diff options
76 files changed, 4490 insertions, 2548 deletions
diff --git a/Documentation/flight_mode_state_machine.odg b/Documentation/flight_mode_state_machine.odg Binary files differindex b630ecb40..2d119bd8c 100644 --- a/Documentation/flight_mode_state_machine.odg +++ b/Documentation/flight_mode_state_machine.odg diff --git a/Documentation/flight_mode_state_machine.pdf b/Documentation/flight_mode_state_machine.pdf Binary files differindex cd234ada7..af41953ee 100644 --- a/Documentation/flight_mode_state_machine.pdf +++ b/Documentation/flight_mode_state_machine.pdf diff --git a/makefiles/config_px4fmu-v1_default.mk b/makefiles/config_px4fmu-v1_default.mk index 213eb651b..ea1e38ff7 100644 --- a/makefiles/config_px4fmu-v1_default.mk +++ b/makefiles/config_px4fmu-v1_default.mk @@ -46,6 +46,7 @@ MODULES += systemcmds/param MODULES += systemcmds/perf MODULES += systemcmds/preflight_check MODULES += systemcmds/pwm +MODULES += systemcmds/esc_calib MODULES += systemcmds/reboot MODULES += systemcmds/top MODULES += systemcmds/tests diff --git a/src/drivers/ardrone_interface/ardrone_interface.c b/src/drivers/ardrone_interface/ardrone_interface.c index 735bdb41a..187820372 100644 --- a/src/drivers/ardrone_interface/ardrone_interface.c +++ b/src/drivers/ardrone_interface/ardrone_interface.c @@ -55,6 +55,7 @@ #include <uORB/uORB.h> #include <uORB/topics/vehicle_status.h> #include <uORB/topics/actuator_controls.h> +#include <uORB/topics/actuator_safety.h> #include <systemlib/systemlib.h> @@ -247,13 +248,13 @@ int ardrone_interface_thread_main(int argc, char *argv[]) memset(&state, 0, sizeof(state)); struct actuator_controls_s actuator_controls; memset(&actuator_controls, 0, sizeof(actuator_controls)); - struct actuator_armed_s armed; - armed.armed = false; + struct actuator_safety_s safety; + safety.armed = false; /* subscribe to attitude, motor setpoints and system state */ int actuator_controls_sub = orb_subscribe(ORB_ID_VEHICLE_ATTITUDE_CONTROLS); int state_sub = orb_subscribe(ORB_ID(vehicle_status)); - int armed_sub = orb_subscribe(ORB_ID(actuator_armed)); + int safety_sub = orb_subscribe(ORB_ID(actuator_safety)); printf("[ardrone_interface] Motors initialized - ready.\n"); fflush(stdout); @@ -322,16 +323,14 @@ int ardrone_interface_thread_main(int argc, char *argv[]) } else { /* MAIN OPERATION MODE */ - /* get a local copy of the vehicle state */ - orb_copy(ORB_ID(vehicle_status), state_sub, &state); /* get a local copy of the actuator controls */ orb_copy(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_controls_sub, &actuator_controls); - orb_copy(ORB_ID(actuator_armed), armed_sub, &armed); + orb_copy(ORB_ID(actuator_safety), safety_sub, &safety); /* for now only spin if armed and immediately shut down * if in failsafe */ - if (armed.armed && !armed.lockdown) { + if (safety.armed && !safety.lockdown) { ardrone_mixing_and_output(ardrone_write, &actuator_controls); } else { diff --git a/src/drivers/blinkm/blinkm.cpp b/src/drivers/blinkm/blinkm.cpp index 3fabfd9a5..a11f88477 100644 --- a/src/drivers/blinkm/blinkm.cpp +++ b/src/drivers/blinkm/blinkm.cpp @@ -116,6 +116,7 @@ #include <poll.h> #include <uORB/uORB.h> #include <uORB/topics/vehicle_status.h> +#include <uORB/topics/actuator_safety.h> #include <uORB/topics/vehicle_gps_position.h> static const float MAX_CELL_VOLTAGE = 4.3f; @@ -376,6 +377,7 @@ BlinkM::led() static int vehicle_status_sub_fd; static int vehicle_gps_position_sub_fd; + static int actuator_safety_sub_fd; static int num_of_cells = 0; static int detected_cells_runcount = 0; @@ -386,6 +388,7 @@ BlinkM::led() static int led_interval = 1000; static int no_data_vehicle_status = 0; + static int no_data_actuator_safety = 0; static int no_data_vehicle_gps_position = 0; static bool topic_initialized = false; @@ -398,6 +401,9 @@ BlinkM::led() vehicle_status_sub_fd = orb_subscribe(ORB_ID(vehicle_status)); orb_set_interval(vehicle_status_sub_fd, 1000); + actuator_safety_sub_fd = orb_subscribe(ORB_ID(actuator_safety)); + orb_set_interval(actuator_safety_sub_fd, 1000); + vehicle_gps_position_sub_fd = orb_subscribe(ORB_ID(vehicle_gps_position)); orb_set_interval(vehicle_gps_position_sub_fd, 1000); @@ -452,12 +458,14 @@ BlinkM::led() if (led_thread_runcount == 15) { /* obtained data for the first file descriptor */ struct vehicle_status_s vehicle_status_raw; + struct actuator_safety_s actuator_safety; struct vehicle_gps_position_s vehicle_gps_position_raw; memset(&vehicle_status_raw, 0, sizeof(vehicle_status_raw)); memset(&vehicle_gps_position_raw, 0, sizeof(vehicle_gps_position_raw)); bool new_data_vehicle_status; + bool new_data_actuator_safety; bool new_data_vehicle_gps_position; orb_check(vehicle_status_sub_fd, &new_data_vehicle_status); @@ -471,6 +479,17 @@ BlinkM::led() no_data_vehicle_status = 3; } + orb_check(actuator_safety_sub_fd, &new_data_actuator_safety); + + if (new_data_actuator_safety) { + orb_copy(ORB_ID(actuator_safety), actuator_safety_sub_fd, &actuator_safety); + no_data_actuator_safety = 0; + } else { + no_data_actuator_safety++; + if(no_data_vehicle_status >= 3) + no_data_vehicle_status = 3; + } + orb_check(vehicle_gps_position_sub_fd, &new_data_vehicle_gps_position); if (new_data_vehicle_gps_position) { @@ -486,15 +505,15 @@ BlinkM::led() /* get number of used satellites in navigation */ num_of_used_sats = 0; - //for(int satloop=0; satloop<20; satloop++) { - for(int satloop=0; satloop<sizeof(vehicle_gps_position_raw.satellite_used); satloop++) { - if(vehicle_gps_position_raw.satellite_used[satloop] == 1) { + + for (unsigned satloop = 0; satloop < (sizeof(vehicle_gps_position_raw.satellite_used) / sizeof(vehicle_gps_position_raw.satellite_used[0])); satloop++) { + if (vehicle_gps_position_raw.satellite_used[satloop] == 1) { num_of_used_sats++; } } - if(new_data_vehicle_status || no_data_vehicle_status < 3){ - if(num_of_cells == 0) { + if (new_data_vehicle_status || no_data_vehicle_status < 3) { + if (num_of_cells == 0) { /* looking for lipo cells that are connected */ printf("<blinkm> checking cells\n"); for(num_of_cells = 2; num_of_cells < 7; num_of_cells++) { @@ -530,7 +549,7 @@ BlinkM::led() } else { /* no battery warnings here */ - if(vehicle_status_raw.flag_system_armed == false) { + if(actuator_safety.armed == false) { /* system not armed */ led_color_1 = LED_RED; led_color_2 = LED_RED; @@ -555,26 +574,27 @@ BlinkM::led() led_blink = LED_BLINK; /* handle 4th led - flightmode indicator */ - switch((int)vehicle_status_raw.flight_mode) { - case VEHICLE_FLIGHT_MODE_MANUAL: - led_color_4 = LED_AMBER; - break; - - case VEHICLE_FLIGHT_MODE_STAB: - led_color_4 = LED_YELLOW; - break; - - case VEHICLE_FLIGHT_MODE_HOLD: - led_color_4 = LED_BLUE; - break; - - case VEHICLE_FLIGHT_MODE_AUTO: - led_color_4 = LED_GREEN; - break; - } +#warning fix this +// switch((int)vehicle_status_raw.flight_mode) { +// case VEHICLE_FLIGHT_MODE_MANUAL: +// led_color_4 = LED_AMBER; +// break; +// +// case VEHICLE_FLIGHT_MODE_STAB: +// led_color_4 = LED_YELLOW; +// break; +// +// case VEHICLE_FLIGHT_MODE_HOLD: +// led_color_4 = LED_BLUE; +// break; +// +// case VEHICLE_FLIGHT_MODE_AUTO: +// led_color_4 = LED_GREEN; +// break; +// } if(new_data_vehicle_gps_position || no_data_vehicle_gps_position < 3) { - /* handling used sat´s */ + /* handling used sat�s */ if(num_of_used_sats >= 7) { led_color_1 = LED_OFF; led_color_2 = LED_OFF; diff --git a/src/drivers/hil/hil.cpp b/src/drivers/hil/hil.cpp index bd027ce0b..15fbf8c88 100644 --- a/src/drivers/hil/hil.cpp +++ b/src/drivers/hil/hil.cpp @@ -75,6 +75,7 @@ #include <systemlib/mixer/mixer.h> #include <uORB/topics/actuator_controls.h> +#include <uORB/topics/actuator_safety.h> #include <uORB/topics/actuator_outputs.h> #include <systemlib/err.h> @@ -108,7 +109,7 @@ private: int _current_update_rate; int _task; int _t_actuators; - int _t_armed; + int _t_safety; orb_advert_t _t_outputs; unsigned _num_outputs; bool _primary_pwm_device; @@ -161,7 +162,7 @@ HIL::HIL() : _current_update_rate(0), _task(-1), _t_actuators(-1), - _t_armed(-1), + _t_safety(-1), _t_outputs(0), _num_outputs(0), _primary_pwm_device(false), @@ -321,8 +322,8 @@ HIL::task_main() /* force a reset of the update rate */ _current_update_rate = 0; - _t_armed = orb_subscribe(ORB_ID(actuator_armed)); - orb_set_interval(_t_armed, 200); /* 5Hz update rate */ + _t_safety = orb_subscribe(ORB_ID(actuator_safety)); + orb_set_interval(_t_safety, 200); /* 5Hz update rate */ /* advertise the mixed control outputs */ actuator_outputs_s outputs; @@ -334,7 +335,7 @@ HIL::task_main() pollfd fds[2]; fds[0].fd = _t_actuators; fds[0].events = POLLIN; - fds[1].fd = _t_armed; + fds[1].fd = _t_safety; fds[1].events = POLLIN; unsigned num_outputs; @@ -426,15 +427,15 @@ HIL::task_main() /* how about an arming update? */ if (fds[1].revents & POLLIN) { - actuator_armed_s aa; + actuator_safety_s aa; /* get new value */ - orb_copy(ORB_ID(actuator_armed), _t_armed, &aa); + orb_copy(ORB_ID(actuator_safety), _t_safety, &aa); } } ::close(_t_actuators); - ::close(_t_armed); + ::close(_t_safety); /* make sure servos are off */ // up_pwm_servo_deinit(); diff --git a/src/drivers/mkblctrl/mkblctrl.cpp b/src/drivers/mkblctrl/mkblctrl.cpp index b54b7aba1..f187f22a6 100644 --- a/src/drivers/mkblctrl/mkblctrl.cpp +++ b/src/drivers/mkblctrl/mkblctrl.cpp @@ -74,6 +74,7 @@ #include <uORB/topics/actuator_controls.h> #include <uORB/topics/actuator_controls_effective.h> #include <uORB/topics/actuator_outputs.h> +#include <uORB/topics/actuator_safety.h> #include <systemlib/err.h> @@ -132,7 +133,7 @@ private: int _current_update_rate; int _task; int _t_actuators; - int _t_armed; + int _t_actuator_safety; unsigned int _motor; int _px4mode; int _frametype; @@ -240,7 +241,7 @@ MK::MK(int bus) : _update_rate(50), _task(-1), _t_actuators(-1), - _t_armed(-1), + _t_actuator_safety(-1), _t_outputs(0), _t_actuators_effective(0), _num_outputs(0), @@ -496,8 +497,8 @@ MK::task_main() /* force a reset of the update rate */ _current_update_rate = 0; - _t_armed = orb_subscribe(ORB_ID(actuator_armed)); - orb_set_interval(_t_armed, 200); /* 5Hz update rate */ + _t_actuator_safety = orb_subscribe(ORB_ID(actuator_safety)); + orb_set_interval(_t_actuator_safety, 200); /* 5Hz update rate */ /* advertise the mixed control outputs */ actuator_outputs_s outputs; @@ -519,7 +520,7 @@ MK::task_main() pollfd fds[2]; fds[0].fd = _t_actuators; fds[0].events = POLLIN; - fds[1].fd = _t_armed; + fds[1].fd = _t_actuator_safety; fds[1].events = POLLIN; log("starting"); @@ -625,13 +626,13 @@ MK::task_main() /* how about an arming update? */ if (fds[1].revents & POLLIN) { - actuator_armed_s aa; + actuator_safety_s as; /* get new value */ - orb_copy(ORB_ID(actuator_armed), _t_armed, &aa); + orb_copy(ORB_ID(actuator_safety), _t_actuator_safety, &as); /* update PWM servo armed status if armed and not locked down */ - mk_servo_arm(aa.armed && !aa.lockdown); + mk_servo_arm(as.armed && !as.lockdown); } @@ -639,7 +640,7 @@ MK::task_main() ::close(_t_actuators); ::close(_t_actuators_effective); - ::close(_t_armed); + ::close(_t_actuator_safety); /* make sure servos are off */ diff --git a/src/drivers/px4fmu/fmu.cpp b/src/drivers/px4fmu/fmu.cpp index 5147ac500..05951f74c 100644 --- a/src/drivers/px4fmu/fmu.cpp +++ b/src/drivers/px4fmu/fmu.cpp @@ -69,6 +69,7 @@ #include <uORB/topics/actuator_controls.h> #include <uORB/topics/actuator_controls_effective.h> #include <uORB/topics/actuator_outputs.h> +#include <uORB/topics/actuator_safety.h> #include <systemlib/err.h> #include <systemlib/ppm_decode.h> @@ -104,7 +105,7 @@ private: unsigned _current_update_rate; int _task; int _t_actuators; - int _t_armed; + int _t_actuator_safety; orb_advert_t _t_outputs; orb_advert_t _t_actuators_effective; unsigned _num_outputs; @@ -174,7 +175,7 @@ PX4FMU::PX4FMU() : _current_update_rate(0), _task(-1), _t_actuators(-1), - _t_armed(-1), + _t_actuator_safety(-1), _t_outputs(0), _t_actuators_effective(0), _num_outputs(0), @@ -376,8 +377,8 @@ PX4FMU::task_main() /* force a reset of the update rate */ _current_update_rate = 0; - _t_armed = orb_subscribe(ORB_ID(actuator_armed)); - orb_set_interval(_t_armed, 200); /* 5Hz update rate */ + _t_actuator_safety = orb_subscribe(ORB_ID(actuator_safety)); + orb_set_interval(_t_actuator_safety, 200); /* 5Hz update rate */ /* advertise the mixed control outputs */ actuator_outputs_s outputs; @@ -396,7 +397,7 @@ PX4FMU::task_main() pollfd fds[2]; fds[0].fd = _t_actuators; fds[0].events = POLLIN; - fds[1].fd = _t_armed; + fds[1].fd = _t_actuator_safety; fds[1].events = POLLIN; unsigned num_outputs = (_mode == MODE_2PWM) ? 2 : 4; @@ -499,13 +500,13 @@ PX4FMU::task_main() /* how about an arming update? */ if (fds[1].revents & POLLIN) { - actuator_armed_s aa; + actuator_safety_s as; /* get new value */ - orb_copy(ORB_ID(actuator_armed), _t_armed, &aa); + orb_copy(ORB_ID(actuator_safety), _t_actuator_safety, &as); /* update PWM servo armed status if armed and not locked down */ - bool set_armed = aa.armed && !aa.lockdown; + bool set_armed = as.armed && !as.lockdown; if (set_armed != _armed) { _armed = set_armed; up_pwm_servo_arm(set_armed); @@ -535,7 +536,7 @@ PX4FMU::task_main() ::close(_t_actuators); ::close(_t_actuators_effective); - ::close(_t_armed); + ::close(_t_actuator_safety); /* make sure servos are off */ up_pwm_servo_deinit(); @@ -1021,12 +1022,12 @@ fake(int argc, char *argv[]) if (handle < 0) errx(1, "advertise failed"); - actuator_armed_s aa; + actuator_safety_s as; - aa.armed = true; - aa.lockdown = false; + as.armed = true; + as.lockdown = false; - handle = orb_advertise(ORB_ID(actuator_armed), &aa); + handle = orb_advertise(ORB_ID(actuator_safety), &as); if (handle < 0) errx(1, "advertise failed 2"); diff --git a/src/drivers/px4io/px4io.cpp b/src/drivers/px4io/px4io.cpp index 19163cebe..df2f18270 100644 --- a/src/drivers/px4io/px4io.cpp +++ b/src/drivers/px4io/px4io.cpp @@ -75,6 +75,7 @@ #include <uORB/topics/actuator_controls.h> #include <uORB/topics/actuator_controls_effective.h> #include <uORB/topics/actuator_outputs.h> +#include <uORB/topics/actuator_safety.h> #include <uORB/topics/vehicle_status.h> #include <uORB/topics/vehicle_command.h> #include <uORB/topics/rc_channels.h> @@ -125,6 +126,21 @@ public: int set_failsafe_values(const uint16_t *vals, unsigned len); /** + * Set the minimum PWM signals when armed + */ + int set_min_values(const uint16_t *vals, unsigned len); + + /** + * Set the maximum PWM signal when armed + */ + int set_max_values(const uint16_t *vals, unsigned len); + + /** + * Set an idle PWM signal that is active right after startup, even when SAFETY_SAFE + */ + int set_idle_values(const uint16_t *vals, unsigned len); + + /** * Print the current status of IO */ void print_status(); @@ -152,7 +168,7 @@ private: /* subscribed topics */ int _t_actuators; ///< actuator controls topic - int _t_armed; ///< system armed control topic + int _t_actuator_safety; ///< system armed control topic int _t_vstatus; ///< system / vehicle status int _t_param; ///< parameter update topic @@ -161,6 +177,7 @@ private: orb_advert_t _to_actuators_effective; ///< effective actuator controls topic orb_advert_t _to_outputs; ///< mixed servo outputs topic orb_advert_t _to_battery; ///< battery status / voltage + orb_advert_t _to_safety; ///< status of safety actuator_outputs_s _outputs; ///< mixed outputs actuator_controls_effective_s _controls_effective; ///< effective controls @@ -327,13 +344,14 @@ PX4IO::PX4IO() : _status(0), _alarms(0), _t_actuators(-1), - _t_armed(-1), + _t_actuator_safety(-1), _t_vstatus(-1), _t_param(-1), _to_input_rc(0), _to_actuators_effective(0), _to_outputs(0), _to_battery(0), + _to_safety(0), _primary_pwm_device(false), _battery_amp_per_volt(90.0f/5.0f), // this matches the 3DR current sensor _battery_amp_bias(0), @@ -387,6 +405,40 @@ PX4IO::init() */ _retries = 2; + /* get IO's last seen FMU state */ + int val = io_reg_get(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_ARMING); + if (val == _io_reg_get_error) { + mavlink_log_emergency(_mavlink_fd, "[IO] ERROR! FAILED READING STATE"); + } + uint16_t arming = val; + + /* get basic software version */ + /* basic configuration */ + usleep(5000); + + unsigned proto_version = io_reg_get(PX4IO_PAGE_CONFIG, PX4IO_P_CONFIG_PROTOCOL_VERSION); + unsigned sw_version = io_reg_get(PX4IO_PAGE_CONFIG, PX4IO_P_CONFIG_SOFTWARE_VERSION); + + if (proto_version != PX4IO_P_CONFIG_PROTOCOL_VERSION_MAGIC) { + mavlink_log_emergency(_mavlink_fd, "[IO] ERROR! PROTO VER MISMATCH: v%u vs v%u\n", + proto_version, + PX4IO_P_CONFIG_PROTOCOL_VERSION_MAGIC); + + mavlink_log_emergency(_mavlink_fd, "[IO] Please update PX4IO firmware."); + log("protocol version mismatch (v%u on IO vs v%u on FMU)", proto_version, PX4IO_P_CONFIG_PROTOCOL_VERSION_MAGIC); + return 1; + } + + if (sw_version != PX4IO_P_CONFIG_SOFTWARE_VERSION_MAGIC) { + mavlink_log_emergency(_mavlink_fd, "[IO] ERROR! SOFTWARE VER MISMATCH: v%u vs v%u\n", + proto_version, + PX4IO_P_CONFIG_SOFTWARE_VERSION_MAGIC); + + mavlink_log_emergency(_mavlink_fd, "[IO] Please update PX4IO firmware."); + log("software version mismatch (v%u on IO vs v%u on FMU)", sw_version, PX4IO_P_CONFIG_SOFTWARE_VERSION_MAGIC); + return 1; + } + /* get some parameters */ _max_actuators = io_reg_get(PX4IO_PAGE_CONFIG, PX4IO_P_CONFIG_ACTUATOR_COUNT); _max_controls = io_reg_get(PX4IO_PAGE_CONFIG, PX4IO_P_CONFIG_CONTROL_COUNT); @@ -412,41 +464,44 @@ PX4IO::init() * in this case. */ - uint16_t reg; + printf("arming 0x%04x%s%s%s%s\n", + arming, + ((arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) ? " FMU_ARMED" : ""), + ((arming & PX4IO_P_SETUP_ARMING_IO_ARM_OK) ? " IO_ARM_OK" : ""), + ((arming & PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK) ? " MANUAL_OVERRIDE_OK" : ""), + ((arming & PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK) ? " INAIR_RESTART_OK" : ""), + ((arming & PX4IO_P_SETUP_ARMING_FAILSAFE_CUSTOM) ? " FAILSAFE CUSTOM" : "")); - /* get IO's last seen FMU state */ - ret = io_reg_get(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_ARMING, ®, sizeof(reg)); - if (ret != OK) - return ret; /* * in-air restart is only tried if the IO board reports it is * already armed, and has been configured for in-air restart */ - if ((reg & PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK) && - (reg & PX4IO_P_SETUP_ARMING_FMU_ARMED)) { + if ((arming & PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK) && + (arming & PX4IO_P_SETUP_ARMING_FMU_ARMED)) { mavlink_log_emergency(_mavlink_fd, "[IO] RECOVERING FROM FMU IN-AIR RESTART"); + log("INAIR RESTART RECOVERY (needs commander app running)"); /* WARNING: COMMANDER app/vehicle status must be initialized. * If this fails (or the app is not started), worst-case IO * remains untouched (so manual override is still available). */ - int vstatus_sub = orb_subscribe(ORB_ID(vehicle_status)); + int safety_sub = orb_subscribe(ORB_ID(actuator_safety)); /* fill with initial values, clear updated flag */ - vehicle_status_s status; + struct actuator_safety_s safety; uint64_t try_start_time = hrt_absolute_time(); bool updated = false; - /* keep checking for an update, ensure we got a recent state, + /* keep checking for an update, ensure we got a arming information, not something that was published a long time ago. */ do { - orb_check(vstatus_sub, &updated); + orb_check(safety_sub, &updated); if (updated) { /* got data, copy and exit loop */ - orb_copy(ORB_ID(vehicle_status), vstatus_sub, &status); + orb_copy(ORB_ID(actuator_safety), safety_sub, &safety); break; } @@ -472,35 +527,41 @@ PX4IO::init() cmd.param6 = 0; cmd.param7 = 0; cmd.command = VEHICLE_CMD_COMPONENT_ARM_DISARM; - cmd.target_system = status.system_id; - cmd.target_component = status.component_id; - cmd.source_system = status.system_id; - cmd.source_component = status.component_id; + // cmd.target_system = status.system_id; + // cmd.target_component = status.component_id; + // cmd.source_system = status.system_id; + // cmd.source_component = status.component_id; /* ask to confirm command */ cmd.confirmation = 1; /* send command once */ - (void)orb_advertise(ORB_ID(vehicle_command), &cmd); + orb_advert_t pub = orb_advertise(ORB_ID(vehicle_command), &cmd); /* spin here until IO's state has propagated into the system */ do { - orb_check(vstatus_sub, &updated); + orb_check(safety_sub, &updated); if (updated) { - orb_copy(ORB_ID(vehicle_status), vstatus_sub, &status); + orb_copy(ORB_ID(actuator_safety), safety_sub, &safety); } - /* wait 10 ms */ - usleep(10000); + /* wait 50 ms */ + usleep(50000); /* abort after 5s */ - if ((hrt_absolute_time() - try_start_time)/1000 > 50000) { + if ((hrt_absolute_time() - try_start_time)/1000 > 2000) { log("failed to recover from in-air restart (2), aborting IO driver init."); return 1; } - /* keep waiting for state change for 10 s */ - } while (!status.flag_system_armed); + /* re-send if necessary */ + if (!safety.armed) { + orb_publish(ORB_ID(vehicle_command), pub, &cmd); + log("re-sending arm cmd"); + } + + /* keep waiting for state change for 2 s */ + } while (!safety.armed); /* regular boot, no in-air restart, init IO */ } else { @@ -510,7 +571,8 @@ PX4IO::init() io_reg_modify(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_ARMING, PX4IO_P_SETUP_ARMING_FMU_ARMED | PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK | - PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK, 0); + PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK | + PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE, 0); /* publish RC config to IO */ ret = io_set_rc_config(); @@ -538,7 +600,7 @@ PX4IO::init() return -errno; } - mavlink_log_info(_mavlink_fd, "[IO] init ok"); + mavlink_log_info(_mavlink_fd, "[IO] init ok (sw v.%u)", sw_version); return OK; } @@ -564,8 +626,8 @@ PX4IO::task_main() ORB_ID(actuator_controls_1)); orb_set_interval(_t_actuators, 20); /* default to 50Hz */ - _t_armed = orb_subscribe(ORB_ID(actuator_armed)); - orb_set_interval(_t_armed, 200); /* 5Hz update rate */ + _t_actuator_safety = orb_subscribe(ORB_ID(actuator_safety)); + orb_set_interval(_t_actuator_safety, 200); /* 5Hz update rate */ _t_vstatus = orb_subscribe(ORB_ID(vehicle_status)); orb_set_interval(_t_vstatus, 200); /* 5Hz update rate max. */ @@ -577,7 +639,7 @@ PX4IO::task_main() pollfd fds[4]; fds[0].fd = _t_actuators; fds[0].events = POLLIN; - fds[1].fd = _t_armed; + fds[1].fd = _t_actuator_safety; fds[1].events = POLLIN; fds[2].fd = _t_vstatus; fds[2].events = POLLIN; @@ -711,24 +773,65 @@ PX4IO::set_failsafe_values(const uint16_t *vals, unsigned len) } int +PX4IO::set_min_values(const uint16_t *vals, unsigned len) +{ + uint16_t regs[_max_actuators]; + + if (len > _max_actuators) + /* fail with error */ + return E2BIG; + + /* copy values to registers in IO */ + return io_reg_set(PX4IO_PAGE_CONTROL_MIN_PWM, 0, vals, len); +} + +int +PX4IO::set_max_values(const uint16_t *vals, unsigned len) +{ + uint16_t regs[_max_actuators]; + + if (len > _max_actuators) + /* fail with error */ + return E2BIG; + + /* copy values to registers in IO */ + return io_reg_set(PX4IO_PAGE_CONTROL_MAX_PWM, 0, vals, len); +} + +int +PX4IO::set_idle_values(const uint16_t *vals, unsigned len) +{ + uint16_t regs[_max_actuators]; + + if (len > _max_actuators) + /* fail with error */ + return E2BIG; + + printf("Sending IDLE values\n"); + + /* copy values to registers in IO */ + return io_reg_set(PX4IO_PAGE_IDLE_PWM, 0, vals, len); +} + + +int PX4IO::io_set_arming_state() { - actuator_armed_s armed; ///< system armed state + actuator_safety_s safety; ///< system armed state vehicle_status_s vstatus; ///< overall system state - orb_copy(ORB_ID(actuator_armed), _t_armed, &armed); + orb_copy(ORB_ID(actuator_safety), _t_actuator_safety, &safety); orb_copy(ORB_ID(vehicle_status), _t_vstatus, &vstatus); uint16_t set = 0; uint16_t clear = 0; - if (armed.armed && !armed.lockdown) { + if (safety.armed && !safety.lockdown) { set |= PX4IO_P_SETUP_ARMING_FMU_ARMED; } else { clear |= PX4IO_P_SETUP_ARMING_FMU_ARMED; } - - if (armed.ready_to_arm) { + if (safety.ready_to_arm) { set |= PX4IO_P_SETUP_ARMING_IO_ARM_OK; } else { clear |= PX4IO_P_SETUP_ARMING_IO_ARM_OK; @@ -861,14 +964,14 @@ PX4IO::io_handle_status(uint16_t status) */ /* check for IO reset - force it back to armed if necessary */ - if (_status & PX4IO_P_STATUS_FLAGS_ARMED && !(status & PX4IO_P_STATUS_FLAGS_ARMED) + if (_status & PX4IO_P_STATUS_FLAGS_SAFETY_OFF && !(status & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) && !(status & PX4IO_P_STATUS_FLAGS_ARM_SYNC)) { /* set the arming flag */ - ret = io_reg_modify(PX4IO_PAGE_STATUS, PX4IO_P_STATUS_FLAGS, 0, PX4IO_P_STATUS_FLAGS_ARMED | PX4IO_P_STATUS_FLAGS_ARM_SYNC); + ret = io_reg_modify(PX4IO_PAGE_STATUS, PX4IO_P_STATUS_FLAGS, 0, PX4IO_P_STATUS_FLAGS_SAFETY_OFF | PX4IO_P_STATUS_FLAGS_ARM_SYNC); /* set new status */ _status = status; - _status &= PX4IO_P_STATUS_FLAGS_ARMED; + _status &= PX4IO_P_STATUS_FLAGS_SAFETY_OFF; } else if (!(_status & PX4IO_P_STATUS_FLAGS_ARM_SYNC)) { /* set the sync flag */ @@ -883,6 +986,29 @@ PX4IO::io_handle_status(uint16_t status) _status = status; } + /** + * Get and handle the safety status + */ + struct actuator_safety_s safety; + safety.timestamp = hrt_absolute_time(); + + orb_copy(ORB_ID(actuator_safety), _t_actuator_safety, &safety); + + if (status & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) { + safety.safety_off = true; + safety.safety_switch_available = true; + } else { + safety.safety_off = false; + safety.safety_switch_available = true; + } + + /* lazily publish the safety status */ + if (_to_safety > 0) { + orb_publish(ORB_ID(actuator_safety), _to_safety, &safety); + } else { + _to_safety = orb_advertise(ORB_ID(actuator_safety), &safety); + } + return ret; } @@ -912,7 +1038,7 @@ PX4IO::io_get_status() io_handle_status(regs[0]); io_handle_alarms(regs[1]); - + /* only publish if battery has a valid minimum voltage */ if (regs[2] > 3300) { battery_status_s battery_status; @@ -946,6 +1072,7 @@ PX4IO::io_get_status() _to_battery = orb_advertise(ORB_ID(battery_status), &battery_status); } } + return ret; } @@ -1183,6 +1310,7 @@ PX4IO::io_reg_modify(uint8_t page, uint8_t offset, uint16_t clearbits, uint16_t uint16_t value; ret = io_reg_get(page, offset, &value, 1); + if (ret) return ret; value &= ~clearbits; @@ -1273,7 +1401,8 @@ PX4IO::print_status() uint16_t flags = io_reg_get(PX4IO_PAGE_STATUS, PX4IO_P_STATUS_FLAGS); printf("status 0x%04x%s%s%s%s%s%s%s%s%s%s%s%s\n", flags, - ((flags & PX4IO_P_STATUS_FLAGS_ARMED) ? " ARMED" : ""), + ((flags & PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED) ? " OUTPUTS_ARMED" : ""), + ((flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) ? " SAFETY_OFF" : " SAFETY_SAFE"), ((flags & PX4IO_P_STATUS_FLAGS_OVERRIDE) ? " OVERRIDE" : ""), ((flags & PX4IO_P_STATUS_FLAGS_RC_OK) ? " RC_OK" : " RC_FAIL"), ((flags & PX4IO_P_STATUS_FLAGS_RC_PPM) ? " PPM" : ""), @@ -1335,12 +1464,14 @@ PX4IO::print_status() /* setup and state */ printf("features 0x%04x\n", io_reg_get(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FEATURES)); uint16_t arming = io_reg_get(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_ARMING); - printf("arming 0x%04x%s%s%s%s\n", + printf("arming 0x%04x%s%s%s%s%s%s\n", arming, ((arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) ? " FMU_ARMED" : ""), ((arming & PX4IO_P_SETUP_ARMING_IO_ARM_OK) ? " IO_ARM_OK" : ""), ((arming & PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK) ? " MANUAL_OVERRIDE_OK" : ""), - ((arming & PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK) ? " INAIR_RESTART_OK" : "")); + ((arming & PX4IO_P_SETUP_ARMING_FAILSAFE_CUSTOM) ? " FAILSAFE_CUSTOM" : ""), + ((arming & PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK) ? " INAIR_RESTART_OK" : ""), + ((arming & PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE) ? " ALWAYS_PWM_ENABLE" : "")); printf("rates 0x%04x default %u alt %u relays 0x%04x\n", io_reg_get(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_PWM_RATES), io_reg_get(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_PWM_DEFAULTRATE), @@ -1367,7 +1498,10 @@ PX4IO::print_status() } printf("failsafe"); for (unsigned i = 0; i < _max_actuators; i++) - printf(" %u", io_reg_get(PX4IO_PAGE_FAILSAFE_PWM, i)); + printf(" %u\n", io_reg_get(PX4IO_PAGE_FAILSAFE_PWM, i)); + printf("\nidle values"); + for (unsigned i = 0; i < _max_actuators; i++) + printf(" %u", io_reg_get(PX4IO_PAGE_IDLE_PWM, i)); printf("\n"); } @@ -1634,6 +1768,11 @@ test(void) if (ioctl(fd, PWM_SERVO_GET_COUNT, (unsigned long)&servo_count)) err(1, "failed to get servo count"); + /* tell IO that its ok to disable its safety with the switch */ + ret = ioctl(fd, PWM_SERVO_SET_ARM_OK, 0); + if (ret != OK) + err(1, "PWM_SERVO_SET_ARM_OK"); + if (ioctl(fd, PWM_SERVO_ARM, 0)) err(1, "failed to arm servos"); @@ -1682,7 +1821,7 @@ test(void) /* Check if user wants to quit */ char c; if (read(console, &c, 1) == 1) { - if (c == 0x03 || c == 0x63) { + if (c == 0x03 || c == 0x63 || c == 'q') { warnx("User abort\n"); close(console); exit(0); @@ -1792,6 +1931,111 @@ px4io_main(int argc, char *argv[]) exit(0); } + if (!strcmp(argv[1], "min")) { + + if (argc < 3) { + errx(1, "min command needs at least one channel value (PWM)"); + } + + if (g_dev != nullptr) { + + /* set values for first 8 channels, fill unassigned channels with 900. */ + uint16_t min[8]; + + for (int i = 0; i < sizeof(min) / sizeof(min[0]); i++) + { + /* set channel to commanline argument or to 900 for non-provided channels */ + if (argc > i + 2) { + min[i] = atoi(argv[i+2]); + if (min[i] < 900 || min[i] > 1200) { + errx(1, "value out of range of 900 < value < 1200. Aborting."); + } + } else { + /* a zero value will the default */ + min[i] = 0; + } + } + + int ret = g_dev->set_min_values(min, sizeof(min) / sizeof(min[0])); + + if (ret != OK) + errx(ret, "failed setting min values"); + } else { + errx(1, "not loaded"); + } + exit(0); + } + + if (!strcmp(argv[1], "max")) { + + if (argc < 3) { + errx(1, "max command needs at least one channel value (PWM)"); + } + + if (g_dev != nullptr) { + + /* set values for first 8 channels, fill unassigned channels with 2100. */ + uint16_t max[8]; + + for (int i = 0; i < sizeof(max) / sizeof(max[0]); i++) + { + /* set channel to commanline argument or to 2100 for non-provided channels */ + if (argc > i + 2) { + max[i] = atoi(argv[i+2]); + if (max[i] < 1800 || max[i] > 2100) { + errx(1, "value out of range of 1800 < value < 2100. Aborting."); + } + } else { + /* a zero value will the default */ + max[i] = 0; + } + } + + int ret = g_dev->set_max_values(max, sizeof(max) / sizeof(max[0])); + + if (ret != OK) + errx(ret, "failed setting max values"); + } else { + errx(1, "not loaded"); + } + exit(0); + } + + if (!strcmp(argv[1], "idle")) { + + if (argc < 3) { + errx(1, "max command needs at least one channel value (PWM)"); + } + + if (g_dev != nullptr) { + + /* set values for first 8 channels, fill unassigned channels with 0. */ + uint16_t idle[8]; + + for (int i = 0; i < sizeof(idle) / sizeof(idle[0]); i++) + { + /* set channel to commanline argument or to 0 for non-provided channels */ + if (argc > i + 2) { + idle[i] = atoi(argv[i+2]); + if (idle[i] < 900 || idle[i] > 2100) { + errx(1, "value out of range of 900 < value < 2100. Aborting."); + } + } else { + /* a zero value will the default */ + idle[i] = 0; + } + } + + int ret = g_dev->set_idle_values(idle, sizeof(idle) / sizeof(idle[0])); + + if (ret != OK) + errx(ret, "failed setting idle values"); + } else { + errx(1, "not loaded"); + } + exit(0); + } + if (!strcmp(argv[1], "recovery")) { if (g_dev != nullptr) { @@ -1919,5 +2163,5 @@ px4io_main(int argc, char *argv[]) monitor(); out: - errx(1, "need a command, try 'start', 'stop', 'status', 'test', 'monitor', 'debug', 'recovery', 'limit', 'current', 'failsafe' or 'update'"); + errx(1, "need a command, try 'start', 'stop', 'status', 'test', 'monitor', 'debug', 'recovery', 'limit', 'current', 'failsafe', 'min, 'max', 'idle' or 'update'"); } diff --git a/src/drivers/stm32/tone_alarm/tone_alarm.cpp b/src/drivers/stm32/tone_alarm/tone_alarm.cpp index 167ef30a8..e1409a815 100644 --- a/src/drivers/stm32/tone_alarm/tone_alarm.cpp +++ b/src/drivers/stm32/tone_alarm/tone_alarm.cpp @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Copyright (C) 2013 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -241,6 +241,8 @@ private: static const unsigned _default_ntunes; static const uint8_t _note_tab[]; + unsigned _default_tune_number; // number of currently playing default tune (0 for none) + const char *_user_tune; const char *_tune; // current tune string @@ -456,6 +458,11 @@ const char * const ToneAlarm::_default_tunes[] = { "O1B8O2G+8E8B8G+8O3E8O2B8O3E8O2B8O3G+8E8B8" "O3G+8O4E4P8E16E16E8E8E8E8E4P8E16E4P8O2E16" "O2E2P64", + "MNT75L1O2G", //arming warning + "MBNT100a8", //battery warning slow + "MBNT255a8a8a8a8a8a8a8a8a8a8a8a8a8a8a8a8" + "a8a8a8a8a8a8a8a8a8a8a8a8a8a8a8a8" + "a8a8a8a8a8a8a8a8a8a8a8a8a8a8a8a8", //battery warning fast // XXX why is there a break before a repetition }; const unsigned ToneAlarm::_default_ntunes = sizeof(_default_tunes) / sizeof(_default_tunes[0]); @@ -471,6 +478,7 @@ extern "C" __EXPORT int tone_alarm_main(int argc, char *argv[]); ToneAlarm::ToneAlarm() : CDev("tone_alarm", "/dev/tone_alarm"), + _default_tune_number(0), _user_tune(nullptr), _tune(nullptr), _next(nullptr) @@ -803,8 +811,12 @@ tune_error: // stop (and potentially restart) the tune tune_end: stop_note(); - if (_repeat) + if (_repeat) { start_tune(_tune); + } else { + _tune = nullptr; + _default_tune_number = 0; + } return; } @@ -873,8 +885,17 @@ ToneAlarm::ioctl(file *filp, int cmd, unsigned long arg) _tune = nullptr; _next = nullptr; } else { - // play the selected tune - start_tune(_default_tunes[arg - 1]); + /* don't interrupt alarms unless they are repeated */ + if (_tune != nullptr && !_repeat) { + /* abort and let the current tune finish */ + result = -EBUSY; + } else if (_repeat && _default_tune_number == arg) { + /* requested repeating tune already playing */ + } else { + // play the selected tune + _default_tune_number = arg; + start_tune(_default_tunes[arg - 1]); + } } } else { result = -EINVAL; diff --git a/src/examples/fixedwing_control/main.c b/src/examples/fixedwing_control/main.c index 27888523b..ae33a3702 100644 --- a/src/examples/fixedwing_control/main.c +++ b/src/examples/fixedwing_control/main.c @@ -380,9 +380,10 @@ int fixedwing_control_thread_main(int argc, char *argv[]) /* control */ - /* if in auto mode, fly global position setpoint */ - if (vstatus.state_machine == SYSTEM_STATE_AUTO || - vstatus.state_machine == SYSTEM_STATE_STABILIZED) { +#warning fix this +#if 0 + if (vstatus.navigation_state == NAVIGATION_STATE_AUTO_ || + vstatus.navigation_state == NAVIGATION_STATE_STABILIZED) { /* simple heading control */ control_heading(&global_pos, &global_sp, &att, &att_sp); @@ -400,6 +401,7 @@ int fixedwing_control_thread_main(int argc, char *argv[]) /* set flaps to zero */ actuators.control[4] = 0.0f; + } else if (vstatus.navigation_state == NAVIGATION_STATE_MANUAL) { /* if in manual mode, decide between attitude stabilization (SAS) and full manual pass-through */ } else if (vstatus.state_machine == SYSTEM_STATE_MANUAL) { if (vstatus.