (param) a new foh element starts now */ + altitude_sp_foh_reset(); + struct position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet(); /* set previous position setpoint to current */ set_previous_pos_setpoint(); + /* Copy previous mission item altitude (can be extended to a copy of the full mission item if needed) */ + if (pos_sp_triplet->previous.valid) { + _mission_item_previous_alt = _mission_item.altitude; + } + /* get home distance state */ bool home_dist_ok = check_dist_1wp(); /* the home dist check provides user feedback, so we initialize it to this */ @@ -470,9 +488,75 @@ Mission::set_mission_items() pos_sp_triplet->next.valid = false; } + /* Save the distance between the current sp and the previous one */ + if (pos_sp_triplet->current.valid && pos_sp_triplet->previous.valid) { + _distance_current_previous = get_distance_to_next_waypoint(pos_sp_triplet->current.lat, + pos_sp_triplet->current.lon, + pos_sp_triplet->previous.lat, + pos_sp_triplet->previous.lon); + } + + _navigator->set_position_setpoint_triplet_updated(); +} + +void +Mission::altitude_sp_foh_update() +{ + struct position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet(); + + /* Don't change setpoint if last and current waypoint are not valid */ + if (!pos_sp_triplet->previous.valid || !pos_sp_triplet->current.valid || + !isfinite(_mission_item_previous_alt)) { + return; + } + + /* Do not try to find a solution if the last waypoint is inside the acceptance radius of the current one */ + if (_distance_current_previous - _mission_item.acceptance_radius < 0.0f) { + return; + } + + /* Don't do FOH for landing and takeoff waypoints, the ground may be near + * and the FW controller has a custom landing logic */ + if (_mission_item.nav_cmd == NAV_CMD_LAND || _mission_item.nav_cmd == NAV_CMD_TAKEOFF) { + return; + } + + + /* Calculate distance to current waypoint */ + float d_current = get_distance_to_next_waypoint(_mission_item.lat, _mission_item.lon, + _navigator->get_global_position()->lat, _navigator->get_global_position()->lon); + + /* Save distance to waypoint if it is the smallest ever achieved, however make sure that + * _min_current_sp_distance_xy is never larger than the distance between the current and the previous wp */ + _min_current_sp_distance_xy = math::min(math::min(d_current, _min_current_sp_distance_xy), + _distance_current_previous); + + /* if the minimal distance is smaller then the acceptance radius, we should be at waypoint alt + * navigator will soon switch to the next waypoint item (if there is one) as soon as we reach this altitude */ + if (_min_current_sp_distance_xy < _mission_item.acceptance_radius) { + pos_sp_triplet->current.alt = _mission_item.altitude; + } else { + /* update the altitude sp of the 'current' item in the sp triplet, but do not update the altitude sp + * of the mission item as it is used to check if the mission item is reached + * The setpoint is set linearly and such that the system reaches the current altitude at the acceptance + * radius around the current waypoint + **/ + float delta_alt = (_mission_item.altitude - _mission_item_previous_alt); + float grad = -delta_alt/(_distance_current_previous - _mission_item.acceptance_radius); + float a = _mission_item_previous_alt - grad * _distance_current_previous; + pos_sp_triplet->current.alt = a + grad * _min_current_sp_distance_xy; + + } + _navigator->set_position_setpoint_triplet_updated(); } +void +Mission::altitude_sp_foh_reset() +{ + _min_current_sp_distance_xy = FLT_MAX; +} + bool Mission::read_mission_item(bool onboard, bool is_current, struct mission_item_s *mission_item) { diff --git a/src/modules/navigator/mission.h b/src/modules/navigator/mission.h index 1edaa5c8a..4737be391 100644 --- a/src/modules/navigator/mission.h +++ b/src/modules/navigator/mission.h @@ -36,6 +36,7 @@ * Navigator mode to access missions * * @author Julian Oes <julian@oes.ch> + * @author Thomas Gubler <thomasgubler@gmail.com> */ #ifndef NAVIGATOR_MISSION_H @@ -75,6 +76,11 @@ public: virtual void on_active(); + enum mission_altitude_mode { + MISSION_ALTMODE_ZOH = 0, + MISSION_ALTMODE_FOH = 1 + }; + private: /** * Update onboard mission topic @@ -103,6 +109,16 @@ private: void set_mission_items(); /** + * Updates the altitude sp to follow a foh + */ + void altitude_sp_foh_update(); + + /** + * Resets the altitude sp foh logic + */ + void altitude_sp_foh_reset(); + + /** * Read current or next mission item from the dataman and watch out for DO_JUMPS * @return true if successful */ @@ -136,6 +152,7 @@ private: control::BlockParamInt _param_onboard_enabled; control::BlockParamFloat _param_takeoff_alt; control::BlockParamFloat _param_dist_1wp; + control::BlockParamInt _param_altmode; struct mission_s _onboard_mission; struct mission_s _offboard_mission; @@ -157,7 +174,13 @@ private: bool _inited; bool _dist_1wp_ok; - MissionFeasibilityChecker missionFeasiblityChecker; /**< class that checks if a mission is feasible */ + MissionFeasibilityChecker _missionFeasiblityChecker; /**< class that checks if a mission is feasible */ + + float _min_current_sp_distance_xy; /**< minimum distance which was achieved to the current waypoint */ + float _mission_item_previous_alt; /**< holds the altitude of the previous mission item, + can be replaced by a full copy of the previous mission item if needed*/ + float _distance_current_previous; /**< distance from previous to current sp in pos_sp_triplet, + only use if current and previous are valid */ }; #endif diff --git a/src/modules/navigator/mission_block.cpp b/src/modules/navigator/mission_block.cpp index 4adf77dce..723caec7c 100644 --- a/src/modules/navigator/mission_block.cpp +++ b/src/modules/navigator/mission_block.cpp @@ -113,6 +113,19 @@ MissionBlock::is_mission_item_reached() if (dist >= 0.0f && dist <= _navigator->get_acceptance_radius()) { _waypoint_position_reached = true; } + } else if (!_navigator->get_vstatus()->is_rotary_wing && + (_mission_item.nav_cmd == NAV_CMD_LOITER_UNLIMITED || + _mission_item.nav_cmd == NAV_CMD_LOITER_TIME_LIMIT || + _mission_item.nav_cmd == NAV_CMD_LOITER_TURN_COUNT)) { + /* Loiter mission item on a non rotary wing: the aircraft is going to circle the + * coordinates with a radius equal to the loiter_radius field. It is not flying + * through the waypoint center. + * Therefore the item is marked as reached once the system reaches the loiter + * radius (+ some margin). Time inside and turn count is handled elsewhere. + */ + if (dist >= 0.0f && dist <= _mission_item.loiter_radius * 1.2f) { + _waypoint_position_reached = true; + } } else { /* for normal mission items used their acceptance radius */ if (dist >= 0.0f && dist <= _mission_item.acceptance_radius) { diff --git a/src/modules/navigator/mission_feasibility_checker.cpp b/src/modules/navigator/mission_feasibility_checker.cpp index 606521f20..7ae7f60cb 100644 --- a/src/modules/navigator/mission_feasibility_checker.cpp +++ b/src/modules/navigator/mission_feasibility_checker.cpp @@ -84,7 +84,12 @@ bool MissionFeasibilityChecker::checkMissionFeasible(bool isRotarywing, dm_item_ bool MissionFeasibilityChecker::checkMissionFeasibleRotarywing(dm_item_t dm_current, size_t nMissionItems, Geofence &geofence, float home_alt) { - return (checkGeofence(dm_current, nMissionItems, geofence) && checkHomePositionAltitude(dm_current, nMissionItems, home_alt)); + /* Perform checks and issue feedback to the user for all checks */ + bool resGeofence = checkGeofence(dm_current, nMissionItems, geofence); + bool resHomeAltitude = checkHomePositionAltitude(dm_current, nMissionItems, home_alt); + + /* Mission is only marked as feasible if all checks return true */ + return (resGeofence && resHomeAltitude); } bool MissionFeasibilityChecker::checkMissionFeasibleFixedwing(dm_item_t dm_current, size_t nMissionItems, Geofence &geofence, float home_alt) @@ -93,7 +98,13 @@ bool MissionFeasibilityChecker::checkMissionFeasibleFixedwing(dm_item_t dm_curre updateNavigationCapabilities(); // warnx("_nav_caps.landing_slope_angle_rad %.4f, _nav_caps.landing_horizontal_slope_displacement %.4f", _nav_caps.landing_slope_angle_rad, _nav_caps.landing_horizontal_slope_displacement); - return (checkFixedWingLanding(dm_current, nMissionItems) && checkGeofence(dm_current, nMissionItems, geofence) && checkHomePositionAltitude(dm_current, nMissionItems, home_alt)); + /* Perform checks and issue feedback to the user for all checks */ + bool resLanding = checkFixedWingLanding(dm_current, nMissionItems); + bool resGeofence = checkGeofence(dm_current, nMissionItems, geofence); + bool resHomeAltitude = checkHomePositionAltitude(dm_current, nMissionItems, home_alt); + + /* Mission is only marked as feasible if all checks return true */ + return (resLanding && resGeofence && resHomeAltitude); } bool MissionFeasibilityChecker::checkGeofence(dm_item_t dm_current, size_t nMissionItems, Geofence &geofence) @@ -216,9 +227,8 @@ bool MissionFeasibilityChecker::checkFixedWingLanding(dm_item_t dm_current, size } } - -// float slope_alt = wp_altitude + _H0 * expf(-math::max(0.0f, _flare_length - wp_distance)/_flare_constant) - _H1_virt; - return false; + /* No landing waypoints