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_SAS) { @@ -465,6 +467,7 @@ int fixedwing_control_thread_main(int argc, char *argv[]) } } } +#endif /* publish rates */ orb_publish(ORB_ID(vehicle_rates_setpoint), rates_pub, &rates_sp); diff --git a/src/examples/flow_position_control/flow_position_control_main.c b/src/examples/flow_position_control/flow_position_control_main.c index c177c8fd2..ecc133f63 100644 --- a/src/examples/flow_position_control/flow_position_control_main.c +++ b/src/examples/flow_position_control/flow_position_control_main.c @@ -55,7 +55,8 @@ #include <drivers/drv_hrt.h> #include <uORB/uORB.h> #include <uORB/topics/parameter_update.h> -#include <uORB/topics/vehicle_status.h> +#include <uORB/topics/actuator_safety.h> +#include <uORB/topics/vehicle_control_mode.h> #include <uORB/topics/vehicle_attitude.h> #include <uORB/topics/manual_control_setpoint.h> #include <uORB/topics/vehicle_local_position.h> @@ -158,7 +159,8 @@ flow_position_control_thread_main(int argc, char *argv[]) const float time_scale = powf(10.0f,-6.0f); /* structures */ - struct vehicle_status_s vstatus; + struct actuator_safety_s safety; + struct vehicle_control_mode_s control_mode; struct vehicle_attitude_s att; struct manual_control_setpoint_s manual; struct filtered_bottom_flow_s filtered_flow; @@ -169,7 +171,8 @@ flow_position_control_thread_main(int argc, char *argv[]) /* subscribe to attitude, motor setpoints and system state */ int parameter_update_sub = orb_subscribe(ORB_ID(parameter_update)); int vehicle_attitude_sub = orb_subscribe(ORB_ID(vehicle_attitude)); - int vehicle_status_sub = orb_subscribe(ORB_ID(vehicle_status)); + int safety_sub = orb_subscribe(ORB_ID(actuator_safety)); + int control_mode_sub = orb_subscribe(ORB_ID(vehicle_control_mode)); int manual_control_setpoint_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); int filtered_bottom_flow_sub = orb_subscribe(ORB_ID(filtered_bottom_flow)); int vehicle_local_position_sub = orb_subscribe(ORB_ID(vehicle_local_position)); @@ -258,7 +261,7 @@ flow_position_control_thread_main(int argc, char *argv[]) perf_begin(mc_loop_perf); /* get a local copy of the vehicle state */ - orb_copy(ORB_ID(vehicle_status), vehicle_status_sub, &vstatus); + orb_copy(ORB_ID(actuator_safety), safety_sub, &safety); /* get a local copy of manual setpoint */ orb_copy(ORB_ID(manual_control_setpoint), manual_control_setpoint_sub, &manual); /* get a local copy of attitude */ @@ -268,7 +271,7 @@ flow_position_control_thread_main(int argc, char *argv[]) /* get a local copy of local position */ orb_copy(ORB_ID(vehicle_local_position), vehicle_local_position_sub, &local_pos); - if (vstatus.state_machine == SYSTEM_STATE_AUTO) + if (control_mode.flag_control_velocity_enabled) { float manual_pitch = manual.pitch / params.rc_scale_pitch; // 0 to 1 float manual_roll = manual.roll / params.rc_scale_roll; // 0 to 1 @@ -490,7 +493,7 @@ flow_position_control_thread_main(int argc, char *argv[]) /* store actual height for speed estimation */ last_local_pos_z = local_pos.z; - speed_sp.thrust_sp = thrust_control; + speed_sp.thrust_sp = thrust_control; //manual.throttle; speed_sp.timestamp = hrt_absolute_time(); /* publish new speed setpoint */ @@ -527,7 +530,6 @@ flow_position_control_thread_main(int argc, char *argv[]) if(isfinite(manual.throttle)) speed_sp.thrust_sp = manual.throttle; } - /* measure in what intervals the controller runs */ perf_count(mc_interval_perf); perf_end(mc_loop_perf); @@ -576,7 +578,8 @@ flow_position_control_thread_main(int argc, char *argv[]) close(parameter_update_sub); close(vehicle_attitude_sub); close(vehicle_local_position_sub); - close(vehicle_status_sub); + close(safety_sub); + close(control_mode_sub); close(manual_control_setpoint_sub); close(speed_sp_pub); diff --git a/src/examples/flow_position_estimator/flow_position_estimator_main.c b/src/examples/flow_position_estimator/flow_position_estimator_main.c index c0b16d2e7..8f84307a7 100644 --- a/src/examples/flow_position_estimator/flow_position_estimator_main.c +++ b/src/examples/flow_position_estimator/flow_position_estimator_main.c @@ -56,7 +56,8 @@ #include <math.h> #include <uORB/uORB.h> #include <uORB/topics/parameter_update.h> -#include <uORB/topics/vehicle_status.h> +#include <uORB/topics/actuator_safety.h> +#include <uORB/topics/vehicle_control_mode.h> #include <uORB/topics/vehicle_attitude.h> #include <uORB/topics/vehicle_attitude_setpoint.h> #include <uORB/topics/vehicle_local_position.h> @@ -143,8 +144,8 @@ int flow_position_estimator_thread_main(int argc, char *argv[]) printf("[flow position estimator] starting\n"); /* rotation matrix for transformation of optical flow speed vectors */ - static const int8_t rotM_flow_sensor[3][3] = {{ 0, 1, 0 }, - { -1, 0, 0 }, + static const int8_t rotM_flow_sensor[3][3] = {{ 0, -1, 0 }, + { 1, 0, 0 }, { 0, 0, 1 }}; // 90deg rotated const float time_scale = powf(10.0f,-6.0f); static float speed[3] = {0.0f, 0.0f, 0.0f}; @@ -158,8 +159,10 @@ int flow_position_estimator_thread_main(int argc, char *argv[]) static float sonar_lp = 0.0f; /* subscribe to vehicle status, attitude, sensors and flow*/ - struct vehicle_status_s vstatus; - memset(&vstatus, 0, sizeof(vstatus)); + struct actuator_safety_s safety; + memset(&safety, 0, sizeof(safety)); + struct vehicle_control_mode_s control_mode; + memset(&control_mode, 0, sizeof(control_mode)); struct vehicle_attitude_s att; memset(&att, 0, sizeof(att)); struct vehicle_attitude_setpoint_s att_sp; @@ -170,8 +173,11 @@ int flow_position_estimator_thread_main(int argc, char *argv[]) /* subscribe to parameter changes */ int parameter_update_sub = orb_subscribe(ORB_ID(parameter_update)); - /* subscribe to vehicle status */ - int vehicle_status_sub = orb_subscribe(ORB_ID(vehicle_status)); + /* subscribe to safety topic */ + int safety_sub = orb_subscribe(ORB_ID(actuator_safety)); + + /* subscribe to safety topic */ + int control_mode_sub = orb_subscribe(ORB_ID(vehicle_control_mode)); /* subscribe to attitude */ int vehicle_attitude_sub = orb_subscribe(ORB_ID(vehicle_attitude)); @@ -218,6 +224,7 @@ int flow_position_estimator_thread_main(int argc, char *argv[]) while (!thread_should_exit) { + if (sensors_ready) { /*This runs at the rate of the sensors */ @@ -263,7 +270,8 @@ int flow_position_estimator_thread_main(int argc, char *argv[]) /* got flow, updating attitude and status as well */ orb_copy(ORB_ID(vehicle_attitude), vehicle_attitude_sub, &att); orb_copy(ORB_ID(vehicle_attitude_setpoint), vehicle_attitude_setpoint_sub, &att_sp); - orb_copy(ORB_ID(vehicle_status), vehicle_status_sub, &vstatus); + orb_copy(ORB_ID(actuator_safety), safety_sub, &safety); + orb_copy(ORB_ID(vehicle_control_mode), control_mode_sub, &control_mode); /* vehicle state estimation */ float sonar_new = flow.ground_distance_m; @@ -273,14 +281,15 @@ int flow_position_estimator_thread_main(int argc, char *argv[]) * -> accept sonar measurements after reaching calibration distance (values between 0.3m and 1.0m for some time) * -> minimum sonar value 0.3m */ + if (!vehicle_liftoff) { - if (vstatus.flag_system_armed && att_sp.thrust > params.minimum_liftoff_thrust && sonar_new > 0.3f && sonar_new < 1.0f) + if (safety.armed && att_sp.thrust > params.minimum_liftoff_thrust && sonar_new > 0.3f && sonar_new < 1.0f) vehicle_liftoff = true; } else { - if (!vstatus.flag_system_armed || (att_sp.thrust < params.minimum_liftoff_thrust && sonar_new <= 0.3f)) + if (!safety.armed || (att_sp.thrust < params.minimum_liftoff_thrust && sonar_new <= 0.3f)) vehicle_liftoff = false; } @@ -347,7 +356,7 @@ int flow_position_estimator_thread_main(int argc, char *argv[]) } /* filtering ground distance */ - if (!vehicle_liftoff || !vstatus.flag_system_armed) + if (!vehicle_liftoff || !safety.armed) { /* not possible to fly */ sonar_valid = false; @@ -444,7 +453,8 @@ int flow_position_estimator_thread_main(int argc, char *argv[]) close(vehicle_attitude_setpoint_sub); close(vehicle_attitude_sub); - close(vehicle_status_sub); + close(safety_sub); + close(control_mode_sub); close(parameter_update_sub); close(optical_flow_sub); diff --git a/src/examples/flow_speed_control/flow_speed_control_main.c b/src/examples/flow_speed_control/flow_speed_control_main.c index 9648728c8..4f60e34f2 100644 --- a/src/examples/flow_speed_control/flow_speed_control_main.c +++ b/src/examples/flow_speed_control/flow_speed_control_main.c @@ -55,7 +55,8 @@ #include <drivers/drv_hrt.h> #include <uORB/uORB.h> #include <uORB/topics/parameter_update.h> -#include <uORB/topics/vehicle_status.h> +#include <uORB/topics/actuator_safety.h> +#include <uORB/topics/vehicle_control_mode.h> #include <uORB/topics/vehicle_attitude.h> #include <uORB/topics/vehicle_attitude_setpoint.h> #include <uORB/topics/vehicle_bodyframe_speed_setpoint.h> @@ -155,7 +156,8 @@ flow_speed_control_thread_main(int argc, char *argv[]) uint32_t counter = 0; /* structures */ - struct vehicle_status_s vstatus; + struct actuator_safety_s safety; + struct vehicle_control_mode_s control_mode; struct filtered_bottom_flow_s filtered_flow; struct vehicle_bodyframe_speed_setpoint_s speed_sp; @@ -164,7 +166,8 @@ flow_speed_control_thread_main(int argc, char *argv[]) /* subscribe to attitude, motor setpoints and system state */ int parameter_update_sub = orb_subscribe(ORB_ID(parameter_update)); int vehicle_attitude_sub = orb_subscribe(ORB_ID(vehicle_attitude)); - int vehicle_status_sub = orb_subscribe(ORB_ID(vehicle_status)); + int safety_sub = orb_subscribe(ORB_ID(actuator_safety)); + int control_mode_sub = orb_subscribe(ORB_ID(vehicle_control_mode)); int filtered_bottom_flow_sub = orb_subscribe(ORB_ID(filtered_bottom_flow)); int vehicle_bodyframe_speed_setpoint_sub = orb_subscribe(ORB_ID(vehicle_bodyframe_speed_setpoint)); @@ -226,14 +229,16 @@ flow_speed_control_thread_main(int argc, char *argv[]) { perf_begin(mc_loop_perf); - /* get a local copy of the vehicle state */ - orb_copy(ORB_ID(vehicle_status), vehicle_status_sub, &vstatus); + /* get a local copy of the safety topic */ + orb_copy(ORB_ID(actuator_safety), safety_sub, &safety); + /* get a local copy of the control mode */ + orb_copy(ORB_ID(vehicle_control_mode), control_mode_sub, &control_mode); /* get a local copy of filtered bottom flow */ orb_copy(ORB_ID(filtered_bottom_flow), filtered_bottom_flow_sub, &filtered_flow); /* get a local copy of bodyframe speed setpoint */ orb_copy(ORB_ID(vehicle_bodyframe_speed_setpoint), vehicle_bodyframe_speed_setpoint_sub, &speed_sp); - if (vstatus.state_machine == SYSTEM_STATE_AUTO) + if (control_mode.flag_control_velocity_enabled) { /* calc new roll/pitch */ float pitch_body = -(speed_sp.vx - filtered_flow.vx) * params.speed_p; @@ -350,7 +355,8 @@ flow_speed_control_thread_main(int argc, char *argv[]) close(vehicle_attitude_sub); close(vehicle_bodyframe_speed_setpoint_sub); close(filtered_bottom_flow_sub); - close(vehicle_status_sub); + close(safety_sub); + close(control_mode_sub); close(att_sp_pub); perf_print_counter(mc_loop_perf); diff --git a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c index 7d3812abd..52dac652b 100755 --- a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c +++ b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c @@ -44,42 +44,42 @@ /* Extended Kalman Filter covariances */ /* gyro process noise */ -PARAM_DEFINE_FLOAT(EKF_ATT_V2_Q0, 1e-4f); -PARAM_DEFINE_FLOAT(EKF_ATT_V2_Q1, 0.08f); -PARAM_DEFINE_FLOAT(EKF_ATT_V2_Q2, 0.009f); +PARAM_DEFINE_FLOAT(EKF_ATT_V3_Q0, 1e-4f); +PARAM_DEFINE_FLOAT(EKF_ATT_V3_Q1, 0.08f); +PARAM_DEFINE_FLOAT(EKF_ATT_V3_Q2, 0.009f); /* gyro offsets process noise */ -PARAM_DEFINE_FLOAT(EKF_ATT_V2_Q3, 0.005f); -PARAM_DEFINE_FLOAT(EKF_ATT_V2_Q4, 0.0f); +PARAM_DEFINE_FLOAT(EKF_ATT_V3_Q3, 0.005f); +PARAM_DEFINE_FLOAT(EKF_ATT_V3_Q4, 0.0f); /* gyro measurement noise */ -PARAM_DEFINE_FLOAT(EKF_ATT_V2_R0, 0.0008f); -PARAM_DEFINE_FLOAT(EKF_ATT_V2_R1, 0.8f); -PARAM_DEFINE_FLOAT(EKF_ATT_V2_R2, 1.0f); +PARAM_DEFINE_FLOAT(EKF_ATT_V3_R0, 0.0008f); +PARAM_DEFINE_FLOAT(EKF_ATT_V3_R1, 10000.0f); +PARAM_DEFINE_FLOAT(EKF_ATT_V3_R2, 1.0f); /* accelerometer measurement noise */ -PARAM_DEFINE_FLOAT(EKF_ATT_V2_R3, 0.0f); +PARAM_DEFINE_FLOAT(EKF_ATT_V3_R3, 0.0f); /* offsets in roll, pitch and yaw of sensor plane and body */ -PARAM_DEFINE_FLOAT(ATT_ROLL_OFFS, 0.0f); -PARAM_DEFINE_FLOAT(ATT_PITCH_OFFS, 0.0f); -PARAM_DEFINE_FLOAT(ATT_YAW_OFFS, 0.0f); +PARAM_DEFINE_FLOAT(ATT_ROLL_OFF3, 0.0f); +PARAM_DEFINE_FLOAT(ATT_PITCH_OFF3, 0.0f); +PARAM_DEFINE_FLOAT(ATT_YAW_OFF3, 0.0f); int parameters_init(struct attitude_estimator_ekf_param_handles *h) { /* PID parameters */ - h->q0 = param_find("EKF_ATT_V2_Q0"); - h->q1 = param_find("EKF_ATT_V2_Q1"); - h->q2 = param_find("EKF_ATT_V2_Q2"); - h->q3 = param_find("EKF_ATT_V2_Q3"); - h->q4 = param_find("EKF_ATT_V2_Q4"); + h->q0 = param_find("EKF_ATT_V3_Q0"); + h->q1 = param_find("EKF_ATT_V3_Q1"); + h->q2 = param_find("EKF_ATT_V3_Q2"); + h->q3 = param_find("EKF_ATT_V3_Q3"); + h->q4 = param_find("EKF_ATT_V3_Q4"); - h->r0 = param_find("EKF_ATT_V2_R0"); - h->r1 = param_find("EKF_ATT_V2_R1"); - h->r2 = param_find("EKF_ATT_V2_R2"); - h->r3 = param_find("EKF_ATT_V2_R3"); + h->r0 = param_find("EKF_ATT_V3_R0"); + h->r1 = param_find("EKF_ATT_V3_R1"); + h->r2 = param_find("EKF_ATT_V3_R2"); + h->r3 = param_find("EKF_ATT_V3_R3"); - h->roll_off = param_find("ATT_ROLL_OFFS"); - h->pitch_off = param_find("ATT_PITCH_OFFS"); - h->yaw_off = param_find("ATT_YAW_OFFS"); + h->roll_off = param_find("ATT_ROLL_OFF3"); + h->pitch_off = param_find("ATT_PITCH_OFF3"); + h->yaw_off = param_find("ATT_YAW_OFF3"); return OK; } diff --git a/src/modules/commander/accelerometer_calibration.c b/src/modules/commander/accelerometer_calibration.c index 48a36ac26..50234a45e 100644 --- a/src/modules/commander/accelerometer_calibration.c +++ b/src/modules/commander/accelerometer_calibration.c @@ -104,32 +104,39 @@ */ #include "accelerometer_calibration.h" +#include "commander_helper.h" +#include <unistd.h> +#include <stdio.h> #include <poll.h> +#include <fcntl.h> +#include <sys/prctl.h> +#include <math.h> +#include <string.h> + + #include <drivers/drv_hrt.h> #include <uORB/topics/sensor_combined.h> #include <drivers/drv_accel.h> #include <systemlib/conversions.h> +#include <systemlib/param/param.h> +#include <systemlib/err.h> #include <mavlink/mavlink_log.h> -void do_accel_calibration(int status_pub, struct vehicle_status_s *status, int mavlink_fd); -int do_accel_calibration_mesurements(int mavlink_fd, float accel_offs[3], float accel_scale[3]); +int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float accel_scale[3]); int detect_orientation(int mavlink_fd, int sub_sensor_combined); int read_accelerometer_avg(int sensor_combined_sub, float accel_avg[3], int samples_num); int mat_invert3(float src[3][3], float dst[3][3]); int calculate_calibration_values(float accel_ref[6][3], float accel_T[3][3], float accel_offs[3], float g); -void do_accel_calibration(int status_pub, struct vehicle_status_s *status, int mavlink_fd) { +void do_accel_calibration(int mavlink_fd) { /* announce change */ mavlink_log_info(mavlink_fd, "accel calibration started"); - /* set to accel calibration mode */ - status->flag_preflight_accel_calibration = true; - state_machine_publish(status_pub, status, mavlink_fd); /* measure and calculate offsets & scales */ float accel_offs[3]; float accel_scale[3]; - int res = do_accel_calibration_mesurements(mavlink_fd, accel_offs, accel_scale); + int res = do_accel_calibration_measurements(mavlink_fd, accel_offs, accel_scale); if (res == OK) { /* measurements complete successfully, set parameters */ @@ -165,24 +172,17 @@ void do_accel_calibration(int status_pub, struct vehicle_status_s *status, int m } mavlink_log_info(mavlink_fd, "accel calibration done"); - tune_confirm(); - sleep(2); - tune_confirm(); - sleep(2); - /* third beep by cal end routine */ + tune_positive(); } else { /* measurements error */ mavlink_log_info(mavlink_fd, "accel calibration aborted"); - tune_error(); - sleep(2); + tune_negative(); } /* exit accel calibration mode */ - status->flag_preflight_accel_calibration = false; - state_machine_publish(status_pub, status, mavlink_fd); } -int do_accel_calibration_mesurements(int mavlink_fd, float accel_offs[3], float accel_scale[3]) { +int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float accel_scale[3]) { const int samples_num = 2500; float accel_ref[6][3]; bool data_collected[6] = { false, false, false, false, false, false }; @@ -232,7 +232,7 @@ int do_accel_calibration_mesurements(int mavlink_fd, float accel_offs[3], float str_ptr = sprintf(str, "meas result for %s: [ %.2f %.2f %.2f ]", orientation_strs[orient], accel_ref[orient][0], accel_ref[orient][1], accel_ref[orient][2]); mavlink_log_info(mavlink_fd, str); data_collected[orient] = true; - tune_confirm(); + tune_neutral(); } close(sensor_combined_sub); @@ -399,7 +399,7 @@ int mat_invert3(float src[3][3], float dst[3][3]) { float det = src[0][0] * (src[1][1] * src[2][2] - src[1][2] * src[2][1]) - src[0][1] * (src[1][0] * src[2][2] - src[1][2] * src[2][0]) + src[0][2] * (src[1][0] * src[2][1] - src[1][1] * src[2][0]); - if (det == 0.0) + if (det == 0.0f) return ERROR; // Singular matrix dst[0][0] = (src[1][1] * src[2][2] - src[1][2] * src[2][1]) / det; diff --git a/src/modules/commander/accelerometer_calibration.h b/src/modules/commander/accelerometer_calibration.h index f93a867ba..3275d9461 100644 --- a/src/modules/commander/accelerometer_calibration.h +++ b/src/modules/commander/accelerometer_calibration.h @@ -44,8 +44,7 @@ #define ACCELEROMETER_CALIBRATION_H_ #include <stdint.h> -#include <uORB/topics/vehicle_status.h> -void do_accel_calibration(int status_pub, struct vehicle_status_s *status, int mavlink_fd); +void do_accel_calibration(int mavlink_fd); #endif /* ACCELEROMETER_CALIBRATION_H_ */ diff --git a/src/modules/commander/airspeed_calibration.c b/src/modules/commander/airspeed_calibration.c new file mode 100644 index 000000000..feaf11aee --- /dev/null +++ b/src/modules/commander/airspeed_calibration.c @@ -0,0 +1,111 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file airspeed_calibration.c + * Airspeed sensor calibration routine + */ + +#include "airspeed_calibration.h" +#include "commander_helper.h" + +#include <stdio.h> +#include <poll.h> +#include <math.h> +#include <drivers/drv_hrt.h> +#include <uORB/topics/sensor_combined.h> +#include <uORB/topics/differential_pressure.h> +#include <mavlink/mavlink_log.h> +#include <systemlib/param/param.h> +#include <systemlib/err.h> + +void do_airspeed_calibration(int mavlink_fd) +{ + /* give directions */ + mavlink_log_info(mavlink_fd, "airspeed calibration starting, keep it still"); + + const int calibration_count = 2500; + + int diff_pres_sub = orb_subscribe(ORB_ID(differential_pressure)); + struct differential_pressure_s diff_pres; + + int calibration_counter = 0; + float diff_pres_offset = 0.0f; + + while (calibration_counter < calibration_count) { + + /* wait blocking for new data */ + struct pollfd fds[1] = { { .fd = diff_pres_sub, .events = POLLIN } }; + + int poll_ret = poll(fds, 1, 1000); + + if (poll_ret) { + orb_copy(ORB_ID(differential_pressure), diff_pres_sub, &diff_pres); + diff_pres_offset += diff_pres.differential_pressure_pa; + calibration_counter++; + + } else if (poll_ret == 0) { + /* any poll failure for 1s is a reason to abort */ + mavlink_log_info(mavlink_fd, "airspeed calibration aborted"); + return; + } + } + + diff_pres_offset = diff_pres_offset / calibration_count; + + if (isfinite(diff_pres_offset)) { + + if (param_set(param_find("SENS_DPRES_OFF"), &(diff_pres_offset))) { + mavlink_log_critical(mavlink_fd, "Setting offs failed!"); + } + + /* auto-save to EEPROM */ + int save_ret = param_save_default(); + + if (save_ret != 0) { + warn("WARNING: auto-save of params to storage failed"); + } + + //char buf[50]; + //sprintf(buf, "[cmd] accel cal: x:%8.4f y:%8.4f z:%8.4f\n", (double)accel_offset[0], (double)accel_offset[1], (double)accel_offset[2]); + //mavlink_log_info(mavlink_fd, buf); + mavlink_log_info(mavlink_fd, "airspeed calibration done"); + + tune_positive(); + + } else { + mavlink_log_info(mavlink_fd, "airspeed calibration FAILED (NaN)"); + } + + close(diff_pres_sub); +} diff --git a/src/modules/commander/airspeed_calibration.h b/src/modules/commander/airspeed_calibration.h new file mode 100644 index 000000000..92f5651ec --- /dev/null +++ b/src/modules/commander/airspeed_calibration.h @@ -0,0 +1,46 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file gyro_calibration.h + * Airspeed sensor calibration routine + */ + +#ifndef AIRSPEED_CALIBRATION_H_ +#define AIRSPEED_CALIBRATION_H_ + +#include <stdint.h> + +void do_airspeed_calibration(int mavlink_fd); + +#endif /* AIRSPEED_CALIBRATION_H_ */
\ No newline at end of file diff --git a/src/modules/commander/baro_calibration.c b/src/modules/commander/baro_calibration.c new file mode 100644 index 000000000..a70594794 --- /dev/null +++ b/src/modules/commander/baro_calibration.c @@ -0,0 +1,54 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file baro_calibration.c + * Barometer calibration routine + */ + +#include "baro_calibration.h" + +#include <poll.h> +#include <math.h> +#include <fcntl.h> +#include <drivers/drv_hrt.h> +#include <uORB/topics/sensor_combined.h> +#include <drivers/drv_baro.h> +#include <mavlink/mavlink_log.h> +#include <systemlib/param/param.h> + +void do_baro_calibration(int mavlink_fd) +{ + // TODO implement this + return; +} diff --git a/src/modules/commander/baro_calibration.h b/src/modules/commander/baro_calibration.h new file mode 100644 index 000000000..ac0f4be36 --- /dev/null +++ b/src/modules/commander/baro_calibration.h @@ -0,0 +1,46 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file mag_calibration.h + * Barometer calibration routine + */ + +#ifndef BARO_CALIBRATION_H_ +#define BARO_CALIBRATION_H_ + +#include <stdint.h> + +void do_baro_calibration(int mavlink_fd); + +#endif /* BARO_CALIBRATION_H_ */
\ No newline at end of file diff --git a/src/modules/commander/calibration_routines.c b/src/modules/commander/calibration_routines.c index a26938637..799cd4269 100644 --- a/src/modules/commander/calibration_routines.c +++ b/src/modules/commander/calibration_routines.c @@ -217,3 +217,4 @@ int sphere_fit_least_squares(const float x[], const float y[], const float z[], return 0; } + diff --git a/src/modules/commander/commander.c b/src/modules/commander/commander.c index 67f053e22..9d52d4f1c 100644 --- a/src/modules/commander/commander.c +++ b/src/modules/commander/commander.c @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Copyright (C) 2013 PX4 Development Team. All rights reserved. * Author: Petri Tanskanen <petri.tanskanen@inf.ethz.ch> * Lorenz Meier <lm@inf.ethz.ch> * Thomas Gubler <thomasgubler@student.ethz.ch> @@ -60,13 +60,9 @@ #include <debug.h> #include <sys/prctl.h> #include <string.h> -#include <drivers/drv_led.h> -#include <drivers/drv_hrt.h> -#include <drivers/drv_tone_alarm.h> -#include "state_machine_helper.h" -#include "systemlib/systemlib.h" #include <math.h> #include <poll.h> + #include <uORB/uORB.h> #include <uORB/topics/sensor_combined.h> #include <uORB/topics/battery_status.h> @@ -77,24 +73,33 @@ #include <uORB/topics/vehicle_local_position.h> #include <uORB/topics/vehicle_gps_position.h> #include <uORB/topics/vehicle_command.h> +#include <uORB/topics/vehicle_control_mode.h> #include <uORB/topics/subsystem_info.h> #include <uORB/topics/actuator_controls.h> +#include <uORB/topics/actuator_safety.h> #include <uORB/topics/parameter_update.h> #include <uORB/topics/differential_pressure.h> #include <mavlink/mavlink_log.h> +#include <drivers/drv_led.h> +#include <drivers/drv_hrt.h> +#include <drivers/drv_tone_alarm.h> + +#include <mavlink/mavlink_log.h> #include <systemlib/param/param.h> #include <systemlib/systemlib.h> #include <systemlib/err.h> +#include <systemlib/cpuload.h> -/* XXX MOVE CALIBRATION TO SENSORS APP THREAD */ -#include <drivers/drv_accel.h> -#include <drivers/drv_gyro.h> -#include <drivers/drv_mag.h> -#include <drivers/drv_baro.h> - +#include "commander_helper.h" +#include "state_machine_helper.h" #include "calibration_routines.h" #include "accelerometer_calibration.h" +#include "gyro_calibration.h" +#include "mag_calibration.h" +#include "baro_calibration.h" +#include "rc_calibration.h" +#include "airspeed_calibration.h" PARAM_DEFINE_INT32(SYS_FAILSAVE_LL, 0); /**< Go into low-level failsafe after 0 ms */ //PARAM_DEFINE_INT32(SYS_FAILSAVE_HL, 0); /**< Go into high-level failsafe after 0 ms */ @@ -102,9 +107,12 @@ PARAM_DEFINE_FLOAT(TRIM_ROLL, 0.0f); PARAM_DEFINE_FLOAT(TRIM_PITCH, 0.0f); PARAM_DEFINE_FLOAT(TRIM_YAW, 0.0f); -#include <systemlib/cpuload.h> + extern struct system_load_s system_load; +#define LOW_VOLTAGE_BATTERY_HYSTERESIS_TIME_MS 1000.0f +#define CRITICAL_VOLTAGE_BATTERY_HYSTERESIS_TIME_MS 100.0f + /* Decouple update interval and hysteris counters, all depends on intervals */ #define COMMANDER_MONITORING_INTERVAL 50000 #define COMMANDER_MONITORING_LOOPSPERMSEC (1/(COMMANDER_MONITORING_INTERVAL/1000.0f)) @@ -121,25 +129,38 @@ extern struct system_load_s system_load; #define GPS_QUALITY_GOOD_HYSTERIS_TIME_MS 5000 #define GPS_QUALITY_GOOD_COUNTER_LIMIT (GPS_QUALITY_GOOD_HYSTERIS_TIME_MS*COMMANDER_MONITORING_LOOPSPERMSEC) +#define LOCAL_POSITION_TIMEOUT 1000000 /**< consider the local position estimate invalid after 1s */ + /* File descriptors */ static int leds; -static int buzzer; static int mavlink_fd; -static bool commander_initialized = false; -static struct vehicle_status_s current_status; /**< Main state machine */ -static orb_advert_t stat_pub; - -// static uint16_t nofix_counter = 0; -// static uint16_t gotfix_counter = 0; - -static unsigned int failsafe_lowlevel_timeout_ms; +/* flags */ +static bool commander_initialized = false; static bool thread_should_exit = false; /**< daemon exit flag */ static bool thread_running = false; /**< daemon status flag */ static int daemon_task; /**< Handle of daemon task / thread */ +/* timout until lowlevel failsafe */ +static unsigned int failsafe_lowlevel_timeout_ms; + +/* tasks waiting for low prio thread */ +enum { + LOW_PRIO_TASK_NONE = 0, + LOW_PRIO_TASK_PARAM_SAVE, + LOW_PRIO_TASK_PARAM_LOAD, + LOW_PRIO_TASK_GYRO_CALIBRATION, + LOW_PRIO_TASK_MAG_CALIBRATION, + LOW_PRIO_TASK_ALTITUDE_CALIBRATION, + LOW_PRIO_TASK_RC_CALIBRATION, + LOW_PRIO_TASK_ACCEL_CALIBRATION, + LOW_PRIO_TASK_AIRSPEED_CALIBRATION +} low_prio_task; + + /* pthread loops */ -static void *orb_receive_loop(void *arg); +void *orb_receive_loop(void *arg); +void *commander_low_prio_loop(void *arg); __EXPORT int commander_main(int argc, char *argv[]); @@ -148,26 +169,24 @@ __EXPORT int commander_main(int argc, char *argv[]); */ int commander_thread_main(int argc, char *argv[]); -static int buzzer_init(void); -static void buzzer_deinit(void); -static int led_init(void); -static void led_deinit(void); -static int led_toggle(int led); -static int led_on(int led); -static int led_off(int led); -static void do_gyro_calibration(int status_pub, struct vehicle_status_s *status); -static void do_mag_calibration(int status_pub, struct vehicle_status_s *status); -static void do_rc_calibration(int status_pub, struct vehicle_status_s *status); -static void handle_command(int status_pub, struct vehicle_status_s *current_status, struct vehicle_command_s *cmd); +int led_init(void); +void led_deinit(void); +int led_toggle(int led); +int led_on(int led); +int led_off(int led); +void do_reboot(void); -int trigger_audio_alarm(uint8_t old_mode, uint8_t old_state, uint8_t new_mode, uint8_t new_state); + +void handle_command(int status_pub, struct vehicle_status_s *current_status, struct vehicle_command_s *cmd, int safety_pub, struct actuator_safety_s *safety); + +// int trigger_audio_alarm(uint8_t old_mode, uint8_t old_state, uint8_t new_mode, uint8_t new_state); /** * Print the correct usage. */ -static void usage(const char *reason); +void usage(const char *reason); /** * Sort calibration values. @@ -179,25 +198,8 @@ static void usage(const char *reason); */ // static void cal_bsort(float a[], int n); -static int buzzer_init() -{ - buzzer = open("/dev/tone_alarm", O_WRONLY); - - if (buzzer < 0) { - warnx("Buzzer: open fail\n"); - return ERROR; - } - - return 0; -} - -static void buzzer_deinit() -{ - close(buzzer); -} - -static int led_init() +int led_init() { leds = open(LED_DEVICE_PATH, 0); @@ -214,12 +216,12 @@ static int led_init() return 0; } -static void led_deinit() +void led_deinit() { close(leds); } -static int led_toggle(int led) +int led_toggle(int led) { static int last_blue = LED_ON; static int last_amber = LED_ON; @@ -231,830 +233,288 @@ static int led_toggle(int led) return ioctl(leds, ((led == LED_BLUE) ? last_blue : last_amber), led); } -static int led_on(int led) +int led_on(int led) { return ioctl(leds, LED_ON, led); } -static int led_off(int led) +int led_off(int led) { return ioctl(leds, LED_OFF, led); } -enum AUDIO_PATTERN { - AUDIO_PATTERN_ERROR = 2, - AUDIO_PATTERN_NOTIFY_POSITIVE = 3, - AUDIO_PATTERN_NOTIFY_NEUTRAL = 4, - AUDIO_PATTERN_NOTIFY_NEGATIVE = 5, - AUDIO_PATTERN_NOTIFY_CHARGE = 6 -}; - -int trigger_audio_alarm(uint8_t old_mode, uint8_t old_state, uint8_t new_mode, uint8_t new_state) -{ - - /* Trigger alarm if going into any error state */ - if (((new_state == SYSTEM_STATE_GROUND_ERROR) && (old_state != SYSTEM_STATE_GROUND_ERROR)) || - ((new_state == SYSTEM_STATE_MISSION_ABORT) && (old_state != SYSTEM_STATE_MISSION_ABORT))) { - ioctl(buzzer, TONE_SET_ALARM, 0); - ioctl(buzzer, TONE_SET_ALARM, AUDIO_PATTERN_ERROR); - } - - /* Trigger neutral on arming / disarming */ - if (((new_state == SYSTEM_STATE_GROUND_READY) && (old_state != SYSTEM_STATE_GROUND_READY))) { - ioctl(buzzer, TONE_SET_ALARM, 0); - ioctl(buzzer, TONE_SET_ALARM, AUDIO_PATTERN_NOTIFY_NEUTRAL); - } - - /* Trigger Tetris on being bored */ - - return 0; -} - -void tune_confirm(void) -{ - ioctl(buzzer, TONE_SET_ALARM, 3); -} - -void tune_error(void) -{ - ioctl(buzzer, TONE_SET_ALARM, 4); -} - -void do_rc_calibration(int status_pub, struct vehicle_status_s *status) -{ - if (current_status.offboard_control_signal_lost) { - mavlink_log_critical(mavlink_fd, "TRIM CAL: ABORT. No RC signal."); - return; - } - - int sub_man = orb_subscribe(ORB_ID(manual_control_setpoint)); - struct manual_control_setpoint_s sp; - orb_copy(ORB_ID(manual_control_setpoint), sub_man, &sp); - - /* set parameters */ - - float p = sp.roll; - param_set(param_find("TRIM_ROLL"), &p); - p = sp.pitch; - param_set(param_find("TRIM_PITCH"), &p); - p = sp.yaw; - param_set(param_find("TRIM_YAW"), &p); - - /* store to permanent storage */ - /* auto-save to EEPROM */ - int save_ret = param_save_default(); - - if (save_ret != 0) { - mavlink_log_critical(mavlink_fd, "TRIM CAL: WARN: auto-save of params failed"); - } - - mavlink_log_info(mavlink_fd, "trim calibration done"); -} - -void do_mag_calibration(int status_pub, struct vehicle_status_s *status) -{ - - /* set to mag calibration mode */ - status->flag_preflight_mag_calibration = true; - state_machine_publish(status_pub, status, mavlink_fd); - - int sub_mag = orb_subscribe(ORB_ID(sensor_mag)); - struct mag_report mag; - - /* 45 seconds */ - uint64_t calibration_interval = 45 * 1000 * 1000; - - /* maximum 2000 values */ - const unsigned int calibration_maxcount = 500; - unsigned int calibration_counter = 0; - - /* limit update rate to get equally spaced measurements over time (in ms) */ - orb_set_interval(sub_mag, (calibration_interval / 1000) / calibration_maxcount); - - // XXX old cal - // * FLT_MIN is not the most negative float number, - // * but the smallest number by magnitude float can - // * represent. Use -FLT_MAX to initialize the most - // * negative number - - // float mag_max[3] = {-FLT_MAX, -FLT_MAX, -FLT_MAX}; - // float mag_min[3] = {FLT_MAX, FLT_MAX, FLT_MAX}; - - int fd = open(MAG_DEVICE_PATH, O_RDONLY); - - /* erase old calibration */ - struct mag_scale mscale_null = { - 0.0f, - 1.0f, - 0.0f, - 1.0f, - 0.0f, - 1.0f, - }; - - if (OK != ioctl(fd, MAGIOCSSCALE, (long unsigned int)&mscale_null)) { - warn("WARNING: failed to set scale / offsets for mag"); - mavlink_log_info(mavlink_fd, "failed to set scale / offsets for mag"); - } - - /* calibrate range */ - if (OK != ioctl(fd, MAGIOCCALIBRATE, fd)) { - warnx("failed to calibrate scale"); - } - - close(fd); - - /* calibrate offsets */ - - // uint64_t calibration_start = hrt_absolute_time(); - - uint64_t axis_deadline = hrt_absolute_time(); - uint64_t calibration_deadline = hrt_absolute_time() + calibration_interval; - - const char axislabels[3] = { 'X', 'Y', 'Z'}; - int axis_index = -1; - - float *x = (float *)malloc(sizeof(float) * calibration_maxcount); - float *y = (float *)malloc(sizeof(float) * calibration_maxcount); - float *z = (float *)malloc(sizeof(float) * calibration_maxcount); - - if (x == NULL || y == NULL || z == NULL) { - warnx("mag cal failed: out of memory"); - mavlink_log_info(mavlink_fd, "mag cal failed: out of memory"); - warnx("x:%p y:%p z:%p\n", x, y, z); - return; - } - - tune_confirm(); - sleep(2); - tune_confirm(); - - while (hrt_absolute_time() < calibration_deadline && - calibration_counter < calibration_maxcount) { - - /* wait blocking for new data */ - struct pollfd fds[1] = { { .fd = sub_mag, .events = POLLIN } }; - - /* user guidance */ - if (hrt_absolute_time() >= axis_deadline && - axis_index < 3) { - - axis_index++; - - char buf[50]; - sprintf(buf, "Please rotate around %c", axislabels[axis_index]); - mavlink_log_info(mavlink_fd, buf); - tune_confirm(); - - axis_deadline += calibration_interval / 3; - } - - if (!(axis_index < 3)) { - break; - } - - // int axis_left = (int64_t)axis_deadline - (int64_t)hrt_absolute_time(); - - // if ((axis_left / 1000) == 0 && axis_left > 0) { - // char buf[50]; - // sprintf(buf, "[cmd] %d seconds left for axis %c", axis_left, axislabels[axis_index]); - // mavlink_log_info(mavlink_fd, buf); - // } - - int poll_ret = poll(fds, 1, 1000); - - if (poll_ret) { - orb_copy(ORB_ID(sensor_mag), sub_mag, &mag); - - x[calibration_counter] = mag.x; - y[calibration_counter] = mag.y; - z[calibration_counter] = mag.z; - - /* get min/max values */ - - // if (mag.x < mag_min[0]) { - // mag_min[0] = mag.x; - // } - // else if (mag.x > mag_max[0]) { - // mag_max[0] = mag.x; - // } - - // if (raw.magnetometer_ga[1] < mag_min[1]) { - // mag_min[1] = raw.magnetometer_ga[1]; - // } - // else if (raw.magnetometer_ga[1] > mag_max[1]) { - // mag_max[1] = raw.magnetometer_ga[1]; - // } - - // if (raw.magnetometer_ga[2] < mag_min[2]) { - // mag_min[2] = raw.magnetometer_ga[2]; - // } - // else if (raw.magnetometer_ga[2] > mag_max[2]) { - // mag_max[2] = raw.magnetometer_ga[2]; - // } - - calibration_counter++; - - } else if (poll_ret == 0) { - /* any poll failure for 1s is a reason to abort */ - mavlink_log_info(mavlink_fd, "mag cal canceled (timed out)"); - break; - } - } - - float sphere_x; - float sphere_y; - float sphere_z; - float sphere_radius; - - sphere_fit_least_squares(x, y, z, calibration_counter, 100, 0.0f, &sphere_x, &sphere_y, &sphere_z, &sphere_radius); - - free(x); - free(y); - free(z); - - if (isfinite(sphere_x) && isfinite(sphere_y) && isfinite(sphere_z)) { - - fd = open(MAG_DEVICE_PATH, 0); - - struct mag_scale mscale; - - if (OK != ioctl(fd, MAGIOCGSCALE, (long unsigned int)&mscale)) - warn("WARNING: failed to get scale / offsets for mag"); - - mscale.x_offset = sphere_x; - mscale.y_offset = sphere_y; - mscale.z_offset = sphere_z; - - if (OK != ioctl(fd, MAGIOCSSCALE, (long unsigned int)&mscale)) - warn("WARNING: failed to set scale / offsets for mag"); - - close(fd); - - /* announce and set new offset */ - - if (param_set(param_find("SENS_MAG_XOFF"), &(mscale.x_offset))) { - warnx("Setting X mag offset failed!\n"); - } - - if (param_set(param_find("SENS_MAG_YOFF"), &(mscale.y_offset))) { - warnx("Setting Y mag offset failed!\n"); - } - - if (param_set(param_find("SENS_MAG_ZOFF"), &(mscale.z_offset))) { - warnx("Setting Z mag offset failed!\n"); - } - - if (param_set(param_find("SENS_MAG_XSCALE"), &(mscale.x_scale))) { - warnx("Setting X mag scale failed!\n"); - } - - if (param_set(param_find("SENS_MAG_YSCALE"), &(mscale.y_scale))) { - warnx("Setting Y mag scale failed!\n"); - } - - if (param_set(param_find("SENS_MAG_ZSCALE"), &(mscale.z_scale))) { - warnx("Setting Z mag scale failed!\n"); - } - - /* auto-save to EEPROM */ - int save_ret = param_save_default(); - - if (save_ret != 0) { - warn("WARNING: auto-save of params to storage failed"); - mavlink_log_info(mavlink_fd, "FAILED storing calibration"); - } - - warnx("\tscale: %.6f %.6f %.6f\n \toffset: %.6f %.6f %.6f\nradius: %.6f GA\n", - (double)mscale.x_scale, (double)mscale.y_scale, (double)mscale.z_scale, - (double)mscale.x_offset, (double)mscale.y_offset, (double)mscale.z_offset, (double)sphere_radius); - - char buf[52]; - sprintf(buf, "mag off: x:%.2f y:%.2f z:%.2f Ga", (double)mscale.x_offset, - (double)mscale.y_offset, (double)mscale.z_offset); - mavlink_log_info(mavlink_fd, buf); - - sprintf(buf, "mag scale: x:%.2f y:%.2f z:%.2f", (double)mscale.x_scale, - (double)mscale.y_scale, (double)mscale.z_scale); - mavlink_log_info(mavlink_fd, buf); - - mavlink_log_info(mavlink_fd, "mag calibration done"); - - tune_confirm(); - sleep(2); - tune_confirm(); - sleep(2); - /* third beep by cal end routine */ - - } else { - mavlink_log_info(mavlink_fd, "mag calibration FAILED (NaN in sphere fit)"); - } - - /* disable calibration mode */ - status->flag_preflight_mag_calibration = false; - state_machine_publish(status_pub, status, mavlink_fd); - - close(sub_mag); -} - -void do_gyro_calibration(int status_pub, struct vehicle_status_s *status) -{ - /* set to gyro calibration mode */ - status->flag_preflight_gyro_calibration = true; - state_machine_publish(status_pub, status, mavlink_fd); - - const int calibration_count = 5000; - - int sub_sensor_combined = orb_subscribe(ORB_ID(sensor_combined)); - struct sensor_combined_s raw; - - int calibration_counter = 0; - float gyro_offset[3] = {0.0f, 0.0f, 0.0f}; - - /* set offsets to zero */ - int fd = open(GYRO_DEVICE_PATH, 0); - struct gyro_scale gscale_null = { - 0.0f, - 1.0f, - 0.0f, - 1.0f, - 0.0f, - 1.0f, - }; - - if (OK != ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gscale_null)) - warn("WARNING: failed to set scale / offsets for gyro"); - - close(fd); - - while (calibration_counter < calibration_count) { - - /* wait blocking for new data */ - struct pollfd fds[1] = { { .fd = sub_sensor_combined, .events = POLLIN } }; - - int poll_ret = poll(fds, 1, 1000); - - if (poll_ret) { - orb_copy(ORB_ID(sensor_combined), sub_sensor_combined, &raw); - gyro_offset[0] += raw.gyro_rad_s[0]; - gyro_offset[1] += raw.gyro_rad_s[1]; - gyro_offset[2] += raw.gyro_rad_s[2]; - calibration_counter++; - - } else if (poll_ret == 0) { - /* any poll failure for 1s is a reason to abort */ - mavlink_log_info(mavlink_fd, "gyro calibration aborted, retry"); - return; - } - } - - gyro_offset[0] = gyro_offset[0] / calibration_count; - gyro_offset[1] = gyro_offset[1] / calibration_count; - gyro_offset[2] = gyro_offset[2] / calibration_count; - - /* exit gyro calibration mode */ - status->flag_preflight_gyro_calibration = false; - state_machine_publish(status_pub, status, mavlink_fd); - - if (isfinite(gyro_offset[0]) && isfinite(gyro_offset[1]) && isfinite(gyro_offset[2])) { - - if (param_set(param_find("SENS_GYRO_XOFF"), &(gyro_offset[0])) - || param_set(param_find("SENS_GYRO_YOFF"), &(gyro_offset[1])) - || param_set(param_find("SENS_GYRO_ZOFF"), &(gyro_offset[2]))) { - mavlink_log_critical(mavlink_fd, "Setting gyro offsets failed!"); - } - - /* set offsets to actual value */ - fd = open(GYRO_DEVICE_PATH, 0); - struct gyro_scale gscale = { - gyro_offset[0], - 1.0f, - gyro_offset[1], - 1.0f, - gyro_offset[2], - 1.0f, - }; - - if (OK != ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gscale)) - warn("WARNING: failed to set scale / offsets for gyro"); - - close(fd); - - /* auto-save to EEPROM */ - int save_ret = param_save_default(); - - if (save_ret != 0) { - warn("WARNING: auto-save of params to storage failed"); - } - - // char buf[50]; - // sprintf(buf, "cal: x:%8.4f y:%8.4f z:%8.4f", (double)gyro_offset[0], (double)gyro_offset[1], (double)gyro_offset[2]); - // mavlink_log_info(mavlink_fd, buf); - mavlink_log_info(mavlink_fd, "gyro calibration done"); - - tune_confirm(); - sleep(2); - tune_confirm(); - sleep(2); - /* third beep by cal end routine */ - - } else { - mavlink_log_info(mavlink_fd, "gyro calibration FAILED (NaN)"); - } - - close(sub_sensor_combined); -} - -void do_airspeed_calibration(int status_pub, struct vehicle_status_s *status) +void do_reboot() { - /* announce change */ - - mavlink_log_info(mavlink_fd, "keep it still"); - /* set to accel calibration mode */ - status->flag_preflight_airspeed_calibration = true; - state_machine_publish(status_pub, status, mavlink_fd); - - const int calibration_count = 2500; - - int diff_pres_sub = orb_subscribe(ORB_ID(differential_pressure)); - struct differential_pressure_s diff_pres; - - int calibration_counter = 0; - float diff_pres_offset = 0.0f; - - while (calibration_counter < calibration_count) { - - /* wait blocking for new data */ - struct pollfd fds[1] = { { .fd = diff_pres_sub, .events = POLLIN } }; - - int poll_ret = poll(fds, 1, 1000); - - if (poll_ret) { - orb_copy(ORB_ID(differential_pressure), diff_pres_sub, &diff_pres); - diff_pres_offset += diff_pres.differential_pressure_pa; - calibration_counter++; - - } else if (poll_ret == 0) { - /* any poll failure for 1s is a reason to abort */ - mavlink_log_info(mavlink_fd, "airspeed calibration aborted"); - return; - } - } - - diff_pres_offset = diff_pres_offset / calibration_count; - - if (isfinite(diff_pres_offset)) { - - if (param_set(param_find("SENS_DPRES_OFF"), &(diff_pres_offset))) { - mavlink_log_critical(mavlink_fd, "Setting offs failed!"); - } - - /* auto-save to EEPROM */ - int save_ret = param_save_default(); - - if (save_ret != 0) { - warn("WARNING: auto-save of params to storage failed"); - } - - //char buf[50]; - //sprintf(buf, "[cmd] accel cal: x:%8.4f y:%8.4f z:%8.4f\n", (double)accel_offset[0], (double)accel_offset[1], (double)accel_offset[2]); - //mavlink_log_info(mavlink_fd, buf); - mavlink_log_info(mavlink_fd, "airspeed calibration done"); - - tune_confirm(); - sleep(2); - tune_confirm(); - sleep(2); - /* third beep by cal end routine */ - - } else { - mavlink_log_info(mavlink_fd, "airspeed calibration FAILED (NaN)"); - } - - /* exit airspeed calibration mode */ - status->flag_preflight_airspeed_calibration = false; - state_machine_publish(status_pub, status, mavlink_fd); - - close(diff_pres_sub); + mavlink_log_critical(mavlink_fd, "REBOOTING SYSTEM"); + usleep(500000); + up_systemreset(); + /* SPECIAL CASE: NEVER RETURNS FROM THIS FUNCTION CALL */ } -void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_status, struct vehicle_command_s *cmd) +void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_status, struct vehicle_command_s *cmd, int safety_pub, struct actuator_safety_s *safety) { /* result of the command */ uint8_t result = VEHICLE_CMD_RESULT_UNSUPPORTED; - /* announce command handling */ - tune_confirm(); - - - /* supported command handling start */ - /* request to set different system mode */ switch (cmd->command) { - case VEHICLE_CMD_DO_SET_MODE: { - if (OK == update_state_machine_mode_request(status_pub, current_vehicle_status, mavlink_fd, (uint8_t)cmd->param1)) { - result = VEHICLE_CMD_RESULT_ACCEPTED; + case VEHICLE_CMD_DO_SET_MODE: - } else { - result = VEHICLE_CMD_RESULT_DENIED; - } - } - break; + /* request to activate HIL */ + if ((int)cmd->param1 & VEHICLE_MODE_FLAG_HIL_ENABLED) { - case VEHICLE_CMD_COMPONENT_ARM_DISARM: { - /* request to arm */ - if ((int)cmd->param1 == 1) { - if (OK == update_state_machine_mode_request(status_pub, current_vehicle_status, mavlink_fd, VEHICLE_MODE_FLAG_SAFETY_ARMED)) { + if (OK == hil_state_transition(status_pub, current_vehicle_status, mavlink_fd, HIL_STATE_ON)) { result = VEHICLE_CMD_RESULT_ACCEPTED; - } else { result = VEHICLE_CMD_RESULT_DENIED; } + } - /* request to disarm */ - - } else if ((int)cmd->param1 == 0) { - if (OK == update_state_machine_mode_request(status_pub, current_vehicle_status, mavlink_fd, VEHICLE_MODE_FLAG_SAFETY_ARMED)) { + if ((int)cmd->param1 & VEHICLE_MODE_FLAG_SAFETY_ARMED) { + if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_ARMED, safety_pub, safety, mavlink_fd)) { result = VEHICLE_CMD_RESULT_ACCEPTED; - } else { result = VEHICLE_CMD_RESULT_DENIED; } - } - } - break; - - /* request for an autopilot reboot */ - case VEHICLE_CMD_PREFLIGHT_REBOOT_SHUTDOWN: { - if ((int)cmd->param1 == 1) { - if (OK == do_state_update(status_pub, current_vehicle_status, mavlink_fd, SYSTEM_STATE_REBOOT)) { - /* SPECIAL CASE: SYSTEM WILL NEVER RETURN HERE */ + } else { + if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_STANDBY, safety_pub, safety, mavlink_fd)) { result = VEHICLE_CMD_RESULT_ACCEPTED; - } else { - /* system may return here */ result = VEHICLE_CMD_RESULT_DENIED; } } - } - break; -// /* request to land */ -// case VEHICLE_CMD_NAV_LAND: -// { -// //TODO: add check if landing possible -// //TODO: add landing maneuver -// -// if (0 == update_state_machine_custom_mode_request(status_pub, current_vehicle_status, SYSTEM_STATE_ARMED)) { -// result = VEHICLE_CMD_RESULT_ACCEPTED; -// } } -// break; -// -// /* request to takeoff */ -// case VEHICLE_CMD_NAV_TAKEOFF: -// { -// //TODO: add check if takeoff possible -// //TODO: add takeoff maneuver -// -// if (0 == update_state_machine_custom_mode_request(status_pub, current_vehicle_status, SYSTEM_STATE_AUTO)) { -// result = VEHICLE_CMD_RESULT_ACCEPTED; -// } -// } -// break; -// - /* preflight calibration */ - case VEHICLE_CMD_PREFLIGHT_CALIBRATION: { - bool handled = false; + break; - /* gyro calibration */ - if ((int)(cmd->param1) == 1) { - /* transition to calibration state */ - do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_PREFLIGHT); - - if (current_status.state_machine == SYSTEM_STATE_PREFLIGHT) { - mavlink_log_info(mavlink_fd, "starting gyro cal"); - tune_confirm(); - do_gyro_calibration(status_pub, ¤t_status); - mavlink_log_info(mavlink_fd, "finished gyro cal"); - tune_confirm(); - do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_STANDBY); - result = VEHICLE_CMD_RESULT_ACCEPTED; + case VEHICLE_CMD_COMPONENT_ARM_DISARM: + /* request to arm */ + if ((int)cmd->param1 == 1) { + if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_ARMED, safety_pub, safety, mavlink_fd)) { + result = VEHICLE_CMD_RESULT_ACCEPTED; } else { - mavlink_log_critical(mavlink_fd, "REJECTING gyro cal"); result = VEHICLE_CMD_RESULT_DENIED; } - - handled = true; - } - - /* magnetometer calibration */ - if ((int)(cmd->param2) == 1) { - /* transition to calibration state */ - do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_PREFLIGHT); - - if (current_status.state_machine == SYSTEM_STATE_PREFLIGHT) { - mavlink_log_info(mavlink_fd, "starting mag cal"); - tune_confirm(); - do_mag_calibration(status_pub, ¤t_status); - mavlink_log_info(mavlink_fd, "finished mag cal"); - tune_confirm(); - do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_STANDBY); + /* request to disarm */ + } else if ((int)cmd->param1 == 0) { + if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_STANDBY, safety_pub, safety, mavlink_fd)) { result = VEHICLE_CMD_RESULT_ACCEPTED; - } else { - mavlink_log_critical(mavlink_fd, "REJECTING mag cal"); result = VEHICLE_CMD_RESULT_DENIED; } - - handled = true; } - /* zero-altitude pressure calibration */ - if ((int)(cmd->param3) == 1) { - /* transition to calibration state */ - do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_PREFLIGHT); + break; - if (current_status.state_machine == SYSTEM_STATE_PREFLIGHT) { - mavlink_log_info(mavlink_fd, "zero altitude cal. not implemented"); - tune_confirm(); + case VEHICLE_CMD_PREFLIGHT_REBOOT_SHUTDOWN: { - } else { - mavlink_log_critical(mavlink_fd, "REJECTING altitude calibration"); - result = VEHICLE_CMD_RESULT_DENIED; - } + /* request for an autopilot reboot */ + if ((int)cmd->param1 == 1) { + if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_REBOOT, safety_pub, safety, mavlink_fd)) { + /* reboot is executed later, after positive tune is sent */ + result = VEHICLE_CMD_RESULT_ACCEPTED; + tune_positive(); + /* SPECIAL CASE: SYSTEM WILL NEVER RETURN HERE */ + do_reboot(); - handled = true; + } else { + /* system may return here */ + result = VEHICLE_CMD_RESULT_DENIED; + tune_negative(); + } + } } + break; - /* trim calibration */ - if ((int)(cmd->param4) == 1) { - /* transition to calibration state */ - do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_PREFLIGHT); - - if (current_status.state_machine == SYSTEM_STATE_PREFLIGHT) { - mavlink_log_info(mavlink_fd, "starting trim cal"); - tune_confirm(); - do_rc_calibration(status_pub, ¤t_status); - mavlink_log_info(mavlink_fd, "finished trim cal"); - tune_confirm(); - do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_STANDBY); - result = VEHICLE_CMD_RESULT_ACCEPTED; - - } else { - mavlink_log_critical(mavlink_fd, "REJECTING trim cal"); - result = VEHICLE_CMD_RESULT_DENIED; - } + // /* request to land */ + // case VEHICLE_CMD_NAV_LAND: + // { + // //TODO: add check if landing possible + // //TODO: add landing maneuver + // + // if (0 == update_state_machine_custom_mode_request(status_pub, current_vehicle_status, SYSTEM_STATE_ARMED)) { + // result = VEHICLE_CMD_RESULT_ACCEPTED; + // } } + // break; + // + // /* request to takeoff */ + // case VEHICLE_CMD_NAV_TAKEOFF: + // { + // //TODO: add check if takeoff possible + // //TODO: add takeoff maneuver + // + // if (0 == update_state_machine_custom_mode_request(status_pub, current_vehicle_status, SYSTEM_STATE_AUTO)) { + // result = VEHICLE_CMD_RESULT_ACCEPTED; + // } + // } + // break; + // + /* preflight calibration */ + case VEHICLE_CMD_PREFLIGHT_CALIBRATION: - handled = true; - } + /* gyro calibration */ + if ((int)(cmd->param1) == 1) { - /* accel calibration */ - if ((int)(cmd->param5) == 1) { - /* transition to calibration state */ - do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_PREFLIGHT); - - if (current_status.state_machine == SYSTEM_STATE_PREFLIGHT) { - mavlink_log_info(mavlink_fd, "CMD starting accel cal"); - tune_confirm(); - do_accel_calibration(status_pub, ¤t_status, mavlink_fd); - tune_confirm(); - mavlink_log_info(mavlink_fd, "CMD finished accel cal"); - do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_STANDBY); - result = VEHICLE_CMD_RESULT_ACCEPTED; + /* check if no other task is scheduled */ + if(low_prio_task == LOW_PRIO_TASK_NONE) { + /* try to go to INIT/PREFLIGHT arming state */ + if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, safety_pub, safety, mavlink_fd)) { + result = VEHICLE_CMD_RESULT_ACCEPTED; + /* now set the task for the low prio thread */ + low_prio_task = LOW_PRIO_TASK_GYRO_CALIBRATION; + } else { + result = VEHICLE_CMD_RESULT_DENIED; + } } else { - mavlink_log_critical(mavlink_fd, "REJECTING accel cal"); - result = VEHICLE_CMD_RESULT_DENIED; + result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED; } - - handled = true; } - /* airspeed calibration */ - if ((int)(cmd->param6) == 1) { //xxx: this is not defined by the mavlink protocol - /* transition to calibration state */ - do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_PREFLIGHT); - - if (current_status.state_machine == SYSTEM_STATE_PREFLIGHT) { - mavlink_log_info(mavlink_fd, "CMD starting airspeed cal"); - tune_confirm(); - do_airspeed_calibration(status_pub, ¤t_status); - tune_confirm(); - mavlink_log_info(mavlink_fd, "CMD finished airspeed cal"); - do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_STANDBY); - result = VEHICLE_CMD_RESULT_ACCEPTED; + /* magnetometer calibration */ + if ((int)(cmd->param2) == 1) { + + /* check if no other task is scheduled */ + if(low_prio_task == LOW_PRIO_TASK_NONE) { + /* try to go to INIT/PREFLIGHT arming state */ + if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, safety_pub, safety, mavlink_fd)) { + result = VEHICLE_CMD_RESULT_ACCEPTED; + /* now set the task for the low prio thread */ + low_prio_task = LOW_PRIO_TASK_MAG_CALIBRATION; + } else { + result = VEHICLE_CMD_RESULT_DENIED; + } } else { - mavlink_log_critical(mavlink_fd, "REJECTING airspeed cal"); - result = VEHICLE_CMD_RESULT_DENIED; + result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED; } - - handled = true; } - /* none found */ - if (!handled) { - //warnx("refusing unsupported calibration request\n"); - mavlink_log_critical(mavlink_fd, "CMD refusing unsup. calib. request"); - result = VEHICLE_CMD_RESULT_UNSUPPORTED; - } - } - break; - case VEHICLE_CMD_PREFLIGHT_STORAGE: { - if (current_status.flag_system_armed && - ((current_status.system_type == VEHICLE_TYPE_QUADROTOR) || - (current_status.system_type == VEHICLE_TYPE_HEXAROTOR) || - (current_status.system_type == VEHICLE_TYPE_OCTOROTOR))) { - /* do not perform expensive memory tasks on multirotors in flight */ - // XXX this is over-safe, as soon as cmd is in low prio thread this can be allowed - mavlink_log_info(mavlink_fd, "REJECTING save cmd while multicopter armed"); + // /* zero-altitude pressure calibration */ + // if ((int)(cmd->param3) == 1) { - } else { + // /* check if no other task is scheduled */ + // if(low_prio_task == LOW_PRIO_TASK_NONE) { - // XXX move this to LOW PRIO THREAD of commander app - /* Read all parameters from EEPROM to RAM */ + // /* try to go to INIT/PREFLIGHT arming state */ + // if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, safety_pub, safety, mavlink_fd)) { + // result = VEHICLE_CMD_RESULT_ACCEPTED; + // /* now set the task for the low prio thread */ + // low_prio_task = LOW_PRIO_TASK_ALTITUDE_CALIBRATION; + // } else { + // result = VEHICLE_CMD_RESULT_DENIED; + // } + // } else { + // result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED; + // } + // } - if (((int)(cmd->param1)) == 0) { - /* read all parameters from EEPROM to RAM */ - int read_ret = param_load_default(); - if (read_ret == OK) { - //warnx("[mavlink pm] Loaded EEPROM params in RAM\n"); - mavlink_log_info(mavlink_fd, "OK loading params from"); - mavlink_log_info(mavlink_fd, param_get_default_file()); - result = VEHICLE_CMD_RESULT_ACCEPTED; + // /* trim calibration */ + // if ((int)(cmd->param4) == 1) { - } else if (read_ret == 1) { - mavlink_log_info(mavlink_fd, "OK no changes in"); - mavlink_log_info(mavlink_fd, param_get_default_file()); - result = VEHICLE_CMD_RESULT_ACCEPTED; + // /* check if no other task is scheduled */ + // if(low_prio_task == LOW_PRIO_TASK_NONE) { - } else { - if (read_ret < -1) { - mavlink_log_info(mavlink_fd, "ERR loading params from"); - mavlink_log_info(mavlink_fd, param_get_default_file()); + // /* try to go to INIT/PREFLIGHT arming state */ + // if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, safety_pub, safety, mavlink_fd)) { + // result = VEHICLE_CMD_RESULT_ACCEPTED; + // /* now set the task for the low prio thread */ + // low_prio_task = LOW_PRIO_TASK_RC_CALIBRATION; + // } else { + // result = VEHICLE_CMD_RESULT_DENIED; + // } + // } else { + // result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED; + // } + // } - } else { - mavlink_log_info(mavlink_fd, "ERR no param file named"); - mavlink_log_info(mavlink_fd, param_get_default_file()); - } - result = VEHICLE_CMD_RESULT_FAILED; + /* accel calibration */ + if ((int)(cmd->param5) == 1) { + + /* check if no other task is scheduled */ + if(low_prio_task == LOW_PRIO_TASK_NONE) { + + /* try to go to INIT/PREFLIGHT arming state */ + if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, safety_pub, safety, mavlink_fd)) { + result = VEHICLE_CMD_RESULT_ACCEPTED; + /* now set the task for the low prio thread */ + low_prio_task = LOW_PRIO_TASK_ACCEL_CALIBRATION; + } else { + result = VEHICLE_CMD_RESULT_DENIED; } + } else { + result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED; + } + } - } else if (((int)(cmd->param1)) == 1) { + /* airspeed calibration */ + if ((int)(cmd->param6) == 1) { - /* write all parameters from RAM to EEPROM */ - int write_ret = param_save_default(); + /* check if no other task is scheduled */ + if(low_prio_task == LOW_PRIO_TASK_NONE) { - if (write_ret == OK) { - mavlink_log_info(mavlink_fd, "OK saved param file"); - mavlink_log_info(mavlink_fd, param_get_default_file()); + /* try to go to INIT/PREFLIGHT arming state */ + if (OK == arming_state_transition(status_pub, current_vehicle_status, ARMING_STATE_INIT, safety_pub, safety, mavlink_fd)) { result = VEHICLE_CMD_RESULT_ACCEPTED; - + /* now set the task for the low prio thread */ + low_prio_task = LOW_PRIO_TASK_AIRSPEED_CALIBRATION; } else { - if (write_ret < -1) { - mavlink_log_info(mavlink_fd, "ERR params file does not exit:"); - mavlink_log_info(mavlink_fd, param_get_default_file()); + result = VEHICLE_CMD_RESULT_DENIED; + } + } else { + result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED; + } + } + break; - } else { - mavlink_log_info(mavlink_fd, "ERR writing params to"); - mavlink_log_info(mavlink_fd, param_get_default_file()); - } + case VEHICLE_CMD_PREFLIGHT_STORAGE: - result = VEHICLE_CMD_RESULT_FAILED; - } + if (((int)(cmd->param1)) == 0) { + + /* check if no other task is scheduled */ + if(low_prio_task == LOW_PRIO_TASK_NONE) { + low_prio_task = LOW_PRIO_TASK_PARAM_LOAD; + result = VEHICLE_CMD_RESULT_ACCEPTED; + } else { + result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED; + } + + + } else if (((int)(cmd->param1)) == 1) { + /* check if no other task is scheduled */ + if(low_prio_task == LOW_PRIO_TASK_NONE) { + low_prio_task = LOW_PRIO_TASK_PARAM_SAVE; + result = VEHICLE_CMD_RESULT_ACCEPTED; } else { - mavlink_log_info(mavlink_fd, "[pm] refusing unsupp. STOR request"); - result = VEHICLE_CMD_RESULT_UNSUPPORTED; + result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED; } } - } break; - default: { - mavlink_log_critical(mavlink_fd, "[cmd] refusing unsupported command"); - result = VEHICLE_CMD_RESULT_UNSUPPORTED; - /* announce command rejection */ - ioctl(buzzer, TONE_SET_ALARM, 4); - } + default: + mavlink_log_critical(mavlink_fd, "[cmd] refusing unsupported command"); + result = VEHICLE_CMD_RESULT_UNSUPPORTED; break; } /* supported command handling stop */ if (result == VEHICLE_CMD_RESULT_FAILED || result == VEHICLE_CMD_RESULT_DENIED || - result == VEHICLE_CMD_RESULT_UNSUPPORTED) { - ioctl(buzzer, TONE_SET_ALARM, 5); + result == VEHICLE_CMD_RESULT_UNSUPPORTED || + result == VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED) { + + tune_negative(); } else if (result == VEHICLE_CMD_RESULT_ACCEPTED) { - tune_confirm(); + + tune_positive(); } /* send any requested ACKs */ @@ -1065,7 +525,7 @@ void handle_command(int status_pub, struct vehicle_status_s *current_vehicle_sta } -static void *orb_receive_loop(void *arg) //handles status information coming from subsystems (present, enabled, health), these values do not indicate the quality (variance) of the signal +void *orb_receive_loop(void *arg) //handles status information coming from subsystems (present, enabled, health), these values do not indicate the quality (variance) of the signal { /* Set thread name */ prctl(PR_SET_NAME, "commander orb rcv", getpid()); @@ -1168,8 +628,7 @@ float battery_remaining_estimate_voltage(float voltage) return ret; } -static void -usage(const char *reason) +void usage(const char *reason) { if (reason) fprintf(stderr, "%s\n", reason); @@ -1235,6 +694,9 @@ int commander_thread_main(int argc, char *argv[]) commander_initialized = false; bool home_position_set = false; + bool battery_tune_played = false; + bool arm_tune_played = false; + /* set parameters */ failsafe_lowlevel_timeout_ms = 0; param_get(param_find("SYS_FAILSAVE_LL"), &failsafe_lowlevel_timeout_ms); @@ -1244,60 +706,108 @@ int commander_thread_main(int argc, char *argv[]) param_t _param_component_id = param_find("MAV_COMP_ID"); /* welcome user */ - warnx("I am in command now!\n"); + warnx("[commander] starting"); /* pthreads for command and subsystem info handling */ // pthread_t command_handling_thread; pthread_t subsystem_info_thread; + pthread_t commander_low_prio_thread; /* initialize */ if (led_init() != 0) { - warnx("ERROR: Failed to initialize leds\n"); + warnx("ERROR: Failed to initialize leds"); } - if (buzzer_init() != 0) { - warnx("ERROR: Failed to initialize buzzer\n"); + if (buzzer_init() != OK) { + warnx("ERROR: Failed to initialize buzzer"); } mavlink_fd = open(MAVLINK_LOG_DEVICE, 0); if (mavlink_fd < 0) { - warnx("ERROR: Failed to open MAVLink log stream, start mavlink app first.\n"); + warnx("ERROR: Failed to open MAVLink log stream, start mavlink app first."); } - + + /* Main state machine */ + struct vehicle_status_s current_status; + orb_advert_t status_pub; /* make sure we are in preflight state */ memset(¤t_status, 0, sizeof(current_status)); - current_status.state_machine = SYSTEM_STATE_PREFLIGHT; - current_status.flag_system_armed = false; + + /* safety topic */ + struct actuator_safety_s safety; + orb_advert_t safety_pub; + /* Initialize safety with all false */ + memset(&safety, 0, sizeof(safety)); + + + /* flags for control apps */ + struct vehicle_control_mode_s control_mode; + orb_advert_t control_mode_pub; + + /* Initialize all flags to false */ + memset(&control_mode, 0, sizeof(control_mode)); + + current_status.navigation_state = NAVIGATION_STATE_INIT; + current_status.arming_state = ARMING_STATE_INIT; + current_status.hil_state = HIL_STATE_OFF; + /* neither manual nor offboard control commands have been received */ current_status.offboard_control_signal_found_once = false; current_status.rc_signal_found_once = false; + /* mark all signals lost as long as they haven't been found */ current_status.rc_signal_lost = true; current_status.offboard_control_signal_lost = true; + /* allow manual override initially */ current_status.flag_external_manual_override_ok = true; + /* flag position info as bad, do not allow auto mode */ - current_status.flag_vector_flight_mode_ok = false; + // current_status.flag_vector_flight_mode_ok = false; + /* set battery warning flag */ current_status.battery_warning = VEHICLE_BATTERY_WARNING_NONE; + /* set safety device detection flag */ + + /* XXX do we need this? */ + //current_status.flag_safety_present = false; + + // XXX for now just set sensors as initialized + current_status.condition_system_sensors_initialized = true; + + // XXX just disable offboard control for now + control_mode.flag_control_offboard_enabled = false; /* advertise to ORB */ - stat_pub = orb_advertise(ORB_ID(vehicle_status), ¤t_status); + status_pub = orb_advertise(ORB_ID(vehicle_status), ¤t_status); /* publish current state machine */ - state_machine_publish(stat_pub, ¤t_status, mavlink_fd); + + /* publish the new state */ + current_status.counter++; + current_status.timestamp = hrt_absolute_time(); + orb_publish(ORB_ID(vehicle_status), status_pub, ¤t_status); + + + safety_pub = orb_advertise(ORB_ID(actuator_safety), &safety); + + /* but also subscribe to it */ + int safety_sub = orb_subscribe(ORB_ID(actuator_safety)); + + control_mode_pub = orb_advertise(ORB_ID(vehicle_control_mode), &control_mode); /* home position */ orb_advert_t home_pub = -1; struct home_position_s home; memset(&home, 0, sizeof(home)); - if (stat_pub < 0) { + if (status_pub < 0) { warnx("ERROR: orb_advertise for topic vehicle_status failed (uorb app running?).\n"); warnx("exiting."); exit(ERROR); } + // XXX needed? mavlink_log_info(mavlink_fd, "system is running"); /* create pthreads */ @@ -1306,9 +816,18 @@ int commander_thread_main(int argc, char *argv[]) pthread_attr_setstacksize(&subsystem_info_attr, 2048); pthread_create(&subsystem_info_thread, &subsystem_info_attr, orb_receive_loop, ¤t_status); + pthread_attr_t commander_low_prio_attr; + pthread_attr_init(&commander_low_prio_attr); + pthread_attr_setstacksize(&commander_low_prio_attr, 2048); + + struct sched_param param; + /* low priority */ + param.sched_priority = SCHED_PRIORITY_DEFAULT - 50; + (void)pthread_attr_setschedparam(&commander_low_prio_attr, ¶m); + pthread_create(&commander_low_prio_thread, &commander_low_prio_attr, commander_low_prio_loop, NULL); + /* Start monitoring loop */ uint16_t counter = 0; - uint8_t flight_env; /* Initialize to 0.0V */ float battery_voltage = 0.0f; @@ -1317,12 +836,14 @@ int commander_thread_main(int argc, char *argv[]) bool critical_battery_voltage_actions_done = false; uint8_t low_voltage_counter = 0; uint16_t critical_voltage_counter = 0; - int16_t mode_switch_rc_value; float bat_remain = 1.0f; uint16_t stick_off_counter = 0; uint16_t stick_on_counter = 0; + /* XXX what exactly is this for? */ + uint64_t last_print_time = 0; + /* Subscribe to manual control data */ int sp_man_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); struct manual_control_setpoint_s sp_man; @@ -1333,11 +854,13 @@ int commander_thread_main(int argc, char *argv[]) struct offboard_control_setpoint_s sp_offboard; memset(&sp_offboard, 0, sizeof(sp_offboard)); + /* Subscribe to global position */ int global_position_sub = orb_subscribe(ORB_ID(vehicle_global_position)); struct vehicle_global_position_s global_position; memset(&global_position, 0, sizeof(global_position)); uint64_t last_global_position_time = 0; + /* Subscribe to local position data */ int local_position_sub = orb_subscribe(ORB_ID(vehicle_local_position)); struct vehicle_local_position_s local_position; memset(&local_position, 0, sizeof(local_position)); @@ -1348,10 +871,13 @@ int commander_thread_main(int argc, char *argv[]) * position estimator and commander. RAW GPS is more than good enough for a * non-flying vehicle. */ + + /* Subscribe to GPS topic */ int gps_sub = orb_subscribe(ORB_ID(vehicle_gps_position)); struct vehicle_gps_position_s gps_position; memset(&gps_position, 0, sizeof(gps_position)); + /* Subscribe to sensor topic */ int sensor_sub = orb_subscribe(ORB_ID(sensor_combined)); struct sensor_combined_s sensors; memset(&sensors, 0, sizeof(sensors)); @@ -1387,7 +913,9 @@ int commander_thread_main(int argc, char *argv[]) thread_running = true; uint64_t start_time = hrt_absolute_time(); - uint64_t failsave_ll_start_time = 0; + + /* XXX use this! */ + //uint64_t failsave_ll_start_time = 0; bool state_changed = true; bool param_init_forced = true; @@ -1396,6 +924,39 @@ int commander_thread_main(int argc, char *argv[]) /* Get current values */ bool new_data; + + /* update parameters */ + orb_check(param_changed_sub, &new_data); + + if (new_data || param_init_forced) { + param_init_forced = false; + /* parameters changed */ + orb_copy(ORB_ID(parameter_update), param_changed_sub, ¶m_changed); + + + /* update parameters */ + if (!safety.armed) { + if (param_get(_param_sys_type, &(current_status.system_type)) != OK) { + warnx("failed setting new system type"); + } + + /* disable manual override for all systems that rely on electronic stabilization */ + if (current_status.system_type == VEHICLE_TYPE_QUADROTOR || + current_status.system_type == VEHICLE_TYPE_HEXAROTOR || + current_status.system_type == VEHICLE_TYPE_OCTOROTOR) { + current_status.flag_external_manual_override_ok = false; + + } else { + current_status.flag_external_manual_override_ok = true; + } + + /* check and update system / component ID */ + param_get(_param_system_id, &(current_status.system_id)); + param_get(_param_component_id, &(current_status.component_id)); + + } + } + orb_check(sp_man_sub, &new_data); if (new_data) { @@ -1428,8 +989,9 @@ int commander_thread_main(int argc, char *argv[]) orb_copy(ORB_ID(vehicle_command), cmd_sub, &cmd); /* handle it */ - handle_command(stat_pub, ¤t_status, &cmd); + handle_command(status_pub, ¤t_status, &cmd, safety_pub, &safety); } + /* update parameters */ orb_check(param_changed_sub, &new_data); @@ -1439,9 +1001,8 @@ int commander_thread_main(int argc, char *argv[]) /* parameters changed */ orb_copy(ORB_ID(parameter_update), param_changed_sub, ¶m_changed); - /* update parameters */ - if (!current_status.flag_system_armed) { + if (!safety.armed) { if (param_get(_param_sys_type, &(current_status.system_type)) != OK) { warnx("failed setting new system type"); } @@ -1459,10 +1020,16 @@ int commander_thread_main(int argc, char *argv[]) /* check and update system / component ID */ param_get(_param_system_id, &(current_status.system_id)); param_get(_param_component_id, &(current_status.component_id)); - } } + /* update safety topic */ + orb_check(safety_sub, &new_data); + + if (new_data) { + orb_copy(ORB_ID(actuator_safety), safety_sub, &safety); + } + /* update global position estimate */ orb_check(global_position_sub, &new_data); @@ -1481,6 +1048,13 @@ int commander_thread_main(int argc, char *argv[]) last_local_position_time = local_position.timestamp; } + /* set the condition to valid if there has recently been a local position estimate */ + if (hrt_absolute_time() - last_local_position_time < LOCAL_POSITION_TIMEOUT) { + current_status.condition_local_position_valid = true; + } else { + current_status.condition_local_position_valid = false; + } + /* update battery status */ orb_check(battery_sub, &new_data); if (new_data) { @@ -1499,10 +1073,11 @@ int commander_thread_main(int argc, char *argv[]) /* Slow but important 8 Hz checks */ if (counter % ((1000000 / COMMANDER_MONITORING_INTERVAL) / 8) == 0) { - /* toggle activity (blue) led at 1 Hz in standby, 10 Hz in armed mode */ - if ((current_status.state_machine == SYSTEM_STATE_GROUND_READY || + + /* XXX if armed */ + if ((false /*current_status.state_machine == SYSTEM_STATE_GROUND_READY || current_status.state_machine == SYSTEM_STATE_AUTO || - current_status.state_machine == SYSTEM_STATE_MANUAL)) { + current_status.state_machine == SYSTEM_STATE_MANUAL*/)) { /* armed, solid */ led_on(LED_AMBER); @@ -1537,45 +1112,18 @@ int commander_thread_main(int argc, char *argv[]) } else if (bat_remain < 0.3f && (low_voltage_counter > LOW_VOLTAGE_BATTERY_COUNTER_LIMIT)) { /* toggle arming (red) at 5 Hz on low battery or error */ led_toggle(LED_AMBER); - - } else { - // /* Constant error indication in standby mode without GPS */ - // if (!current_status.gps_valid) { - // led_on(LED_AMBER); - - // } else { - // led_off(LED_AMBER); - // } } - if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0) { - /* compute system load */ - uint64_t interval_runtime = system_load.tasks[0].total_runtime - last_idle_time; - - if (last_idle_time > 0) - current_status.load = 1000 - (interval_runtime / 1000); //system load is time spent in non-idle - - last_idle_time = system_load.tasks[0].total_runtime; - } } - // // XXX Export patterns and threshold to parameters - /* Trigger audio event for low battery */ - if (bat_remain < 0.1f && battery_voltage_valid && (counter % ((1000000 / COMMANDER_MONITORING_INTERVAL) / 4) == 0)) { - /* For less than 10%, start be really annoying at 5 Hz */ - ioctl(buzzer, TONE_SET_ALARM, 0); - ioctl(buzzer, TONE_SET_ALARM, 3); - - } else if (bat_remain < 0.1f && battery_voltage_valid && (counter % ((1000000 / COMMANDER_MONITORING_INTERVAL) / 4) == 2)) { - ioctl(buzzer, TONE_SET_ALARM, 0); + if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0) { + /* compute system load */ + uint64_t interval_runtime = system_load.tasks[0].total_runtime - last_idle_time; - } else if (bat_remain < 0.2f && battery_voltage_valid && (counter % ((1000000 / COMMANDER_MONITORING_INTERVAL) / 2) == 0)) { - /* For less than 20%, start be slightly annoying at 1 Hz */ - ioctl(buzzer, TONE_SET_ALARM, 0); - tune_confirm(); + if (last_idle_time > 0) + current_status.load = 1000 - (interval_runtime / 1000); //system load is time spent in non-idle - } else if (bat_remain < 0.2f && battery_voltage_valid && (counter % ((1000000 / COMMANDER_MONITORING_INTERVAL) / 2) == 2)) { - ioctl(buzzer, TONE_SET_ALARM, 0); + last_idle_time = system_load.tasks[0].total_runtime; } /* Check battery voltage */ @@ -1599,13 +1147,14 @@ int commander_thread_main(int argc, char *argv[]) low_voltage_counter++; } - /* Critical, this is rather