or no waypoints */ + return true; } void MissionFeasibilityChecker::updateNavigationCapabilities() diff --git a/src/modules/navigator/mission_params.c b/src/modules/navigator/mission_params.c index d15e1e771..04c01fe51 100644 --- a/src/modules/navigator/mission_params.c +++ b/src/modules/navigator/mission_params.c @@ -82,3 +82,16 @@ PARAM_DEFINE_INT32(MIS_ONBOARD_EN, 1); * @group Mission */ PARAM_DEFINE_FLOAT(MIS_DIST_1WP, 500); + +/** + * Altitude setpoint mode + * + * 0: the system will follow a zero order hold altitude setpoint + * 1: the system will follow a first order hold altitude setpoint + * values follow the definition in enum mission_altitude_mode + * + * @min 0 + * @max 1 + * @group Mission + */ +PARAM_DEFINE_INT32(MIS_ALTMODE, 0); diff --git a/src/modules/navigator/navigator_main.cpp b/src/modules/navigator/navigator_main.cpp index 331a9a728..042c46afd 100644 --- a/src/modules/navigator/navigator_main.cpp +++ b/src/modules/navigator/navigator_main.cpp @@ -353,6 +353,8 @@ Navigator::task_main() case NAVIGATION_STATE_ACRO: case NAVIGATION_STATE_ALTCTL: case NAVIGATION_STATE_POSCTL: + case NAVIGATION_STATE_LAND: + case NAVIGATION_STATE_TERMINATION: _navigation_mode = nullptr; _can_loiter_at_sp = false; break; @@ -368,8 +370,6 @@ Navigator::task_main() case NAVIGATION_STATE_AUTO_RTGS: _navigation_mode = &_rtl; /* TODO: change this to something else */ break; - case NAVIGATION_STATE_LAND: - case NAVIGATION_STATE_TERMINATION: case NAVIGATION_STATE_OFFBOARD: _navigation_mode = &_offboard; break; diff --git a/src/modules/px4iofirmware/mixer.cpp b/src/modules/px4iofirmware/mixer.cpp index 606c639f9..3e19333d8 100644 --- a/src/modules/px4iofirmware/mixer.cpp +++ b/src/modules/px4iofirmware/mixer.cpp @@ -58,7 +58,7 @@ extern "C" { /* * Maximum interval in us before FMU signal is considered lost */ -#define FMU_INPUT_DROP_LIMIT_US 200000 +#define FMU_INPUT_DROP_LIMIT_US 500000 /* XXX need to move the RC_CHANNEL_FUNCTION out of rc_channels.h and into systemlib */ #define ROLL 0 @@ -98,7 +98,8 @@ mixer_tick(void) { /* check that we are receiving fresh data from the FMU */ - if (hrt_elapsed_time(&system_state.fmu_data_received_time) > FMU_INPUT_DROP_LIMIT_US) { + if ((system_state.fmu_data_received_time == 0) || + hrt_elapsed_time(&system_state.fmu_data_received_time) > FMU_INPUT_DROP_LIMIT_US) { /* too long without FMU input, time to go to failsafe */ if (r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) { @@ -109,6 +110,9 @@ mixer_tick(void) } else { r_status_flags |= PX4IO_P_STATUS_FLAGS_FMU_OK; + + /* this flag is never cleared once OK */ + r_status_flags |= PX4IO_P_STATUS_FLAGS_FMU_INITIALIZED; } /* default to failsafe mixing - it will be forced below if flag is set */ @@ -139,7 +143,9 @@ mixer_tick(void) (r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK) && (r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK) && !(r_setup_arming & PX4IO_P_SETUP_ARMING_RC_HANDLING_DISABLED) && - !(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK)) { + !(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) && + /* do not enter manual override if we asked for termination failsafe and FMU is lost */ + !(r_setup_arming & PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE)) { /* if allowed, mix from RC inputs directly */ source = MIX_OVERRIDE; @@ -155,29 +161,11 @@ mixer_tick(void) } /* - * Check if we should force failsafe - and do it if we have to - */ - if (r_setup_arming & PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE) { - source = MIX_FAILSAFE; - } - - /* - * Set failsafe status flag depending on mixing source - */ - if (source == MIX_FAILSAFE) { - r_status_flags |= PX4IO_P_STATUS_FLAGS_FAILSAFE; - } else { - r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_FAILSAFE); - } - - /* * Decide whether the servos should be armed right now. * * We must be armed, and we must have a PWM source; either raw from * FMU or from the mixer. * - * XXX correct behaviour for failsafe may require an additional case - * here. */ should_arm = ( /* IO initialised without error */ (r_status_flags & PX4IO_P_STATUS_FLAGS_INIT_OK) @@ -195,6 +183,38 @@ mixer_tick(void) && (r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK); /* + * Check if failsafe termination is set - if yes, + * set the force failsafe flag once entering the first + * failsafe condition. + */ + if ( /* if we have requested flight termination style failsafe (noreturn) */ + (r_setup_arming & PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE) && + /* and we ended up in a failsafe condition */ + (source == MIX_FAILSAFE) && + /* and we should be armed, so we intended to provide outputs */ + should_arm && + /* and FMU is initialized */ + (r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_INITIALIZED)) { + r_setup_arming |= PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE; + } + + /* + * Check if we should force failsafe - and do it if we have to + */ + if (r_setup_arming & PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE) { + source = MIX_FAILSAFE; + } + + /* + * Set failsafe status flag depending on mixing source + */ + if (source == MIX_FAILSAFE) { + r_status_flags |= PX4IO_P_STATUS_FLAGS_FAILSAFE; + } else { + r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_FAILSAFE); + } + + /* * Run the mixers. */ if (source == MIX_FAILSAFE) { diff --git a/src/modules/px4iofirmware/protocol.h b/src/modules/px4iofirmware/protocol.h index 050783687..4739f6e40 100644 --- a/src/modules/px4iofirmware/protocol.h +++ b/src/modules/px4iofirmware/protocol.h @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2012, 2013 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 @@ -111,6 +111,7 @@ #define PX4IO_P_STATUS_FLAGS_INIT_OK (1 << 10) /* initialisation of the IO completed without error */ #define PX4IO_P_STATUS_FLAGS_FAILSAFE (1 << 11) /* failsafe is active */ #define PX4IO_P_STATUS_FLAGS_SAFETY_OFF (1 << 12) /* safety is off */ +#define PX4IO_P_STATUS_FLAGS_FMU_INITIALIZED (1 << 13) /* FMU was initialized and OK once */ #define PX4IO_P_STATUS_ALARMS 3 /* alarm flags - alarms latch, write 1 to a bit to clear it */ #define PX4IO_P_STATUS_ALARMS_VBATT_LOW (1 << 0) /* [1] VBatt is very close to regulator dropout */ @@ -180,6 +181,7 @@ #define PX4IO_P_SETUP_ARMING_RC_HANDLING_DISABLED (1 << 6) /* Disable the IO-internal evaluation of the RC */ #define PX4IO_P_SETUP_ARMING_LOCKDOWN (1 << 7) /* If set, the system operates normally, but won't actuate any servos */ #define PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE (1 << 8) /* If set, the system will always output the failsafe values */ +#define PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE (1 << 9) /* If set, the system will never return from a failsafe, but remain in failsafe once triggered. */ #define PX4IO_P_SETUP_PWM_RATES 2 /* bitmask, 0 = low rate, 1 = high rate */ #define PX4IO_P_SETUP_PWM_DEFAULTRATE 3 /* 'low' PWM frame output rate in Hz */ diff --git a/src/modules/px4iofirmware/registers.c b/src/modules/px4iofirmware/registers.c index 43161aa70..7a5a5e484 100644 --- a/src/modules/px4iofirmware/registers.c +++ b/src/modules/px4iofirmware/registers.c @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (c) 2012, 2013 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 @@ -190,7 +190,8 @@ volatile uint16_t r_page_setup[] = PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE | \ PX4IO_P_SETUP_ARMING_RC_HANDLING_DISABLED | \ PX4IO_P_SETUP_ARMING_LOCKDOWN | \ - PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE) + PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE | \ + PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE) #define PX4IO_P_SETUP_RATES_VALID ((1 << PX4IO_SERVO_COUNT) - 1) #define PX4IO_P_SETUP_RELAYS_VALID ((1 << PX4IO_RELAY_CHANNELS) - 1) @@ -285,7 +286,9 @@ registers_set(uint8_t page, uint8_t offset, const uint16_t *values, unsigned num while ((offset < PX4IO_CONTROL_CHANNELS) && (num_values > 0)) { /* XXX range-check value? */ - r_page_servos[offset] = *values; + if (*values != PWM_IGNORE_THIS_CHANNEL) { + r_page_servos[offset] = *values; + } offset++; num_values--; @@ -516,6 +519,19 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value) r_status_flags |= PX4IO_P_STATUS_FLAGS_INIT_OK; } + /* + * If the failsafe termination flag is set, do not allow the autopilot to unset it + */ + value |= (r_setup_arming & PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE); + + /* + * If failsafe termination is enabled and force failsafe bit is set, do not allow + * the autopilot to clear it. + */ + if (r_setup_arming & PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE) { + value |= (r_setup_arming & PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE); + } + r_setup_arming = value; break; diff --git a/src/modules/sdlog2/sdlog2.c b/src/modules/sdlog2/sdlog2.c index 6c4b49452..e13593077 100644 --- a/src/modules/sdlog2/sdlog2.c +++ b/src/modules/sdlog2/sdlog2.c @@ -76,6 +76,7 @@ #include <uORB/topics/vehicle_gps_position.h> #include <uORB/topics/satellite_info.h> #include <uORB/topics/vehicle_vicon_position.h> +#include <uORB/topics/vision_position_estimate.h> #include <uORB/topics/vehicle_global_velocity_setpoint.h> #include <uORB/topics/optical_flow.h> #include <uORB/topics/battery_status.h> @@ -934,6 +935,7 @@ int sdlog2_thread_main(int argc, char *argv[]) struct vehicle_global_position_s global_pos; struct position_setpoint_triplet_s triplet; struct vehicle_vicon_position_s vicon_pos; + struct vision_position_estimate vision_pos; struct optical_flow_s flow; struct rc_channels_s rc; struct differential_pressure_s diff_pres; @@ -984,6 +986,7 @@ int sdlog2_thread_main(int argc, char *argv[]) struct log_EST1_s log_EST1; struct log_PWR_s log_PWR; struct log_VICN_s log_VICN; + struct log_VISN_s log_VISN; struct log_GS0A_s log_GS0A; struct log_GS0B_s log_GS0B; struct log_GS1A_s log_GS1A; @@ -1013,6 +1016,7 @@ int sdlog2_thread_main(int argc, char *argv[]) int gps_pos_sub; int sat_info_sub; int vicon_pos_sub; + int vision_pos_sub; int flow_sub; int rc_sub; int airspeed_sub; @@ -1043,6 +1047,7 @@ int sdlog2_thread_main(int argc, char *argv[]) subs.global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position)); subs.triplet_sub = orb_subscribe(ORB_ID(position_setpoint_triplet)); subs.vicon_pos_sub = orb_subscribe(ORB_ID(vehicle_vicon_position)); + subs.vision_pos_sub = orb_subscribe(ORB_ID(vision_position_estimate)); subs.flow_sub = orb_subscribe(ORB_ID(optical_flow)); subs.rc_sub = orb_subscribe(ORB_ID(rc_channels)); subs.airspeed_sub = orb_subscribe(ORB_ID(airspeed)); @@ -1427,6 +1432,11 @@ int sdlog2_thread_main(int argc, char *argv[]) log_msg.body.log_GPOS.vel_d = buf.global_pos.vel_d; log_msg.body.log_GPOS.eph = buf.global_pos.eph; log_msg.body.log_GPOS.epv = buf.global_pos.epv; + if (buf.global_pos.terrain_alt_valid) { + log_msg.body.log_GPOS.terrain_alt = buf.global_pos.terrain_alt; + } else { + log_msg.body.log_GPOS.terrain_alt = -1.0f; + } LOGBUFFER_WRITE_AND_COUNT(GPOS); } @@ -1460,6 +1470,22 @@ int sdlog2_thread_main(int argc, char *argv[]) LOGBUFFER_WRITE_AND_COUNT(VICN); } + /* --- VISION POSITION --- */ + if (copy_if_updated(ORB_ID(vision_position_estimate), subs.vision_pos_sub, &buf.vision_pos)) { + log_msg.msg_type = LOG_VISN_MSG; + log_msg.body.log_VISN.x = buf.vision_pos.x; + log_msg.body.log_VISN.y = buf.vision_pos.y; + log_msg.body.log_VISN.z = buf.vision_pos.z; + log_msg.body.log_VISN.vx = buf.vision_pos.vx; + log_msg.body.log_VISN.vy = buf.vision_pos.vy; + log_msg.body.log_VISN.vz = buf.vision_pos.vz; + log_msg.body.log_VISN.qx = buf.vision_pos.q[0]; + log_msg.body.log_VISN.qy = buf.vision_pos.q[1]; + log_msg.body.log_VISN.qz = buf.vision_pos.q[2]; + log_msg.body.log_VISN.qw = buf.vision_pos.q[3]; + LOGBUFFER_WRITE_AND_COUNT(VISN); + } + /* --- FLOW --- */ if (copy_if_updated(ORB_ID(optical_flow), subs.flow_sub, &buf.flow)) { log_msg.msg_type = LOG_FLOW_MSG; diff --git a/src/modules/sdlog2/sdlog2_messages.h b/src/modules/sdlog2/sdlog2_messages.h index fb7609435..d2845eb75 100644 --- a/src/modules/sdlog2/sdlog2_messages.h +++ b/src/modules/sdlog2/sdlog2_messages.h @@ -220,6 +220,7 @@ struct log_GPOS_s { float vel_d; float eph; float epv; + float terrain_alt; }; /* --- GPSP - GLOBAL POSITION SETPOINT --- */ @@ -391,6 +392,20 @@ struct log_TEL_s { uint64_t heartbeat_time; }; +/* --- VISN - VISION POSITION --- */ +#define LOG_VISN_MSG 38 +struct log_VISN_s { + float x; + float y; + float z; + float vx; + float vy; + float vz; + float qx; + float qy; + float qz; + float qw; +}; /********** SYSTEM MESSAGES, ID > 0x80 **********/ @@ -435,7 +450,7 @@ static const struct log_format_s log_formats[] = { 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(GPOS, "LLfffffff", "Lat,Lon,Alt,VelN,VelE,VelD,EPH,EPV,TALT"), 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"), @@ -449,6 +464,7 @@ static const struct log_format_s log_formats[] = { LOG_FORMAT(EST1, "ffffffffffffffff", "s12,s13,s14,s15,s16,s17,s18,s19,s20,s21,s22,s23,s24,s25,s26,s27"), LOG_FORMAT(PWR, "fffBBBBB", "Periph5V,Servo5V,RSSI,UsbOk,BrickOk,ServoOk,PeriphOC,HipwrOC"), LOG_FORMAT(VICN, "ffffff", "X,Y,Z,Roll,Pitch,Yaw"), + LOG_FORMAT(VISN, "ffffffffff", "X,Y,Z,VX,VY,VZ,QuatX,QuatY,QuatZ,QuatW"), LOG_FORMAT(GS0A, "BBBBBBBBBBBBBBBB", "s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,s10,s11,s12,s13,s14,s15"), LOG_FORMAT(GS0B, "BBBBBBBBBBBBBBBB", "s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,s10,s11,s12,s13,s14,s15"), LOG_FORMAT(GS1A, "BBBBBBBBBBBBBBBB", "s0,s1,s2,s3,s4,s5,s6,s7,s8,s9,s10,s11,s12,s13,s14,s15"), diff --git a/src/modules/sensors/sensor_params.c b/src/modules/sensors/sensor_params.c index 7ce6ef5ef..229bfe3ce 100644 --- a/src/modules/sensors/sensor_params.c +++ b/src/modules/sensors/sensor_params.c @@ -214,6 +214,16 @@ PARAM_DEFINE_FLOAT(SENS_DPRES_OFF, 0.0f); */ PARAM_DEFINE_FLOAT(SENS_DPRES_ANSC, 0); +/** + * QNH for barometer + * + * @min 500 + * @max 1500 + * @group Sensor Calibration + * @unit hPa + */ +PARAM_DEFINE_FLOAT(SENS_BARO_QNH, 1013.25f); + /** * Board rotation diff --git a/src/modules/sensors/sensors.cpp b/src/modules/sensors/sensors.cpp index 4e8a8c01d..cdcb428dd 100644 --- a/src/modules/sensors/sensors.cpp +++ b/src/modules/sensors/sensors.cpp @@ -143,6 +143,12 @@ #define STICK_ON_OFF_LIMIT 0.75f +/* oddly, ERROR is not defined for c++ */ +#ifdef ERROR +# undef ERROR +#endif +static const int ERROR = -1; + /** * Sensor app start / stop handling function * @@ -235,7 +241,7 @@ private: 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 */ hrt_abstime _battery_current_timestamp; /**< timestamp of last battery current reading */ @@ -258,7 +264,7 @@ private: int board_rotation; int external_mag_rotation; - + float board_offset[3]; int rc_map_roll; @@ -301,6 +307,8 @@ private: float battery_voltage_scaling; float battery_current_scaling; + float baro_qnh; + } _parameters; /**< local copies of interesting parameters */ struct { @@ -354,9 +362,11 @@ private: param_t board_rotation; param_t external_mag_rotation; - + param_t board_offset[3]; + param_t baro_qnh; + } _parameter_handles; /**< handles for interesting parameters */ @@ -462,12 +472,6 @@ private: namespace sensors { -/* oddly, ERROR is not defined for c++ */ -#ifdef ERROR -# undef ERROR -#endif -static const int ERROR = -1; - Sensors *g_sensors = nullptr; } @@ -611,12 +615,15 @@ Sensors::Sensors() : /* rotations */ _parameter_handles.board_rotation = param_find("SENS_BOARD_ROT"); _parameter_handles.external_mag_rotation = param_find("SENS_EXT_MAG_ROT"); - + /* rotation offsets */ _parameter_handles.board_offset[0] = param_find("SENS_BOARD_X_OFF"); _parameter_handles.board_offset[1] = param_find("SENS_BOARD_Y_OFF"); _parameter_handles.board_offset[2] = param_find("SENS_BOARD_Z_OFF"); + /* Barometer QNH */ + _parameter_handles.baro_qnh = param_find("SENS_BARO_QNH"); + /* fetch initial parameter values */ parameters_update(); } @@ -828,19 +835,37 @@ Sensors::parameters_update() get_rot_matrix((enum Rotation)_parameters.board_rotation, &_board_rotation); get_rot_matrix((enum Rotation)_parameters.external_mag_rotation, &_external_mag_rotation); - + param_get(_parameter_handles.board_offset[0], &(_parameters.board_offset[0])); param_get(_parameter_handles.board_offset[1], &(_parameters.board_offset[1])); param_get(_parameter_handles.board_offset[2], &(_parameters.board_offset[2])); - + /** fine tune board offset on parameter update **/ - math::Matrix<3, 3> board_rotation_offset; + math::Matrix<3, 3> board_rotation_offset; board_rotation_offset.from_euler( M_DEG_TO_RAD_F * _parameters.board_offset[0], M_DEG_TO_RAD_F * _parameters.board_offset[1], M_DEG_TO_RAD_F * _parameters.board_offset[2]); - + _board_rotation = _board_rotation * board_rotation_offset; + /* update barometer qnh setting */ + param_get(_parameter_handles.baro_qnh, &(_parameters.baro_qnh)); + int fd; + fd = open(BARO_DEVICE_PATH, 0); + if (fd < 0) { + warn("%s", BARO_DEVICE_PATH); + errx(1, "FATAL: no barometer found"); + + } else { + int ret = ioctl(fd, BAROIOCSMSLPRESSURE, (unsigned long)(_parameters.baro_qnh * 100)); + if (ret) { + warnx("qnh could not be set"); + close(fd); + return ERROR; + } + close(fd); + } + return OK; } @@ -1204,16 +1229,18 @@ Sensors::diff_pres_poll(struct sensor_combined_s &raw) if (updated) { orb_copy(ORB_ID(differential_pressure), _diff_pres_sub, &_diff_pres); - raw.differential_pressure_pa = _diff_pres.differential_pressure_pa; + raw.differential_pressure_pa = _diff_pres.differential_pressure_raw_pa; raw.differential_pressure_timestamp = _diff_pres.timestamp; raw.differential_pressure_filtered_pa = _diff_pres.differential_pressure_filtered_pa; 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); + + /* don't risk to feed negative airspeed into the system */ + _airspeed.indicated_airspeed_m_s = math::max(0.0f, calc_indicated_airspeed(_diff_pres.differential_pressure_filtered_pa)); + _airspeed.true_airspeed_m_s = math::max(0.0f, 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 */ @@ -1432,12 +1459,10 @@ Sensors::adc_poll(struct sensor_combined_s &raw) if (voltage > 0.4f && (_parameters.diff_pres_analog_scale > 0.0f)) { float diff_pres_pa_raw = voltage * _parameters.diff_pres_analog_scale - _parameters.diff_pres_offset_pa; - float diff_pres_pa = (diff_pres_pa_raw > 0.0f) ? diff_pres_pa_raw : 