an emergency, kill signal to sdlog and change state machine */ + /* Critical, this is rather an emergency, change state machine */ else if (battery_voltage_valid && (bat_remain < 0.1f /* XXX MAGIC NUMBER */) && (false == critical_battery_voltage_actions_done && true == low_battery_voltage_actions_done)) { if (critical_voltage_counter > CRITICAL_VOLTAGE_BATTERY_COUNTER_LIMIT) { critical_battery_voltage_actions_done = true; mavlink_log_critical(mavlink_fd, "[cmd] EMERGENCY! CRITICAL BATTERY!"); current_status.battery_warning = VEHICLE_BATTERY_WARNING_ALERT; - state_machine_emergency(stat_pub, ¤t_status, mavlink_fd); + // XXX implement this + // state_machine_emergency(status_pub, ¤t_status, mavlink_fd); } critical_voltage_counter++; @@ -1617,6 +1166,14 @@ int commander_thread_main(int argc, char *argv[]) /* End battery voltage check */ + /* If in INIT state, try to proceed to STANDBY state */ + if (current_status.arming_state == ARMING_STATE_INIT) { + // XXX check for sensors + arming_state_transition(status_pub, ¤t_status, ARMING_STATE_STANDBY, safety_pub, &safety, mavlink_fd); + } else { + // XXX: Add emergency stuff if sensors are lost + } + /* * Check for valid position information. @@ -1628,53 +1185,53 @@ int commander_thread_main(int argc, char *argv[]) */ /* store current state to reason later about a state change */ - bool vector_flight_mode_ok = current_status.flag_vector_flight_mode_ok; - bool global_pos_valid = current_status.flag_global_position_valid; - bool local_pos_valid = current_status.flag_local_position_valid; - bool airspeed_valid = current_status.flag_airspeed_valid; + // bool vector_flight_mode_ok = current_status.flag_vector_flight_mode_ok; + bool global_pos_valid = current_status.condition_global_position_valid; + bool local_pos_valid = current_status.condition_local_position_valid; + bool airspeed_valid = current_status.condition_airspeed_valid; + /* check for global or local position updates, set a timeout of 2s */ - if (hrt_absolute_time() - last_global_position_time < 2000000) { - current_status.flag_global_position_valid = true; + if (hrt_absolute_time() - last_global_position_time < 2000000 && hrt_absolute_time() > 2000000) { + current_status.condition_global_position_valid = true; // XXX check for controller status and home position as well } else { - current_status.flag_global_position_valid = false; + current_status.condition_global_position_valid = false; } - if (hrt_absolute_time() - last_local_position_time < 2000000) { - current_status.flag_local_position_valid = true; + if (hrt_absolute_time() - last_local_position_time < 2000000 && hrt_absolute_time() > 2000000) { + current_status.condition_local_position_valid = true; // XXX check for controller status and home position as well } else { - current_status.flag_local_position_valid = false; + current_status.condition_local_position_valid = false; } /* Check for valid airspeed/differential pressure measurements */ - if (hrt_absolute_time() - last_diff_pres_time < 2000000) { - current_status.flag_airspeed_valid = true; + if (hrt_absolute_time() - last_diff_pres_time < 2000000 && hrt_absolute_time() > 2000000) { + current_status.condition_airspeed_valid = true; } else { - current_status.flag_airspeed_valid = false; + current_status.condition_airspeed_valid = false; } /* * Consolidate global position and local position valid flags * for vector flight mode. */ - if (current_status.flag_local_position_valid || - current_status.flag_global_position_valid) { - current_status.flag_vector_flight_mode_ok = true; + // if (current_status.condition_local_position_valid || + // current_status.condition_global_position_valid) { + // current_status.flag_vector_flight_mode_ok = true; - } else { - current_status.flag_vector_flight_mode_ok = false; - } + // } else { + // current_status.flag_vector_flight_mode_ok = false; + // } /* consolidate state change, flag as changed if required */ - if (vector_flight_mode_ok != current_status.flag_vector_flight_mode_ok || - global_pos_valid != current_status.flag_global_position_valid || - local_pos_valid != current_status.flag_local_position_valid || - airspeed_valid != current_status.flag_airspeed_valid) { + if (global_pos_valid != current_status.condition_global_position_valid || + local_pos_valid != current_status.condition_local_position_valid || + airspeed_valid != current_status.condition_airspeed_valid) { state_changed = true; } @@ -1688,18 +1245,20 @@ int commander_thread_main(int argc, char *argv[]) * 2) The system has not aquired position lock before * 3) The system is not armed (on the ground) */ - if (!current_status.flag_valid_launch_position && - !vector_flight_mode_ok && current_status.flag_vector_flight_mode_ok && - !current_status.flag_system_armed) { - /* first time a valid position, store it and emit it */ - - // XXX implement storage and publication of RTL position - current_status.flag_valid_launch_position = true; - current_status.flag_auto_flight_mode_ok = true; - state_changed = true; - } + // if (!current_status.flag_valid_launch_position && + // !vector_flight_mode_ok && current_status.flag_vector_flight_mode_ok && + // !current_status.flag_system_armed) { + // first time a valid position, store it and emit it + + // // XXX implement storage and publication of RTL position + // current_status.flag_valid_launch_position = true; + // current_status.flag_auto_flight_mode_ok = true; + // state_changed = true; + // } + + orb_check(gps_sub, &new_data); + if (new_data) { - if (orb_check(ORB_ID(vehicle_gps_position), &new_data)) { orb_copy(ORB_ID(vehicle_gps_position), gps_sub, &gps_position); @@ -1724,10 +1283,10 @@ int commander_thread_main(int argc, char *argv[]) if (gps_position.fix_type == GPS_FIX_TYPE_3D && (hdop_m < hdop_threshold_m) - && (vdop_m < vdop_threshold_m) + && (vdop_m < vdop_threshold_m) // XXX note that vdop is 0 for mtk && !home_position_set && (hrt_absolute_time() - gps_position.timestamp_position < 2000000) - && !current_status.flag_system_armed) { + && !safety.armed) { warnx("setting home position"); /* copy position data to uORB home message, store it locally as well */ @@ -1750,7 +1309,7 @@ int commander_thread_main(int argc, char *argv[]) /* mark home position as set */ home_position_set = true; - tune_confirm(); + tune_positive(); } } @@ -1760,100 +1319,268 @@ int commander_thread_main(int argc, char *argv[]) if ((hrt_absolute_time() - sp_man.timestamp) < 100000) { - // /* - // * Check if manual control modes have to be switched - // */ - // if (!isfinite(sp_man.manual_mode_switch)) { - // warnx("man mode sw not finite\n"); - - // /* this switch is not properly mapped, set default */ - // if ((current_status.system_type == VEHICLE_TYPE_QUADROTOR) || - // (current_status.system_type == VEHICLE_TYPE_HEXAROTOR) || - // (current_status.system_type == VEHICLE_TYPE_OCTOROTOR)) { - - // /* assuming a rotary wing, fall back to SAS */ - // current_status.manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_SAS; - // current_status.flag_control_attitude_enabled = true; - // current_status.flag_control_rates_enabled = true; - // } else { - - // /* assuming a fixed wing, fall back to direct pass-through */ - // current_status.manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_DIRECT; - // current_status.flag_control_attitude_enabled = false; - // current_status.flag_control_rates_enabled = false; - // } + /* + * Check if manual control modes have to be switched + */ + if (!isfinite(sp_man.mode_switch)) { - // } else if (sp_man.manual_mode_switch < -STICK_ON_OFF_LIMIT) { + warnx("mode sw not finite"); + /* no valid stick position, go to default */ + current_status.mode_switch = MODE_SWITCH_MANUAL; - // /* bottom stick position, set direct mode for vehicles supporting it */ - // if ((current_status.system_type == VEHICLE_TYPE_QUADROTOR) || - // (current_status.system_type == VEHICLE_TYPE_HEXAROTOR) || - // (current_status.system_type == VEHICLE_TYPE_OCTOROTOR)) { + } else if (sp_man.mode_switch < -STICK_ON_OFF_LIMIT) { - // /* assuming a rotary wing, fall back to SAS */ - // current_status.manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_SAS; - // current_status.flag_control_attitude_enabled = true; - // current_status.flag_control_rates_enabled = true; - // } else { + /* bottom stick position, go to manual mode */ + current_status.mode_switch = MODE_SWITCH_MANUAL; - // /* assuming a fixed wing, set to direct pass-through as requested */ - // current_status.manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_DIRECT; - // current_status.flag_control_attitude_enabled = false; - // current_status.flag_control_rates_enabled = false; - // } + } else if (sp_man.mode_switch > STICK_ON_OFF_LIMIT) { - // } else if (sp_man.manual_mode_switch > STICK_ON_OFF_LIMIT) { + /* top stick position, set auto/mission for all vehicle types */ + current_status.mode_switch = MODE_SWITCH_AUTO; - // /* top stick position, set SAS for all vehicle types */ - // current_status.manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_SAS; - // current_status.flag_control_attitude_enabled = true; - // current_status.flag_control_rates_enabled = true; + } else { - // } else { - // /* center stick position, set rate control */ - // current_status.manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_RATES; - // current_status.flag_control_attitude_enabled = false; - // current_status.flag_control_rates_enabled = true; - // } + /* center stick position, set seatbelt/simple control */ + current_status.mode_switch = MODE_SWITCH_SEATBELT; + } // warnx("man ctrl mode: %d\n", (int)current_status.manual_control_mode); /* - * Check if manual stability control modes have to be switched - */ - if (!isfinite(sp_man.manual_sas_switch)) { + * Check if land/RTL is requested + */ + if (!isfinite(sp_man.return_switch)) { /* this switch is not properly mapped, set default */ - current_status.manual_sas_mode = VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_ABS; + current_status.return_switch = RETURN_SWITCH_NONE; - } else if (sp_man.manual_sas_switch < -STICK_ON_OFF_LIMIT) { + } else if (sp_man.return_switch < -STICK_ON_OFF_LIMIT) { /* bottom stick position, set altitude hold */ - current_status.manual_sas_mode = VEHICLE_MANUAL_SAS_MODE_ALTITUDE; + current_status.return_switch = RETURN_SWITCH_NONE; - } else if (sp_man.manual_sas_switch > STICK_ON_OFF_LIMIT) { + } else if (sp_man.return_switch > STICK_ON_OFF_LIMIT) { /* top stick position */ - current_status.manual_sas_mode = VEHICLE_MANUAL_SAS_MODE_SIMPLE; + current_status.return_switch = RETURN_SWITCH_RETURN; } else { /* center stick position, set default */ - current_status.manual_sas_mode = VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_ABS; + current_status.return_switch = RETURN_SWITCH_NONE; + } + + /* check mission switch */ + if (!isfinite(sp_man.mission_switch)) { + + /* this switch is not properly mapped, set default */ + current_status.mission_switch = MISSION_SWITCH_NONE; + + } else if (sp_man.mission_switch > STICK_ON_OFF_LIMIT) { + + /* top switch position */ + current_status.mission_switch = MISSION_SWITCH_MISSION; + + } else if (sp_man.mission_switch < -STICK_ON_OFF_LIMIT) { + + /* bottom switch position */ + current_status.mission_switch = MISSION_SWITCH_NONE; + + } else { + + /* center switch position, set default */ + current_status.mission_switch = MISSION_SWITCH_NONE; // XXX default? + } + + /* Now it's time to handle the stick inputs */ + + switch (current_status.arming_state) { + + /* evaluate the navigation state when disarmed */ + case ARMING_STATE_STANDBY: + + /* just manual, XXX this might depend on the return switch */ + if (current_status.mode_switch == MODE_SWITCH_MANUAL) { + + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_MANUAL_STANDBY, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // These is not supposed to happen + warnx("ERROR: Navigation state MANUAL_STANDBY rejected"); + } + + /* Try seatbelt or fallback to manual */ + } else if (current_status.mode_switch == MODE_SWITCH_SEATBELT) { + + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_SEATBELT_STANDBY, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // fallback to MANUAL_STANDBY + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_MANUAL_STANDBY, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // These is not supposed to happen + warnx("ERROR: Navigation state MANUAL_STANDBY rejected"); + } + } + + /* Try auto or fallback to seatbelt or even manual */ + } else if (current_status.mode_switch == MODE_SWITCH_AUTO) { + + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_AUTO_STANDBY, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // first fallback to SEATBELT_STANDY + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_SEATBELT_STANDBY, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // or fallback to MANUAL_STANDBY + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_MANUAL_STANDBY, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // These is not supposed to happen + warnx("ERROR: Navigation state MANUAL_STANDBY rejected"); + } + } + } + } + + break; + + /* evaluate the navigation state when armed */ + case ARMING_STATE_ARMED: + + /* Always accept manual mode */ + if (current_status.mode_switch == MODE_SWITCH_MANUAL) { + + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_MANUAL, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // These is not supposed to happen + warnx("ERROR: Navigation state MANUAL rejected"); + } + + /* SEATBELT_STANDBY (fallback: MANUAL) */ + } else if (current_status.mode_switch == MODE_SWITCH_SEATBELT + && current_status.return_switch == RETURN_SWITCH_NONE) { + + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_SEATBELT, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // fallback to MANUAL_STANDBY + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_MANUAL, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // These is not supposed to happen + warnx("ERROR: Navigation state MANUAL rejected"); + } + } + + /* SEATBELT_DESCENT (fallback: MANUAL) */ + } else if (current_status.mode_switch == MODE_SWITCH_SEATBELT + && current_status.return_switch == RETURN_SWITCH_RETURN) { + + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_SEATBELT_DESCENT, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // fallback to MANUAL_STANDBY + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_MANUAL, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // These is not supposed to happen + warnx("ERROR: Navigation state MANUAL rejected"); + } + } + + /* AUTO_LOITER (fallback: SEATBELT, MANUAL) */ + } else if (current_status.mode_switch == MODE_SWITCH_AUTO + && current_status.return_switch == RETURN_SWITCH_NONE + && current_status.mission_switch == MISSION_SWITCH_NONE) { + + /* we might come from the disarmed state AUTO_STANDBY */ + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_AUTO_READY, control_mode_pub, &control_mode, mavlink_fd) != OK) { + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_SEATBELT, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // fallback to MANUAL_STANDBY + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_MANUAL, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // These is not supposed to happen + warnx("ERROR: Navigation state MANUAL rejected"); + } + } + /* or from some other armed state like SEATBELT or MANUAL */ + } else if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_AUTO_LOITER, control_mode_pub, &control_mode, mavlink_fd) != OK) { + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_SEATBELT, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // fallback to MANUAL_STANDBY + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_MANUAL, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // These is not supposed to happen + warnx("ERROR: Navigation state MANUAL rejected"); + } + } + } + + /* AUTO_MISSION (fallback: SEATBELT, MANUAL) */ + } else if (current_status.mode_switch == MODE_SWITCH_AUTO + && current_status.return_switch == RETURN_SWITCH_NONE + && current_status.mission_switch == MISSION_SWITCH_MISSION) { + + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_AUTO_MISSION, control_mode_pub, &control_mode, mavlink_fd) != OK) { + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_SEATBELT, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // fallback to MANUAL_STANDBY + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_MANUAL, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // These is not supposed to happen + warnx("ERROR: Navigation state MANUAL rejected"); + } + } + } + + /* AUTO_RTL (fallback: SEATBELT_DESCENT, MANUAL) */ + } else if (current_status.mode_switch == MODE_SWITCH_AUTO + && current_status.return_switch == RETURN_SWITCH_RETURN + && (current_status.mission_switch == MISSION_SWITCH_NONE || current_status.mission_switch == MISSION_SWITCH_MISSION)) { + + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_AUTO_RTL, control_mode_pub, &control_mode, mavlink_fd) != OK) { + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_SEATBELT_DESCENT, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // fallback to MANUAL_STANDBY + if (navigation_state_transition(status_pub, ¤t_status, NAVIGATION_STATE_MANUAL, control_mode_pub, &control_mode, mavlink_fd) != OK) { + // These is not supposed to happen + warnx("ERROR: Navigation state MANUAL rejected"); + } + } + } + } + break; + + // XXX we might be missing something that triggers a transition from RTL to LAND + + case ARMING_STATE_ARMED_ERROR: + + // XXX work out fail-safe scenarios + break; + + case ARMING_STATE_STANDBY_ERROR: + + // XXX work out fail-safe scenarios + break; + + case ARMING_STATE_REBOOT: + + // XXX I don't think we should end up here + break; + + case ARMING_STATE_IN_AIR_RESTORE: + + // XXX not sure what to do here + break; + default: + break; + } + /* handle the case where RC signal was regained */ + if (!current_status.rc_signal_found_once) { + current_status.rc_signal_found_once = true; + mavlink_log_critical(mavlink_fd, "DETECTED RC SIGNAL FIRST TIME."); + + } else { + if (current_status.rc_signal_lost) { + mavlink_log_critical(mavlink_fd, "[cmd] RECOVERY - RC SIGNAL GAINED!"); + } } /* - * Check if left stick is in lower left position --> switch to standby state. - * Do this only for multirotors, not for fixed wing aircraft. - */ - if (((current_status.system_type == VEHICLE_TYPE_QUADROTOR) || - (current_status.system_type == VEHICLE_TYPE_HEXAROTOR) || - (current_status.system_type == VEHICLE_TYPE_OCTOROTOR) - ) && - ((sp_man.yaw < -STICK_ON_OFF_LIMIT)) && - (sp_man.throttle < STICK_THRUST_RANGE * 0.2f)) { + * Check if left stick is in lower left position --> switch to standby state. + * Do this only for multirotors, not for fixed wing aircraft. + */ + // printf("checking\n"); + if ((sp_man.yaw < -STICK_ON_OFF_LIMIT) && (sp_man.throttle < STICK_THRUST_RANGE * 0.2f)) { if (stick_off_counter > STICK_ON_OFF_COUNTER_LIMIT) { - update_state_machine_disarm(stat_pub, ¤t_status, mavlink_fd); - stick_on_counter = 0; + + if((current_status.system_type == VEHICLE_TYPE_QUADROTOR) || + (current_status.system_type == VEHICLE_TYPE_HEXAROTOR) || + (current_status.system_type == VEHICLE_TYPE_OCTOROTOR) + ) { + arming_state_transition(status_pub, ¤t_status, ARMING_STATE_STANDBY, safety_pub, &safety, mavlink_fd); + tune_positive(); + + } else { + mavlink_log_critical(mavlink_fd, "STICK DISARM not allowed"); + tune_negative(); + } + stick_off_counter = 0; } else { stick_off_counter++; @@ -1864,8 +1591,9 @@ int commander_thread_main(int argc, char *argv[]) /* check if left stick is in lower right position --> arm */ if (sp_man.yaw > STICK_ON_OFF_LIMIT && sp_man.throttle < STICK_THRUST_RANGE * 0.2f) { if (stick_on_counter > STICK_ON_OFF_COUNTER_LIMIT) { - update_state_machine_arm(stat_pub, ¤t_status, mavlink_fd); + arming_state_transition(status_pub, ¤t_status, ARMING_STATE_ARMED, safety_pub, &safety, mavlink_fd); stick_on_counter = 0; + tune_positive(); } else { stick_on_counter++; @@ -1873,49 +1601,24 @@ int commander_thread_main(int argc, char *argv[]) } } - /* check manual override switch - switch to manual or auto mode */ - if (sp_man.manual_override_switch > STICK_ON_OFF_LIMIT) { - /* enable manual override */ - update_state_machine_mode_manual(stat_pub, ¤t_status, mavlink_fd); - - } else if (sp_man.manual_override_switch < -STICK_ON_OFF_LIMIT) { - // /* check auto mode switch for correct mode */ - // if (sp_man.auto_mode_switch > STICK_ON_OFF_LIMIT) { - // /* enable guided mode */ - // update_state_machine_mode_guided(stat_pub, ¤t_status, mavlink_fd); - - // } else if (sp_man.auto_mode_switch < -STICK_ON_OFF_LIMIT) { - // XXX hardcode to auto for now - update_state_machine_mode_auto(stat_pub, ¤t_status, mavlink_fd); - - // } - - } else { - /* center stick position, set SAS for all vehicle types */ - update_state_machine_mode_stabilized(stat_pub, ¤t_status, mavlink_fd); - } - - /* handle the case where RC signal was regained */ - if (!current_status.rc_signal_found_once) { - current_status.rc_signal_found_once = true; - mavlink_log_critical(mavlink_fd, "DETECTED RC SIGNAL FIRST TIME."); - - } else { - if (current_status.rc_signal_lost) mavlink_log_critical(mavlink_fd, "[cmd] RECOVERY - RC SIGNAL GAINED!"); - } - current_status.rc_signal_cutting_off = false; current_status.rc_signal_lost = false; current_status.rc_signal_lost_interval = 0; } else { - static uint64_t last_print_time = 0; /* print error message for first RC glitch and then every 5 s / 5000 ms) */ if (!current_status.rc_signal_cutting_off || ((hrt_absolute_time() - last_print_time) > 5000000)) { /* only complain if the offboard control is NOT active */ current_status.rc_signal_cutting_off = true; mavlink_log_critical(mavlink_fd, "CRITICAL - NO REMOTE SIGNAL!"); + + if (!current_status.rc_signal_cutting_off) { + printf("Reason: not rc_signal_cutting_off\n"); + } else { + printf("last print time: %llu\n", last_print_time); + } + last_print_time = hrt_absolute_time(); } @@ -1947,60 +1650,60 @@ int commander_thread_main(int argc, char *argv[]) if (!current_status.rc_signal_found_once && sp_offboard.timestamp != 0) { if ((hrt_absolute_time() - sp_offboard.timestamp) < 5000000) { - /* decide about attitude control flag, enable in att/pos/vel */ - bool attitude_ctrl_enabled = (sp_offboard.mode == OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE || - sp_offboard.mode == OFFBOARD_CONTROL_MODE_DIRECT_VELOCITY || - sp_offboard.mode == OFFBOARD_CONTROL_MODE_DIRECT_POSITION); + // /* decide about attitude control flag, enable in att/pos/vel */ + // bool attitude_ctrl_enabled = (sp_offboard.mode == OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE || + // sp_offboard.mode == OFFBOARD_CONTROL_MODE_DIRECT_VELOCITY || + // sp_offboard.mode == OFFBOARD_CONTROL_MODE_DIRECT_POSITION); - /* decide about rate control flag, enable it always XXX (for now) */ - bool rates_ctrl_enabled = true; + // /* decide about rate control flag, enable it always XXX (for now) */ + // bool rates_ctrl_enabled = true; - /* set up control mode */ - if (current_status.flag_control_attitude_enabled != attitude_ctrl_enabled) { - current_status.flag_control_attitude_enabled = attitude_ctrl_enabled; - state_changed = true; - } + // /* set up control mode */ + // if (current_status.flag_control_attitude_enabled != attitude_ctrl_enabled) { + // current_status.flag_control_attitude_enabled = attitude_ctrl_enabled; + // state_changed = true; + // } - if (current_status.flag_control_rates_enabled != rates_ctrl_enabled) { - current_status.flag_control_rates_enabled = rates_ctrl_enabled; - state_changed = true; - } + // if (current_status.flag_control_rates_enabled != rates_ctrl_enabled) { + // current_status.flag_control_rates_enabled = rates_ctrl_enabled; + // state_changed = true; + // } - /* handle the case where offboard control signal was regained */ - if (!current_status.offboard_control_signal_found_once) { - current_status.offboard_control_signal_found_once = true; - /* enable offboard control, disable manual input */ - current_status.flag_control_manual_enabled = false; - current_status.flag_control_offboard_enabled = true; - state_changed = true; - tune_confirm(); + // /* handle the case where offboard control signal was regained */ + // if (!current_status.offboard_control_signal_found_once) { + // current_status.offboard_control_signal_found_once = true; + // /* enable offboard control, disable manual input */ + // current_status.flag_control_manual_enabled = false; + // current_status.flag_control_offboard_enabled = true; + // state_changed = true; + // tune_positive(); - mavlink_log_critical(mavlink_fd, "DETECTED OFFBOARD SIGNAL FIRST"); + // mavlink_log_critical(mavlink_fd, "DETECTED OFFBOARD SIGNAL FIRST"); - } else { - if (current_status.offboard_control_signal_lost) { - mavlink_log_critical(mavlink_fd, "RECOVERY OFFBOARD CONTROL"); - state_changed = true; - tune_confirm(); - } - } + // } else { + // if (current_status.offboard_control_signal_lost) { + // mavlink_log_critical(mavlink_fd, "RECOVERY OFFBOARD CONTROL"); + // state_changed = true; + // tune_positive(); + // } + // } current_status.offboard_control_signal_weak = false; current_status.offboard_control_signal_lost = false; current_status.offboard_control_signal_lost_interval = 0; + // XXX check if this is correct /* arm / disarm on request */ - if (sp_offboard.armed && !current_status.flag_system_armed) { - update_state_machine_arm(stat_pub, ¤t_status, mavlink_fd); - /* switch to stabilized mode = takeoff */ - update_state_machine_mode_stabilized(stat_pub, ¤t_status, mavlink_fd); + if (sp_offboard.armed && !safety.armed) { + + arming_state_transition(status_pub, ¤t_status, ARMING_STATE_ARMED, safety_pub, &safety, mavlink_fd); + + } else if (!sp_offboard.armed && safety.armed) { - } else if (!sp_offboard.armed && current_status.flag_system_armed) { - update_state_machine_disarm(stat_pub, ¤t_status, mavlink_fd); + arming_state_transition(status_pub, ¤t_status, ARMING_STATE_STANDBY, safety_pub, &safety, mavlink_fd); } } else { - static uint64_t last_print_time = 0; /* print error message for first RC glitch and then every 5 s / 5000 ms) */ if (!current_status.offboard_control_signal_weak || ((hrt_absolute_time() - last_print_time) > 5000000)) { @@ -2016,7 +1719,7 @@ int commander_thread_main(int argc, char *argv[]) if (current_status.offboard_control_signal_lost_interval > 100000) { current_status.offboard_control_signal_lost = true; current_status.failsave_lowlevel_start_time = hrt_absolute_time(); - tune_confirm(); + tune_positive(); /* kill motors after timeout */ if (hrt_absolute_time() - current_status.failsave_lowlevel_start_time > failsafe_lowlevel_timeout_ms * 1000) { @@ -2028,29 +1731,60 @@ int commander_thread_main(int argc, char *argv[]) } + + current_status.counter++; current_status.timestamp = hrt_absolute_time(); + // XXX this is missing /* If full run came back clean, transition to standby */ - if (current_status.state_machine == SYSTEM_STATE_PREFLIGHT && - current_status.flag_preflight_gyro_calibration == false && - current_status.flag_preflight_mag_calibration == false && - current_status.flag_preflight_accel_calibration == false) { - /* All ok, no calibration going on, go to standby */ - do_state_update(stat_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_STANDBY); - } + // if (current_status.state_machine == SYSTEM_STATE_PREFLIGHT && + // current_status.flag_preflight_gyro_calibration == false && + // current_status.flag_preflight_mag_calibration == false && + // current_status.flag_preflight_accel_calibration == false) { + // /* All ok, no calibration going on, go to standby */ + // do_state_update(status_pub, ¤t_status, mavlink_fd, SYSTEM_STATE_STANDBY); + // } /* publish at least with 1 Hz */ if (counter % (1000000 / COMMANDER_MONITORING_INTERVAL) == 0 || state_changed) { - publish_armed_status(¤t_status); - orb_publish(ORB_ID(vehicle_status), stat_pub, ¤t_status); + + orb_publish(ORB_ID(vehicle_status), status_pub, ¤t_status); state_changed = false; } + + /* Store old modes to detect and act on state transitions */ voltage_previous = current_status.voltage_battery; + + /* play tone according to evaluation result */ + /* check if we recently armed */ + if (!arm_tune_played && safety.armed && ( !safety.safety_switch_available || (safety.safety_off && safety.safety_switch_available))) { + if (tune_arm() == OK) + arm_tune_played = true; + + /* Trigger audio event for low battery */ + } else if (bat_remain < 0.1f && battery_voltage_valid) { + if (tune_critical_bat() == OK) + battery_tune_played = true; + } else if (bat_remain < 0.2f && battery_voltage_valid) { + if (tune_low_bat() == OK) + battery_tune_played = true; + } else if(battery_tune_played) { + tune_stop(); + battery_tune_played = false; + } + + /* reset arm_tune_played when disarmed */ + if (!(safety.armed && ( !safety.safety_switch_available || (safety.safety_off && safety.safety_switch_available)))) { + arm_tune_played = false; + } + + + /* XXX use this voltage_previous */ fflush(stdout); counter++; usleep(COMMANDER_MONITORING_INTERVAL); @@ -2059,6 +1793,7 @@ int commander_thread_main(int argc, char *argv[]) /* wait for threads to complete */ // pthread_join(command_handling_thread, NULL); pthread_join(subsystem_info_thread, NULL); + pthread_join(commander_low_prio_thread, NULL); /* close fds */ led_deinit(); @@ -2069,10 +1804,93 @@ int commander_thread_main(int argc, char *argv[]) close(sensor_sub); close(cmd_sub); - warnx("exiting..\n"); + warnx("exiting"); fflush(stdout); thread_running = false; return 0; } + + +void *commander_low_prio_loop(void *arg) +{ + /* Set thread name */ + prctl(PR_SET_NAME, "commander low prio", getpid()); + + while (!thread_should_exit) { + + switch (low_prio_task) { + + case LOW_PRIO_TASK_PARAM_LOAD: + + if (0 == param_load_default()) { + mavlink_log_info(mavlink_fd, "Param load success"); + } else { + mavlink_log_critical(mavlink_fd, "Param load ERROR"); + tune_error(); + } + low_prio_task = LOW_PRIO_TASK_NONE; + break; + + case LOW_PRIO_TASK_PARAM_SAVE: + + if (0 == param_save_default()) { + mavlink_log_info(mavlink_fd, "Param save success"); + } else { + mavlink_log_critical(mavlink_fd, "Param save ERROR"); + tune_error(); + } + low_prio_task = LOW_PRIO_TASK_NONE; + break; + + case LOW_PRIO_TASK_GYRO_CALIBRATION: + + do_gyro_calibration(mavlink_fd); + + low_prio_task = LOW_PRIO_TASK_NONE; + break; + + case LOW_PRIO_TASK_MAG_CALIBRATION: + + do_mag_calibration(mavlink_fd); + + low_prio_task = LOW_PRIO_TASK_NONE; + break; + + case LOW_PRIO_TASK_ALTITUDE_CALIBRATION: + + // do_baro_calibration(mavlink_fd); + + case LOW_PRIO_TASK_RC_CALIBRATION: + + // do_rc_calibration(mavlink_fd); + + low_prio_task = LOW_PRIO_TASK_NONE; + break; + + case LOW_PRIO_TASK_ACCEL_CALIBRATION: + + do_accel_calibration(mavlink_fd); + + low_prio_task = LOW_PRIO_TASK_NONE; + break; + + case LOW_PRIO_TASK_AIRSPEED_CALIBRATION: + + do_airspeed_calibration(mavlink_fd); + + low_prio_task = LOW_PRIO_TASK_NONE; + break; + + case LOW_PRIO_TASK_NONE: + default: + /* slow down to 10Hz */ + usleep(100000); + break; + } + + } + + return 0; +} diff --git a/src/modules/commander/commander.h b/src/modules/commander/commander.h index 04b4e72ab..6e57c0ba5 100644 --- a/src/modules/commander/commander.h +++ b/src/modules/commander/commander.h @@ -49,10 +49,6 @@ #ifndef COMMANDER_H_ #define COMMANDER_H_ -#define LOW_VOLTAGE_BATTERY_HYSTERESIS_TIME_MS 1000.0f -#define CRITICAL_VOLTAGE_BATTERY_HYSTERESIS_TIME_MS 100.0f -void tune_confirm(void); -void tune_error(void); #endif /* COMMANDER_H_ */ diff --git a/src/modules/commander/commander_helper.c b/src/modules/commander/commander_helper.c new file mode 100644 index 000000000..a75b5dec3 --- /dev/null +++ b/src/modules/commander/commander_helper.c @@ -0,0 +1,129 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * Author: Thomas Gubler <thomasgubler@student.ethz.ch> + * Julian Oes <joes@student.ethz.ch> + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * 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 commander_helper.c + * Commander helper functions implementations + */ + +#include <stdio.h> +#include <unistd.h> +#include <stdint.h> +#include <stdbool.h> +#include <fcntl.h> + +#include <uORB/uORB.h> +#include <uORB/topics/vehicle_status.h> +#include <uORB/topics/actuator_controls.h> +#include <uORB/topics/vehicle_control_mode.h> +#include <systemlib/err.h> +#include <drivers/drv_hrt.h> +#include <drivers/drv_tone_alarm.h> + +#include "commander_helper.h" + +bool is_multirotor(const struct vehicle_status_s *current_status) +{ + return ((current_status->system_type == VEHICLE_TYPE_QUADROTOR) || + (current_status->system_type == VEHICLE_TYPE_HEXAROTOR) || + (current_status->system_type == VEHICLE_TYPE_OCTOROTOR) || + (current_status->system_type == VEHICLE_TYPE_TRICOPTER)); +} + +bool is_rotary_wing(const struct vehicle_status_s *current_status) +{ + return is_multirotor(current_status) || (current_status->system_type == VEHICLE_TYPE_HELICOPTER) + || (current_status->system_type == VEHICLE_TYPE_COAXIAL); +} + +static int buzzer; + +int buzzer_init() +{ + buzzer = open("/dev/tone_alarm", O_WRONLY); + + if (buzzer < 0) { + warnx("Buzzer: open fail\n"); + return ERROR; + } + + return OK; +} + +void buzzer_deinit() +{ + close(buzzer); +} + +void tune_error() +{ + ioctl(buzzer, TONE_SET_ALARM, 2); +} + +void tune_positive() +{ + ioctl(buzzer, TONE_SET_ALARM, 3); +} + +void tune_neutral() +{ + ioctl(buzzer, TONE_SET_ALARM, 4); +} + +void tune_negative() +{ + ioctl(buzzer, TONE_SET_ALARM, 5); +} + +int tune_arm() +{ + return ioctl(buzzer, TONE_SET_ALARM, 12); +} + +int tune_critical_bat() +{ + return ioctl(buzzer, TONE_SET_ALARM, 14); +} + +int tune_low_bat() +{ + return ioctl(buzzer, TONE_SET_ALARM, 13); +} + +void tune_stop() +{ + ioctl(buzzer, TONE_SET_ALARM, 0); +} + diff --git a/src/modules/commander/commander_helper.h b/src/modules/commander/commander_helper.h new file mode 100644 index 000000000..ea96d72a6 --- /dev/null +++ b/src/modules/commander/commander_helper.h @@ -0,0 +1,66 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * Author: Thomas Gubler <thomasgubler@student.ethz.ch> + * Julian Oes <joes@student.ethz.ch> + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * 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 commander_helper.h + * Commander helper functions definitions + */ + +#ifndef COMMANDER_HELPER_H_ +#define COMMANDER_HELPER_H_ + +#include <uORB/uORB.h> +#include <uORB/topics/vehicle_status.h> +#include <uORB/topics/actuator_safety.h> +#include <uORB/topics/vehicle_control_mode.h> + + +bool is_multirotor(const struct vehicle_status_s *current_status); +bool is_rotary_wing(const struct vehicle_status_s *current_status); + +int buzzer_init(void); +void buzzer_deinit(void); + +void tune_error(void); +void tune_positive(void); +void tune_neutral(void); +void tune_negative(void); +int tune_arm(void); +int tune_critical_bat(void); +int tune_low_bat(void); + +void tune_stop(void); + +#endif /* COMMANDER_HELPER_H_ */ diff --git a/src/modules/commander/gyro_calibration.c b/src/modules/commander/gyro_calibration.c new file mode 100644 index 000000000..f452910c9 --- /dev/null +++ b/src/modules/commander/gyro_calibration.c @@ -0,0 +1,151 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file gyro_calibration.c + * Gyroscope calibration routine + */ + +#include "gyro_calibration.h" +#include "commander_helper.h" + +#include <stdio.h> +#include <fcntl.h> +#include <poll.h> +#include <math.h> +#include <drivers/drv_hrt.h> +#include <uORB/topics/sensor_combined.h> +#include <drivers/drv_gyro.h> +#include <mavlink/mavlink_log.h> +#include <systemlib/param/param.h> +#include <systemlib/err.h> + + +void do_gyro_calibration(int mavlink_fd) +{ + mavlink_log_info(mavlink_fd, "gyro calibration starting, hold still"); + + const int calibration_count = 5000; + + int sub_sensor_combined = orb_subscribe(ORB_ID(sensor_combined)); + struct sensor_combined_s raw; + + int calibration_counter = 0; + float gyro_offset[3] = {0.0f, 0.0f, 0.0f}; + + /* set offsets to zero */ + int fd = open(GYRO_DEVICE_PATH, 0); + struct gyro_scale gscale_null = { + 0.0f, + 1.0f, + 0.0f, + 1.0f, + 0.0f, + 1.0f, + }; + + if (OK != ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gscale_null)) + warn("WARNING: failed to set scale / offsets for gyro"); + + close(fd); + + while (calibration_counter < calibration_count) { + + /* wait blocking for new data */ + struct pollfd fds[1] = { { .fd = sub_sensor_combined, .events = POLLIN } }; + + int poll_ret = poll(fds, 1, 1000); + + if (poll_ret) { + orb_copy(ORB_ID(sensor_combined), sub_sensor_combined, &raw); + gyro_offset[0] += raw.gyro_rad_s[0]; + gyro_offset[1] += raw.gyro_rad_s[1]; + gyro_offset[2] += raw.gyro_rad_s[2]; + calibration_counter++; + + } else if (poll_ret == 0) { + /* any poll failure for 1s is a reason to abort */ + mavlink_log_info(mavlink_fd, "gyro calibration aborted, retry"); + return; + } + } + + gyro_offset[0] = gyro_offset[0] / calibration_count; + gyro_offset[1] = gyro_offset[1] / calibration_count; + gyro_offset[2] = gyro_offset[2] / calibration_count; + + if (isfinite(gyro_offset[0]) && isfinite(gyro_offset[1]) && isfinite(gyro_offset[2])) { + + if (param_set(param_find("SENS_GYRO_XOFF"), &(gyro_offset[0])) + || param_set(param_find("SENS_GYRO_YOFF"), &(gyro_offset[1])) + || param_set(param_find("SENS_GYRO_ZOFF"), &(gyro_offset[2]))) { + mavlink_log_critical(mavlink_fd, "Setting gyro offsets failed!"); + } + + /* set offsets to actual value */ + fd = open(GYRO_DEVICE_PATH, 0); + struct gyro_scale gscale = { + gyro_offset[0], + 1.0f, + gyro_offset[1], + 1.0f, + gyro_offset[2], + 1.0f, + }; + + if (OK != ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gscale)) + warn("WARNING: failed to set scale / offsets for gyro"); + + close(fd); + + /* auto-save to EEPROM */ + int save_ret = param_save_default(); + + if (save_ret != 0) { + warn("WARNING: auto-save of params to storage failed"); + } + + // char buf[50]; + // sprintf(buf, "cal: x:%8.4f y:%8.4f z:%8.4f", (double)gyro_offset[0], (double)gyro_offset[1], (double)gyro_offset[2]); + // mavlink_log_info(mavlink_fd, buf); + mavlink_log_info(mavlink_fd, "gyro calibration done"); + + tune_positive(); + /* third beep by cal end routine */ + + } else { + mavlink_log_info(mavlink_fd, "gyro calibration FAILED (NaN)"); + } + + close(sub_sensor_combined); +} diff --git a/src/modules/commander/gyro_calibration.h b/src/modules/commander/gyro_calibration.h new file mode 100644 index 000000000..cd262507d --- /dev/null +++ b/src/modules/commander/gyro_calibration.h @@ -0,0 +1,46 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file gyro_calibration.h + * Gyroscope calibration routine + */ + +#ifndef GYRO_CALIBRATION_H_ +#define GYRO_CALIBRATION_H_ + +#include <stdint.h> + +void do_gyro_calibration(int mavlink_fd); + +#endif /* GYRO_CALIBRATION_H_ */
\ No newline at end of file diff --git a/src/modules/commander/mag_calibration.c b/src/modules/commander/mag_calibration.c new file mode 100644 index 000000000..dbd31a7e7 --- /dev/null +++ b/src/modules/commander/mag_calibration.c @@ -0,0 +1,278 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file mag_calibration.c + * Magnetometer calibration routine + */ + +#include "mag_calibration.h" +#include "commander_helper.h" +#include "calibration_routines.h" + +#include <stdio.h> +#include <stdlib.h> +#include <string.h> +#include <poll.h> +#include <math.h> +#include <fcntl.h> +#include <drivers/drv_hrt.h> +#include <uORB/topics/sensor_combined.h> +#include <drivers/drv_mag.h> +#include <mavlink/mavlink_log.h> +#include <systemlib/param/param.h> +#include <systemlib/err.h> + + +void do_mag_calibration(int mavlink_fd) +{ + mavlink_log_info(mavlink_fd, "mag calibration starting, hold still"); + + int sub_mag = orb_subscribe(ORB_ID(sensor_mag)); + struct mag_report mag; + + /* 45 seconds */ + uint64_t calibration_interval = 45 * 1000 * 1000; + + /* maximum 2000 values */ + const unsigned int calibration_maxcount = 500; + unsigned int calibration_counter = 0; + + /* limit update rate to get equally spaced measurements over time (in ms) */ + orb_set_interval(sub_mag, (calibration_interval / 1000) / calibration_maxcount); + + int fd = open(MAG_DEVICE_PATH, O_RDONLY); + + /* erase old calibration */ + struct mag_scale mscale_null = { + 0.0f, + 1.0f, + 0.0f, + 1.0f, + 0.0f, + 1.0f, + }; + + if (OK != ioctl(fd, MAGIOCSSCALE, (long unsigned int)&mscale_null)) { + warn("WARNING: failed to set scale / offsets for mag"); + mavlink_log_info(mavlink_fd, "failed to set scale / offsets for mag"); + } + + /* calibrate range */ + if (OK != ioctl(fd, MAGIOCCALIBRATE, fd)) { + warnx("failed to calibrate scale"); + } + + close(fd); + + /* calibrate offsets */ + + // uint64_t calibration_start = hrt_absolute_time(); + + uint64_t axis_deadline = hrt_absolute_time(); + uint64_t calibration_deadline = hrt_absolute_time() + calibration_interval; + + const char axislabels[3] = { 'X', 'Y', 'Z'}; + int axis_index = -1; + + float *x = (float *)malloc(sizeof(float) * calibration_maxcount); + float *y = (float *)malloc(sizeof(float) * calibration_maxcount); + float *z = (float *)malloc(sizeof(float) * calibration_maxcount); + + if (x == NULL || y == NULL || z == NULL) { + warnx("mag cal failed: out of memory"); + mavlink_log_info(mavlink_fd, "mag cal failed: out of memory"); + warnx("x:%p y:%p z:%p\n", x, y, z); + return; + } + + while (hrt_absolute_time() < calibration_deadline && + calibration_counter < calibration_maxcount) { + + /* wait blocking for new data */ + struct pollfd fds[1] = { { .fd = sub_mag, .events = POLLIN } }; + + /* user guidance */ + if (hrt_absolute_time() >= axis_deadline && + axis_index < 3) { + + axis_index++; + + char buf[50]; + sprintf(buf, "please rotate around %c", axislabels[axis_index]); + mavlink_log_info(mavlink_fd, buf); + tune_neutral(); + + axis_deadline += calibration_interval / 3; + } + + if (!(axis_index < 3)) { + break; + } + + // int axis_left = (int64_t)axis_deadline - (int64_t)hrt_absolute_time(); + + // if ((axis_left / 1000) == 0 && axis_left > 0) { + // char buf[50]; + // sprintf(buf, "[cmd] %d seconds left for axis %c", axis_left, axislabels[axis_index]); + // mavlink_log_info(mavlink_fd, buf); + // } + + int poll_ret = poll(fds, 1, 1000); + + if (poll_ret) { + orb_copy(ORB_ID(sensor_mag), sub_mag, &mag); + + x[calibration_counter] = mag.x; + y[calibration_counter] = mag.y; + z[calibration_counter] = mag.z; + + /* get min/max values */ + + // if (mag.x < mag_min[0]) { + // mag_min[0] = mag.x; + // } + // else if (mag.x > mag_max[0]) { + // mag_max[0] = mag.x; + // } + + // if (raw.magnetometer_ga[1] < mag_min[1]) { + // mag_min[1] = raw.magnetometer_ga[1]; + // } + // else if (raw.magnetometer_ga[1] > mag_max[1]) { + // mag_max[1] = raw.magnetometer_ga[1]; + // } + + // if (raw.magnetometer_ga[2] < mag_min[2]) { + // mag_min[2] = raw.magnetometer_ga[2]; + // } + // else if (raw.magnetometer_ga[2] > mag_max[2]) { + // mag_max[2] = raw.magnetometer_ga[2]; + // } + + calibration_counter++; + + } else if (poll_ret == 0) { + /* any poll failure for 1s is a reason to abort */ + mavlink_log_info(mavlink_fd, "mag cal canceled (timed out)"); + break; + } + } + + float sphere_x; + float sphere_y; + float sphere_z; + float sphere_radius; + + sphere_fit_least_squares(x, y, z, calibration_counter, 100, 0.0f, &sphere_x, &sphere_y, &sphere_z, &sphere_radius); + + free(x); + free(y); + free(z); + + if (isfinite(sphere_x) && isfinite(sphere_y) && isfinite(sphere_z)) { + + fd = open(MAG_DEVICE_PATH, 0); + + struct mag_scale mscale; + + if (OK != ioctl(fd, MAGIOCGSCALE, (long unsigned int)&mscale)) + warn("WARNING: failed to get scale / offsets for mag"); + + mscale.x_offset = sphere_x; + mscale.y_offset = sphere_y; + mscale.z_offset = sphere_z; + + if (OK != ioctl(fd, MAGIOCSSCALE, (long unsigned int)&mscale)) + warn("WARNING: failed to set scale / offsets for mag"); + + close(fd); + + /* announce and set new offset */ + + if (param_set(param_find("SENS_MAG_XOFF"), &(mscale.x_offset))) { + warnx("Setting X mag offset failed!\n"); + } + + if (param_set(param_find("SENS_MAG_YOFF"), &(mscale.y_offset))) { + warnx("Setting Y mag offset failed!\n"); + } + + if (param_set(param_find("SENS_MAG_ZOFF"), &(mscale.z_offset))) { + warnx("Setting Z mag offset failed!\n"); + } + + if (param_set(param_find("SENS_MAG_XSCALE"), &(mscale.x_scale))) { + warnx("Setting X mag scale failed!\n"); + } + + if (param_set(param_find("SENS_MAG_YSCALE"), &(mscale.y_scale))) { + warnx("Setting Y mag scale failed!\n"); + } + + if (param_set(param_find("SENS_MAG_ZSCALE"), &(mscale.z_scale))) { + warnx("Setting Z mag scale failed!\n"); + } + + /* auto-save to EEPROM */ + int save_ret = param_save_default(); + + if (save_ret != 0) { + warn("WARNING: auto-save of params to storage failed"); + mavlink_log_info(mavlink_fd, "FAILED storing calibration"); + } + + warnx("\tscale: %.6f %.6f %.6f\n \toffset: %.6f %.6f %.6f\nradius: %.6f GA\n", + (double)mscale.x_scale, (double)mscale.y_scale, (double)mscale.z_scale, + (double)mscale.x_offset, (double)mscale.y_offset, (double)mscale.z_offset, (double)sphere_radius); + + char buf[52]; + sprintf(buf, "mag off: x:%.2f y:%.2f z:%.2f Ga", (double)mscale.x_offset, + (double)mscale.y_offset, (double)mscale.z_offset); + mavlink_log_info(mavlink_fd, buf); + + sprintf(buf, "mag scale: x:%.2f y:%.2f z:%.2f", (double)mscale.x_scale, + (double)mscale.y_scale, (double)mscale.z_scale); + mavlink_log_info(mavlink_fd, buf); + + mavlink_log_info(mavlink_fd, "mag calibration done"); + + tune_positive(); + /* third beep by cal end routine */ + + } else { + mavlink_log_info(mavlink_fd, "mag calibration FAILED (NaN in sphere fit)"); + } + + close(sub_mag); +}
\ No newline at end of file diff --git a/src/modules/commander/mag_calibration.h b/src/modules/commander/mag_calibration.h new file mode 100644 index 000000000..fd2085f14 --- /dev/null +++ b/src/modules/commander/mag_calibration.h @@ -0,0 +1,46 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file mag_calibration.h + * Magnetometer calibration routine + */ + +#ifndef MAG_CALIBRATION_H_ +#define MAG_CALIBRATION_H_ + +#include <stdint.h> + +void do_mag_calibration(int mavlink_fd); + +#endif /* MAG_CALIBRATION_H_ */
\ No newline at end of file diff --git a/src/modules/commander/module.mk b/src/modules/commander/module.mk index fe44e955a..fef8e366b 100644 --- a/src/modules/commander/module.mk +++ b/src/modules/commander/module.mk @@ -38,6 +38,12 @@ MODULE_COMMAND = commander SRCS = commander.c \ state_machine_helper.c \ + commander_helper.c \ calibration_routines.c \ - accelerometer_calibration.c + accelerometer_calibration.c \ + gyro_calibration.c \ + mag_calibration.c \ + baro_calibration.c \ + rc_calibration.c \ + airspeed_calibration.c diff --git a/src/modules/commander/rc_calibration.c b/src/modules/commander/rc_calibration.c new file mode 100644 index 000000000..9aa6b86fe --- /dev/null +++ b/src/modules/commander/rc_calibration.c @@ -0,0 +1,83 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file rc_calibration.c + * Remote Control calibration routine + */ + +#include "rc_calibration.h" +#include "commander_helper.h" + +#include <poll.h> +#include <uORB/topics/sensor_combined.h> +#include <uORB/topics/manual_control_setpoint.h> +#include <mavlink/mavlink_log.h> +#include <systemlib/param/param.h> +#include <systemlib/err.h> + + +void do_rc_calibration(int mavlink_fd) +{ + mavlink_log_info(mavlink_fd, "trim calibration starting"); + + /* XXX fix this */ + // if (current_status.offboard_control_signal_lost) { + // mavlink_log_critical(mavlink_fd, "TRIM CAL: ABORT. No RC signal."); + // return; + // } + + int sub_man = orb_subscribe(ORB_ID(manual_control_setpoint)); + struct manual_control_setpoint_s sp; + orb_copy(ORB_ID(manual_control_setpoint), sub_man, &sp); + + /* set parameters */ + float p = sp.roll; + param_set(param_find("TRIM_ROLL"), &p); + p = sp.pitch; + param_set(param_find("TRIM_PITCH"), &p); + p = sp.yaw; + param_set(param_find("TRIM_YAW"), &p); + + /* store to permanent storage */ + /* auto-save */ + int save_ret = param_save_default(); + + if (save_ret != 0) { + mavlink_log_critical(mavlink_fd, "TRIM CAL: WARN: auto-save of params failed"); + } + + tune_positive(); + + mavlink_log_info(mavlink_fd, "trim calibration done"); +}
\ No newline at end of file diff --git a/src/modules/commander/rc_calibration.h b/src/modules/commander/rc_calibration.h new file mode 100644 index 000000000..6505c7364 --- /dev/null +++ b/src/modules/commander/rc_calibration.h @@ -0,0 +1,46 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file rc_calibration.h + * Remote Control calibration routine + */ + +#ifndef RC_CALIBRATION_H_ +#define RC_CALIBRATION_H_ + +#include <stdint.h> + +void do_rc_calibration(int mavlink_fd); + +#endif /* RC_CALIBRATION_H_ */
\ No newline at end of file diff --git a/src/modules/commander/state_machine_helper.c b/src/modules/commander/state_machine_helper.c index ab728c7bb..c15fc91a0 100644 --- a/src/modules/commander/state_machine_helper.c +++ b/src/modules/commander/state_machine_helper.c @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Copyright (C) 2013 PX4 Development Team. All rights reserved. * Author: Thomas Gubler <thomasgubler@student.ethz.ch> * Julian Oes <joes@student.ethz.ch> * @@ -40,257 +40,532 @@ #include <stdio.h> #include <unistd.h> +#include <stdint.h> +#include <stdbool.h> #include <uORB/uORB.h> #include <uORB/topics/vehicle_status.h> #include <uORB/topics/actuator_controls.h> +#include <uORB/topics/vehicle_control_mode.h> #include <systemlib/systemlib.h> +#include <systemlib/param/param.h> +#include <systemlib/err.h> #include <drivers/drv_hrt.h> #include <mavlink/mavlink_log.h> #include "state_machine_helper.h" +#include "commander_helper.h" -static const char *system_state_txt[] = { - "SYSTEM_STATE_PREFLIGHT", - "SYSTEM_STATE_STANDBY", - "SYSTEM_STATE_GROUND_READY", - "SYSTEM_STATE_MANUAL", - "SYSTEM_STATE_STABILIZED", - "SYSTEM_STATE_AUTO", - "SYSTEM_STATE_MISSION_ABORT", - "SYSTEM_STATE_EMCY_LANDING", - "SYSTEM_STATE_EMCY_CUTOFF", - "SYSTEM_STATE_GROUND_ERROR", - "SYSTEM_STATE_REBOOT", - -}; -/** - * Transition from one state to another - */ -int do_state_update(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, commander_state_machine_t new_state) -{ - int invalid_state = false; - int ret = ERROR; - - commander_state_machine_t old_state = current_status->state_machine; - - switch (new_state) { - case SYSTEM_STATE_MISSION_ABORT: { - /* Indoor or outdoor */ - // if (flight_environment_parameter == PX4_FLIGHT_ENVIRONMENT_OUTDOOR) { - ret = do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_EMCY_LANDING); - - // } else { - // ret = do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_EMCY_CUTOFF); - // } - } - break; - - case SYSTEM_STATE_EMCY_LANDING: - /* Tell the controller to land */ - - /* set system flags according to state */ - current_status->flag_system_armed = true; - - warnx("EMERGENCY LANDING!\n"); - mavlink_log_critical(mavlink_fd, "EMERGENCY LANDING!"); - break; - - case SYSTEM_STATE_EMCY_CUTOFF: - /* Tell the controller to cutoff the motors (thrust = 0) */ - - /* set system flags according to state */ - current_status->flag_system_armed = false; - - warnx("EMERGENCY MOTOR CUTOFF!\n"); - mavlink_log_critical(mavlink_fd, "EMERGENCY MOTOR CUTOFF!"); - break; - - case SYSTEM_STATE_GROUND_ERROR: +int arming_state_transition(int status_pub, struct vehicle_status_s *current_state, arming_state_t new_arming_state, int safety_pub, struct actuator_safety_s *safety, const int mavlink_fd) { - /* set system flags according to state */ - /* prevent actuators from arming */ - current_status->flag_system_armed = false; - - warnx("GROUND ERROR, locking down propulsion system\n"); - mavlink_log_critical(mavlink_fd, "GROUND ERROR, locking down system"); - break; - - case SYSTEM_STATE_PREFLIGHT: - if (current_status->state_machine == SYSTEM_STATE_STANDBY - || current_status->state_machine == SYSTEM_STATE_PREFLIGHT) { - /* set system flags according to state */ - current_status->flag_system_armed = false; - mavlink_log_critical(mavlink_fd, "Switched to PREFLIGHT state"); + int ret = ERROR; - } else { - invalid_state = true; - mavlink_log_critical(mavlink_fd, "REFUSED to switch to PREFLIGHT state"); - } + /* only check transition if the new state is actually different from the current one */ + if (new_arming_state == current_state->arming_state) { + ret = OK; + } else { - break; - - case SYSTEM_STATE_REBOOT: - if (current_status->state_machine == SYSTEM_STATE_STANDBY - || current_status->state_machine == SYSTEM_STATE_PREFLIGHT - || current_status->flag_hil_enabled) { - invalid_state = false; - /* set system flags according to state */ - current_status->flag_system_armed = false; - mavlink_log_critical(mavlink_fd, "REBOOTING SYSTEM"); - usleep(500000); - up_systemreset(); - /* SPECIAL CASE: NEVER RETURNS FROM THIS FUNCTION CALL */ - - } else { - invalid_state = true; - mavlink_log_critical(mavlink_fd, "REFUSED to REBOOT"); + switch (new_arming_state) { + case ARMING_STATE_INIT: + + /* allow going back from INIT for calibration */ + if (current_state->arming_state == ARMING_STATE_STANDBY) { + ret = OK; + safety->armed = false; + safety->ready_to_arm = false; + } + break; + case ARMING_STATE_STANDBY: + + /* allow coming from INIT and disarming from ARMED */ + if (current_state->arming_state == ARMING_STATE_INIT + || current_state->arming_state == ARMING_STATE_ARMED) { + + /* sensors need to be initialized for STANDBY state */ + if (current_state->condition_system_sensors_initialized) { + ret = OK; + safety->armed = false; + safety->ready_to_arm = true; + } else { + mavlink_log_critical(mavlink_fd, "Rej. STANDBY state, sensors not initialized"); + } + } + break; + case ARMING_STATE_ARMED: + + /* allow arming from STANDBY and IN-AIR-RESTORE */ + if (current_state->arming_state == ARMING_STATE_STANDBY + || current_state->arming_state == ARMING_STATE_IN_AIR_RESTORE) { + + /* XXX conditions for arming? */ + ret = OK; + safety->armed = true; + } + break; + case ARMING_STATE_ARMED_ERROR: + + /* an armed error happens when ARMED obviously */ + if (current_state->arming_state == ARMING_STATE_ARMED) { + + /* XXX conditions for an error state? */ + ret = OK; + safety->armed = true; + } + break; + case ARMING_STATE_STANDBY_ERROR: + /* a disarmed error happens when in STANDBY or in INIT or after ARMED_ERROR */ + if (current_state->arming_state == ARMING_STATE_STANDBY + || current_state->arming_state == ARMING_STATE_INIT + || current_state->arming_state == ARMING_STATE_ARMED_ERROR) { + ret = OK; + safety->armed = false; + safety->ready_to_arm = false; + } + break; + case ARMING_STATE_REBOOT: + + /* an armed error happens when ARMED obviously */ + if (current_state->arming_state == ARMING_STATE_INIT + || current_state->arming_state == ARMING_STATE_STANDBY + || current_state->arming_state == ARMING_STATE_STANDBY_ERROR) { + + ret = OK; + safety->armed = false; + safety->ready_to_arm = false; + + } + break; + case ARMING_STATE_IN_AIR_RESTORE: + + /* XXX implement */ + break; + default: + break; } - break; - - case SYSTEM_STATE_STANDBY: - /* set system flags according to state */ - - /* standby enforces disarmed */ - current_status->flag_system_armed = false; - - mavlink_log_critical(mavlink_fd, "Switched to STANDBY state"); - break; - - case SYSTEM_STATE_GROUND_READY: - - /* set system flags according to state */ - - /* ground ready has motors / actuators armed */ - current_status->flag_system_armed = true; - - mavlink_log_critical(mavlink_fd, "Switched to GROUND READY state"); - break; - - case SYSTEM_STATE_AUTO: + if (ret == OK) { + current_state->arming_state = new_arming_state; + current_state->counter++; + current_state->timestamp = hrt_absolute_time(); + orb_publish(ORB_ID(vehicle_status), status_pub, current_state); - /* set system flags according to state */ - - /* auto is airborne and in auto mode, motors armed */ - current_status->flag_system_armed = true; + safety->timestamp = hrt_absolute_time(); + orb_publish(ORB_ID(actuator_safety), safety_pub, safety); + } + } - mavlink_log_critical(mavlink_fd, "Switched to FLYING / AUTO mode"); - break; + return ret; +} - case SYSTEM_STATE_STABILIZED: - /* set system flags according to state */ - current_status->flag_system_armed = true; - mavlink_log_critical(mavlink_fd, "Switched to FLYING / STABILIZED mode"); - break; +/* + * This functions does not evaluate any input flags but only checks if the transitions + * are valid. + */ +int navigation_state_transition(int status_pub, struct vehicle_status_s *current_state, navigation_state_t new_navigation_state, int control_mode_pub, struct vehicle_control_mode_s *control_mode, const int mavlink_fd) { - case SYSTEM_STATE_MANUAL: + int ret = ERROR; - /* set system flags according to state */ - current_status->flag_system_armed = true; + /* only check transition if the new state is actually different from the current one */ + if (new_navigation_state == current_state->navigation_state) { + ret = OK; + } else { - mavlink_log_critical(mavlink_fd, "Switched to FLYING / MANUAL mode"); - break; + switch (new_navigation_state) { + case NAVIGATION_STATE_INIT: + + /* transitions back to INIT are possible for calibration */ + if (current_state->navigation_state == NAVIGATION_STATE_MANUAL_STANDBY + || current_state->navigation_state == NAVIGATION_STATE_SEATBELT_STANDBY + || current_state->navigation_state == NAVIGATION_STATE_AUTO_STANDBY) { + + ret = OK; + control_mode->flag_control_rates_enabled = false; + control_mode->flag_control_attitude_enabled = false; + control_mode->flag_control_velocity_enabled = false; + control_mode->flag_control_position_enabled = false; + control_mode->flag_control_manual_enabled = false; + } + break; + + case NAVIGATION_STATE_MANUAL_STANDBY: + + /* transitions from INIT and other STANDBY states as well as MANUAL are possible */ + if (current_state->navigation_state == NAVIGATION_STATE_INIT + || current_state->navigation_state == NAVIGATION_STATE_SEATBELT_STANDBY + || current_state->navigation_state == NAVIGATION_STATE_AUTO_STANDBY + || current_state->navigation_state == NAVIGATION_STATE_MANUAL) { + + /* need to be disarmed first */ + if (current_state->arming_state != ARMING_STATE_STANDBY) { + mavlink_log_critical(mavlink_fd, "Rej. MANUAL_STANDBY: not disarmed"); + tune_negative(); + } else { + ret = OK; + control_mode->flag_control_rates_enabled = true; + control_mode->flag_control_attitude_enabled = true; + control_mode->flag_control_velocity_enabled = false; + control_mode->flag_control_position_enabled = false; + control_mode->flag_control_manual_enabled = true; + } + } + break; + + case NAVIGATION_STATE_MANUAL: + + /* need to be armed first */ + if (current_state->arming_state != ARMING_STATE_ARMED) { + mavlink_log_critical(mavlink_fd, "Rej. MANUAL: not armed"); + tune_negative(); + } else { + ret = OK; + control_mode->flag_control_rates_enabled = true; + control_mode->flag_control_attitude_enabled = true; + control_mode->flag_control_velocity_enabled = false; + control_mode->flag_control_position_enabled = false; + control_mode->flag_control_manual_enabled = true; + } + break; + + case NAVIGATION_STATE_SEATBELT_STANDBY: + + /* transitions from INIT and other STANDBY states as well as SEATBELT and SEATBELT_DESCENT are possible */ + if (current_state->navigation_state == NAVIGATION_STATE_INIT + || current_state->navigation_state == NAVIGATION_STATE_MANUAL_STANDBY + || current_state->navigation_state == NAVIGATION_STATE_AUTO_STANDBY + || current_state->navigation_state == NAVIGATION_STATE_SEATBELT + || current_state->navigation_state == NAVIGATION_STATE_SEATBELT_DESCENT) { + + /* need to be disarmed and have a position estimate */ + if (current_state->arming_state != ARMING_STATE_STANDBY) { + mavlink_log_critical(mavlink_fd, "Rej. SEATBELT_STANDBY: not disarmed"); + tune_negative(); + } else if (!current_state->condition_local_position_valid) { + mavlink_log_critical(mavlink_fd, "Rej. SEATBELT_STANDBY: no position estimate"); + tune_negative(); + } else { + ret = OK; + control_mode->flag_control_rates_enabled = true; + control_mode->flag_control_attitude_enabled = true; + control_mode->flag_control_velocity_enabled = true; + control_mode->flag_control_position_enabled = false; + control_mode->flag_control_manual_enabled = false; + } + } + break; + + case NAVIGATION_STATE_SEATBELT: + + /* transitions from all AUTO modes except AUTO_STANDBY and except MANUAL_STANDBY and INIT*/ + if (current_state->navigation_state == NAVIGATION_STATE_SEATBELT_STANDBY + || current_state->navigation_state == NAVIGATION_STATE_SEATBELT_DESCENT + || current_state->navigation_state == NAVIGATION_STATE_MANUAL + || current_state->navigation_state == NAVIGATION_STATE_AUTO_LAND + || current_state->navigation_state == NAVIGATION_STATE_AUTO_LOITER + || current_state->navigation_state == NAVIGATION_STATE_AUTO_MISSION + || current_state->navigation_state == NAVIGATION_STATE_AUTO_READY + || current_state->navigation_state == NAVIGATION_STATE_AUTO_RTL + || current_state->navigation_state == NAVIGATION_STATE_AUTO_TAKEOFF) { + + /* need to be armed and have a position estimate */ + if (current_state->arming_state != ARMING_STATE_ARMED) { + mavlink_log_critical(mavlink_fd, "Rej. SEATBELT: not armed"); + tune_negative(); + } else if (!current_state->condition_local_position_valid) { + mavlink_log_critical(mavlink_fd, "Rej. SEATBELT: no pos estimate"); + tune_negative(); + } else { + ret = OK; + control_mode->flag_control_rates_enabled = true; + control_mode->flag_control_attitude_enabled = true; + control_mode->flag_control_velocity_enabled = true; + control_mode->flag_control_position_enabled = false; + control_mode->flag_control_manual_enabled = false; + } + } + break; + + case NAVIGATION_STATE_SEATBELT_DESCENT: + + /* transitions from all AUTO modes except AUTO_STANDBY and except MANUAL_STANDBY and INIT and SEATBELT_STANDBY */ + if (current_state->navigation_state == NAVIGATION_STATE_SEATBELT + || current_state->navigation_state == NAVIGATION_STATE_MANUAL + || current_state->navigation_state == NAVIGATION_STATE_AUTO_LAND + || current_state->navigation_state == NAVIGATION_STATE_AUTO_LOITER + || current_state->navigation_state == NAVIGATION_STATE_AUTO_MISSION + || current_state->navigation_state == NAVIGATION_STATE_AUTO_READY + || current_state->navigation_state == NAVIGATION_STATE_AUTO_RTL + || current_state->navigation_state == NAVIGATION_STATE_AUTO_TAKEOFF) { + + /* need to be armed and have a position estimate */ + if (current_state->arming_state != ARMING_STATE_ARMED) { + mavlink_log_critical(mavlink_fd, "Rej. SEATBELT_DESCENT: not armed"); + tune_negative(); + } else if (!current_state->condition_local_position_valid) { + mavlink_log_critical(mavlink_fd, "Rej. SEATBELT_DESCENT: no pos estimate"); + tune_negative(); + } else { + ret = OK; + control_mode->flag_control_rates_enabled = true; + control_mode->flag_control_attitude_enabled = true; + control_mode->flag_control_velocity_enabled = true; + control_mode->flag_control_position_enabled = false; + control_mode->flag_control_manual_enabled = false; + } + } + break; + + case NAVIGATION_STATE_AUTO_STANDBY: + + /* transitions from INIT or from other STANDBY modes or from AUTO READY */ + if (current_state->navigation_state == NAVIGATION_STATE_INIT + || current_state->navigation_state == NAVIGATION_STATE_MANUAL_STANDBY + || current_state->navigation_state == NAVIGATION_STATE_SEATBELT_STANDBY + || current_state->navigation_state == NAVIGATION_STATE_AUTO_READY) { + + /* need to be disarmed and have a position and home lock */ + if (current_state->arming_state != ARMING_STATE_STANDBY) { + mavlink_log_critical(mavlink_fd, "Rej. AUTO_STANDBY: not disarmed"); + tune_negative(); + } else if (!current_state->condition_global_position_valid) { + mavlink_log_critical(mavlink_fd, "Rej. AUTO_STANDBY: no pos lock"); + tune_negative(); + } else if (!current_state->condition_home_position_valid) { + mavlink_log_critical(mavlink_fd, "Rej. AUTO_STANDBY: no home pos"); + tune_negative(); + } else { + ret = OK; + control_mode->flag_control_rates_enabled = true; + control_mode->flag_control_attitude_enabled = true; + control_mode->flag_control_velocity_enabled = true; + control_mode->flag_control_position_enabled = true; + control_mode->flag_control_manual_enabled = false; + } + } + break; + + case NAVIGATION_STATE_AUTO_READY: + + /* transitions from AUTO_STANDBY or AUTO_LAND */ + if (current_state->navigation_state == NAVIGATION_STATE_AUTO_STANDBY + || current_state->navigation_state == NAVIGATION_STATE_AUTO_LAND) { + + // XXX flag test needed? + + /* need to be armed and have a position and home lock */ + if (current_state->arming_state != ARMING_STATE_ARMED) { + mavlink_log_critical(mavlink_fd, "Rej. AUTO_READY: not armed"); + tune_negative(); + } else { + ret = OK; + control_mode->flag_control_rates_enabled = true; + control_mode->flag_control_attitude_enabled = true; + control_mode->flag_control_velocity_enabled = true; + control_mode->flag_control_position_enabled = true; + control_mode->flag_control_manual_enabled = false; + } + } + break; + + case NAVIGATION_STATE_AUTO_TAKEOFF: + + /* only transitions from AUTO_READY */ + if (current_state->navigation_state == NAVIGATION_STATE_AUTO_READY) { + + ret = OK; + control_mode->flag_control_rates_enabled = true; + control_mode->flag_control_attitude_enabled = true; + control_mode->flag_control_velocity_enabled = true; + control_mode->flag_control_position_enabled = true; + control_mode->flag_control_manual_enabled = false; + } + break; + + case NAVIGATION_STATE_AUTO_LOITER: + + /* from everywhere flying except AUTO_LAND and SEATBELT_DESCENT */ + if (current_state->navigation_state == NAVIGATION_STATE_AUTO_TAKEOFF + || current_state->navigation_state == NAVIGATION_STATE_AUTO_MISSION + || current_state->navigation_state == NAVIGATION_STATE_AUTO_RTL + || current_state->navigation_state == NAVIGATION_STATE_SEATBELT + || current_state->navigation_state == NAVIGATION_STATE_MANUAL) { + + /* need to have a position and home lock */ + if (!current_state->condition_global_position_valid) { + mavlink_log_critical(mavlink_fd, "Rej. AUTO_LOITER: no pos lock"); + tune_negative(); + } else if (!current_state->condition_home_position_valid) { + mavlink_log_critical(mavlink_fd, "Rej. AUTO_LOITER: no home pos"); + tune_negative(); + } else { + ret = OK; + control_mode->flag_control_rates_enabled = true; + control_mode->flag_control_attitude_enabled = true; + control_mode->flag_control_velocity_enabled = true; + control_mode->flag_control_position_enabled = true; + control_mode->flag_control_manual_enabled = false; + } + } + break; + + case NAVIGATION_STATE_AUTO_MISSION: + + /* from everywhere flying except AUTO_LAND and SEATBELT_DESCENT */ + if (current_state->navigation_state == NAVIGATION_STATE_AUTO_TAKEOFF + || current_state->navigation_state == NAVIGATION_STATE_AUTO_LOITER + || current_state->navigation_state == NAVIGATION_STATE_AUTO_RTL + || current_state->navigation_state == NAVIGATION_STATE_SEATBELT + || current_state->navigation_state == NAVIGATION_STATE_MANUAL) { + + /* need to have a mission ready */ + if (!current_state-> condition_auto_mission_available) { + mavlink_log_critical(mavlink_fd, "Rej. AUTO_MISSION: no mission available"); + tune_negative(); + } else { + ret = OK; + control_mode->flag_control_rates_enabled = true; + control_mode->flag_control_attitude_enabled = true; + control_mode->flag_control_velocity_enabled = true; + control_mode->flag_control_position_enabled = true; + control_mode->flag_control_manual_enabled = false; + } + } + break; + + case NAVIGATION_STATE_AUTO_RTL: + + /* from everywhere flying except AUTO_LAND and SEATBELT_DESCENT */ + if (current_state->navigation_state == NAVIGATION_STATE_AUTO_TAKEOFF + || current_state->navigation_state == NAVIGATION_STATE_AUTO_MISSION + || current_state->navigation_state == NAVIGATION_STATE_AUTO_LOITER + || current_state->navigation_state == NAVIGATION_STATE_SEATBELT + || current_state->navigation_state == NAVIGATION_STATE_MANUAL) { + + /* need to have a position and home lock */ + if (!current_state->condition_global_position_valid) { + mavlink_log_critical(mavlink_fd, "Rej. AUTO_RTL: no pos lock"); + tune_negative(); + } else if (!current_state->condition_home_position_valid) { + mavlink_log_critical(mavlink_fd, "Rej. AUTO_RTL: no home pos"); + tune_negative(); + } else { + ret = OK; + control_mode->flag_control_rates_enabled = true; + control_mode->flag_control_attitude_enabled = true; + control_mode->flag_control_velocity_enabled = true; + control_mode->flag_control_position_enabled = true; + control_mode->flag_control_manual_enabled = false; + } + } + break; + + case NAVIGATION_STATE_AUTO_LAND: + /* after AUTO_RTL or when in AUTO_LOITER or AUTO_MISSION */ + if (current_state->navigation_state == NAVIGATION_STATE_AUTO_RTL + || current_state->navigation_state == NAVIGATION_STATE_AUTO_MISSION + || current_state->navigation_state == NAVIGATION_STATE_AUTO_LOITER) { + + /* need to have a position and home lock */ + if (!current_state->condition_global_position_valid) { + mavlink_log_critical(mavlink_fd, "Rej. AUTO_LAND: no pos lock"); + tune_negative(); + } else if (!current_state->condition_home_position_valid) { + mavlink_log_critical(mavlink_fd, "Rej. AUTO_LAND: no home pos"); + tune_negative(); + } else { + ret = OK; + control_mode->flag_control_rates_enabled = true; + control_mode->flag_control_attitude_enabled = true; + control_mode->flag_control_velocity_enabled = true; + control_mode->flag_control_position_enabled = true; + control_mode->flag_control_manual_enabled = false; + } + } + break; + + default: + break; + } - default: - invalid_state = true; - break; - } + if (ret == OK) { + current_state->navigation_state = new_navigation_state; + current_state->counter++; + current_state->timestamp = hrt_absolute_time(); + orb_publish(ORB_ID(vehicle_status), status_pub, current_state); - if (invalid_state == false || old_state != new_state) { - current_status->state_machine = new_state; - state_machine_publish(status_pub, current_status, mavlink_fd); - publish_armed_status(current_status); - ret = OK; + control_mode->timestamp = hrt_absolute_time(); + orb_publish(ORB_ID(vehicle_control_mode), control_mode_pub, control_mode); + } } - if (invalid_state) { - mavlink_log_critical(mavlink_fd, "REJECTING invalid state transition"); - ret = ERROR; - } + return ret; } -void state_machine_publish(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) -{ - /* publish the new state */ - current_status->counter++; - current_status->timestamp = hrt_absolute_time(); - /* assemble state vector based on flag values */ - if (current_status->flag_control_rates_enabled) { - current_status->onboard_control_sensors_present |= 0x400; +/** +* Transition from one hil state to another +*/ +int hil_state_transition(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, hil_state_t new_state) +{ + bool valid_transition = false; + int ret = ERROR; - } else { - current_status->onboard_control_sensors_present &= ~0x400; - } + warnx("Current state: %d, requested state: %d", current_status->hil_state, new_state); - current_status->onboard_control_sensors_present |= (current_status->flag_control_attitude_enabled) ? 0x800 : 0; - current_status->onboard_control_sensors_present |= (current_status->flag_control_attitude_enabled) ? 