0.0f; _diff_pres.timestamp = t; - _diff_pres.differential_pressure_pa = diff_pres_pa; _diff_pres.differential_pressure_raw_pa = diff_pres_pa_raw; - _diff_pres.differential_pressure_filtered_pa = (_diff_pres.differential_pressure_filtered_pa * 0.9f) + (diff_pres_pa * 0.1f); + _diff_pres.differential_pressure_filtered_pa = (_diff_pres.differential_pressure_filtered_pa * 0.9f) + (diff_pres_pa_raw * 0.1f); _diff_pres.temperature = -1000.0f; /* announce the airspeed if needed, just publish else */ diff --git a/src/modules/systemlib/mixer/mixer.h b/src/modules/systemlib/mixer/mixer.h index cdf60febc..17989558e 100644 --- a/src/modules/systemlib/mixer/mixer.h +++ b/src/modules/systemlib/mixer/mixer.h @@ -130,6 +130,9 @@ #include <nuttx/config.h> #include "drivers/drv_mixer.h" + +#include <uORB/topics/multirotor_motor_limits.h> + #include "mixer_load.h" /** @@ -531,6 +534,9 @@ private: float _yaw_scale; float _idle_speed; + orb_advert_t _limits_pub; + multirotor_motor_limits_s _limits; + unsigned _rotor_count; const Rotor *_rotors; diff --git a/src/modules/systemlib/mixer/mixer_multirotor.cpp b/src/modules/systemlib/mixer/mixer_multirotor.cpp index 4b22a46d0..57e17b67d 100644 --- a/src/modules/systemlib/mixer/mixer_multirotor.cpp +++ b/src/modules/systemlib/mixer/mixer_multirotor.cpp @@ -36,7 +36,8 @@ * * Multi-rotor mixers. */ - +#include <uORB/uORB.h> +#include <uORB/topics/multirotor_motor_limits.h> #include <nuttx/config.h> #include <sys/types.h> @@ -302,6 +303,11 @@ MultirotorMixer::mix(float *outputs, unsigned space) float min_out = 0.0f; float max_out = 0.0f; + _limits.roll_pitch = false; + _limits.yaw = false; + _limits.throttle_upper = false; + _limits.throttle_lower = false; + /* perform initial mix pass yielding unbounded outputs, ignore yaw */ for (unsigned i = 0; i < _rotor_count; i++) { float out = roll * _rotors[i].roll_scale + @@ -311,6 +317,7 @@ MultirotorMixer::mix(float *outputs, unsigned space) /* limit yaw if it causes outputs clipping */ if (out >= 0.0f && out < -yaw * _rotors[i].yaw_scale) { yaw = -out / _rotors[i].yaw_scale; + _limits.yaw = true; } /* calculate min and max output values */ @@ -332,6 +339,7 @@ MultirotorMixer::mix(float *outputs, unsigned space) for (unsigned i = 0; i < _rotor_count; i++) { outputs[i] = scale_in * (roll * _rotors[i].roll_scale + pitch * _rotors[i].pitch_scale) + thrust; } + _limits.roll_pitch = true; } else { /* roll/pitch mixed without limiting, add yaw control */ @@ -344,6 +352,7 @@ MultirotorMixer::mix(float *outputs, unsigned space) float scale_out; if (max_out > 1.0f) { scale_out = 1.0f / max_out; + _limits.throttle_upper = true; } else { scale_out = 1.0f; @@ -351,9 +360,20 @@ MultirotorMixer::mix(float *outputs, unsigned space) /* scale outputs to range _idle_speed..1, and do final limiting */ for (unsigned i = 0; i < _rotor_count; i++) { + if (outputs[i] < _idle_speed) { + _limits.throttle_lower = true; + } outputs[i] = constrain(_idle_speed + (outputs[i] * (1.0f - _idle_speed) * scale_out), _idle_speed, 1.0f); } +#if defined(CONFIG_ARCH_BOARD_PX4FMU_V1) || defined(CONFIG_ARCH_BOARD_PX4FMU_V2) + /* publish/advertise motor limits if running on FMU */ + if (_limits_pub > 0) { + orb_publish(ORB_ID(multirotor_motor_limits), _limits_pub, &_limits); + } else { + _limits_pub = orb_advertise(ORB_ID(multirotor_motor_limits), &_limits); + } +#endif return _rotor_count; } diff --git a/src/modules/systemlib/param/param.c b/src/modules/systemlib/param/param.c index e44e6cdb0..6b8d0e634 100644 --- a/src/modules/systemlib/param/param.c +++ b/src/modules/systemlib/param/param.c @@ -322,7 +322,8 @@ param_get_value_ptr(param_t param) v = ¶m_info_base[param].val; } - if (param_type(param) == PARAM_TYPE_STRUCT) { + if (param_type(param) >= PARAM_TYPE_STRUCT + && param_type(param) <= PARAM_TYPE_STRUCT_MAX) { result = v->p; } else { diff --git a/src/modules/systemlib/param/param.h b/src/modules/systemlib/param/param.h index 084cd931a..dc73b37e9 100644 --- a/src/modules/systemlib/param/param.h +++ b/src/modules/systemlib/param/param.h @@ -307,7 +307,7 @@ __EXPORT int param_load_default(void); struct param_info_s __param__##_name = { \ #_name, \ PARAM_TYPE_STRUCT + sizeof(_default), \ - .val.p = &_default; \ + .val.p = &_default \ } /** diff --git a/src/modules/uORB/objects_common.cpp b/src/modules/uORB/objects_common.cpp index f7d5f8737..b921865eb 100644 --- a/src/modules/uORB/objects_common.cpp +++ b/src/modules/uORB/objects_common.cpp @@ -192,6 +192,9 @@ ORB_DEFINE(actuator_outputs_1, struct actuator_outputs_s); ORB_DEFINE(actuator_outputs_2, struct actuator_outputs_s); ORB_DEFINE(actuator_outputs_3, struct actuator_outputs_s); +#include "topics/multirotor_motor_limits.h" +ORB_DEFINE(multirotor_motor_limits, struct multirotor_motor_limits_s); + #include "topics/telemetry_status.h" ORB_DEFINE(telemetry_status_0, struct telemetry_status_s); ORB_DEFINE(telemetry_status_1, struct telemetry_status_s); diff --git a/src/modules/uORB/topics/differential_pressure.h b/src/modules/uORB/topics/differential_pressure.h index cd48d3cb2..7342fcf04 100644 --- a/src/modules/uORB/topics/differential_pressure.h +++ b/src/modules/uORB/topics/differential_pressure.h @@ -54,7 +54,6 @@ struct differential_pressure_s { 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 */ diff --git a/src/modules/uORB/topics/multirotor_motor_limits.h b/src/modules/uORB/topics/multirotor_motor_limits.h new file mode 100644 index 000000000..44c51e4d9 --- /dev/null +++ b/src/modules/uORB/topics/multirotor_motor_limits.h @@ -0,0 +1,69 @@ +/**************************************************************************** + * + * 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 multirotor_motor_limits.h + * + * Definition of multirotor_motor_limits topic + */ + +#ifndef MULTIROTOR_MOTOR_LIMITS_H_ +#define MULTIROTOR_MOTOR_LIMITS_H_ + +#include "../uORB.h" +#include <stdint.h> + +/** + * @addtogroup topics + * @{ + */ + +/** + * Motor limits + */ +struct multirotor_motor_limits_s { + uint8_t roll_pitch : 1; // roll/pitch limit reached + uint8_t yaw : 1; // yaw limit reached + uint8_t throttle_lower : 1; // lower throttle limit reached + uint8_t throttle_upper : 1; // upper throttle limit reached + uint8_t reserved : 4; +}; + +/** + * @} + */ + +/* register this as object request broker structure */ +ORB_DECLARE(multirotor_motor_limits); + +#endif diff --git a/src/modules/uORB/topics/vehicle_command.h b/src/modules/uORB/topics/vehicle_command.h index 7db33d98b..44aa50572 100644 --- a/src/modules/uORB/topics/vehicle_command.h +++ b/src/modules/uORB/topics/vehicle_command.h @@ -1,9 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2008-2012 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_command.h * Definition of the vehicle command uORB topic. + * + * @author Thomas Gubler <thomasgubler@student.ethz.ch> + * @author Julian Oes <joes@student.ethz.ch> + * @author Lorenz Meier <lm@inf.ethz.ch> */ #ifndef TOPIC_VEHICLE_COMMAND_H_ @@ -52,6 +53,9 @@ * but can contain additional ones. */ enum VEHICLE_CMD { + VEHICLE_CMD_CUSTOM_0 = 0, /* test command */ + VEHICLE_CMD_CUSTOM_1 = 1, /* test command */ + VEHICLE_CMD_CUSTOM_2 = 2, /* test command */ 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| */ @@ -87,7 +91,8 @@ enum VEHICLE_CMD { 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, /* | */ + VEHICLE_CMD_PAYLOAD_PREPARE_DEPLOY = 30001, /**< Prepare a payload deployment in the flight plan */ + VEHICLE_CMD_PAYLOAD_CONTROL_DEPLOY = 30002 /**< Control a pre-programmed payload deployment */ }; /** @@ -115,8 +120,8 @@ struct vehicle_command_s { float param2; /**< Parameter 2, as defined by MAVLink VEHICLE_CMD enum. */ float param3; /**< Parameter 3, as defined by MAVLink VEHICLE_CMD enum. */ float param4; /**< Parameter 4, as defined by MAVLink VEHICLE_CMD enum. */ - float param5; /**< Parameter 5, as defined by MAVLink VEHICLE_CMD enum. */ - float param6; /**< Parameter 6, as defined by MAVLink VEHICLE_CMD enum. */ + double param5; /**< Parameter 5, as defined by MAVLink VEHICLE_CMD enum. */ + double param6; /**< Parameter 6, as defined by MAVLink VEHICLE_CMD enum. */ float param7; /**< Parameter 7, as defined by MAVLink VEHICLE_CMD enum. */ enum VEHICLE_CMD command; /**< Command ID, as defined MAVLink by VEHICLE_CMD enum. */ uint8_t target_system; /**< System which should execute the command */ diff --git a/src/modules/uORB/topics/vehicle_global_position.h b/src/modules/uORB/topics/vehicle_global_position.h index 25137c1c6..c3bb3b893 100644 --- a/src/modules/uORB/topics/vehicle_global_position.h +++ b/src/modules/uORB/topics/vehicle_global_position.h @@ -72,6 +72,8 @@ struct vehicle_global_position_s { float yaw; /**< Yaw in radians -PI..+PI. */ float eph; /**< Standard deviation of position estimate horizontally */ float epv; /**< Standard deviation of position vertically */ + float terrain_alt; /**< Terrain altitude in m, WGS84 */ + bool terrain_alt_valid; /**< Terrain altitude estimate is valid */ }; /** diff --git a/src/modules/uavcan/esc_controller.cpp b/src/modules/uavcan/actuators/esc.cpp index 406eba88c..223d94731 100644 --- a/src/modules/uavcan/esc_controller.cpp +++ b/src/modules/uavcan/actuators/esc.cpp @@ -32,12 +32,12 @@ ****************************************************************************/ /** - * @file esc_controller.cpp + * @file esc.cpp * * @author Pavel Kirienko <pavel.kirienko@gmail.com> */ -#include "esc_controller.hpp" +#include "esc.hpp" #include <systemlib/err.h> UavcanEscController::UavcanEscController(uavcan::INode &node) : diff --git a/src/modules/uavcan/esc_controller.hpp b/src/modules/uavcan/actuators/esc.hpp index 559ede561..cf0988210 100644 --- a/src/modules/uavcan/esc_controller.hpp +++ b/src/modules/uavcan/actuators/esc.hpp @@ -32,7 +32,7 @@ ****************************************************************************/ /** - * @file esc_controller.hpp + * @file esc.hpp * * UAVCAN <--> ORB bridge for ESC messages: * uavcan.equipment.esc.RawCommand diff --git a/src/modules/uavcan/module.mk b/src/modules/uavcan/module.mk index 3865f2468..f92bc754f 100644 --- a/src/modules/uavcan/module.mk +++ b/src/modules/uavcan/module.mk @@ -40,10 +40,19 @@ MODULE_COMMAND = uavcan MAXOPTIMIZATION = -Os -SRCS += uavcan_main.cpp \ - uavcan_clock.cpp \ - esc_controller.cpp \ - gnss_receiver.cpp +# Main +SRCS += uavcan_main.cpp \ + uavcan_clock.cpp \ + uavcan_params.c + +# Actuators +SRCS += actuators/esc.cpp + +# Sensors +SRCS += sensors/sensor_bridge.cpp \ + sensors/gnss.cpp \ + sensors/mag.cpp \ + sensors/baro.cpp # # libuavcan diff --git a/src/modules/uavcan/sensors/baro.cpp b/src/modules/uavcan/sensors/baro.cpp new file mode 100644 index 000000000..80c5e3828 --- /dev/null +++ b/src/modules/uavcan/sensors/baro.cpp @@ -0,0 +1,117 @@ +/**************************************************************************** + * + * 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. + * + ****************************************************************************/ + +/** + * @author Pavel Kirienko <pavel.kirienko@gmail.com> + */ + +#include "baro.hpp" +#include <cmath> + +static const orb_id_t BARO_TOPICS[2] = { + ORB_ID(sensor_baro0), + ORB_ID(sensor_baro1) +}; + +const char *const UavcanBarometerBridge::NAME = "baro"; + +UavcanBarometerBridge::UavcanBarometerBridge(uavcan::INode& node) : +UavcanCDevSensorBridgeBase("uavcan_baro", "/dev/uavcan/baro", BARO_DEVICE_PATH, BARO_TOPICS), +_sub_air_data(node) +{ +} + +int UavcanBarometerBridge::init() +{ + int res = device::CDev::init(); + if (res < 0) { + return res; + } + + res = _sub_air_data.start(AirDataCbBinder(this, &UavcanBarometerBridge::air_data_sub_cb)); + if (res < 0) { + log("failed to start uavcan sub: %d", res); + return res; + } + return 0; +} + +int UavcanBarometerBridge::ioctl(struct file *filp, int cmd, unsigned long arg) +{ + switch (cmd) { + case BAROIOCSMSLPRESSURE: { + if ((arg < 80000) || (arg > 120000)) { + return -EINVAL; + } else { + log("new msl pressure %u", _msl_pressure); + _msl_pressure = arg; + return OK; + } + } + case BAROIOCGMSLPRESSURE: { + return _msl_pressure; + } + default: { + return CDev::ioctl(filp, cmd, arg); + } + } +} + +void UavcanBarometerBridge::air_data_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::air_data::StaticAirData> &msg) +{ + auto report = ::baro_report(); + + report.timestamp = msg.getUtcTimestamp().toUSec(); + if (report.timestamp == 0) { + report.timestamp = msg.getMonotonicTimestamp().toUSec(); + } + + report.temperature = msg.static_temperature; + report.pressure = msg.static_pressure / 100.0F; // Convert to millibar + + /* + * Altitude computation + * Refer to the MS5611 driver for details + */ + const double T1 = 15.0 + 273.15; // temperature at base height in Kelvin + const double a = -6.5 / 1000; // temperature gradient in degrees per metre + const double g = 9.80665; // gravity constant in m/s/s + const double R = 287.05; // ideal gas constant in J/kg/K + + const double p1 = _msl_pressure / 1000.0; // current pressure at MSL in kPa + const double p = double(msg.static_pressure) / 1000.0; // measured pressure in kPa + + report.altitude = (((std::pow((p / p1), (-(a * R) / g))) * T1) - T1) / a; + + publish(msg.getSrcNodeID().get(), &report); +} diff --git a/src/modules/uavcan/sensors/baro.hpp b/src/modules/uavcan/sensors/baro.hpp new file mode 100644 index 000000000..9d470219e --- /dev/null +++ b/src/modules/uavcan/sensors/baro.hpp @@ -0,0 +1,68 @@ +/**************************************************************************** + * + * 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. + * + ****************************************************************************/ + +/** + * @author Pavel Kirienko <pavel.kirienko@gmail.com> + */ + +#pragma once + +#include "sensor_bridge.hpp" +#include <drivers/drv_baro.h> + +#include <uavcan/equipment/air_data/StaticAirData.hpp> + +class UavcanBarometerBridge : public UavcanCDevSensorBridgeBase +{ +public: + static const char *const NAME; + + UavcanBarometerBridge(uavcan::INode& node); + + const char *get_name() const override { return NAME; } + + int init() override; + +private: + int ioctl(struct file *filp, int cmd, unsigned long arg) override; + + void air_data_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::air_data::StaticAirData> &msg); + + typedef uavcan::MethodBinder<UavcanBarometerBridge*, + void (UavcanBarometerBridge::*) + (const uavcan::ReceivedDataStructure<uavcan::equipment::air_data::StaticAirData>&)> + AirDataCbBinder; + + uavcan::Subscriber<uavcan::equipment::air_data::StaticAirData, AirDataCbBinder> _sub_air_data; + unsigned _msl_pressure = 101325; +}; diff --git a/src/modules/uavcan/gnss_receiver.cpp b/src/modules/uavcan/sensors/gnss.cpp index ba1fe5e49..24afe6aaf 100644 --- a/src/modules/uavcan/gnss_receiver.cpp +++ b/src/modules/uavcan/sensors/gnss.cpp @@ -32,52 +32,72 @@ ****************************************************************************/ /** - * @file gnss_receiver.cpp + * @file gnss.cpp * * @author Pavel Kirienko <pavel.kirienko@gmail.com> * @author Andrew Chambers <achamber@gmail.com> * */ -#include "gnss_receiver.hpp" +#include "gnss.hpp" #include <systemlib/err.h> #include <mathlib/mathlib.h> -#define MM_PER_CM 10 // Millimeters per centimeter +const char *const UavcanGnssBridge::NAME = "gnss"; -UavcanGnssReceiver::UavcanGnssReceiver(uavcan::INode &node) : +UavcanGnssBridge::UavcanGnssBridge(uavcan::INode &node) : _node(node), -_uavcan_sub_status(node), +_sub_fix(node), _report_pub(-1) { } -int UavcanGnssReceiver::init() +int UavcanGnssBridge::init() { - int res = -1; - - // GNSS fix subscription - res = _uavcan_sub_status.start(FixCbBinder(this, &UavcanGnssReceiver::gnss_fix_sub_cb)); + int res = _sub_fix.start(FixCbBinder(this, &UavcanGnssBridge::gnss_fix_sub_cb)); if (res < 0) { warnx("GNSS fix sub failed %i", res); return res; } + return res; +} - // Clear the uORB GPS report - memset(&_report, 0, sizeof(_report)); +unsigned UavcanGnssBridge::get_num_redundant_channels() const +{ + return (_receiver_node_id < 0) ? 0 : 1; +} - return res; +void UavcanGnssBridge::print_status() const +{ + printf("RX errors: %d, receiver node id: ", _sub_fix.getFailureCount()); + if (_receiver_node_id < 0) { + printf("N/A\n"); + } else { + printf("%d\n", _receiver_node_id); + } } -void UavcanGnssReceiver::gnss_fix_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::gnss::Fix> &msg) +void UavcanGnssBridge::gnss_fix_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::gnss::Fix> &msg) { - _report.timestamp_position = hrt_absolute_time(); - _report.lat = msg.lat_1e7; - _report.lon = msg.lon_1e7; - _report.alt = msg.alt_1e2 * MM_PER_CM; // Convert from centimeter (1e2) to millimeters (1e3) + // This bridge does not support redundant GNSS receivers yet. + if (_receiver_node_id < 0) { + _receiver_node_id = msg.getSrcNodeID().get(); + warnx("GNSS receiver node ID: %d", _receiver_node_id); + } else { + if (_receiver_node_id != msg.getSrcNodeID().get()) { + return; // This GNSS receiver is the redundant one, ignore it. + } + } + + auto report = ::vehicle_gps_position_s(); + + report.timestamp_position = hrt_absolute_time(); + report.lat = msg.latitude_deg_1e8 / 10; + report.lon = msg.longitude_deg_1e8 / 10; + report.alt = msg.height_msl_mm; - _report.timestamp_variance = _report.timestamp_position; + report.timestamp_variance = report.timestamp_position; // Check if the msg contains valid covariance information @@ -90,19 +110,19 @@ void UavcanGnssReceiver::gnss_fix_sub_cb(const uavcan::ReceivedDataStructure<uav // Horizontal position uncertainty const float horizontal_pos_variance = math::max(pos_cov[0], pos_cov[4]); - _report.eph = (horizontal_pos_variance > 0) ? sqrtf(horizontal_pos_variance) : -1.0F; + report.eph = (horizontal_pos_variance > 0) ? sqrtf(horizontal_pos_variance) : -1.0F; // Vertical position uncertainty - _report.epv = (pos_cov[8] > 0) ? sqrtf(pos_cov[8]) : -1.0F; + report.epv = (pos_cov[8] > 0) ? sqrtf(pos_cov[8]) : -1.0F; } else { - _report.eph = -1.0F; - _report.epv = -1.0F; + report.eph = -1.0F; + report.epv = -1.0F; } if (valid_velocity_covariance) { float vel_cov[9]; msg.velocity_covariance.unpackSquareMatrix(vel_cov); - _report.s_variance_m_s = math::max(math::max(vel_cov[0], vel_cov[4]), vel_cov[8]); + report.s_variance_m_s = math::max(math::max(vel_cov[0], vel_cov[4]), vel_cov[8]); /* There