0x1000 : 0; - current_status->onboard_control_sensors_present |= (current_status->flag_control_velocity_enabled || current_status->flag_control_position_enabled) ? 0x2000 : 0; - current_status->onboard_control_sensors_present |= (current_status->flag_control_velocity_enabled || current_status->flag_control_position_enabled) ? 0x4000 : 0; + if (current_status->hil_state == new_state) { + warnx("Hil state not changed"); + valid_transition = true; - current_status->onboard_control_sensors_enabled |= (current_status->flag_control_rates_enabled) ? 0x400 : 0; - current_status->onboard_control_sensors_enabled |= (current_status->flag_control_attitude_enabled) ? 0x800 : 0; - current_status->onboard_control_sensors_enabled |= (current_status->flag_control_attitude_enabled) ? 0x1000 : 0; - current_status->onboard_control_sensors_enabled |= (current_status->flag_control_velocity_enabled || current_status->flag_control_position_enabled) ? 0x2000 : 0; - current_status->onboard_control_sensors_enabled |= (current_status->flag_control_velocity_enabled || current_status->flag_control_position_enabled) ? 0x4000 : 0; + } else { - orb_publish(ORB_ID(vehicle_status), status_pub, current_status); - printf("[cmd] new state: %s\n", system_state_txt[current_status->state_machine]); -} + switch (new_state) { -void publish_armed_status(const struct vehicle_status_s *current_status) -{ - struct actuator_armed_s armed; - armed.armed = current_status->flag_system_armed; + case HIL_STATE_OFF: - /* XXX allow arming by external components on multicopters only if not yet armed by RC */ - /* XXX allow arming only if core sensors are ok */ - armed.ready_to_arm = true; + if (current_status->arming_state == ARMING_STATE_INIT + || current_status->arming_state == ARMING_STATE_STANDBY) { - /* lock down actuators if required, only in HIL */ - armed.lockdown = (current_status->flag_hil_enabled) ? true : false; - orb_advert_t armed_pub = orb_advertise(ORB_ID(actuator_armed), &armed); - orb_publish(ORB_ID(actuator_armed), armed_pub, &armed); -} + current_status->flag_hil_enabled = false; + mavlink_log_critical(mavlink_fd, "Switched to OFF hil state"); + valid_transition = true; + } + break; + case HIL_STATE_ON: -/* - * Private functions, update the state machine - */ -void state_machine_emergency_always_critical(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) -{ - warnx("EMERGENCY HANDLER\n"); - /* Depending on the current state go to one of the error states */ + if (current_status->arming_state == ARMING_STATE_INIT + || current_status->arming_state == ARMING_STATE_STANDBY) { - if (current_status->state_machine == SYSTEM_STATE_PREFLIGHT || current_status->state_machine == SYSTEM_STATE_STANDBY || current_status->state_machine == SYSTEM_STATE_GROUND_READY) { - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_GROUND_ERROR); + current_status->flag_hil_enabled = true; + mavlink_log_critical(mavlink_fd, "Switched to ON hil state"); + valid_transition = true; + } + break; - } else if (current_status->state_machine == SYSTEM_STATE_AUTO || current_status->state_machine == SYSTEM_STATE_MANUAL) { - - // DO NOT abort mission - //do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_MISSION_ABORT); - - } else { - warnx("Unknown system state: #%d\n", current_status->state_machine); + default: + warnx("Unknown hil state"); + break; + } } -} -void state_machine_emergency(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) //do not call state_machine_emergency_always_critical if we are in manual mode for these errors -{ - if (current_status->state_machine != SYSTEM_STATE_MANUAL) { //if we are in manual: user can react to errors themself - state_machine_emergency_always_critical(status_pub, current_status, mavlink_fd); + if (valid_transition) { + current_status->hil_state = new_state; + + current_status->counter++; + current_status->timestamp = hrt_absolute_time(); + orb_publish(ORB_ID(vehicle_status), status_pub, current_status); + ret = OK; } else { - //global_data_send_mavlink_statustext_message_out("[cmd] ERROR: take action immediately! (did not switch to error state because the system is in manual mode)", MAV_SEVERITY_CRITICAL); + mavlink_log_critical(mavlink_fd, "REJECTING invalid hil state transition"); } + return ret; } @@ -405,353 +680,76 @@ void state_machine_emergency(int status_pub, struct vehicle_status_s *current_st // } -// void update_state_machine_subsystem_healthy(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type) -// { -// current_status->onboard_control_sensors_health |= 1 << *subsystem_type; -// current_status->counter++; -// current_status->timestamp = hrt_absolute_time(); -// orb_publish(ORB_ID(vehicle_status), status_pub, current_status); - -// switch (*subsystem_type) { -// case SUBSYSTEM_TYPE_GYRO: -// //TODO state machine change (recovering) -// break; - -// case SUBSYSTEM_TYPE_ACC: -// //TODO state machine change -// break; - -// case SUBSYSTEM_TYPE_MAG: -// //TODO state machine change -// break; - -// case SUBSYSTEM_TYPE_GPS: -// //TODO state machine change -// break; - -// default: -// break; -// } - - -// } - - -// void update_state_machine_subsystem_unhealthy(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type) -// { -// bool previosly_healthy = (bool)(current_status->onboard_control_sensors_health & 1 << *subsystem_type); -// current_status->onboard_control_sensors_health &= ~(1 << *subsystem_type); -// current_status->counter++; -// current_status->timestamp = hrt_absolute_time(); -// orb_publish(ORB_ID(vehicle_status), status_pub, current_status); - -// /* if we received unhealthy message more than *_HEALTH_COUNTER_LIMIT, switch to error state */ - -// switch (*subsystem_type) { -// case SUBSYSTEM_TYPE_GYRO: -// //global_data_send_mavlink_statustext_message_out("Commander: gyro unhealthy", MAV_SEVERITY_CRITICAL); - -// if (previosly_healthy) //only throw emergency if previously healthy -// state_machine_emergency_always_critical(status_pub, current_status); - -// break; - -// case SUBSYSTEM_TYPE_ACC: -// //global_data_send_mavlink_statustext_message_out("Commander: accelerometer unhealthy", MAV_SEVERITY_CRITICAL); - -// if (previosly_healthy) //only throw emergency if previously healthy -// state_machine_emergency_always_critical(status_pub, current_status); - -// break; - -// case SUBSYSTEM_TYPE_MAG: -// //global_data_send_mavlink_statustext_message_out("Commander: magnetometer unhealthy", MAV_SEVERITY_CRITICAL); - -// if (previosly_healthy) //only throw emergency if previously healthy -// state_machine_emergency_always_critical(status_pub, current_status); - -// break; - -// case SUBSYSTEM_TYPE_GPS: -// // //TODO: remove this block -// // break; -// // /////////////////// -// //global_data_send_mavlink_statustext_message_out("Commander: GPS unhealthy", MAV_SEVERITY_CRITICAL); - -// // printf("previosly_healthy = %u\n", previosly_healthy); -// if (previosly_healthy) //only throw emergency if previously healthy -// state_machine_emergency(status_pub, current_status); - -// break; - -// default: -// break; -// } - -// } - - -/* END SUBSYSTEM/EMERGENCY FUNCTIONS*/ - - -void update_state_machine_got_position_fix(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) -{ - /* Depending on the current state switch state */ - if (current_status->state_machine == SYSTEM_STATE_PREFLIGHT) { - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STANDBY); - } -} - -void update_state_machine_no_position_fix(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) -{ - /* Depending on the current state switch state */ - if (current_status->state_machine == SYSTEM_STATE_STANDBY || current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_AUTO) { - state_machine_emergency(status_pub, current_status, mavlink_fd); - } -} - -void update_state_machine_arm(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) -{ - if (current_status->state_machine == SYSTEM_STATE_STANDBY) { - printf("[cmd] arming\n"); - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_GROUND_READY); - } -} - -void update_state_machine_disarm(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) -{ - if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_PREFLIGHT) { - printf("[cmd] going standby\n"); - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STANDBY); - - } else if (current_status->state_machine == SYSTEM_STATE_STABILIZED || current_status->state_machine == SYSTEM_STATE_AUTO) { - printf("[cmd] MISSION ABORT!\n"); - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STANDBY); - } -} - -void update_state_machine_mode_manual(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) -{ - int old_mode = current_status->flight_mode; - current_status->flight_mode = VEHICLE_FLIGHT_MODE_MANUAL; - - current_status->flag_control_manual_enabled = true; - - /* set behaviour based on airframe */ - if ((current_status->system_type == VEHICLE_TYPE_QUADROTOR) || - (current_status->system_type == VEHICLE_TYPE_HEXAROTOR) || - (current_status->system_type == VEHICLE_TYPE_OCTOROTOR)) { - - /* assuming a rotary wing, set to SAS */ - current_status->manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_SAS; - current_status->flag_control_attitude_enabled = true; - current_status->flag_control_rates_enabled = true; - - } else { - - /* assuming a fixed wing, set to direct pass-through */ - current_status->manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_DIRECT; - current_status->flag_control_attitude_enabled = false; - current_status->flag_control_rates_enabled = false; - } - - if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd); - - if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_STABILIZED || current_status->state_machine == SYSTEM_STATE_AUTO) { - printf("[cmd] manual mode\n"); - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_MANUAL); - } -} - -void update_state_machine_mode_stabilized(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) -{ - if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_STABILIZED || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_AUTO) { - int old_mode = current_status->flight_mode; - int old_manual_control_mode = current_status->manual_control_mode; - current_status->flight_mode = VEHICLE_FLIGHT_MODE_MANUAL; - current_status->manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_SAS; - current_status->flag_control_attitude_enabled = true; - current_status->flag_control_rates_enabled = true; - current_status->flag_control_manual_enabled = true; - - if (old_mode != current_status->flight_mode || - old_manual_control_mode != current_status->manual_control_mode) { - printf("[cmd] att stabilized mode\n"); - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_MANUAL); - state_machine_publish(status_pub, current_status, mavlink_fd); - } - - } -} - -void update_state_machine_mode_guided(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) -{ - if (!current_status->flag_vector_flight_mode_ok) { - mavlink_log_critical(mavlink_fd, "NO POS LOCK, REJ. GUIDED MODE"); - tune_error(); - return; - } - - if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_AUTO) { - printf("[cmd] position guided mode\n"); - int old_mode = current_status->flight_mode; - current_status->flight_mode = VEHICLE_FLIGHT_MODE_STAB; - current_status->flag_control_manual_enabled = false; - current_status->flag_control_attitude_enabled = true; - current_status->flag_control_rates_enabled = true; - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STABILIZED); - - if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd); - - } -} - -void update_state_machine_mode_auto(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) -{ - if (!current_status->flag_vector_flight_mode_ok) { - mavlink_log_critical(mavlink_fd, "NO POS LOCK, REJ. AUTO MODE"); - return; - } - - if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_STABILIZED) { - printf("[cmd] auto mode\n"); - int old_mode = current_status->flight_mode; - current_status->flight_mode = VEHICLE_FLIGHT_MODE_AUTO; - current_status->flag_control_manual_enabled = false; - current_status->flag_control_attitude_enabled = true; - current_status->flag_control_rates_enabled = true; - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_AUTO); - - if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd); - } -} - - -uint8_t update_state_machine_mode_request(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, uint8_t mode) -{ - uint8_t ret = 1; - - /* Switch on HIL if in standby and not already in HIL mode */ - if ((mode & VEHICLE_MODE_FLAG_HIL_ENABLED) - && !current_status->flag_hil_enabled) { - if ((current_status->state_machine == SYSTEM_STATE_STANDBY)) { - /* Enable HIL on request */ - current_status->flag_hil_enabled = true; - ret = OK; - state_machine_publish(status_pub, current_status, mavlink_fd); - publish_armed_status(current_status); - printf("[cmd] Enabling HIL, locking down all actuators for safety.\n\t(Arming the system will not activate them while in HIL mode)\n"); - - } else if (current_status->state_machine != SYSTEM_STATE_STANDBY && - current_status->flag_system_armed) { - - mavlink_log_critical(mavlink_fd, "REJECTING HIL, disarm first!") - - } else { - - mavlink_log_critical(mavlink_fd, "REJECTING HIL, not in standby.") - } - } - - /* switch manual / auto */ - if (mode & VEHICLE_MODE_FLAG_AUTO_ENABLED) { - update_state_machine_mode_auto(status_pub, current_status, mavlink_fd); - - } else if (mode & VEHICLE_MODE_FLAG_STABILIZED_ENABLED) { - update_state_machine_mode_stabilized(status_pub, current_status, mavlink_fd); - - } else if (mode & VEHICLE_MODE_FLAG_GUIDED_ENABLED) { - update_state_machine_mode_guided(status_pub, current_status, mavlink_fd); - - } else if (mode & VEHICLE_MODE_FLAG_MANUAL_INPUT_ENABLED) { - update_state_machine_mode_manual(status_pub, current_status, mavlink_fd); - } - - /* vehicle is disarmed, mode requests arming */ - if (!(current_status->flag_system_armed) && (mode & VEHICLE_MODE_FLAG_SAFETY_ARMED)) { - /* only arm in standby state */ - // XXX REMOVE - if (current_status->state_machine == SYSTEM_STATE_STANDBY || current_status->state_machine == SYSTEM_STATE_PREFLIGHT) { - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_GROUND_READY); - ret = OK; - printf("[cmd] arming due to command request\n"); - } - } - - /* vehicle is armed, mode requests disarming */ - if (current_status->flag_system_armed && !(mode & VEHICLE_MODE_FLAG_SAFETY_ARMED)) { - /* only disarm in ground ready */ - if (current_status->state_machine == SYSTEM_STATE_GROUND_READY) { - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STANDBY); - ret = OK; - printf("[cmd] disarming due to command request\n"); - } - } - - /* NEVER actually switch off HIL without reboot */ - if (current_status->flag_hil_enabled && !(mode & VEHICLE_MODE_FLAG_HIL_ENABLED)) { - warnx("DENYING request to switch off HIL. Please power cycle (safety reasons)\n"); - mavlink_log_critical(mavlink_fd, "Power-cycle to exit HIL"); - ret = ERROR; - } - - return ret; -} - -uint8_t update_state_machine_custom_mode_request(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, uint8_t custom_mode) //TODO: add more checks to avoid state switching in critical situations -{ - commander_state_machine_t current_system_state = current_status->state_machine; - - uint8_t ret = 1; - - switch (custom_mode) { - case SYSTEM_STATE_GROUND_READY: - break; - - case SYSTEM_STATE_STANDBY: - break; - - case SYSTEM_STATE_REBOOT: - printf("try to reboot\n"); - - if (current_system_state == SYSTEM_STATE_STANDBY - || current_system_state == SYSTEM_STATE_PREFLIGHT - || current_status->flag_hil_enabled) { - printf("system will reboot\n"); - mavlink_log_critical(mavlink_fd, "Rebooting.."); - usleep(200000); - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_REBOOT); - ret = 0; - } - - break; - - case SYSTEM_STATE_AUTO: - printf("try to switch to auto/takeoff\n"); - - if (current_system_state == SYSTEM_STATE_GROUND_READY || current_system_state == SYSTEM_STATE_MANUAL) { - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_AUTO); - printf("state: auto\n"); - ret = 0; - } - - break; - - case SYSTEM_STATE_MANUAL: - printf("try to switch to manual\n"); - - if (current_system_state == SYSTEM_STATE_GROUND_READY || current_system_state == SYSTEM_STATE_AUTO) { - do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_MANUAL); - printf("state: manual\n"); - ret = 0; - } - - break; - - default: - break; - } - - return ret; -} +///* END SUBSYSTEM/EMERGENCY FUNCTIONS*/ +// +//int update_state_machine_mode_request(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, uint8_t mode) +//{ +// int ret = 1; +// +//// /* Switch on HIL if in standby and not already in HIL mode */ +//// if ((mode & VEHICLE_MODE_FLAG_HIL_ENABLED) +//// && !current_status->flag_hil_enabled) { +//// if ((current_status->state_machine == SYSTEM_STATE_STANDBY)) { +//// /* Enable HIL on request */ +//// current_status->flag_hil_enabled = true; +//// ret = OK; +//// state_machine_publish(status_pub, current_status, mavlink_fd); +//// publish_armed_status(current_status); +//// printf("[cmd] Enabling HIL, locking down all actuators for safety.\n\t(Arming the system will not activate them while in HIL mode)\n"); +//// +//// } else if (current_status->state_machine != SYSTEM_STATE_STANDBY && +//// current_status->flag_fmu_armed) { +//// +//// mavlink_log_critical(mavlink_fd, "REJECTING HIL, disarm first!") +//// +//// } else { +//// +//// mavlink_log_critical(mavlink_fd, "REJECTING HIL, not in standby.") +//// } +//// } +// +// /* switch manual / auto */ +// if (mode & VEHICLE_MODE_FLAG_AUTO_ENABLED) { +// update_state_machine_mode_auto(status_pub, current_status, mavlink_fd); +// +// } else if (mode & VEHICLE_MODE_FLAG_STABILIZED_ENABLED) { +// update_state_machine_mode_stabilized(status_pub, current_status, mavlink_fd); +// +// } else if (mode & VEHICLE_MODE_FLAG_GUIDED_ENABLED) { +// update_state_machine_mode_guided(status_pub, current_status, mavlink_fd); +// +// } else if (mode & VEHICLE_MODE_FLAG_MANUAL_INPUT_ENABLED) { +// update_state_machine_mode_manual(status_pub, current_status, mavlink_fd); +// } +// +// /* vehicle is disarmed, mode requests arming */ +// if (!(current_status->flag_fmu_armed) && (mode & VEHICLE_MODE_FLAG_SAFETY_ARMED)) { +// /* only arm in standby state */ +// // XXX REMOVE +// if (current_status->state_machine == SYSTEM_STATE_STANDBY || current_status->state_machine == SYSTEM_STATE_PREFLIGHT) { +// do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_GROUND_READY); +// ret = OK; +// printf("[cmd] arming due to command request\n"); +// } +// } +// +// /* vehicle is armed, mode requests disarming */ +// if (current_status->flag_fmu_armed && !(mode & VEHICLE_MODE_FLAG_SAFETY_ARMED)) { +// /* only disarm in ground ready */ +// if (current_status->state_machine == SYSTEM_STATE_GROUND_READY) { +// do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STANDBY); +// ret = OK; +// printf("[cmd] disarming due to command request\n"); +// } +// } +// +// /* NEVER actually switch off HIL without reboot */ +// if (current_status->flag_hil_enabled && !(mode & VEHICLE_MODE_FLAG_HIL_ENABLED)) { +// warnx("DENYING request to switch off HIL. Please power cycle (safety reasons)\n"); +// mavlink_log_critical(mavlink_fd, "Power-cycle to exit HIL"); +// ret = ERROR; +// } +// +// return ret; +//} diff --git a/src/modules/commander/state_machine_helper.h b/src/modules/commander/state_machine_helper.h index 2f2ccc729..b553a4b56 100644 --- a/src/modules/commander/state_machine_helper.h +++ b/src/modules/commander/state_machine_helper.h @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Copyright (C) 2013 PX4 Development Team. All rights reserved. * Author: Thomas Gubler <thomasgubler@student.ethz.ch> * Julian Oes <joes@student.ethz.ch> * @@ -46,164 +46,14 @@ #include <uORB/uORB.h> #include <uORB/topics/vehicle_status.h> +#include <uORB/topics/actuator_safety.h> +#include <uORB/topics/vehicle_control_mode.h> -/** - * Switch to new state with no checking. - * - * do_state_update: this is the functions that all other functions have to call in order to update the state. - * the function does not question the state change, this must be done before - * The function performs actions that are connected with the new state (buzzer, reboot, ...) - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - * - * @return 0 (macro OK) or 1 on error (macro ERROR) - */ -int do_state_update(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, commander_state_machine_t new_state); - -/* These functions decide if an emergency exits and then switch to SYSTEM_STATE_MISSION_ABORT or SYSTEM_STATE_GROUND_ERROR */ -// void update_state_machine_subsystem_present(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type); -// void update_state_machine_subsystem_notpresent(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type); - -// void update_state_machine_subsystem_enabled(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type); -// void update_state_machine_subsystem_disabled(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type); - -// void update_state_machine_subsystem_healthy(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type); -// void update_state_machine_subsystem_unhealthy(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type); - - -/** - * Handle state machine if got position fix - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -void update_state_machine_got_position_fix(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd); - -/** - * Handle state machine if position fix lost - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -void update_state_machine_no_position_fix(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd); - -/** - * Handle state machine if user wants to arm - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -void update_state_machine_arm(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd); - -/** - * Handle state machine if user wants to disarm - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -void update_state_machine_disarm(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd); - -/** - * Handle state machine if mode switch is manual - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -void update_state_machine_mode_manual(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd); - -/** - * Handle state machine if mode switch is stabilized - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -void update_state_machine_mode_stabilized(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd); - -/** - * Handle state machine if mode switch is guided - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -void update_state_machine_mode_guided(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd); - -/** - * Handle state machine if mode switch is auto - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -void update_state_machine_mode_auto(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd); - -/** - * Publish current state information - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -void state_machine_publish(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd); - - -/* - * Functions that handle incoming requests to change the state machine or a parameter (probably from the mavlink app). - * If the request is obeyed the functions return 0 - * - */ - -/** - * Handles *incoming request* to switch to a specific state, if state change is successful returns 0 - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -uint8_t update_state_machine_mode_request(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, uint8_t mode); -/** - * Handles *incoming request* to switch to a specific custom state, if state change is successful returns 0 - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -uint8_t update_state_machine_custom_mode_request(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, uint8_t custom_mode); - -/** - * Always switches to critical mode under any circumstances. - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -void state_machine_emergency_always_critical(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd); - -/** - * Switches to emergency if required. - * - * @param status_pub file descriptor for state update topic publication - * @param current_status pointer to the current state machine to operate on - * @param mavlink_fd file descriptor for MAVLink statustext messages - */ -void state_machine_emergency(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd); - -/** - * Publish the armed state depending on the current system state - * - * @param current_status the current system status - */ -void publish_armed_status(const struct vehicle_status_s *current_status); +int arming_state_transition(int status_pub, struct vehicle_status_s *current_state, arming_state_t new_arming_state, int safety_pub, struct actuator_safety_s *safety, const int mavlink_fd); +int navigation_state_transition(int status_pub, struct vehicle_status_s *current_state, navigation_state_t new_navigation_state, int control_mode_pub, struct vehicle_control_mode_s *control_mode, const int mavlink_fd); +int hil_state_transition(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, hil_state_t new_state); #endif /* STATE_MACHINE_HELPER_H_ */ diff --git a/src/modules/controllib/fixedwing.cpp b/src/modules/controllib/fixedwing.cpp index 77b2ac806..9435959e9 100644 --- a/src/modules/controllib/fixedwing.cpp +++ b/src/modules/controllib/fixedwing.cpp @@ -39,6 +39,7 @@ #include "fixedwing.hpp" + namespace control { @@ -210,8 +211,9 @@ void BlockMultiModeBacksideAutopilot::update() for (unsigned i = 4; i < NUM_ACTUATOR_CONTROLS; i++) _actuators.control[i] = 0.0f; +#warning this if is incomplete, should be based on flags // only update guidance in auto mode - if (_status.state_machine == SYSTEM_STATE_AUTO) { + if (_status.navigation_state == NAVIGATION_STATE_AUTO_MISSION) { // update guidance _guide.update(_pos, _att, _posCmd.current, _lastPosCmd.current); } @@ -220,9 +222,10 @@ void BlockMultiModeBacksideAutopilot::update() // once the system switches from manual or auto to stabilized // the setpoint should update to loitering around this position +#warning should be base on flags // handle autopilot modes - if (_status.state_machine == SYSTEM_STATE_AUTO || - _status.state_machine == SYSTEM_STATE_STABILIZED) { + if (_status.navigation_state == NAVIGATION_STATE_AUTO_MISSION || + _status.navigation_state == NAVIGATION_STATE_SEATBELT) { // update guidance _guide.update(_pos, _att, _posCmd.current, _lastPosCmd.current); @@ -280,15 +283,16 @@ void BlockMultiModeBacksideAutopilot::update() _actuators.control[CH_THR] : _manual.throttle; } - } else if (_status.state_machine == SYSTEM_STATE_MANUAL) { - - if (_status.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_DIRECT) { - _actuators.control[CH_AIL] = _manual.roll; - _actuators.control[CH_ELV] = _manual.pitch; - _actuators.control[CH_RDR] = _manual.yaw; - _actuators.control[CH_THR] = _manual.throttle; + } else if (_status.navigation_state == NAVIGATION_STATE_MANUAL) { - } else if (_status.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_SAS) { +#warning fix here too +// if (_status.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_DIRECT) { +// _actuators.control[CH_AIL] = _manual.roll; +// _actuators.control[CH_ELV] = _manual.pitch; +// _actuators.control[CH_RDR] = _manual.yaw; +// _actuators.control[CH_THR] = _manual.throttle; +// +// } else if (_status.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_SAS) { // calculate velocity, XXX should be airspeed, but using ground speed for now // for the purpose of control we will limit the velocity feedback between @@ -344,7 +348,8 @@ void BlockMultiModeBacksideAutopilot::update() _actuators.control[CH_THR] = (_actuators.control[CH_THR] < _manual.throttle) ? _actuators.control[CH_THR] : _manual.throttle; } - } +#warning fix this +// } // body rates controller, disabled for now else if (0 /*_status.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_SAS*/) { diff --git a/src/modules/fixedwing_att_control/fixedwing_att_control_att.c b/src/modules/fixedwing_att_control/fixedwing_att_control_att.c index 2aeca3a98..68c176459 100644 --- a/src/modules/fixedwing_att_control/fixedwing_att_control_att.c +++ b/src/modules/fixedwing_att_control/fixedwing_att_control_att.c @@ -142,7 +142,7 @@ int fixedwing_att_control_attitude(const struct vehicle_attitude_setpoint_s *att } /* Roll (P) */ - rates_sp->roll = pid_calculate(&roll_controller, att_sp->roll_body, att->roll, 0, 0); + rates_sp->roll = pid_calculate(&roll_controller, att_sp->roll_body, att->roll, 0, 0, NULL, NULL, NULL); /* Pitch (P) */ @@ -152,7 +152,7 @@ int fixedwing_att_control_attitude(const struct vehicle_attitude_setpoint_s *att /* set pitch plus feedforward roll compensation */ rates_sp->pitch = pid_calculate(&pitch_controller, att_sp->pitch_body + pitch_sp_rollcompensation, - att->pitch, 0, 0); + att->pitch, 0, 0, NULL, NULL, NULL); /* Yaw (from coordinated turn constraint or lateral force) */ rates_sp->yaw = (att->rollspeed * rates_sp->roll + 9.81f * sinf(att->roll) * cosf(att->pitch) + speed_body[0] * rates_sp->pitch * sinf(att->roll)) diff --git a/src/modules/fixedwing_att_control/fixedwing_att_control_main.c b/src/modules/fixedwing_att_control/fixedwing_att_control_main.c index 6c9c137bb..b96fc3e5a 100644 --- a/src/modules/fixedwing_att_control/fixedwing_att_control_main.c +++ b/src/modules/fixedwing_att_control/fixedwing_att_control_main.c @@ -186,87 +186,88 @@ int fixedwing_att_control_thread_main(int argc, char *argv[]) /* control */ - if (vstatus.state_machine == SYSTEM_STATE_AUTO || - vstatus.state_machine == SYSTEM_STATE_STABILIZED) { - /* attitude control */ - fixedwing_att_control_attitude(&att_sp, &att, speed_body, &rates_sp); - - /* angular rate control */ - fixedwing_att_control_rates(&rates_sp, gyro, &actuators); - - /* pass through throttle */ - actuators.control[3] = att_sp.thrust; - - /* set flaps to zero */ - actuators.control[4] = 0.0f; - - } else if (vstatus.state_machine == SYSTEM_STATE_MANUAL) { - if (vstatus.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_SAS) { - - /* if the RC signal is lost, try to stay level and go slowly back down to ground */ - if (vstatus.rc_signal_lost) { - - /* put plane into loiter */ - att_sp.roll_body = 0.3f; - att_sp.pitch_body = 0.0f; - - /* limit throttle to 60 % of last value if sane */ - if (isfinite(manual_sp.throttle) && - (manual_sp.throttle >= 0.0f) && - (manual_sp.throttle <= 1.0f)) { - att_sp.thrust = 0.6f * manual_sp.throttle; - - } else { - att_sp.thrust = 0.0f; - } - - att_sp.yaw_body = 0; - - // XXX disable yaw control, loiter - - } else { - - att_sp.roll_body = manual_sp.roll; - att_sp.pitch_body = manual_sp.pitch; - att_sp.yaw_body = 0; - att_sp.thrust = manual_sp.throttle; - } - - att_sp.timestamp = hrt_absolute_time(); - - /* attitude control */ - fixedwing_att_control_attitude(&att_sp, &att, speed_body, &rates_sp); - - /* angular rate control */ - fixedwing_att_control_rates(&rates_sp, gyro, &actuators); - - /* pass through throttle */ - actuators.control[3] = att_sp.thrust; - - /* pass through flaps */ - if (isfinite(manual_sp.flaps)) { - actuators.control[4] = manual_sp.flaps; - - } else { - actuators.control[4] = 0.0f; - } - - } else if (vstatus.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_DIRECT) { - /* directly pass through values */ - actuators.control[0] = manual_sp.roll; - /* positive pitch means negative actuator -> pull up */ - actuators.control[1] = manual_sp.pitch; - actuators.control[2] = manual_sp.yaw; - actuators.control[3] = manual_sp.throttle; - - if (isfinite(manual_sp.flaps)) { - actuators.control[4] = manual_sp.flaps; - - } else { - actuators.control[4] = 0.0f; - } - } - } +#warning fix this +// if (vstatus.state_machine == SYSTEM_STATE_AUTO || +// vstatus.state_machine == SYSTEM_STATE_STABILIZED) { +// /* attitude control */ +// fixedwing_att_control_attitude(&att_sp, &att, speed_body, &rates_sp); +// +// /* angular rate control */ +// fixedwing_att_control_rates(&rates_sp, gyro, &actuators); +// +// /* pass through throttle */ +// actuators.control[3] = att_sp.thrust; +// +// /* set flaps to zero */ +// actuators.control[4] = 0.0f; +// +// } else if (vstatus.state_machine == SYSTEM_STATE_MANUAL) { +// if (vstatus.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_SAS) { +// +// /* if the RC signal is lost, try to stay level and go slowly back down to ground */ +// if (vstatus.rc_signal_lost) { +// +// /* put plane into loiter */ +// att_sp.roll_body = 0.3f; +// att_sp.pitch_body = 0.0f; +// +// /* limit throttle to 60 % of last value if sane */ +// if (isfinite(manual_sp.throttle) && +// (manual_sp.throttle >= 0.0f) && +// (manual_sp.throttle <= 1.0f)) { +// att_sp.thrust = 0.6f * manual_sp.throttle; +// +// } else { +// att_sp.thrust = 0.0f; +// } +// +// att_sp.yaw_body = 0; +// +// // XXX disable yaw control, loiter +// +// } else { +// +// att_sp.roll_body = manual_sp.roll; +// att_sp.pitch_body = manual_sp.pitch; +// att_sp.yaw_body = 0; +// att_sp.thrust = manual_sp.throttle; +// } +// +// att_sp.timestamp = hrt_absolute_time(); +// +// /* attitude control */ +// fixedwing_att_control_attitude(&att_sp, &att, speed_body, &rates_sp); +// +// /* angular rate control */ +// fixedwing_att_control_rates(&rates_sp, gyro, &actuators); +// +// /* pass through throttle */ +// actuators.control[3] = att_sp.thrust; +// +// /* pass through flaps */ +// if (isfinite(manual_sp.flaps)) { +// actuators.control[4] = manual_sp.flaps; +// +// } else { +// actuators.control[4] = 0.0f; +// } +// +// } else if (vstatus.