is a nonlinear relationship between the velocity vector and the heading. * Use Jacobian to transform velocity covariance to heading covariance @@ -118,36 +138,36 @@ void UavcanGnssReceiver::gnss_fix_sub_cb(const uavcan::ReceivedDataStructure<uav float vel_e = msg.ned_velocity[1]; float vel_n_sq = vel_n * vel_n; float vel_e_sq = vel_e * vel_e; - _report.c_variance_rad = + report.c_variance_rad = (vel_e_sq * vel_cov[0] + -2 * vel_n * vel_e * vel_cov[1] + // Covariance matrix is symmetric vel_n_sq* vel_cov[4]) / ((vel_n_sq + vel_e_sq) * (vel_n_sq + vel_e_sq)); } else { - _report.s_variance_m_s = -1.0F; - _report.c_variance_rad = -1.0F; + report.s_variance_m_s = -1.0F; + report.c_variance_rad = -1.0F; } - _report.fix_type = msg.status; + report.fix_type = msg.status; - _report.timestamp_velocity = _report.timestamp_position; - _report.vel_n_m_s = msg.ned_velocity[0]; - _report.vel_e_m_s = msg.ned_velocity[1]; - _report.vel_d_m_s = msg.ned_velocity[2]; - _report.vel_m_s = sqrtf(_report.vel_n_m_s * _report.vel_n_m_s + _report.vel_e_m_s * _report.vel_e_m_s + _report.vel_d_m_s * _report.vel_d_m_s); - _report.cog_rad = atan2f(_report.vel_e_m_s, _report.vel_n_m_s); - _report.vel_ned_valid = true; + report.timestamp_velocity = report.timestamp_position; + report.vel_n_m_s = msg.ned_velocity[0]; + report.vel_e_m_s = msg.ned_velocity[1]; + report.vel_d_m_s = msg.ned_velocity[2]; + report.vel_m_s = sqrtf(report.vel_n_m_s * report.vel_n_m_s + report.vel_e_m_s * report.vel_e_m_s + report.vel_d_m_s * report.vel_d_m_s); + report.cog_rad = atan2f(report.vel_e_m_s, report.vel_n_m_s); + report.vel_ned_valid = true; - _report.timestamp_time = _report.timestamp_position; - _report.time_gps_usec = uavcan::UtcTime(msg.gnss_timestamp).toUSec(); // Convert to microseconds + report.timestamp_time = report.timestamp_position; + report.time_gps_usec = uavcan::UtcTime(msg.gnss_timestamp).toUSec(); // Convert to microseconds - _report.satellites_used = msg.sats_used; + report.satellites_used = msg.sats_used; if (_report_pub > 0) { - orb_publish(ORB_ID(vehicle_gps_position), _report_pub, &_report); + orb_publish(ORB_ID(vehicle_gps_position), _report_pub, &report); } else { - _report_pub = orb_advertise(ORB_ID(vehicle_gps_position), &_report); + _report_pub = orb_advertise(ORB_ID(vehicle_gps_position), &report); } } diff --git a/src/modules/uavcan/gnss_receiver.hpp b/src/modules/uavcan/sensors/gnss.hpp index 18df8da2f..e8466b401 100644 --- a/src/modules/uavcan/gnss_receiver.hpp +++ b/src/modules/uavcan/sensors/gnss.hpp @@ -32,7 +32,7 @@ ****************************************************************************/ /** - * @file gnss_receiver.hpp + * @file gnss.hpp * * UAVCAN --> ORB bridge for GNSS messages: * uavcan.equipment.gnss.Fix @@ -51,12 +51,22 @@ #include <uavcan/uavcan.hpp> #include <uavcan/equipment/gnss/Fix.hpp> -class UavcanGnssReceiver +#include "sensor_bridge.hpp" + +class UavcanGnssBridge : public IUavcanSensorBridge { public: - UavcanGnssReceiver(uavcan::INode& node); + static const char *const NAME; + + UavcanGnssBridge(uavcan::INode& node); + + const char *get_name() const override { return NAME; } + + int init() override; - int init(); + unsigned get_num_redundant_channels() const override; + + void print_status() const override; private: /** @@ -64,21 +74,14 @@ private: */ void gnss_fix_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::gnss::Fix> &msg); - - typedef uavcan::MethodBinder<UavcanGnssReceiver*, - void (UavcanGnssReceiver::*)(const uavcan::ReceivedDataStructure<uavcan::equipment::gnss::Fix>&)> + typedef uavcan::MethodBinder<UavcanGnssBridge*, + void (UavcanGnssBridge::*)(const uavcan::ReceivedDataStructure<uavcan::equipment::gnss::Fix>&)> FixCbBinder; - /* - * libuavcan related things - */ - uavcan::INode &_node; - uavcan::Subscriber<uavcan::equipment::gnss::Fix, FixCbBinder> _uavcan_sub_status; + uavcan::INode &_node; + uavcan::Subscriber<uavcan::equipment::gnss::Fix, FixCbBinder> _sub_fix; + int _receiver_node_id = -1; - /* - * uORB - */ - struct vehicle_gps_position_s _report; ///< uORB topic for gnss position - orb_advert_t _report_pub; ///< uORB pub for gnss position + orb_advert_t _report_pub; ///< uORB pub for gnss position }; diff --git a/src/modules/uavcan/sensors/mag.cpp b/src/modules/uavcan/sensors/mag.cpp new file mode 100644 index 000000000..8e6a9a22f --- /dev/null +++ b/src/modules/uavcan/sensors/mag.cpp @@ -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. + * + ****************************************************************************/ + +/** + * @author Pavel Kirienko <pavel.kirienko@gmail.com> + */ + +#include "mag.hpp" + +static const orb_id_t MAG_TOPICS[3] = { + ORB_ID(sensor_mag0), + ORB_ID(sensor_mag1), + ORB_ID(sensor_mag2) +}; + +const char *const UavcanMagnetometerBridge::NAME = "mag"; + +UavcanMagnetometerBridge::UavcanMagnetometerBridge(uavcan::INode& node) : +UavcanCDevSensorBridgeBase("uavcan_mag", "/dev/uavcan/mag", MAG_DEVICE_PATH, MAG_TOPICS), +_sub_mag(node) +{ + _scale.x_scale = 1.0F; + _scale.y_scale = 1.0F; + _scale.z_scale = 1.0F; +} + +int UavcanMagnetometerBridge::init() +{ + int res = device::CDev::init(); + if (res < 0) { + return res; + } + + res = _sub_mag.start(MagCbBinder(this, &UavcanMagnetometerBridge::mag_sub_cb)); + if (res < 0) { + log("failed to start uavcan sub: %d", res); + return res; + } + return 0; +} + +int UavcanMagnetometerBridge::ioctl(struct file *filp, int cmd, unsigned long arg) +{ + switch (cmd) { + case MAGIOCSSCALE: { + std::memcpy(&_scale, reinterpret_cast<const void*>(arg), sizeof(_scale)); + return 0; + } + case MAGIOCGSCALE: { + std::memcpy(reinterpret_cast<void*>(arg), &_scale, sizeof(_scale)); + return 0; + } + case MAGIOCSELFTEST: { + return 0; // Nothing to do + } + case MAGIOCGEXTERNAL: { + return 0; // We don't want anyone to transform the coordinate frame, so we declare it onboard + } + case MAGIOCSSAMPLERATE: { + return 0; // Pretend that this stuff is supported to keep the sensor app happy + } + case MAGIOCCALIBRATE: + case MAGIOCGSAMPLERATE: + case MAGIOCSRANGE: + case MAGIOCGRANGE: + case MAGIOCSLOWPASS: + case MAGIOCEXSTRAP: + case MAGIOCGLOWPASS: { + return -EINVAL; + } + default: { + return CDev::ioctl(filp, cmd, arg); + } + } +} + +void UavcanMagnetometerBridge::mag_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::ahrs::Magnetometer> &msg) +{ + auto report = ::mag_report(); + + report.range_ga = 1.3F; // Arbitrary number, doesn't really mean anything + + report.timestamp = msg.getUtcTimestamp().toUSec(); + if (report.timestamp == 0) { + report.timestamp = msg.getMonotonicTimestamp().toUSec(); + } + + report.x = (msg.magnetic_field[0] - _scale.x_offset) * _scale.x_scale; + report.y = (msg.magnetic_field[1] - _scale.y_offset) * _scale.y_scale; + report.z = (msg.magnetic_field[2] - _scale.z_offset) * _scale.z_scale; + + publish(msg.getSrcNodeID().get(), &report); +} diff --git a/src/modules/uavcan/sensors/mag.hpp b/src/modules/uavcan/sensors/mag.hpp new file mode 100644 index 000000000..6d413a8f7 --- /dev/null +++ b/src/modules/uavcan/sensors/mag.hpp @@ -0,0 +1,68 @@ +/**************************************************************************** + * + * 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. + * + ****************************************************************************/ + +/** + * @author Pavel Kirienko <pavel.kirienko@gmail.com> + */ + +#pragma once + +#include "sensor_bridge.hpp" +#include <drivers/drv_mag.h> + +#include <uavcan/equipment/ahrs/Magnetometer.hpp> + +class UavcanMagnetometerBridge : public UavcanCDevSensorBridgeBase +{ +public: + static const char *const NAME; + + UavcanMagnetometerBridge(uavcan::INode& node); + + const char *get_name() const override { return NAME; } + + int init() override; + +private: + int ioctl(struct file *filp, int cmd, unsigned long arg) override; + + void mag_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::ahrs::Magnetometer> &msg); + + typedef uavcan::MethodBinder<UavcanMagnetometerBridge*, + void (UavcanMagnetometerBridge::*) + (const uavcan::ReceivedDataStructure<uavcan::equipment::ahrs::Magnetometer>&)> + MagCbBinder; + + uavcan::Subscriber<uavcan::equipment::ahrs::Magnetometer, MagCbBinder> _sub_mag; + mag_scale _scale = {}; +}; diff --git a/src/modules/uavcan/sensors/sensor_bridge.cpp b/src/modules/uavcan/sensors/sensor_bridge.cpp new file mode 100644 index 000000000..9608ce680 --- /dev/null +++ b/src/modules/uavcan/sensors/sensor_bridge.cpp @@ -0,0 +1,158 @@ +/**************************************************************************** + * + * 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. + * + ****************************************************************************/ + +/** + * @author Pavel Kirienko <pavel.kirienko@gmail.com> + */ + +#include "sensor_bridge.hpp" +#include <cassert> + +#include "gnss.hpp" +#include "mag.hpp" +#include "baro.hpp" + +/* + * IUavcanSensorBridge + */ +void IUavcanSensorBridge::make_all(uavcan::INode &node, List<IUavcanSensorBridge*> &list) +{ + list.add(new UavcanBarometerBridge(node)); + list.add(new UavcanMagnetometerBridge(node)); + list.add(new UavcanGnssBridge(node)); +} + +/* + * UavcanCDevSensorBridgeBase + */ +UavcanCDevSensorBridgeBase::~UavcanCDevSensorBridgeBase() +{ + for (unsigned i = 0; i < _max_channels; i++) { + if (_channels[i].node_id >= 0) { + (void)unregister_class_devname(_class_devname, _channels[i].class_instance); + } + } + delete [] _orb_topics; + delete [] _channels; +} + +void UavcanCDevSensorBridgeBase::publish(const int node_id, const void *report) +{ + assert(report != nullptr); + + Channel *channel = nullptr; + + // Checking if such channel already exists + for (unsigned i = 0; i < _max_channels; i++) { + if (_channels[i].node_id == node_id) { + channel = _channels + i; + break; + } + } + + // No such channel - try to create one + if (channel == nullptr) { + if (_out_of_channels) { + return; // Give up immediately - saves some CPU time + } + + log("adding channel %d...", node_id); + + // Search for the first free channel + for (unsigned i = 0; i < _max_channels; i++) { + if (_channels[i].node_id < 0) { + channel = _channels + i; + break; + } + } + + // No free channels left + if (channel == nullptr) { + _out_of_channels = true; + log("out of channels"); + return; + } + + // Ask the CDev helper which class instance we can take + const int class_instance = register_class_devname(_class_devname); + if (class_instance < 0 || class_instance >= int(_max_channels)) { + _out_of_channels = true; + log("out of class instances"); + (void)unregister_class_devname(_class_devname, class_instance); + return; + } + + // Publish to the appropriate topic, abort on failure + channel->orb_id = _orb_topics[class_instance]; + channel->node_id = node_id; + channel->class_instance = class_instance; + + channel->orb_advert = orb_advertise(channel->orb_id, report); + if (channel->orb_advert < 0) { + log("ADVERTISE FAILED"); + (void)unregister_class_devname(_class_devname, class_instance); + *channel = Channel(); + return; + } + + log("channel %d class instance %d ok", channel->node_id, channel->class_instance); + } + assert(channel != nullptr); + + (void)orb_publish(channel->orb_id, channel->orb_advert, report); +} + +unsigned UavcanCDevSensorBridgeBase::get_num_redundant_channels() const +{ + unsigned out = 0; + for (unsigned i = 0; i < _max_channels; i++) { + if (_channels[i].node_id >= 0) { + out += 1; + } + } + return out; +} + +void UavcanCDevSensorBridgeBase::print_status() const +{ + printf("devname: %s\n", _class_devname); + + for (unsigned i = 0; i < _max_channels; i++) { + if (_channels[i].node_id >= 0) { + printf("channel %d: node id %d --> class instance %d\n", + i, _channels[i].node_id, _channels[i].class_instance); + } else { + printf("channel %d: empty\n", i); + } + } +} diff --git a/src/modules/uavcan/sensors/sensor_bridge.hpp b/src/modules/uavcan/sensors/sensor_bridge.hpp new file mode 100644 index 000000000..1316f7ecc --- /dev/null +++ b/src/modules/uavcan/sensors/sensor_bridge.hpp @@ -0,0 +1,131 @@ +/**************************************************************************** + * + * 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. + * + ****************************************************************************/ + +/** + * @author Pavel Kirienko <pavel.kirienko@gmail.com> + */ + +#pragma once + +#include <containers/List.hpp> +#include <uavcan/uavcan.hpp> +#include <drivers/device/device.h> +#include <drivers/drv_orb_dev.h> + +/** + * A sensor bridge class must implement this interface. + */ +class IUavcanSensorBridge : uavcan::Noncopyable, public ListNode<IUavcanSensorBridge*> +{ +public: + static constexpr unsigned MAX_NAME_LEN = 20; + + virtual ~IUavcanSensorBridge() { } + + /** + * Returns ASCII name of the bridge. + */ + virtual const char *get_name() const = 0; + + /** + * Starts the bridge. + * @return Non-negative value on success, negative on error. + */ + virtual int init() = 0; + + /** + * Returns number of active redundancy channels. + */ + virtual unsigned get_num_redundant_channels() const = 0; + + /** + * Prints current status in a human readable format to stdout. + */ + virtual void print_status() const = 0; + + /** + * Sensor bridge factory. + * Creates a bridge object by its ASCII name, e.g. "gnss", "mag". + * @return nullptr if such bridge can't be created. + */ + static void make_all(uavcan::INode &node, List<IUavcanSensorBridge*> &list); +}; + +/** + * This is the base class for redundant sensors with an independent ORB topic per each redundancy channel. + * For example, sensor_mag0, sensor_mag1, etc. + */ +class UavcanCDevSensorBridgeBase : public IUavcanSensorBridge, public device::CDev +{ + struct Channel + { + int node_id = -1; + orb_id_t orb_id = nullptr; + orb_advert_t orb_advert = -1; + int class_instance = -1; + }; + + const unsigned _max_channels; + const char *const _class_devname; + orb_id_t *const _orb_topics; + Channel *const _channels; + bool _out_of_channels = false; + +protected: + template <unsigned MaxChannels> + UavcanCDevSensorBridgeBase(const char *name, const char *devname, const char *class_devname, + const orb_id_t (&orb_topics)[MaxChannels]) : + device::CDev(name, devname), + _max_channels(MaxChannels), + _class_devname(class_devname), + _orb_topics(new orb_id_t[MaxChannels]), + _channels(new Channel[MaxChannels]) + { + memcpy(_orb_topics, orb_topics, sizeof(orb_id_t) * MaxChannels); + } + + /** + * Sends one measurement into appropriate ORB topic. + * New redundancy channels will be registered automatically. + * @param node_id Sensor's Node ID + * @param report Pointer to ORB message object + */ + void publish(const int node_id, const void *report); + +public: + virtual ~UavcanCDevSensorBridgeBase(); + + unsigned get_num_redundant_channels() const override; + + void print_status() const override; +}; diff --git a/src/modules/uavcan/uavcan_clock.cpp b/src/modules/uavcan/uavcan_clock.cpp index e41d5f953..fe8ba406a 100644 --- a/src/modules/uavcan/uavcan_clock.cpp +++ b/src/modules/uavcan/uavcan_clock.cpp @@ -62,6 +62,8 @@ void adjustUtc(uavcan::UtcDuration adjustment) (void)adjustment; } +uavcan::uint64_t getUtcUSecFromCanInterrupt(); + uavcan::uint64_t getUtcUSecFromCanInterrupt() { return 0; diff --git a/src/modules/uavcan/uavcan_main.cpp b/src/modules/uavcan/uavcan_main.cpp index 4535b6d6a..a8485ee44 100644 --- a/src/modules/uavcan/uavcan_main.cpp +++ b/src/modules/uavcan/uavcan_main.cpp @@ -38,8 +38,10 @@ #include <fcntl.h> #include <systemlib/err.h> #include <systemlib/systemlib.h> +#include <systemlib/param/param.h> #include <systemlib/mixer/mixer.h> #include <systemlib/board_serial.h> +#include <systemlib/scheduling_priorities.h> #include <version/version.h> #include <arch/board/board.h> #include <arch/chip/chip.h> @@ -65,16 +67,18 @@ UavcanNode *UavcanNode::_instance; UavcanNode::UavcanNode(uavcan::ICanDriver &can_driver, uavcan::ISystemClock &system_clock) : CDev("uavcan", UAVCAN_DEVICE_PATH), _node(can_driver, system_clock), - _esc_controller(_node), - _gnss_receiver(_node) + _node_mutex(), + _esc_controller(_node) { _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)); + const int res = pthread_mutex_init(&_node_mutex, nullptr); + if (res < 0) { + std::abort(); + } } UavcanNode::~UavcanNode() @@ -99,10 +103,18 @@ UavcanNode::~UavcanNode() } /* clean up the alternate device node */ - // unregister_driver(PWM_OUTPUT_DEVICE_PATH); + // unregister_driver(PWM_OUTPUT_DEVICE_PATH); ::close(_armed_sub); + // Removing the sensor bridges + auto br = _sensor_bridges.getHead(); + while (br != nullptr) { + auto next = br->getSibling(); + delete br; + br = next; + } + _instance = nullptr; } @@ -164,7 +176,7 @@ int UavcanNode::start(uavcan::NodeID node_id, uint32_t bitrate) * Start the task. Normally it should never exit. */ static auto run_trampoline = [](int, char *[]) {return UavcanNode::_instance->run();}; - _instance->_task = task_spawn_cmd("uavcan", SCHED_DEFAULT, SCHED_PRIORITY_DEFAULT, StackSize, + _instance->_task = task_spawn_cmd("uavcan", SCHED_DEFAULT, SCHED_PRIORITY_ACTUATOR_OUTPUTS, StackSize, static_cast<main_t>(run_trampoline), nullptr); if (_instance->_task < 0) { @@ -214,11 +226,12 @@ int UavcanNode::init(uavcan::NodeID node_id) { int ret = -1; - /* do regular cdev init */ + // Do regular cdev init ret = CDev::init(); - if (ret != OK) + if (ret != OK) { return ret; + } _node.setName("org.pixhawk.pixhawk"); @@ -226,14 +239,24 @@ int UavcanNode::init(uavcan::NodeID node_id) fill_node_info(); - /* initializing the bridges UAVCAN <--> uORB */ + // Actuators ret = _esc_controller.init(); - if (ret < 0) + if (ret < 0) { return ret; + } - ret = _gnss_receiver.init(); - if (ret < 0) - return ret; + // Sensor bridges + IUavcanSensorBridge::make_all(_node, _sensor_bridges); + auto br = _sensor_bridges.getHead(); + while (br != nullptr) { + ret = br->init(); + if (ret < 0) { + warnx("cannot init sensor bridge '%s' (%d)", br->get_name(), ret); + return ret; + } + warnx("sensor bridge '%s' init ok", br->get_name()); + br = br->getSibling(); + } return _node.start(); } @@ -248,6 +271,8 @@ void UavcanNode::node_spin_once() int UavcanNode::run() { + (void)pthread_mutex_lock(&_node_mutex); + const unsigned PollTimeoutMs = 50; // XXX figure out the output