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_DIRECT) { +// /* directly pass through values */ +// actuators.control[0] = manual_sp.roll; +// /* positive pitch means negative actuator -> pull up */ +// actuators.control[1] = manual_sp.pitch; +// actuators.control[2] = manual_sp.yaw; +// actuators.control[3] = manual_sp.throttle; +// +// if (isfinite(manual_sp.flaps)) { +// actuators.control[4] = manual_sp.flaps; +// +// } else { +// actuators.control[4] = 0.0f; +// } +// } +// } /* publish rates */ orb_publish(ORB_ID(vehicle_rates_setpoint), rates_pub, &rates_sp); diff --git a/src/modules/fixedwing_att_control/fixedwing_att_control_rate.c b/src/modules/fixedwing_att_control/fixedwing_att_control_rate.c index cdab39edc..66854592a 100644 --- a/src/modules/fixedwing_att_control/fixedwing_att_control_rate.c +++ b/src/modules/fixedwing_att_control/fixedwing_att_control_rate.c @@ -196,11 +196,11 @@ int fixedwing_att_control_rates(const struct vehicle_rates_setpoint_s *rate_sp, /* roll rate (PI) */ - actuators->control[0] = pid_calculate(&roll_rate_controller, rate_sp->roll, rates[0], 0.0f, deltaT); + actuators->control[0] = pid_calculate(&roll_rate_controller, rate_sp->roll, rates[0], 0.0f, deltaT, NULL, NULL, NULL); /* pitch rate (PI) */ - actuators->control[1] = -pid_calculate(&pitch_rate_controller, rate_sp->pitch, rates[1], 0.0f, deltaT); + actuators->control[1] = -pid_calculate(&pitch_rate_controller, rate_sp->pitch, rates[1], 0.0f, deltaT, NULL, NULL, NULL); /* yaw rate (PI) */ - actuators->control[2] = pid_calculate(&yaw_rate_controller, rate_sp->yaw, rates[2], 0.0f, deltaT); + actuators->control[2] = pid_calculate(&yaw_rate_controller, rate_sp->yaw, rates[2], 0.0f, deltaT, NULL, NULL, NULL); counter++; diff --git a/src/modules/fixedwing_pos_control/fixedwing_pos_control_main.c b/src/modules/fixedwing_pos_control/fixedwing_pos_control_main.c index 73df3fb9e..87a942ffb 100644 --- a/src/modules/fixedwing_pos_control/fixedwing_pos_control_main.c +++ b/src/modules/fixedwing_pos_control/fixedwing_pos_control_main.c @@ -271,7 +271,7 @@ int fixedwing_pos_control_thread_main(int argc, char *argv[]) pid_set_parameters(&heading_controller, p.heading_p, 0, 0, 0, 10000.0f); //arbitrary high limit pid_set_parameters(&heading_rate_controller, p.headingr_p, p.headingr_i, 0, 0, p.roll_lim); pid_set_parameters(&altitude_controller, p.altitude_p, 0, 0, 0, p.pitch_lim); - pid_set_parameters(&offtrack_controller, p.xtrack_p, 0, 0, 0, 60.0f * M_DEG_TO_RAD); //TODO: remove hardcoded value + pid_set_parameters(&offtrack_controller, p.xtrack_p, 0, 0, 0, 60.0f * M_DEG_TO_RAD_F); //TODO: remove hardcoded value } /* only run controller if attitude changed */ @@ -319,7 +319,7 @@ int fixedwing_pos_control_thread_main(int argc, char *argv[]) // XXX what is xtrack_err.past_end? if (distance_res == OK /*&& !xtrack_err.past_end*/) { - float delta_psi_c = pid_calculate(&offtrack_controller, 0, xtrack_err.distance, 0.0f, 0.0f); //p.xtrack_p * xtrack_err.distance + float delta_psi_c = pid_calculate(&offtrack_controller, 0, xtrack_err.distance, 0.0f, 0.0f, NULL, NULL, NULL); //p.xtrack_p * xtrack_err.distance float psi_c = psi_track + delta_psi_c; float psi_e = psi_c - att.yaw; @@ -336,7 +336,7 @@ int fixedwing_pos_control_thread_main(int argc, char *argv[]) } /* calculate roll setpoint, do this artificially around zero */ - float delta_psi_rate_c = pid_calculate(&heading_controller, psi_e, 0.0f, 0.0f, 0.0f); + float delta_psi_rate_c = pid_calculate(&heading_controller, psi_e, 0.0f, 0.0f, 0.0f, NULL, NULL, NULL); float psi_rate_track = 0; //=V_gr/r_track , this will be needed for implementation of arc following float psi_rate_c = delta_psi_rate_c + psi_rate_track; @@ -359,7 +359,7 @@ int fixedwing_pos_control_thread_main(int argc, char *argv[]) float psi_rate_e_scaled = psi_rate_e * ground_speed / 9.81f; //* V_gr / g - attitude_setpoint.roll_body = pid_calculate(&heading_rate_controller, psi_rate_e_scaled, 0.0f, 0.0f, deltaT); + attitude_setpoint.roll_body = pid_calculate(&heading_rate_controller, psi_rate_e_scaled, 0.0f, 0.0f, deltaT, NULL, NULL, NULL); if (verbose) { printf("psi_rate_c %.4f ", (double)psi_rate_c); @@ -379,7 +379,7 @@ int fixedwing_pos_control_thread_main(int argc, char *argv[]) if (pos_updated) { //TODO: take care of relative vs. ab. altitude - attitude_setpoint.pitch_body = pid_calculate(&altitude_controller, global_setpoint.altitude, global_pos.alt, 0.0f, 0.0f); + attitude_setpoint.pitch_body = pid_calculate(&altitude_controller, global_setpoint.altitude, global_pos.alt, 0.0f, 0.0f, NULL, NULL, NULL); } diff --git a/src/modules/gpio_led/gpio_led.c b/src/modules/gpio_led/gpio_led.c index 43cbe74c7..618095d0b 100644 --- a/src/modules/gpio_led/gpio_led.c +++ b/src/modules/gpio_led/gpio_led.c @@ -51,6 +51,7 @@ #include <systemlib/err.h> #include <uORB/uORB.h> #include <uORB/topics/vehicle_status.h> +#include <uORB/topics/actuator_safety.h> #include <poll.h> #include <drivers/drv_gpio.h> @@ -60,6 +61,8 @@ struct gpio_led_s { int pin; struct vehicle_status_s status; int vehicle_status_sub; + struct actuator_safety_s safety; + int actuator_safety_sub; bool led_state; int counter; }; @@ -168,10 +171,15 @@ void gpio_led_cycle(FAR void *arg) if (status_updated) orb_copy(ORB_ID(vehicle_status), priv->vehicle_status_sub, &priv->status); + orb_check(priv->vehicle_status_sub, &status_updated); + + if (status_updated) + orb_copy(ORB_ID(actuator_safety), priv->actuator_safety_sub, &priv->safety); + /* select pattern for current status */ int pattern = 0; - if (priv->status.flag_system_armed) { + if (priv->safety.armed) { if (priv->status.battery_warning == VEHICLE_BATTERY_WARNING_NONE) { pattern = 0x3f; // ****** solid (armed) @@ -180,11 +188,10 @@ void gpio_led_cycle(FAR void *arg) } } else { - if (priv->status.state_machine == SYSTEM_STATE_PREFLIGHT) { + if (priv->safety.ready_to_arm) { pattern = 0x00; // ______ off (disarmed, preflight check) - } else if (priv->status.state_machine == SYSTEM_STATE_STANDBY && - priv->status.battery_warning == VEHICLE_BATTERY_WARNING_NONE) { + } else if (priv->safety.ready_to_arm && priv->status.battery_warning == VEHICLE_BATTERY_WARNING_NONE) { pattern = 0x38; // ***___ slow blink (disarmed, ready) } else { diff --git a/src/modules/mavlink/mavlink.c b/src/modules/mavlink/mavlink.c index 5b8345e7e..f6c371c7c 100644 --- a/src/modules/mavlink/mavlink.c +++ b/src/modules/mavlink/mavlink.c @@ -187,95 +187,88 @@ get_mavlink_mode_and_state(uint8_t *mavlink_state, uint8_t *mavlink_mode) /* reset MAVLink mode bitfield */ *mavlink_mode = 0; - /* set mode flags independent of system state */ + /** + * Set mode flags + **/ /* HIL */ if (v_status.flag_hil_enabled) { *mavlink_mode |= MAV_MODE_FLAG_HIL_ENABLED; } - /* manual input */ - if (v_status.flag_control_manual_enabled) { - *mavlink_mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED; - } - - /* attitude or rate control */ - if (v_status.flag_control_attitude_enabled || - v_status.flag_control_rates_enabled) { - *mavlink_mode |= MAV_MODE_FLAG_STABILIZE_ENABLED; - } - - /* vector control */ - if (v_status.flag_control_velocity_enabled || - v_status.flag_control_position_enabled) { - *mavlink_mode |= MAV_MODE_FLAG_GUIDED_ENABLED; - } - /* autonomous mode */ - if (v_status.state_machine == SYSTEM_STATE_AUTO) { + if (v_status.navigation_state == NAVIGATION_STATE_AUTO_LAND + || v_status.navigation_state == NAVIGATION_STATE_AUTO_LOITER + || v_status.navigation_state == NAVIGATION_STATE_AUTO_MISSION + || v_status.navigation_state == NAVIGATION_STATE_AUTO_READY + || v_status.navigation_state == NAVIGATION_STATE_AUTO_RTL + || v_status.navigation_state == NAVIGATION_STATE_AUTO_STANDBY + || v_status.navigation_state == NAVIGATION_STATE_AUTO_TAKEOFF) { *mavlink_mode |= MAV_MODE_FLAG_AUTO_ENABLED; } /* set arming state */ - if (armed.armed) { + if (v_status.arming_state == ARMING_STATE_ARMED + || v_status.arming_state == ARMING_STATE_ARMED_ERROR) { *mavlink_mode |= MAV_MODE_FLAG_SAFETY_ARMED; } else { *mavlink_mode &= ~MAV_MODE_FLAG_SAFETY_ARMED; } - switch (v_status.state_machine) { - case SYSTEM_STATE_PREFLIGHT: - if (v_status.flag_preflight_gyro_calibration || - v_status.flag_preflight_mag_calibration || - v_status.flag_preflight_accel_calibration) { - *mavlink_state = MAV_STATE_CALIBRATING; + if (v_status.navigation_state == NAVIGATION_STATE_MANUAL + || v_status.navigation_state == NAVIGATION_STATE_MANUAL_STANDBY) { - } else { - *mavlink_state = MAV_STATE_UNINIT; - } + *mavlink_mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED; + } - break; + if (v_status.navigation_state == NAVIGATION_STATE_SEATBELT + || v_status.navigation_state == NAVIGATION_STATE_SEATBELT_DESCENT + || v_status.navigation_state == NAVIGATION_STATE_SEATBELT_STANDBY) { - case SYSTEM_STATE_STANDBY: - *mavlink_state = MAV_STATE_STANDBY; - break; + *mavlink_mode |= MAV_MODE_FLAG_GUIDED_ENABLED; + } - case SYSTEM_STATE_GROUND_READY: - *mavlink_state = MAV_STATE_ACTIVE; - break; - case SYSTEM_STATE_MANUAL: - *mavlink_state = MAV_STATE_ACTIVE; - break; + /** + * Set mavlink state + **/ - case SYSTEM_STATE_STABILIZED: - *mavlink_state = MAV_STATE_ACTIVE; - break; + /* set calibration state */ + if (v_status.flag_preflight_calibration) { - case SYSTEM_STATE_AUTO: - *mavlink_state = MAV_STATE_ACTIVE; - break; + *mavlink_state = MAV_STATE_CALIBRATING; - case SYSTEM_STATE_MISSION_ABORT: - *mavlink_state = MAV_STATE_EMERGENCY; - break; + } else if (v_status.flag_system_emergency) { - case SYSTEM_STATE_EMCY_LANDING: *mavlink_state = MAV_STATE_EMERGENCY; - break; - case SYSTEM_STATE_EMCY_CUTOFF: - *mavlink_state = MAV_STATE_EMERGENCY; - break; + // XXX difference between active and armed? is AUTO_READY active? + } else if (v_status.navigation_state == NAVIGATION_STATE_AUTO_LAND + || v_status.navigation_state == NAVIGATION_STATE_AUTO_LOITER + || v_status.navigation_state == NAVIGATION_STATE_AUTO_MISSION + || v_status.navigation_state == NAVIGATION_STATE_AUTO_RTL + || v_status.navigation_state == NAVIGATION_STATE_AUTO_TAKEOFF + || v_status.navigation_state == NAVIGATION_STATE_SEATBELT + || v_status.navigation_state == NAVIGATION_STATE_SEATBELT_DESCENT + || v_status.navigation_state == NAVIGATION_STATE_MANUAL) { - case SYSTEM_STATE_GROUND_ERROR: - *mavlink_state = MAV_STATE_EMERGENCY; - break; + *mavlink_state = MAV_STATE_ACTIVE; - case SYSTEM_STATE_REBOOT: - *mavlink_state = MAV_STATE_POWEROFF; - break; + } else if (v_status.navigation_state == NAVIGATION_STATE_AUTO_STANDBY + || v_status.navigation_state == NAVIGATION_STATE_AUTO_READY // XXX correct? + || v_status.navigation_state == NAVIGATION_STATE_SEATBELT_STANDBY + || v_status.navigation_state == NAVIGATION_STATE_MANUAL_STANDBY) { + + *mavlink_state = MAV_STATE_STANDBY; + + } else if (v_status.navigation_state == NAVIGATION_STATE_INIT) { + + *mavlink_state = MAV_STATE_UNINIT; + } else { + + warnx("Unknown mavlink state"); + *mavlink_state = MAV_STATE_CRITICAL; } } @@ -571,6 +564,7 @@ int mavlink_thread_main(int argc, char *argv[]) default: usage(); + break; } } @@ -681,7 +675,7 @@ int mavlink_thread_main(int argc, char *argv[]) get_mavlink_mode_and_state(&mavlink_state, &mavlink_mode); /* send heartbeat */ - mavlink_msg_heartbeat_send(chan, mavlink_system.type, MAV_AUTOPILOT_PX4, mavlink_mode, v_status.state_machine, mavlink_state); + mavlink_msg_heartbeat_send(chan, mavlink_system.type, MAV_AUTOPILOT_PX4, mavlink_mode, v_status.navigation_state, mavlink_state); /* switch HIL mode if required */ set_hil_on_off(v_status.flag_hil_enabled); diff --git a/src/modules/mavlink/orb_listener.c b/src/modules/mavlink/orb_listener.c index 0597555ab..a9a611998 100644 --- a/src/modules/mavlink/orb_listener.c +++ b/src/modules/mavlink/orb_listener.c @@ -71,7 +71,7 @@ struct vehicle_local_position_s local_pos; struct vehicle_status_s v_status; struct rc_channels_s rc; struct rc_input_values rc_raw; -struct actuator_armed_s armed; +struct actuator_safety_s safety; struct actuator_controls_effective_s actuators_0; struct vehicle_attitude_s att; @@ -111,7 +111,7 @@ static void l_global_position_setpoint(const struct listener *l); static void l_local_position_setpoint(const struct listener *l); static void l_attitude_setpoint(const struct listener *l); static void l_actuator_outputs(const struct listener *l); -static void l_actuator_armed(const struct listener *l); +static void l_actuator_safety(const struct listener *l); static void l_manual_control_setpoint(const struct listener *l); static void l_vehicle_attitude_controls(const struct listener *l); static void l_debug_key_value(const struct listener *l); @@ -136,7 +136,7 @@ static const struct listener listeners[] = { {l_actuator_outputs, &mavlink_subs.act_1_sub, 1}, {l_actuator_outputs, &mavlink_subs.act_2_sub, 2}, {l_actuator_outputs, &mavlink_subs.act_3_sub, 3}, - {l_actuator_armed, &mavlink_subs.armed_sub, 0}, + {l_actuator_safety, &mavlink_subs.safety_sub, 0}, {l_manual_control_setpoint, &mavlink_subs.man_control_sp_sub, 0}, {l_vehicle_attitude_controls, &mavlink_subs.actuators_sub, 0}, {l_debug_key_value, &mavlink_subs.debug_key_value, 0}, @@ -270,7 +270,7 @@ l_vehicle_status(const struct listener *l) { /* immediately communicate state changes back to user */ orb_copy(ORB_ID(vehicle_status), status_sub, &v_status); - orb_copy(ORB_ID(actuator_armed), mavlink_subs.armed_sub, &armed); + orb_copy(ORB_ID(actuator_safety), mavlink_subs.safety_sub, &safety); /* enable or disable HIL */ set_hil_on_off(v_status.flag_hil_enabled); @@ -285,7 +285,7 @@ l_vehicle_status(const struct listener *l) mavlink_system.type, MAV_AUTOPILOT_PX4, mavlink_mode, - v_status.state_machine, + v_status.navigation_state, mavlink_state); } @@ -467,7 +467,7 @@ l_actuator_outputs(const struct listener *l) act_outputs.output[7]); /* only send in HIL mode */ - if (mavlink_hil_enabled && armed.armed) { + if (mavlink_hil_enabled && safety.armed) { /* translate the current syste state to mavlink state and mode */ uint8_t mavlink_state = 0; @@ -539,9 +539,9 @@ l_actuator_outputs(const struct listener *l) } void -l_actuator_armed(const struct listener *l) +l_actuator_safety(const struct listener *l) { - orb_copy(ORB_ID(actuator_armed), mavlink_subs.armed_sub, &armed); + orb_copy(ORB_ID(actuator_safety), mavlink_subs.safety_sub, &safety); } void @@ -674,7 +674,7 @@ uorb_receive_thread(void *arg) /* handle the poll result */ if (poll_ret == 0) { - mavlink_missionlib_send_gcs_string("[mavlink] No telemetry data for 1 s"); + /* silent */ } else if (poll_ret < 0) { mavlink_missionlib_send_gcs_string("[mavlink] ERROR reading uORB data"); @@ -760,8 +760,8 @@ uorb_receive_start(void) orb_set_interval(mavlink_subs.act_3_sub, 100); /* 10Hz updates */ /* --- ACTUATOR ARMED VALUE --- */ - mavlink_subs.armed_sub = orb_subscribe(ORB_ID(actuator_armed)); - orb_set_interval(mavlink_subs.armed_sub, 100); /* 10Hz updates */ + mavlink_subs.safety_sub = orb_subscribe(ORB_ID(actuator_safety)); + orb_set_interval(mavlink_subs.safety_sub, 100); /* 10Hz updates */ /* --- MAPPED MANUAL CONTROL INPUTS --- */ mavlink_subs.man_control_sp_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); diff --git a/src/modules/mavlink/orb_topics.h b/src/modules/mavlink/orb_topics.h index 73e278dc6..3b968b911 100644 --- a/src/modules/mavlink/orb_topics.h +++ b/src/modules/mavlink/orb_topics.h @@ -55,10 +55,12 @@ #include <uORB/topics/vehicle_global_position_set_triplet.h> #include <uORB/topics/vehicle_attitude_setpoint.h> #include <uORB/topics/vehicle_rates_setpoint.h> +#include <uORB/topics/vehicle_control_mode.h> #include <uORB/topics/optical_flow.h> #include <uORB/topics/actuator_outputs.h> #include <uORB/topics/actuator_controls_effective.h> #include <uORB/topics/actuator_controls.h> +#include <uORB/topics/actuator_safety.h> #include <uORB/topics/manual_control_setpoint.h> #include <uORB/topics/telemetry_status.h> #include <uORB/topics/debug_key_value.h> @@ -75,7 +77,7 @@ struct mavlink_subscriptions { int act_3_sub; int gps_sub; int man_control_sp_sub; - int armed_sub; + int safety_sub; int actuators_sub; int local_pos_sub; int spa_sub; diff --git a/src/modules/mavlink_onboard/mavlink.c b/src/modules/mavlink_onboard/mavlink.c index cb6d6b16a..35d53b880 100644 --- a/src/modules/mavlink_onboard/mavlink.c +++ b/src/modules/mavlink_onboard/mavlink.c @@ -274,83 +274,89 @@ void mavlink_update_system(void) } void -get_mavlink_mode_and_state(const struct vehicle_status_s *v_status, const struct actuator_armed_s *armed, +get_mavlink_mode_and_state(const struct vehicle_control_mode_s *control_mode, const struct actuator_safety_s *safety, uint8_t *mavlink_state, uint8_t *mavlink_mode) { /* reset MAVLink mode bitfield */ *mavlink_mode = 0; /* set mode flags independent of system state */ - if (v_status->flag_control_manual_enabled) { + if (control_mode->flag_control_manual_enabled) { *mavlink_mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED; } - if (v_status->flag_hil_enabled) { + if (safety->hil_enabled) { *mavlink_mode |= MAV_MODE_FLAG_HIL_ENABLED; } /* set arming state */ - if (armed->armed) { + if (safety->armed) { *mavlink_mode |= MAV_MODE_FLAG_SAFETY_ARMED; } else { *mavlink_mode &= ~MAV_MODE_FLAG_SAFETY_ARMED; } - switch (v_status->state_machine) { - case SYSTEM_STATE_PREFLIGHT: - if (v_status->flag_preflight_gyro_calibration || - v_status->flag_preflight_mag_calibration || - v_status->flag_preflight_accel_calibration) { - *mavlink_state = MAV_STATE_CALIBRATING; - } else { - *mavlink_state = MAV_STATE_UNINIT; - } - break; - - case SYSTEM_STATE_STANDBY: - *mavlink_state = MAV_STATE_STANDBY; - break; - - case SYSTEM_STATE_GROUND_READY: - *mavlink_state = MAV_STATE_ACTIVE; - break; - - case SYSTEM_STATE_MANUAL: - *mavlink_state = MAV_STATE_ACTIVE; - *mavlink_mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED; - break; - - case SYSTEM_STATE_STABILIZED: - *mavlink_state = MAV_STATE_ACTIVE; - *mavlink_mode |= MAV_MODE_FLAG_STABILIZE_ENABLED; - break; - - case SYSTEM_STATE_AUTO: - *mavlink_state = MAV_STATE_ACTIVE; + if (control_mode->flag_control_velocity_enabled) { *mavlink_mode |= MAV_MODE_FLAG_GUIDED_ENABLED; - break; - - case SYSTEM_STATE_MISSION_ABORT: - *mavlink_state = MAV_STATE_EMERGENCY; - break; - - case SYSTEM_STATE_EMCY_LANDING: - *mavlink_state = MAV_STATE_EMERGENCY; - break; - - case SYSTEM_STATE_EMCY_CUTOFF: - *mavlink_state = MAV_STATE_EMERGENCY; - break; - - case SYSTEM_STATE_GROUND_ERROR: - *mavlink_state = MAV_STATE_EMERGENCY; - break; - - case SYSTEM_STATE_REBOOT: - *mavlink_state = MAV_STATE_POWEROFF; - break; + } else { + *mavlink_mode &= ~MAV_MODE_FLAG_GUIDED_ENABLED; } +// switch (v_status->state_machine) { +// case SYSTEM_STATE_PREFLIGHT: +// if (v_status->flag_preflight_gyro_calibration || +// v_status->flag_preflight_mag_calibration || +// v_status->flag_preflight_accel_calibration) { +// *mavlink_state = MAV_STATE_CALIBRATING; +// } else { +// *mavlink_state = MAV_STATE_UNINIT; +// } +// break; +// +// case SYSTEM_STATE_STANDBY: +// *mavlink_state = MAV_STATE_STANDBY; +// break; +// +// case SYSTEM_STATE_GROUND_READY: +// *mavlink_state = MAV_STATE_ACTIVE; +// break; +// +// case SYSTEM_STATE_MANUAL: +// *mavlink_state = MAV_STATE_ACTIVE; +// *mavlink_mode |= MAV_MODE_FLAG_MANUAL_INPUT_ENABLED; +// break; +// +// case SYSTEM_STATE_STABILIZED: +// *mavlink_state = MAV_STATE_ACTIVE; +// *mavlink_mode |= MAV_MODE_FLAG_STABILIZE_ENABLED; +// break; +// +// case SYSTEM_STATE_AUTO: +// *mavlink_state = MAV_STATE_ACTIVE; +// *mavlink_mode |= MAV_MODE_FLAG_GUIDED_ENABLED; +// break; +// +// case SYSTEM_STATE_MISSION_ABORT: +// *mavlink_state = MAV_STATE_EMERGENCY; +// break; +// +// case SYSTEM_STATE_EMCY_LANDING: +// *mavlink_state = MAV_STATE_EMERGENCY; +// break; +// +// case SYSTEM_STATE_EMCY_CUTOFF: +// *mavlink_state = MAV_STATE_EMERGENCY; +// break; +// +// case SYSTEM_STATE_GROUND_ERROR: +// *mavlink_state = MAV_STATE_EMERGENCY; +// break; +// +// case SYSTEM_STATE_REBOOT: +// *mavlink_state = MAV_STATE_POWEROFF; +// break; +// } + } /** @@ -362,8 +368,10 @@ int mavlink_thread_main(int argc, char *argv[]) char *device_name = "/dev/ttyS1"; baudrate = 57600; + /* XXX this is never written? */ struct vehicle_status_s v_status; - struct actuator_armed_s armed; + struct vehicle_control_mode_s control_mode; + struct actuator_safety_s safety; /* work around some stupidity in task_create's argv handling */ argc -= 2; @@ -431,10 +439,10 @@ int mavlink_thread_main(int argc, char *argv[]) /* translate the current system state to mavlink state and mode */ uint8_t mavlink_state = 0; uint8_t mavlink_mode = 0; - get_mavlink_mode_and_state(&v_status, &armed, &mavlink_state, &mavlink_mode); + get_mavlink_mode_and_state(&control_mode, &safety, &mavlink_state, &mavlink_mode); /* send heartbeat */ - mavlink_msg_heartbeat_send(chan, mavlink_system.type, MAV_AUTOPILOT_PX4, mavlink_mode, v_status.state_machine, mavlink_state); + mavlink_msg_heartbeat_send(chan, mavlink_system.type, MAV_AUTOPILOT_PX4, mavlink_mode, v_status.navigation_state, mavlink_state); /* send status (values already copied in the section above) */ mavlink_msg_sys_status_send(chan, diff --git a/src/modules/mavlink_onboard/mavlink_receiver.c b/src/modules/mavlink_onboard/mavlink_receiver.c index 0acbea675..2d406fb9f 100644 --- a/src/modules/mavlink_onboard/mavlink_receiver.c +++ b/src/modules/mavlink_onboard/mavlink_receiver.c @@ -328,4 +328,4 @@ receive_start(int uart) pthread_t thread; pthread_create(&thread, &receiveloop_attr, receive_thread, &uart); return thread; -}
\ No newline at end of file +} diff --git a/src/modules/mavlink_onboard/orb_topics.h b/src/modules/mavlink_onboard/orb_topics.h index f18f56243..f01f09e12 100644 --- a/src/modules/mavlink_onboard/orb_topics.h +++ b/src/modules/mavlink_onboard/orb_topics.h @@ -52,9 +52,11 @@ #include <uORB/topics/vehicle_vicon_position.h> #include <uORB/topics/vehicle_global_position_setpoint.h> #include <uORB/topics/vehicle_attitude_setpoint.h> +#include <uORB/topics/vehicle_control_mode.h> #include <uORB/topics/optical_flow.h> #include <uORB/topics/actuator_outputs.h> #include <uORB/topics/actuator_controls.h> +#include <uORB/topics/actuator_safety.h> #include <uORB/topics/manual_control_setpoint.h> #include <uORB/topics/debug_key_value.h> #include <drivers/drv_rc_input.h> @@ -69,7 +71,7 @@ struct mavlink_subscriptions { int act_3_sub; int gps_sub; int man_control_sp_sub; - int armed_sub; + int safety_sub; int actuators_sub; int local_pos_sub; int spa_sub; diff --git a/src/modules/mavlink_onboard/util.h b/src/modules/mavlink_onboard/util.h index 38a4db372..c6a2e52bf 100644 --- a/src/modules/mavlink_onboard/util.h +++ b/src/modules/mavlink_onboard/util.h @@ -50,5 +50,6 @@ extern volatile bool thread_should_exit; /** * Translate the custom state into standard mavlink modes and state. */ -extern void get_mavlink_mode_and_state(const struct vehicle_status_s *v_status, const struct actuator_armed_s *armed, +extern void +get_mavlink_mode_and_state(const struct vehicle_control_mode_s *control_mode, const struct actuator_safety_s *safety, uint8_t *mavlink_state, uint8_t *mavlink_mode); diff --git a/src/modules/multirotor_att_control/multirotor_att_control_main.c b/src/modules/multirotor_att_control/multirotor_att_control_main.c index 99f25cfe9..70a61fc4e 100644 --- a/src/modules/multirotor_att_control/multirotor_att_control_main.c +++ b/src/modules/multirotor_att_control/multirotor_att_control_main.c @@ -57,12 +57,14 @@ #include <drivers/drv_hrt.h> #include <uORB/uORB.h> #include <drivers/drv_gyro.h> -#include <uORB/topics/vehicle_status.h> +#include <uORB/topics/vehicle_control_mode.h> +#include <uORB/topics/actuator_safety.h> #include <uORB/topics/vehicle_attitude.h> #include <uORB/topics/vehicle_attitude_setpoint.h> #include <uORB/topics/manual_control_setpoint.h> #include <uORB/topics/offboard_control_setpoint.h> #include <uORB/topics/vehicle_rates_setpoint.h> +#include <uORB/topics/vehicle_control_debug.h> #include <uORB/topics/sensor_combined.h> #include <uORB/topics/actuator_controls.h> #include <uORB/topics/parameter_update.h> @@ -83,14 +85,17 @@ static int mc_task; static bool motor_test_mode = false; static orb_advert_t actuator_pub; +static orb_advert_t control_debug_pub; -static struct vehicle_status_s state; static int mc_thread_main(int argc, char *argv[]) { /* declare and safely initialize all structs */ - memset(&state, 0, sizeof(state)); + struct vehicle_control_mode_s control_mode; + memset(&control_mode, 0, sizeof(control_mode)); + struct actuator_safety_s safety; + memset(&safety, 0, sizeof(safety)); struct vehicle_attitude_s att; memset(&att, 0, sizeof(att)); struct vehicle_attitude_setpoint_s att_sp; @@ -107,12 +112,16 @@ mc_thread_main(int argc, char *argv[]) struct actuator_controls_s actuators; memset(&actuators, 0, sizeof(actuators)); + struct vehicle_control_debug_s control_debug; + memset(&control_debug, 0, sizeof(control_debug)); + /* subscribe to attitude, motor setpoints and system state */ int att_sub = orb_subscribe(ORB_ID(vehicle_attitude)); int param_sub = orb_subscribe(ORB_ID(parameter_update)); int att_setpoint_sub = orb_subscribe(ORB_ID(vehicle_attitude_setpoint)); int setpoint_sub = orb_subscribe(ORB_ID(offboard_control_setpoint)); - int state_sub = orb_subscribe(ORB_ID(vehicle_status)); + int control_mode_sub = orb_subscribe(ORB_ID(vehicle_control_mode)); + int safety_sub = orb_subscribe(ORB_ID(actuator_safety)); int manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); int sensor_sub = orb_subscribe(ORB_ID(sensor_combined)); @@ -133,6 +142,8 @@ mc_thread_main(int argc, char *argv[]) for (unsigned i = 0; i < NUM_ACTUATOR_CONTROLS; i++) { actuators.control[i] = 0.0f; } + + control_debug_pub = orb_advertise(ORB_ID(vehicle_control_debug), &control_debug); actuator_pub = orb_advertise(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, &actuators); orb_advert_t att_sp_pub = orb_advertise(ORB_ID(vehicle_attitude_setpoint), &att_sp); @@ -150,7 +161,9 @@ mc_thread_main(int argc, char *argv[]) /* store last control mode to detect mode switches */ bool flag_control_manual_enabled = false; bool flag_control_attitude_enabled = false; - bool flag_system_armed = false; + bool flag_armed = false; + bool flag_control_position_enabled = false; + bool flag_control_velocity_enabled = false; /* store if yaw position or yaw speed has been changed */ bool control_yaw_position = true; @@ -162,7 +175,6 @@ mc_thread_main(int argc, char *argv[]) param_t failsafe_throttle_handle = param_find("MC_RCLOSS_THR"); float failsafe_throttle = 0.0f; - while (!thread_should_exit) { /* wait for a sensor update, check for exit condition every 500 ms */ @@ -175,7 +187,6 @@ mc_thread_main(int argc, char *argv[]) } else if (ret == 0) { /* no return value, ignore */ } else { - /* only update parameters if they changed */ if (fds[1].revents & POLLIN) { /* read from param to clear updated flag */ @@ -193,10 +204,16 @@ mc_thread_main(int argc, char *argv[]) /* get a local copy of system state */ bool updated; - orb_check(state_sub, &updated); + orb_check(control_mode_sub, &updated); + + if (updated) { + orb_copy(ORB_ID(vehicle_control_mode), control_mode_sub, &control_mode); + } + + orb_check(safety_sub, &updated); if (updated) { - orb_copy(ORB_ID(vehicle_status), state_sub, &state); + orb_copy(ORB_ID(actuator_safety), safety_sub, &safety); } /* get a local copy of manual setpoint */ @@ -215,9 +232,8 @@ mc_thread_main(int argc, char *argv[]) /* get a local copy of the current sensor values */ orb_copy(ORB_ID(sensor_combined), sensor_sub, &raw); - /** STEP 1: Define which input is the dominating control input */ - if (state.flag_control_offboard_enabled) { + if (control_mode.flag_control_offboard_enabled) { /* offboard inputs */ if (offboard_sp.mode == OFFBOARD_CONTROL_MODE_DIRECT_RATES) { rates_sp.roll = offboard_sp.p1; @@ -240,102 +256,51 @@ mc_thread_main(int argc, char *argv[]) } - } else if (state.flag_control_manual_enabled) { - - if (state.flag_control_attitude_enabled) { - + } else if (control_mode.flag_control_manual_enabled) { + if (control_mode.flag_control_attitude_enabled) { /* initialize to current yaw if switching to manual or att control */ - if (state.flag_control_attitude_enabled != flag_control_attitude_enabled || - state.flag_control_manual_enabled != flag_control_manual_enabled || - state.flag_system_armed != flag_system_armed) { + if (control_mode.flag_control_attitude_enabled != flag_control_attitude_enabled || + control_mode.flag_control_manual_enabled != flag_control_manual_enabled || + safety.armed != flag_armed) { att_sp.yaw_body = att.yaw; } static bool rc_loss_first_time = true; /* if the RC signal is lost, try to stay level and go slowly back down to ground */ - if (state.rc_signal_lost) { - /* the failsafe throttle is stored as a parameter, as it depends on the copter and the payload */ - param_get(failsafe_throttle_handle, &failsafe_throttle); - att_sp.roll_body = 0.0f; - att_sp.pitch_body = 0.0f; - /* - * Only go to failsafe throttle if last known throttle was - * high enough to create some lift to make hovering state likely. - * - * This is to prevent that someone landing, but not disarming his - * multicopter (throttle = 0) does not make it jump up in the air - * if shutting down his remote. - */ - if (isfinite(manual.throttle) && manual.throttle > 0.2f) { - att_sp.thrust = failsafe_throttle; - - } else { - att_sp.thrust = 0.0f; - } - - /* keep current yaw, do not attempt to go to north orientation, - * since if the pilot regains RC control, he will be lost regarding - * the current orientation. - */ - if (rc_loss_first_time) - att_sp.yaw_body = att.yaw; + rc_loss_first_time = true; - rc_loss_first_time = false; + att_sp.roll_body = manual.roll; + att_sp.pitch_body = manual.pitch; - } else { - rc_loss_first_time = true; + /* set attitude if arming */ + if (!flag_control_attitude_enabled && safety.armed) { + att_sp.yaw_body = att.yaw; + } - att_sp.roll_body = manual.roll; - att_sp.pitch_body = manual.pitch; + /* only move setpoint if manual input is != 0 */ + if ((manual.yaw < -0.01f || 0.01f < manual.yaw) && manual.throttle > 0.1f) { + rates_sp.yaw = manual.yaw; + control_yaw_position = false; + first_time_after_yaw_speed_control = true; - /* set attitude if arming */ - if (!flag_control_attitude_enabled && state.flag_system_armed) { + } else { + if (first_time_after_yaw_speed_control) { att_sp.yaw_body = att.yaw; + first_time_after_yaw_speed_control = false; } - /* act if stabilization is active or if the (nonsense) direct pass through mode is set */ - if (state.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_SAS || - state.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_DIRECT) { - - if (state.manual_sas_mode == VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_RATE) { - rates_sp.yaw = manual.yaw; - control_yaw_position = false; - - } else { - /* - * This mode SHOULD be the default mode, which is: - * VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_ABS - * - * However, we fall back to this setting for all other (nonsense) - * settings as well. - */ - - /* only move setpoint if manual input is != 0 */ - if ((manual.yaw < -0.01f || 0.01f < manual.yaw) && manual.throttle > 0.3f) { - rates_sp.yaw = manual.yaw; - control_yaw_position = false; - first_time_after_yaw_speed_control = true; - - } else { - if (first_time_after_yaw_speed_control) { - att_sp.yaw_body = att.yaw; - first_time_after_yaw_speed_control = false; - } - - control_yaw_position = true; - } - } - } - - att_sp.thrust = manual.throttle; - att_sp.timestamp = hrt_absolute_time(); + control_yaw_position = true; } + att_sp.thrust = manual.throttle; + att_sp.timestamp = hrt_absolute_time(); + /* STEP 2: publish the controller output */ orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp); + if (motor_test_mode) { printf("testmode"); att_sp.roll_body = 0.0f; @@ -348,23 +313,26 @@ mc_thread_main(int argc, char *argv[]) } } else { - /* manual rate inputs, from RC control or joystick */ - if (state.flag_control_rates_enabled && - state.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_RATES) { - rates_sp.roll = manual.roll; - rates_sp.pitch = manual.pitch; - rates_sp.yaw = manual.yaw; - rates_sp.thrust = manual.throttle; - rates_sp.timestamp = hrt_absolute_time(); - } + //XXX TODO add acro mode here + + /* manual rate inputs, from RC control or joystick */ +// if (state.flag_control_rates_enabled && +// state.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_RATES) { +// rates_sp.roll = manual.roll; +// +// rates_sp.pitch = manual.pitch; +// rates_sp.yaw = manual.yaw; +// rates_sp.thrust = manual.throttle; +// rates_sp.timestamp = hrt_absolute_time(); +// } } } /** STEP 3: Identify the controller setup to run and set up the inputs correctly */ - if (state.flag_control_attitude_enabled) { - multirotor_control_attitude(&att_sp, &att, &rates_sp, control_yaw_position); + if (control_mode.flag_control_attitude_enabled) { + multirotor_control_attitude(&att_sp, &att, &rates_sp, control_yaw_position, &control_debug_pub, &control_debug); orb_publish(ORB_ID(vehicle_rates_setpoint), rates_sp_pub, &rates_sp); } @@ -372,7 +340,8 @@ mc_thread_main(int argc, char *argv[]) /* measure in what intervals the controller runs */ perf_count(mc_interval_perf); - float gyro[3]; + float rates[3]; + float rates_acc[3]; /* get current rate setpoint */ bool rates_sp_valid = false; @@ -383,17 +352,21 @@ mc_thread_main(int argc, char *argv[]) } /* apply controller */ - gyro[0] = att.rollspeed; - gyro[1] = att.pitchspeed; - gyro[2] = att.yawspeed; + rates[0] = att.rollspeed; + rates[1] = att.pitchspeed; + rates[2] = att.yawspeed; - multirotor_control_rates(&rates_sp, gyro, &actuators); + multirotor_control_rates(&rates_sp, rates, &actuators, &control_debug_pub, &control_debug); orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators); - /* update state */ - flag_control_attitude_enabled = state.flag_control_attitude_enabled; - flag_control_manual_enabled = state.flag_control_manual_enabled; - flag_system_armed = state.flag_system_armed; + orb_publish(ORB_ID(vehicle_control_debug), control_debug_pub, &control_debug); + + /* update control_mode */ + flag_control_attitude_enabled = control_mode.flag_control_attitude_enabled; + flag_control_manual_enabled = control_mode.flag_control_manual_enabled; + flag_control_position_enabled = control_mode.flag_control_position_enabled; + flag_control_velocity_enabled = control_mode.flag_control_velocity_enabled; + flag_armed = safety.armed; perf_end(mc_loop_perf); } /* end of poll call for attitude updates */ @@ -410,7 +383,7 @@ mc_thread_main(int argc, char *argv[]) close(att_sub); - close(state_sub); + close(control_mode_sub); close(manual_sub); close(actuator_pub); close(att_sp_pub); diff --git a/src/modules/multirotor_att_control/multirotor_attitude_control.c b/src/modules/multirotor_att_control/multirotor_attitude_control.c index 8f19c6a4b..083311674 100644 --- a/src/modules/multirotor_att_control/multirotor_attitude_control.c +++ b/src/modules/multirotor_att_control/multirotor_attitude_control.c @@ -65,50 +65,29 @@ PARAM_DEFINE_FLOAT(MC_YAWPOS_P, 0.3f); PARAM_DEFINE_FLOAT(MC_YAWPOS_I, 0.15f); PARAM_DEFINE_FLOAT(MC_YAWPOS_D, 0.0f); -//PARAM_DEFINE_FLOAT(MC_YAWPOS_AWU, 1.0f); -//PARAM_DEFINE_FLOAT(MC_YAWPOS_LIM, 3.0f); PARAM_DEFINE_FLOAT(MC_ATT_P, 0.2f); PARAM_DEFINE_FLOAT(MC_ATT_I, 0.0f); PARAM_DEFINE_FLOAT(MC_ATT_D, 0.05f); -//PARAM_DEFINE_FLOAT(MC_ATT_AWU, 0.05f); -//PARAM_DEFINE_FLOAT(MC_ATT_LIM, 0.4f); - -//PARAM_DEFINE_FLOAT(MC_ATT_XOFF, 0.0f); -//PARAM_DEFINE_FLOAT(MC_ATT_YOFF, 0.0f); struct mc_att_control_params { float yaw_p; float yaw_i; float yaw_d; - //float yaw_awu; - //float yaw_lim; float att_p; float att_i; float att_d; - //float att_awu; - //float att_lim; - - //float att_xoff; - //float att_yoff; }; struct mc_att_control_param_handles { param_t yaw_p; param_t yaw_i; param_t yaw_d; - //param_t yaw_awu; - //param_t yaw_lim; param_t att_p; param_t att_i; param_t att_d; - //param_t att_awu; - //param_t att_lim; - - //param_t att_xoff; - //param_t att_yoff; }; /** @@ -130,17 +109,10 @@ static int parameters_init(struct mc_att_control_param_handles *h) h->yaw_p = param_find("MC_YAWPOS_P"); h->yaw_i = param_find("MC_YAWPOS_I"); h->yaw_d = param_find("MC_YAWPOS_D"); - //h->yaw_awu = param_find("MC_YAWPOS_AWU"); - //h->yaw_lim = param_find("MC_YAWPOS_LIM"); h->att_p = param_find("MC_ATT_P"); h->att_i = param_find("MC_ATT_I"); h->att_d = param_find("MC_ATT_D"); - //h->att_awu = param_find("MC_ATT_AWU"); - //h->att_lim = param_find("MC_ATT_LIM"); - - //h->att_xoff = param_find("MC_ATT_XOFF"); - //h->att_yoff = param_find("MC_ATT_YOFF"); return OK; } @@ -150,23 +122,17 @@ static int parameters_update(const struct mc_att_control_param_handles *h, struc param_get(h->yaw_p, &(p->yaw_p)); param_get(h->yaw_i, &(p->yaw_i)); param_get(h->yaw_d, &(p->yaw_d)); - //param_get(h->yaw_awu, &(p->yaw_awu)); - //param_get(h->yaw_lim, &(p->yaw_lim)); param_get(h->att_p, &(p->att_p)); param_get(h->att_i, &(p->att_i)); param_get(h->att_d, &(p->att_d)); - //param_get(h->att_awu, &(p->att_awu)); - //param_get(h->att_lim, &(p->att_lim)); - - //param_get(h->att_xoff, &(p->att_xoff)); - //param_get(h->att_yoff, &(p->att_yoff)); return OK; } void multirotor_control_attitude(const struct vehicle_attitude_setpoint_s *att_sp, - const struct vehicle_attitude_s *att, struct vehicle_rates_setpoint_s *rates_sp, bool control_yaw_position) + const struct vehicle_attitude_s *att, struct vehicle_rates_setpoint_s *rates_sp, bool control_yaw_position, + const orb_advert_t *control_debug_pub, struct vehicle_control_debug_s *control_debug) { static uint64_t last_run = 0; static uint64_t last_input = 0; @@ -207,7 +173,7 @@ void multirotor_control_attitude(const struct vehicle_attitude_setpoint_s *att_s /* apply parameters */ pid_set_parameters(&pitch_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f); - pid_set_parameters(&roll_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f); + pid_set_parameters(&roll_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f); } /* reset