count @@ -291,8 +316,13 @@ int UavcanNode::run() _groups_subscribed = _groups_required; } + // Mutex is unlocked while the thread is blocked on IO multiplexing + (void)pthread_mutex_unlock(&_node_mutex); + const int poll_ret = ::poll(_poll_fds, _poll_fds_num, PollTimeoutMs); + (void)pthread_mutex_lock(&_node_mutex); + node_spin_once(); // Non-blocking // this would be bad... @@ -352,7 +382,6 @@ int UavcanNode::run() // Output to the bus _esc_controller.update_outputs(outputs.output, outputs.noutputs); } - } // Check arming state @@ -376,10 +405,7 @@ int UavcanNode::run() } int -UavcanNode::control_callback(uintptr_t handle, - uint8_t control_group, - uint8_t control_index, - float &input) +UavcanNode::control_callback(uintptr_t handle, uint8_t control_group, uint8_t control_index, float &input) { const actuator_controls_s *controls = (actuator_controls_s *)handle; @@ -520,8 +546,23 @@ UavcanNode::print_info() warnx("not running, start first"); } - warnx("actuators control groups: sub: %u / req: %u / fds: %u", (unsigned)_groups_subscribed, (unsigned)_groups_required, _poll_fds_num); - warnx("mixer: %s", (_mixers == nullptr) ? "NONE" : "OK"); + (void)pthread_mutex_lock(&_node_mutex); + + // ESC mixer status + printf("ESC actuators control groups: sub: %u / req: %u / fds: %u\n", + (unsigned)_groups_subscribed, (unsigned)_groups_required, _poll_fds_num); + printf("ESC mixer: %s\n", (_mixers == nullptr) ? "NONE" : "OK"); + + // Sensor bridges + auto br = _sensor_bridges.getHead(); + while (br != nullptr) { + printf("Sensor '%s':\n", br->get_name()); + br->print_status(); + printf("\n"); + br = br->getSibling(); + } + + (void)pthread_mutex_unlock(&_node_mutex); } /* @@ -529,79 +570,57 @@ UavcanNode::print_info() */ static void print_usage() { - warnx("usage: uavcan start <node_id> [can_bitrate]"); + warnx("usage: \n" + "\tuavcan {start|status|stop}"); } extern "C" __EXPORT int uavcan_main(int argc, char *argv[]); int uavcan_main(int argc, char *argv[]) { - constexpr unsigned DEFAULT_CAN_BITRATE = 1000000; - if (argc < 2) { print_usage(); ::exit(1); } if (!std::strcmp(argv[1], "start")) { - if (argc < 3) { - print_usage(); - ::exit(1); + if (UavcanNode::instance()) { + errx(1, "already started"); } - /* - * Node ID - */ - const int node_id = atoi(argv[2]); + // Node ID + int32_t node_id = 0; + (void)param_get(param_find("UAVCAN_NODE_ID"), &node_id); if (node_id < 0 || node_id > uavcan::NodeID::Max || !uavcan::NodeID(node_id).isUnicast()) { warnx("Invalid Node ID %i", node_id); ::exit(1); } - /* - * CAN bitrate - */ - unsigned bitrate = 0; - - if (argc > 3) { - bitrate = atol(argv[3]); - } - - if (bitrate <= 0) { - bitrate = DEFAULT_CAN_BITRATE; - } + // CAN bitrate + int32_t bitrate = 0; + (void)param_get(param_find("UAVCAN_BITRATE"), &bitrate); - if (UavcanNode::instance()) { - errx(1, "already started"); - } - - /* - * Start - */ + // Start warnx("Node ID %u, bitrate %u", node_id, bitrate); return UavcanNode::start(node_id, bitrate); - } /* commands below require the app to be started */ - UavcanNode *inst = UavcanNode::instance(); + UavcanNode *const inst = UavcanNode::instance(); if (!inst) { errx(1, "application not running"); } if (!std::strcmp(argv[1], "status") || !std::strcmp(argv[1], "info")) { - - inst->print_info(); - return OK; + inst->print_info(); + ::exit(0); } if (!std::strcmp(argv[1], "stop")) { - - delete inst; - inst = nullptr; - return OK; + delete inst; + ::exit(0); } print_usage(); diff --git a/src/modules/uavcan/uavcan_main.hpp b/src/modules/uavcan/uavcan_main.hpp index 05b66fd7b..be7db9741 100644 --- a/src/modules/uavcan/uavcan_main.hpp +++ b/src/modules/uavcan/uavcan_main.hpp @@ -42,8 +42,8 @@ #include <uORB/topics/actuator_outputs.h> #include <uORB/topics/actuator_armed.h> -#include "esc_controller.hpp" -#include "gnss_receiver.hpp" +#include "actuators/esc.hpp" +#include "sensors/sensor_bridge.hpp" /** * @file uavcan_main.hpp @@ -77,12 +77,10 @@ public: static int start(uavcan::NodeID node_id, uint32_t bitrate); - Node& getNode() { return _node; } + Node& get_node() { return _node; } - static int control_callback(uintptr_t handle, - uint8_t control_group, - uint8_t control_index, - float &input); + // TODO: move the actuator mixing stuff into the ESC controller class + static int control_callback(uintptr_t handle, uint8_t control_group, uint8_t control_index, float &input); void subscribe(); @@ -109,8 +107,11 @@ private: static UavcanNode *_instance; ///< singleton pointer Node _node; ///< library instance + pthread_mutex_t _node_mutex; + UavcanEscController _esc_controller; - UavcanGnssReceiver _gnss_receiver; + + List<IUavcanSensorBridge*> _sensor_bridges; ///< List of active sensor bridges MixerGroup *_mixers = nullptr; diff --git a/src/modules/uavcan/uavcan_params.c b/src/modules/uavcan/uavcan_params.c new file mode 100644 index 000000000..e6ea8a8fb --- /dev/null +++ b/src/modules/uavcan/uavcan_params.c @@ -0,0 +1,73 @@ +/**************************************************************************** + * + * 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. + * + ****************************************************************************/ + +/** + * @author Pavel Kirienko <pavel.kirienko@gmail.com> + */ + +#include <nuttx/config.h> +#include <systemlib/param/param.h> + +/** + * Enable UAVCAN. + * + * Enables support for UAVCAN-interfaced actuators and sensors. + * + * @min 0 + * @max 1 + * @group UAVCAN + */ +PARAM_DEFINE_INT32(UAVCAN_ENABLE, 0); + +/** + * UAVCAN Node ID. + * + * Read the specs at http://uavcan.org to learn more about Node ID. + * + * @min 1 + * @max 125 + * @group UAVCAN + */ +PARAM_DEFINE_INT32(UAVCAN_NODE_ID, 1); + +/** + * UAVCAN CAN bus bitrate. + * + * @min 20000 + * @max 1000000 + * @group UAVCAN + */ +PARAM_DEFINE_INT32(UAVCAN_BITRATE, 1000000); + + + diff --git a/src/modules/unit_test/unit_test.cpp b/src/modules/unit_test/unit_test.cpp index 02d1af481..be3b9461a 100644 --- a/src/modules/unit_test/unit_test.cpp +++ b/src/modules/unit_test/unit_test.cpp @@ -56,3 +56,8 @@ void UnitTest::printAssert(const char* msg, const char* test, const char* file, { warnx("Assertion failed: %s - %s (%s:%d)", msg, test, file, line); } + +void UnitTest::printCompare(const char* msg, const char *v1_text, int v1, const char *v2_text, int v2, const char* file, int line) +{ + warnx("Compare failed: %s - (%s:%d) (%s:%d) (%s:%d)", msg, v1_text, v1, v2_text, v2, file, line); +} diff --git a/src/modules/unit_test/unit_test.h b/src/modules/unit_test/unit_test.h index 32eb8c308..1a5489709 100644 --- a/src/modules/unit_test/unit_test.h +++ b/src/modules/unit_test/unit_test.h @@ -52,11 +52,15 @@ INLINE_GLOBAL(const char*, mu_last_test) UnitTest(); virtual ~UnitTest(); + + virtual void init(void) { }; + virtual void cleanup(void) { }; virtual void runTests(void) = 0; void printResults(void); void printAssert(const char* msg, const char* test, const char* file, int line); + void printCompare(const char* msg, const char *v1_text, int v1, const char *v2_text, int v2, const char* file, int line); #define ut_assert(message, test) \ do { \ @@ -68,10 +72,23 @@ INLINE_GLOBAL(const char*, mu_last_test) } \ } while (0) +#define ut_compare(message, v1, v2) \ + do { \ + int _v1 = v1; \ + int _v2 = v2; \ + if (_v1 != _v2) { \ + printCompare(message, #v1, _v1, #v2, _v2, __FILE__, __LINE__); \ + return false; \ + } else { \ + mu_assertion()++; \ + } \ + } while (0) + #define ut_run_test(test) \ do { \ warnx("RUNNING TEST: %s", #test); \ mu_tests_run()++; \ + init(); \ if (!test()) { \ warnx("TEST FAILED: %s", #test); \ mu_tests_failed()++; \ @@ -79,6 +96,7 @@ INLINE_GLOBAL(const char*, mu_last_test) warnx("TEST PASSED: %s", #test); \ mu_tests_passed()++; \ } \ + cleanup(); \ } while (0) }; diff --git a/src/systemcmds/pwm/pwm.c b/src/systemcmds/pwm/pwm.c index c8d698b86..478c2a772 100644 --- a/src/systemcmds/pwm/pwm.c +++ b/src/systemcmds/pwm/pwm.c @@ -654,9 +654,28 @@ pwm_main(int argc, char *argv[]) } } exit(0); + } else if (!strcmp(argv[1], "terminatefail")) { + + if (argc < 3) { + errx(1, "arg missing [on|off]"); + } else { + + if (!strcmp(argv[2], "on")) { + /* force failsafe */ + ret = ioctl(fd, PWM_SERVO_SET_TERMINATION_FAILSAFE, 1); + } else { + /* force failsafe */ + ret = ioctl(fd, PWM_SERVO_SET_TERMINATION_FAILSAFE, 0); + } + + if (ret != OK) { + warnx("FAILED setting termination failsafe %s", argv[2]); + } + } + exit(0); } - usage("specify arm|disarm|rate|failsafe|disarmed|min|max|test|info|forcefail"); + usage("specify arm|disarm|rate|failsafe\n\t\tdisarmed|min|max|test|info|forcefail|terminatefail"); return 0; } diff --git a/src/systemcmds/tests/test_sensors.c b/src/systemcmds/tests/test_sensors.c index a4f17eebd..e005bf9c1 100644 --- a/src/systemcmds/tests/test_sensors.c +++ b/src/systemcmds/tests/test_sensors.c @@ -331,7 +331,7 @@ mag(int argc, char *argv[]) float len = sqrtf(buf.x * buf.x + buf.y * buf.y + buf.z * buf.z); - if (len < 1.0f || len > 3.0f) { + if (len < 0.25f || len > 3.0f) { warnx("MAG scale error!"); return ERROR; } diff --git a/uavcan b/uavcan -Subproject 6980ee824074aa2f7a62221bf6040ee41111952 +Subproject 286adbcc56c4b093143b647ec7546abb149cd53 |