integral if on ground */ @@ -221,11 +187,13 @@ void multirotor_control_attitude(const struct vehicle_attitude_setpoint_s *att_s /* control pitch (forward) output */ rates_sp->pitch = pid_calculate(&pitch_controller, att_sp->pitch_body , - att->pitch, att->pitchspeed, deltaT); + att->pitch, att->pitchspeed, deltaT, &control_debug->pitch_p, &control_debug->pitch_i, &control_debug->pitch_d); /* control roll (left/right) output */ rates_sp->roll = pid_calculate(&roll_controller, att_sp->roll_body , - att->roll, att->rollspeed, deltaT); + att->roll, att->rollspeed, deltaT, NULL, NULL, NULL); + + // printf("rates_sp: %4.4f, att setpoint: %4.4f\n, pitch: %4.4f, pitchspeed: %4.4f, dT: %4.4f", rates_sp->pitch, att_sp->pitch_body, att->pitch, att->pitchspeed, deltaT); if (control_yaw_position) { /* control yaw rate */ diff --git a/src/modules/multirotor_att_control/multirotor_attitude_control.h b/src/modules/multirotor_att_control/multirotor_attitude_control.h index e78f45c47..6dd5b39fd 100644 --- a/src/modules/multirotor_att_control/multirotor_attitude_control.h +++ b/src/modules/multirotor_att_control/multirotor_attitude_control.h @@ -58,8 +58,11 @@ #include <uORB/topics/vehicle_attitude_setpoint.h> #include <uORB/topics/vehicle_rates_setpoint.h> #include <uORB/topics/actuator_controls.h> +#include <uORB/topics/vehicle_control_debug.h> + void multirotor_control_attitude(const struct vehicle_attitude_setpoint_s *att_sp, - const struct vehicle_attitude_s *att, struct vehicle_rates_setpoint_s *rates_sp, bool control_yaw_position); + const struct vehicle_attitude_s *att, struct vehicle_rates_setpoint_s *rates_sp, bool control_yaw_position, + const orb_advert_t *control_debug_pub, struct vehicle_control_debug_s *control_debug); #endif /* MULTIROTOR_ATTITUDE_CONTROL_H_ */ diff --git a/src/modules/multirotor_att_control/multirotor_rate_control.c b/src/modules/multirotor_att_control/multirotor_rate_control.c index e58d357d5..ee8c37580 100644 --- a/src/modules/multirotor_att_control/multirotor_rate_control.c +++ b/src/modules/multirotor_att_control/multirotor_rate_control.c @@ -58,6 +58,9 @@ #include <systemlib/param/param.h> #include <systemlib/err.h> #include <drivers/drv_hrt.h> +#include <uORB/uORB.h> + + PARAM_DEFINE_FLOAT(MC_YAWRATE_P, 0.0f); /* same on Flamewheel */ PARAM_DEFINE_FLOAT(MC_YAWRATE_D, 0.0f); @@ -152,7 +155,8 @@ static int parameters_update(const struct mc_rate_control_param_handles *h, stru } void multirotor_control_rates(const struct vehicle_rates_setpoint_s *rate_sp, - const float rates[], struct actuator_controls_s *actuators) + const float rates[], struct actuator_controls_s *actuators, + const orb_advert_t *control_debug_pub, struct vehicle_control_debug_s *control_debug) { static uint64_t last_run = 0; const float deltaT = (hrt_absolute_time() - last_run) / 1000000.0f; @@ -172,8 +176,13 @@ void multirotor_control_rates(const struct vehicle_rates_setpoint_s *rate_sp, static struct mc_rate_control_params p; static struct mc_rate_control_param_handles h; + float pitch_control_last = 0.0f; + float roll_control_last = 0.0f; + static bool initialized = false; + float diff_filter_factor = 1.0f; + /* initialize the pid controllers when the function is called for the first time */ if (initialized == false) { parameters_init(&h); @@ -201,11 +210,13 @@ void multirotor_control_rates(const struct vehicle_rates_setpoint_s *rate_sp, /* control pitch (forward) output */ float pitch_control = pid_calculate(&pitch_rate_controller, rate_sp->pitch , - rates[1], 0.0f, deltaT); + rates[1], 0.0f, deltaT, + &control_debug->pitch_rate_p, &control_debug->pitch_rate_i, &control_debug->pitch_rate_d); /* control roll (left/right) output */ float roll_control = pid_calculate(&roll_rate_controller, rate_sp->roll , - rates[0], 0.0f, deltaT); + rates[0], 0.0f, deltaT, + &control_debug->roll_rate_p, &control_debug->roll_rate_i, &control_debug->roll_rate_d); /* control yaw rate */ //XXX use library here float yaw_rate_control = p.yawrate_p * (rate_sp->yaw - rates[2]); diff --git a/src/modules/multirotor_att_control/multirotor_rate_control.h b/src/modules/multirotor_att_control/multirotor_rate_control.h index 362b5ed86..695ff3e16 100644 --- a/src/modules/multirotor_att_control/multirotor_rate_control.h +++ b/src/modules/multirotor_att_control/multirotor_rate_control.h @@ -57,8 +57,10 @@ #include <uORB/topics/vehicle_attitude.h> #include <uORB/topics/vehicle_rates_setpoint.h> #include <uORB/topics/actuator_controls.h> +#include <uORB/topics/vehicle_control_debug.h> void multirotor_control_rates(const struct vehicle_rates_setpoint_s *rate_sp, - const float rates[], struct actuator_controls_s *actuators); + const float rates[], struct actuator_controls_s *actuators, + const orb_advert_t *control_debug_pub, struct vehicle_control_debug_s *control_debug); #endif /* MULTIROTOR_RATE_CONTROL_H_ */ diff --git a/src/modules/px4iofirmware/mixer.cpp b/src/modules/px4iofirmware/mixer.cpp index a2193b526..fe9166779 100644 --- a/src/modules/px4iofirmware/mixer.cpp +++ b/src/modules/px4iofirmware/mixer.cpp @@ -59,6 +59,12 @@ extern "C" { */ #define FMU_INPUT_DROP_LIMIT_US 200000 +/* + * Time that the ESCs need to initialize + */ + #define ESC_INIT_TIME_US 1000000 + #define ESC_RAMP_TIME_US 2000000 + /* XXX need to move the RC_CHANNEL_FUNCTION out of rc_channels.h and into systemlib */ #define ROLL 0 #define PITCH 1 @@ -68,6 +74,17 @@ extern "C" { /* current servo arm/disarm state */ static bool mixer_servos_armed = false; +static bool should_arm = false; +static bool should_always_enable_pwm = false; +static uint64_t esc_init_time; + +enum esc_state_e { + ESC_OFF, + ESC_INIT, + ESC_RAMP, + ESC_ON +}; +static esc_state_e esc_state; /* selected control values and count for mixing */ enum mixer_source { @@ -98,7 +115,7 @@ mixer_tick(void) if (r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) { isr_debug(1, "AP RX timeout"); } - r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_FMU_OK | PX4IO_P_STATUS_FLAGS_RAW_PWM); + r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_FMU_OK); r_status_alarms |= PX4IO_P_STATUS_ALARMS_FMU_LOST; } else { @@ -112,12 +129,11 @@ mixer_tick(void) * Decide which set of controls we're using. */ - /* do not mix if mixer is invalid or if RAW_PWM mode is on and FMU is good */ + /* do not mix if RAW_PWM mode is on and FMU is good */ if ((r_status_flags & PX4IO_P_STATUS_FLAGS_RAW_PWM) && - !(r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK)) { + (r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK)) { - /* don't actually mix anything - we already have raw PWM values or - not a valid mixer. */ + /* don't actually mix anything - we already have raw PWM values */ source = MIX_NONE; } else { @@ -167,6 +183,48 @@ mixer_tick(void) float outputs[IO_SERVO_COUNT]; unsigned mixed; + uint16_t ramp_promille; + + /* update esc init state, but only if we are truely armed and not just PWM enabled */ + if (mixer_servos_armed && should_arm) { + + switch (esc_state) { + + /* after arming, some ESCs need an initalization period, count the time from here */ + case ESC_OFF: + esc_init_time = hrt_absolute_time(); + esc_state = ESC_INIT; + break; + + /* after waiting long enough for the ESC initialization, we can start with the ramp to start the ESCs */ + case ESC_INIT: + if (hrt_elapsed_time(&esc_init_time) > ESC_INIT_TIME_US) { + esc_state = ESC_RAMP; + } + break; + + /* then ramp until the min speed is reached */ + case ESC_RAMP: + if (hrt_elapsed_time(&esc_init_time) > (ESC_INIT_TIME_US + ESC_RAMP_TIME_US)) { + esc_state = ESC_ON; + } + break; + + case ESC_ON: + default: + + break; + } + } else { + esc_state = ESC_OFF; + } + + /* do the calculations during the ramp for all at once */ + if(esc_state == ESC_RAMP) { + ramp_promille = (1000*(hrt_elapsed_time(&esc_init_time)-ESC_INIT_TIME_US))/ESC_RAMP_TIME_US; + } + + /* mix */ mixed = mixer_group.mix(&outputs[0], IO_SERVO_COUNT); @@ -176,9 +234,27 @@ mixer_tick(void) /* save actuator values for FMU readback */ r_page_actuators[i] = FLOAT_TO_REG(outputs[i]); - /* scale to servo output */ - r_page_servos[i] = (outputs[i] * 600.0f) + 1500; - + switch (esc_state) { + case ESC_INIT: + r_page_servos[i] = (outputs[i] * 600 + 1500); + break; + + case ESC_RAMP: + r_page_servos[i] = (outputs[i] + * (ramp_promille*r_page_servo_control_max[i] + (1000-ramp_promille)*2100 - ramp_promille*r_page_servo_control_min[i] - (1000-ramp_promille)*900)/2/1000 + + (ramp_promille*r_page_servo_control_max[i] + (1000-ramp_promille)*2100 + ramp_promille*r_page_servo_control_min[i] + (1000-ramp_promille)*900)/2/1000); + break; + + case ESC_ON: + r_page_servos[i] = (outputs[i] + * (r_page_servo_control_max[i] - r_page_servo_control_min[i])/2 + + (r_page_servo_control_max[i] + r_page_servo_control_min[i])/2); + break; + + case ESC_OFF: + default: + break; + } } for (unsigned i = mixed; i < IO_SERVO_COUNT; i++) r_page_servos[i] = 0; @@ -193,30 +269,46 @@ mixer_tick(void) * XXX correct behaviour for failsafe may require an additional case * here. */ - bool should_arm = ( - /* FMU is armed */ (r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) && - /* IO is armed */ (r_status_flags & PX4IO_P_STATUS_FLAGS_ARMED) && - /* there is valid input via direct PWM or mixer */ (r_status_flags & (PX4IO_P_STATUS_FLAGS_RAW_PWM | PX4IO_P_STATUS_FLAGS_MIXER_OK)) && - /* IO initialised without error */ (r_status_flags & PX4IO_P_STATUS_FLAGS_INIT_OK) && - /* FMU is available or FMU is not available but override is an option */ - ((r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) || (!(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) && (r_setup_arming & PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK) )) + should_arm = ( + /* IO initialised without error */ (r_status_flags & PX4IO_P_STATUS_FLAGS_INIT_OK) + /* and IO is armed */ && (r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) + /* and FMU is armed */ && ( + ((r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) + /* and there is valid input via or mixer */ && (r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK) ) + /* or direct PWM is set */ || (r_status_flags & PX4IO_P_STATUS_FLAGS_RAW_PWM) + /* or failsafe was set manually */ || (r_setup_arming & PX4IO_P_SETUP_ARMING_FAILSAFE_CUSTOM) + ) ); - if (should_arm && !mixer_servos_armed) { + should_always_enable_pwm = (r_setup_arming & PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE) + && (r_status_flags & PX4IO_P_STATUS_FLAGS_INIT_OK) + && (r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK); + + if ((should_arm || should_always_enable_pwm) && !mixer_servos_armed) { /* need to arm, but not armed */ up_pwm_servo_arm(true); mixer_servos_armed = true; + r_status_flags |= PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED; + isr_debug(5, "> PWM enabled"); - } else if (!should_arm && mixer_servos_armed) { + } else if ((!should_arm && !should_always_enable_pwm) && mixer_servos_armed) { /* armed but need to disarm */ up_pwm_servo_arm(false); mixer_servos_armed = false; + r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED); + isr_debug(5, "> PWM disabled"); + } - if (mixer_servos_armed) { + if (mixer_servos_armed && should_arm) { /* update the servo outputs. */ for (unsigned i = 0; i < IO_SERVO_COUNT; i++) up_pwm_servo_set(i, r_page_servos[i]); + + } else if (mixer_servos_armed && should_always_enable_pwm) { + /* set the idle servo outputs. */ + for (unsigned i = 0; i < IO_SERVO_COUNT; i++) + up_pwm_servo_set(i, r_page_servo_idle[i]); } } @@ -265,9 +357,8 @@ static unsigned mixer_text_length = 0; void mixer_handle_text(const void *buffer, size_t length) { - /* do not allow a mixer change while fully armed */ - if (/* FMU is armed */ (r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) && - /* IO is armed */ (r_status_flags & PX4IO_P_STATUS_FLAGS_ARMED)) { + /* do not allow a mixer change while outputs armed */ + if ((r_status_flags & PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED)) { return; } @@ -344,6 +435,7 @@ mixer_set_failsafe() * Check if a custom failsafe value has been written, * or if the mixer is not ok and bail out. */ + if ((r_setup_arming & PX4IO_P_SETUP_ARMING_FAILSAFE_CUSTOM) || !(r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK)) return; diff --git a/src/modules/px4iofirmware/protocol.h b/src/modules/px4iofirmware/protocol.h index 674f9dddd..0e477a200 100644 --- a/src/modules/px4iofirmware/protocol.h +++ b/src/modules/px4iofirmware/protocol.h @@ -75,10 +75,13 @@ #define REG_TO_FLOAT(_reg) ((float)REG_TO_SIGNED(_reg) / 10000.0f) #define FLOAT_TO_REG(_float) SIGNED_TO_REG((int16_t)((_float) * 10000.0f)) +#define PX4IO_P_CONFIG_PROTOCOL_VERSION_MAGIC 2 +#define PX4IO_P_CONFIG_SOFTWARE_VERSION_MAGIC 2 + /* static configuration page */ #define PX4IO_PAGE_CONFIG 0 -#define PX4IO_P_CONFIG_PROTOCOL_VERSION 0 /* magic numbers TBD */ -#define PX4IO_P_CONFIG_SOFTWARE_VERSION 1 /* magic numbers TBD */ +#define PX4IO_P_CONFIG_PROTOCOL_VERSION 0 /* magic numbers */ +#define PX4IO_P_CONFIG_SOFTWARE_VERSION 1 /* magic numbers */ #define PX4IO_P_CONFIG_BOOTLOADER_VERSION 2 /* get this how? */ #define PX4IO_P_CONFIG_MAX_TRANSFER 3 /* maximum I2C transfer size */ #define PX4IO_P_CONFIG_CONTROL_COUNT 4 /* hardcoded max control count supported */ @@ -93,7 +96,7 @@ #define PX4IO_P_STATUS_CPULOAD 1 #define PX4IO_P_STATUS_FLAGS 2 /* monitoring flags */ -#define PX4IO_P_STATUS_FLAGS_ARMED (1 << 0) /* arm-ok and locally armed */ +#define PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED (1 << 0) /* arm-ok and locally armed */ #define PX4IO_P_STATUS_FLAGS_OVERRIDE (1 << 1) /* in manual override */ #define PX4IO_P_STATUS_FLAGS_RC_OK (1 << 2) /* RC input is valid */ #define PX4IO_P_STATUS_FLAGS_RC_PPM (1 << 3) /* PPM input is valid */ @@ -105,6 +108,7 @@ #define PX4IO_P_STATUS_FLAGS_ARM_SYNC (1 << 9) /* the arming state between IO and FMU is in sync */ #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_ALARMS 3 /* alarm flags - alarms latch, write 1 to a bit to clear it */ #define PX4IO_P_STATUS_ALARMS_VBATT_LOW (1 << 0) /* VBatt is very close to regulator dropout */ @@ -151,6 +155,7 @@ #define PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK (1 << 2) /* OK to switch to manual override via override RC channel */ #define PX4IO_P_SETUP_ARMING_FAILSAFE_CUSTOM (1 << 3) /* use custom failsafe values, not 0 values of mixer */ #define PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK (1 << 4) /* OK to try in-air restart */ +#define PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE (1 << 5) /* Output of PWM right after startup enabled to help ESCs initialize and prevent them from beeping */ #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 */ @@ -183,6 +188,15 @@ /* PWM failsafe values - zero disables the output */ #define PX4IO_PAGE_FAILSAFE_PWM 105 /* 0..CONFIG_ACTUATOR_COUNT-1 */ +/* PWM minimum values for certain ESCs */ +#define PX4IO_PAGE_CONTROL_MIN_PWM 106 /* 0..CONFIG_ACTUATOR_COUNT-1 */ + +/* PWM maximum values for certain ESCs */ +#define PX4IO_PAGE_CONTROL_MAX_PWM 107 /* 0..CONFIG_ACTUATOR_COUNT-1 */ + +/* PWM idle values that are active, even when SAFETY_SAFE */ +#define PX4IO_PAGE_IDLE_PWM 108 /* 0..CONFIG_ACTUATOR_COUNT-1 */ + /** * As-needed mixer data upload. * diff --git a/src/modules/px4iofirmware/px4io.h b/src/modules/px4iofirmware/px4io.h index 272cdb7bf..042e7fe66 100644 --- a/src/modules/px4iofirmware/px4io.h +++ b/src/modules/px4iofirmware/px4io.h @@ -77,6 +77,9 @@ extern volatile uint16_t r_page_setup[]; /* PX4IO_PAGE_SETUP */ extern volatile uint16_t r_page_controls[]; /* PX4IO_PAGE_CONTROLS */ extern uint16_t r_page_rc_input_config[]; /* PX4IO_PAGE_RC_INPUT_CONFIG */ extern uint16_t r_page_servo_failsafe[]; /* PX4IO_PAGE_FAILSAFE_PWM */ +extern uint16_t r_page_servo_control_min[]; /* PX4IO_PAGE_CONTROL_MIN_PWM */ +extern uint16_t r_page_servo_control_max[]; /* PX4IO_PAGE_CONTROL_MAX_PWM */ +extern uint16_t r_page_servo_idle[]; /* PX4IO_PAGE_IDLE_PWM */ /* * Register aliases. diff --git a/src/modules/px4iofirmware/registers.c b/src/modules/px4iofirmware/registers.c index df7d6dcd3..bd13f3b7d 100644 --- a/src/modules/px4iofirmware/registers.c +++ b/src/modules/px4iofirmware/registers.c @@ -57,8 +57,8 @@ static void pwm_configure_rates(uint16_t map, uint16_t defaultrate, uint16_t alt * Static configuration parameters. */ static const uint16_t r_page_config[] = { - [PX4IO_P_CONFIG_PROTOCOL_VERSION] = 1, /* XXX hardcoded magic number */ - [PX4IO_P_CONFIG_SOFTWARE_VERSION] = 1, /* XXX hardcoded magic number */ + [PX4IO_P_CONFIG_PROTOCOL_VERSION] = PX4IO_P_CONFIG_PROTOCOL_VERSION_MAGIC, + [PX4IO_P_CONFIG_SOFTWARE_VERSION] = PX4IO_P_CONFIG_SOFTWARE_VERSION_MAGIC, [PX4IO_P_CONFIG_BOOTLOADER_VERSION] = 3, /* XXX hardcoded magic number */ [PX4IO_P_CONFIG_MAX_TRANSFER] = 64, /* XXX hardcoded magic number */ [PX4IO_P_CONFIG_CONTROL_COUNT] = PX4IO_CONTROL_CHANNELS, @@ -146,7 +146,9 @@ volatile uint16_t r_page_setup[] = #define PX4IO_P_SETUP_ARMING_VALID (PX4IO_P_SETUP_ARMING_FMU_ARMED | \ PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK | \ PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK | \ - PX4IO_P_SETUP_ARMING_IO_ARM_OK) + PX4IO_P_SETUP_ARMING_IO_ARM_OK) | \ + PX4IO_P_SETUP_ARMING_FAILSAFE_CUSTOM | \ + PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE #define PX4IO_P_SETUP_RATES_VALID ((1 << IO_SERVO_COUNT) - 1) #define PX4IO_P_SETUP_RELAYS_VALID ((1 << PX4IO_RELAY_CHANNELS) - 1) @@ -184,6 +186,30 @@ uint16_t r_page_rc_input_config[MAX_CONTROL_CHANNELS * PX4IO_P_RC_CONFIG_STRIDE */ uint16_t r_page_servo_failsafe[IO_SERVO_COUNT] = { 0 }; +/** + * PAGE 106 + * + * minimum PWM values when armed + * + */ +uint16_t r_page_servo_control_min[IO_SERVO_COUNT] = { 900, 900, 900, 900, 900, 900, 900, 900 }; + +/** + * PAGE 107 + * + * maximum PWM values when armed + * + */ +uint16_t r_page_servo_control_max[IO_SERVO_COUNT] = { 2100, 2100, 2100, 2100, 2100, 2100, 2100, 2100 }; + +/** + * PAGE 108 + * + * idle PWM values for difficult ESCs + * + */ +uint16_t r_page_servo_idle[IO_SERVO_COUNT] = { 900, 900, 900, 900, 900, 900, 900, 900 }; + void registers_set(uint8_t page, uint8_t offset, const uint16_t *values, unsigned num_values) { @@ -247,6 +273,75 @@ registers_set(uint8_t page, uint8_t offset, const uint16_t *values, unsigned num } break; + case PX4IO_PAGE_CONTROL_MIN_PWM: + + /* copy channel data */ + while ((offset < IO_SERVO_COUNT) && (num_values > 0)) { + + if (*values == 0) + /* set to default */ + r_page_servo_control_min[offset] = 900; + + else if (*values > 1200) + r_page_servo_control_min[offset] = 1200; + else if (*values < 900) + r_page_servo_control_min[offset] = 900; + else + r_page_servo_control_min[offset] = *values; + + offset++; + num_values--; + values++; + } + break; + + case PX4IO_PAGE_CONTROL_MAX_PWM: + + /* copy channel data */ + while ((offset < IO_SERVO_COUNT) && (num_values > 0)) { + + if (*values == 0) + /* set to default */ + r_page_servo_control_max[offset] = 2100; + + else if (*values > 2100) + r_page_servo_control_max[offset] = 2100; + else if (*values < 1800) + r_page_servo_control_max[offset] = 1800; + else + r_page_servo_control_max[offset] = *values; + + offset++; + num_values--; + values++; + } + break; + + case PX4IO_PAGE_IDLE_PWM: + + /* copy channel data */ + while ((offset < IO_SERVO_COUNT) && (num_values > 0)) { + + if (*values == 0) + /* set to default */ + r_page_servo_idle[offset] = 0; + + else if (*values < 900) + r_page_servo_idle[offset] = 900; + else if (*values > 2100) + r_page_servo_idle[offset] = 2100; + else + r_page_servo_idle[offset] = *values; + + /* flag the failsafe values as custom */ + r_setup_arming |= PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE; + + offset++; + num_values--; + values++; + } + break; + /* handle text going to the mixer parser */ case PX4IO_PAGE_MIXERLOAD: mixer_handle_text(values, num_values * sizeof(*values)); @@ -317,9 +412,11 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value) * so that an in-air reset of FMU can not lead to a * lockup of the IO arming state. */ - if ((r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) && !(value & PX4IO_P_SETUP_ARMING_FMU_ARMED)) { - r_status_flags &= ~PX4IO_P_STATUS_FLAGS_ARMED; - } + + // XXX do not reset IO's safety state by FMU for now + // if ((r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) && !(value & PX4IO_P_SETUP_ARMING_FMU_ARMED)) { + // r_status_flags &= ~PX4IO_P_STATUS_FLAGS_ARMED; + // } r_setup_arming = value; @@ -367,9 +464,8 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value) case PX4IO_PAGE_RC_CONFIG: { - /* do not allow a RC config change while fully armed */ - if (/* FMU is armed */ (r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) && - /* IO is armed */ (r_status_flags & PX4IO_P_STATUS_FLAGS_ARMED)) { + /* do not allow a RC config change while outputs armed */ + if ((r_status_flags & PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED)) { break; } @@ -583,6 +679,15 @@ registers_get(uint8_t page, uint8_t offset, uint16_t **values, unsigned *num_val case PX4IO_PAGE_FAILSAFE_PWM: SELECT_PAGE(r_page_servo_failsafe); break; + case PX4IO_PAGE_CONTROL_MIN_PWM: + SELECT_PAGE(r_page_servo_control_min); + break; + case PX4IO_PAGE_CONTROL_MAX_PWM: + SELECT_PAGE(r_page_servo_control_max); + break; + case PX4IO_PAGE_IDLE_PWM: + SELECT_PAGE(r_page_servo_idle); + break; default: return -1; diff --git a/src/modules/px4iofirmware/safety.c b/src/modules/px4iofirmware/safety.c index 4dbecc274..95335f038 100644 --- a/src/modules/px4iofirmware/safety.c +++ b/src/modules/px4iofirmware/safety.c @@ -110,7 +110,7 @@ safety_check_button(void *arg) * state machine, keep ARM_COUNTER_THRESHOLD the same * length in all cases of the if/else struct below. */ - if (safety_button_pressed && !(r_status_flags & PX4IO_P_STATUS_FLAGS_ARMED) && + if (safety_button_pressed && !(r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) && (r_setup_arming & PX4IO_P_SETUP_ARMING_IO_ARM_OK)) { if (counter < ARM_COUNTER_THRESHOLD) { @@ -118,18 +118,18 @@ safety_check_button(void *arg) } else if (counter == ARM_COUNTER_THRESHOLD) { /* switch to armed state */ - r_status_flags |= PX4IO_P_STATUS_FLAGS_ARMED; + r_status_flags |= PX4IO_P_STATUS_FLAGS_SAFETY_OFF; counter++; } - } else if (safety_button_pressed && (r_status_flags & PX4IO_P_STATUS_FLAGS_ARMED)) { + } else if (safety_button_pressed && (r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF)) { if (counter < ARM_COUNTER_THRESHOLD) { counter++; } else if (counter == ARM_COUNTER_THRESHOLD) { /* change to disarmed state and notify the FMU */ - r_status_flags &= ~PX4IO_P_STATUS_FLAGS_ARMED; + r_status_flags &= ~PX4IO_P_STATUS_FLAGS_SAFETY_OFF; counter++; } @@ -140,7 +140,7 @@ safety_check_button(void *arg) /* Select the appropriate LED flash pattern depending on the current IO/FMU arm state */ uint16_t pattern = LED_PATTERN_FMU_REFUSE_TO_ARM; - if (r_status_flags & PX4IO_P_STATUS_FLAGS_ARMED) { + if (r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) { if (r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) { pattern = LED_PATTERN_IO_FMU_ARMED; diff --git a/src/modules/sdlog2/sdlog2.c b/src/modules/sdlog2/sdlog2.c index deac9e20b..31da81f5c 100644 --- a/src/modules/sdlog2/sdlog2.c +++ b/src/modules/sdlog2/sdlog2.c @@ -60,6 +60,7 @@ #include <drivers/drv_hrt.h> #include <uORB/uORB.h> +#include <uORB/topics/actuator_safety.h> #include <uORB/topics/vehicle_status.h> #include <uORB/topics/sensor_combined.h> #include <uORB/topics/vehicle_attitude.h> @@ -74,6 +75,7 @@ #include <uORB/topics/vehicle_global_position.h> #include <uORB/topics/vehicle_gps_position.h> #include <uORB/topics/vehicle_vicon_position.h> +#include <uORB/topics/vehicle_control_debug.h> #include <uORB/topics/optical_flow.h> #include <uORB/topics/battery_status.h> #include <uORB/topics/differential_pressure.h> @@ -190,7 +192,7 @@ static int file_copy(const char *file_old, const char *file_new); static void handle_command(struct vehicle_command_s *cmd); -static void handle_status(struct vehicle_status_s *cmd); +static void handle_status(struct actuator_safety_s *safety); /** * Create folder for current logging session. Store folder name in 'log_folder'. @@ -614,7 +616,8 @@ int sdlog2_thread_main(int argc, char *argv[]) /* --- IMPORTANT: DEFINE NUMBER OF ORB STRUCTS TO WAIT FOR HERE --- */ /* number of messages */ - const ssize_t fdsc = 17; + const ssize_t fdsc = 20; + /* Sanity check variable and index */ ssize_t fdsc_count = 0; /* file descriptors to wait for */ @@ -623,6 +626,9 @@ int sdlog2_thread_main(int argc, char *argv[]) struct vehicle_status_s buf_status; memset(&buf_status, 0, sizeof(buf_status)); + struct actuator_safety_s buf_safety; + memset(&buf_safety, 0, sizeof(buf_safety)); + /* warning! using union here to save memory, elements should be used separately! */ union { struct vehicle_command_s cmd; @@ -638,6 +644,7 @@ int sdlog2_thread_main(int argc, char *argv[]) struct vehicle_global_position_s global_pos; struct vehicle_gps_position_s gps_pos; struct vehicle_vicon_position_s vicon_pos; + struct vehicle_control_debug_s control_debug; struct optical_flow_s flow; struct rc_channels_s rc; struct differential_pressure_s diff_pres; @@ -648,6 +655,7 @@ int sdlog2_thread_main(int argc, char *argv[]) struct { int cmd_sub; int status_sub; + int safety_sub; int sensor_sub; int att_sub; int att_sp_sub; @@ -660,6 +668,7 @@ int sdlog2_thread_main(int argc, char *argv[]) int global_pos_sub; int gps_pos_sub; int vicon_pos_sub; + int control_debug_sub; int flow_sub; int rc_sub; int airspeed_sub; @@ -680,6 +689,7 @@ int sdlog2_thread_main(int argc, char *argv[]) struct log_GPS_s log_GPS; struct log_ATTC_s log_ATTC; struct log_STAT_s log_STAT; + struct log_CTRL_s log_CTRL; struct log_RC_s log_RC; struct log_OUT0_s log_OUT0; struct log_AIRS_s log_AIRS; @@ -699,6 +709,12 @@ int sdlog2_thread_main(int argc, char *argv[]) fds[fdsc_count].events = POLLIN; fdsc_count++; + /* --- SAFETY --- */ + subs.safety_sub = orb_subscribe(ORB_ID(actuator_safety)); + fds[fdsc_count].fd = subs.safety_sub; + fds[fdsc_count].events = POLLIN; + fdsc_count++; + /* --- VEHICLE STATUS --- */ subs.status_sub = orb_subscribe(ORB_ID(vehicle_status)); fds[fdsc_count].fd = subs.status_sub; @@ -777,6 +793,12 @@ int sdlog2_thread_main(int argc, char *argv[]) fds[fdsc_count].events = POLLIN; fdsc_count++; + /* --- CONTROL DEBUG --- */ + subs.control_debug_sub = orb_subscribe(ORB_ID(vehicle_control_debug)); + fds[fdsc_count].fd = subs.control_debug_sub; + fds[fdsc_count].events = POLLIN; + fdsc_count++; + /* --- OPTICAL FLOW --- */ subs.flow_sub = orb_subscribe(ORB_ID(optical_flow)); fds[fdsc_count].fd = subs.flow_sub; @@ -854,22 +876,33 @@ int sdlog2_thread_main(int argc, char *argv[]) handled_topics++; } - /* --- VEHICLE STATUS - LOG MANAGEMENT --- */ + /* --- SAFETY- LOG MANAGEMENT --- */ if (fds[ifds++].revents & POLLIN) { - orb_copy(ORB_ID(vehicle_status), subs.status_sub, &buf_status); + orb_copy(ORB_ID(actuator_safety), subs.safety_sub, &buf_safety); if (log_when_armed) { - handle_status(&buf_status); + handle_status(&buf_safety); } handled_topics++; } + /* --- VEHICLE STATUS - LOG MANAGEMENT --- */ + if (fds[ifds++].revents & POLLIN) { + orb_copy(ORB_ID(vehicle_status), subs.status_sub, &buf_status); + + //if (log_when_armed) { + // handle_status(&buf_safety); + //} + + //handled_topics++; + } + if (!logging_enabled || !check_data || handled_topics >= poll_ret) { continue; } - ifds = 1; // Begin from fds[1] again + ifds = 2; // Begin from fds[2] again pthread_mutex_lock(&logbuffer_mutex); @@ -882,11 +915,16 @@ int sdlog2_thread_main(int argc, char *argv[]) if (fds[ifds++].revents & POLLIN) { // Don't orb_copy, it's already done few lines above log_msg.msg_type = LOG_STAT_MSG; - log_msg.body.log_STAT.state = (unsigned char) buf_status.state_machine; - log_msg.body.log_STAT.flight_mode = (unsigned char) buf_status.flight_mode; - log_msg.body.log_STAT.manual_control_mode = (unsigned char) buf_status.manual_control_mode; - log_msg.body.log_STAT.manual_sas_mode = (unsigned char) buf_status.manual_sas_mode; - log_msg.body.log_STAT.armed = (unsigned char) buf_status.flag_system_armed; + // XXX fix this + // log_msg.body.log_STAT.state = (unsigned char) buf_status.state_machine; + // log_msg.body.log_STAT.flight_mode = (unsigned char) buf_status.flight_mode; + // log_msg.body.log_STAT.manual_control_mode = (unsigned char) buf_status.manual_control_mode; + // log_msg.body.log_STAT.manual_sas_mode = (unsigned char) buf_status.manual_sas_mode; + log_msg.body.log_STAT.state = 0; + log_msg.body.log_STAT.flight_mode = 0; + log_msg.body.log_STAT.manual_control_mode = 0; + log_msg.body.log_STAT.manual_sas_mode = 0; + log_msg.body.log_STAT.armed = (unsigned char) buf_safety.armed; /* XXX fmu armed correct? */ log_msg.body.log_STAT.battery_voltage = buf_status.voltage_battery; log_msg.body.log_STAT.battery_current = buf_status.current_battery; log_msg.body.log_STAT.battery_remaining = buf_status.battery_remaining; @@ -977,6 +1015,9 @@ int sdlog2_thread_main(int argc, char *argv[]) log_msg.body.log_ATT.roll_rate = buf.att.rollspeed; log_msg.body.log_ATT.pitch_rate = buf.att.pitchspeed; log_msg.body.log_ATT.yaw_rate = buf.att.yawspeed; + log_msg.body.log_ATT.roll_acc = buf.att.rollacc; + log_msg.body.log_ATT.pitch_acc = buf.att.pitchacc; + log_msg.body.log_ATT.yaw_acc = buf.att.yawacc; LOGBUFFER_WRITE_AND_COUNT(ATT); } @@ -1073,6 +1114,27 @@ int sdlog2_thread_main(int argc, char *argv[]) // TODO not implemented yet } + /* --- CONTROL DEBUG --- */ + if (fds[ifds++].revents & POLLIN) { + orb_copy(ORB_ID(vehicle_control_debug), subs.control_debug_sub, &buf.control_debug); + + log_msg.msg_type = LOG_CTRL_MSG; + log_msg.body.log_CTRL.roll_p = buf.control_debug.roll_p; + log_msg.body.log_CTRL.roll_i = buf.control_debug.roll_i; + log_msg.body.log_CTRL.roll_d = buf.control_debug.roll_d; + log_msg.body.log_CTRL.roll_rate_p = buf.control_debug.roll_rate_p; + log_msg.body.log_CTRL.roll_rate_i = buf.control_debug.roll_rate_i; + log_msg.body.log_CTRL.roll_rate_d = buf.control_debug.roll_rate_d; + log_msg.body.log_CTRL.pitch_p = buf.control_debug.pitch_p; + log_msg.body.log_CTRL.pitch_i = buf.control_debug.pitch_i; + log_msg.body.log_CTRL.pitch_d = buf.control_debug.pitch_d; + log_msg.body.log_CTRL.pitch_rate_p = buf.control_debug.pitch_rate_p; + log_msg.body.log_CTRL.pitch_rate_i = buf.control_debug.pitch_rate_i; + log_msg.body.log_CTRL.pitch_rate_d = buf.control_debug.pitch_rate_d; + + LOGBUFFER_WRITE_AND_COUNT(CTRL); + } + /* --- FLOW --- */ if (fds[ifds++].revents & POLLIN) { orb_copy(ORB_ID(optical_flow), subs.flow_sub, &buf.flow); @@ -1225,10 +1287,10 @@ void handle_command(struct vehicle_command_s *cmd) } } -void handle_status(struct vehicle_status_s *status) +void handle_status(struct actuator_safety_s *safety) { - if (status->flag_system_armed != flag_system_armed) { - flag_system_armed = status->flag_system_armed; + if (safety->armed != flag_system_armed) { + flag_system_armed = safety->armed; if (flag_system_armed) { sdlog2_start_log(); diff --git a/src/modules/sdlog2/sdlog2_messages.h b/src/modules/sdlog2/sdlog2_messages.h index 4a66fe116..358637f93 100644 --- a/src/modules/sdlog2/sdlog2_messages.h +++ b/src/modules/sdlog2/sdlog2_messages.h @@ -63,6 +63,9 @@ struct log_ATT_s { float roll_rate; float pitch_rate; float yaw_rate; + float roll_acc; + float pitch_acc; + float yaw_acc; }; /* --- ATSP - ATTITUDE SET POINT --- */ @@ -160,27 +163,44 @@ struct log_STAT_s { unsigned char battery_warning; }; +/* --- CTRL - CONTROL DEBUG --- */ +#define LOG_CTRL_MSG 11 +struct log_CTRL_s { + float roll_p; + float roll_i; + float roll_d; + float roll_rate_p; + float roll_rate_i; + float roll_rate_d; + float pitch_p; + float pitch_i; + float pitch_d; + float pitch_rate_p; + float pitch_rate_i; + float pitch_rate_d; +}; + /* --- RC - RC INPUT CHANNELS --- */ -#define LOG_RC_MSG 11 +#define LOG_RC_MSG 12 struct log_RC_s { float channel[8]; }; /* --- OUT0 - ACTUATOR_0 OUTPUT --- */ -#define LOG_OUT0_MSG 12 +#define LOG_OUT0_MSG 13 struct log_OUT0_s { float output[8]; }; /* --- AIRS - AIRSPEED --- */ -#define LOG_AIRS_MSG 13 +#define LOG_AIRS_MSG 14 struct log_AIRS_s { float indicated_airspeed; float true_airspeed; }; /* --- ARSP - ATTITUDE RATE SET POINT --- */ -#define LOG_ARSP_MSG 14 +#define LOG_ARSP_MSG 15 struct log_ARSP_s { float roll_rate_sp; float pitch_rate_sp; @@ -188,7 +208,7 @@ struct log_ARSP_s { }; /* --- FLOW - OPTICAL FLOW --- */ -#define LOG_FLOW_MSG 15 +#define LOG_FLOW_MSG 16 struct log_FLOW_s { int16_t flow_raw_x; int16_t flow_raw_y; @@ -215,7 +235,7 @@ struct log_GPOS_s { static const struct log_format_s log_formats[] = { LOG_FORMAT(TIME, "Q", "StartTime"), - LOG_FORMAT(ATT, "ffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate"), + LOG_FORMAT(ATT, "fffffffff", "Roll,Pitch,Yaw,RollR,PitchR,YawR,RollA,PitchA,YawA"), LOG_FORMAT(ATSP, "ffff", "RollSP,PitchSP,YawSP,ThrustSP"), LOG_FORMAT(IMU, "fffffffff", "AccX,AccY,AccZ,GyroX,GyroY,GyroZ,MagX,MagY,MagZ"), LOG_FORMAT(SENS, "ffff", "BaroPres,BaroAlt,BaroTemp,DiffPres"), @@ -224,6 +244,7 @@ static const struct log_format_s log_formats[] = { LOG_FORMAT(GPS, "QBffLLfffff", "GPSTime,FixType,EPH,EPV,Lat,Lon,Alt,VelN,VelE,VelD,Cog"), LOG_FORMAT(ATTC, "ffff", "Roll,Pitch,Yaw,Thrust"), LOG_FORMAT(STAT, "BBBBBfffB", "State,FlightMode,CtlMode,SASMode,Armed,BatV,BatC,BatRem,BatWarn"), + LOG_FORMAT(CTRL, "ffffffffffff", "RP,RI,RD,RRP,RRI,RRD,PP,PI,PD,PRP,PRI,PRD"), LOG_FORMAT(RC, "ffffffff", "Ch0,Ch1,Ch2,Ch3,Ch4,Ch5,Ch6,Ch7"), LOG_FORMAT(OUT0, "ffffffff", "Out0,Out1,Out2,Out3,Out4,Out5,Out6,Out7"), LOG_FORMAT(AIRS, "ff", "IndSpeed,TrueSpeed"), diff --git a/src/modules/sensors/sensor_params.c b/src/modules/sensors/sensor_params.c index f6f4d60c7..7077972aa 100644 --- a/src/modules/sensors/sensor_params.c +++ b/src/modules/sensors/sensor_params.c @@ -164,13 +164,11 @@ PARAM_DEFINE_INT32(RC_MAP_PITCH, 2); PARAM_DEFINE_INT32(RC_MAP_THROTTLE, 3); PARAM_DEFINE_INT32(RC_MAP_YAW, 4); -PARAM_DEFINE_INT32(RC_MAP_OVER_SW, 5); -PARAM_DEFINE_INT32(RC_MAP_MODE_SW, 6); +PARAM_DEFINE_INT32(RC_MAP_MODE_SW, 5); +PARAM_DEFINE_INT32(RC_MAP_RETURN_SW, 6); +PARAM_DEFINE_INT32(RC_MAP_MISSIO_SW, 0); -PARAM_DEFINE_INT32(RC_MAP_MAN_SW, 0); -PARAM_DEFINE_INT32(RC_MAP_SAS_SW, 0); -PARAM_DEFINE_INT32(RC_MAP_RTL_SW, 0); -PARAM_DEFINE_INT32(RC_MAP_OFFB_SW, 0); +//PARAM_DEFINE_INT32(RC_MAP_OFFB_SW, 0); PARAM_DEFINE_INT32(RC_MAP_FLAPS, 0); diff --git a/src/modules/sensors/sensors.cpp b/src/modules/sensors/sensors.cpp index 1ded14a91..49a1da83b 100644 --- a/src/modules/sensors/sensors.cpp +++ b/src/modules/sensors/sensors.cpp @@ -208,13 +208,11 @@ private: int rc_map_yaw; int rc_map_throttle; - int rc_map_manual_override_sw; - int rc_map_auto_mode_sw; + int rc_map_mode_sw; + int rc_map_return_sw; + int rc_map_mission_sw; - int rc_map_manual_mode_sw; - int rc_map_sas_mode_sw; - int rc_map_rtl_sw; - int rc_map_offboard_ctrl_mode_sw; +// int rc_map_offboard_ctrl_mode_sw; int rc_map_flaps; @@ -256,13 +254,11 @@ private: param_t rc_map_yaw; param_t rc_map_throttle; - param_t rc_map_manual_override_sw; - param_t rc_map_auto_mode_sw; + param_t rc_map_mode_sw; + param_t rc_map_return_sw; + param_t rc_map_mission_sw; - param_t rc_map_manual_mode_sw; - param_t rc_map_sas_mode_sw; - param_t rc_map_rtl_sw; - param_t rc_map_offboard_ctrl_mode_sw; +// param_t rc_map_offboard_ctrl_mode_sw; param_t rc_map_flaps; @@ -462,16 +458,15 @@ Sensors::Sensors() : _parameter_handles.rc_map_throttle = param_find("RC_MAP_THROTTLE"); /* mandatory mode switches, mapped to channel 5 and 6 per default */ - _parameter_handles.rc_map_manual_override_sw = param_find("RC_MAP_OVER_SW"); - _parameter_handles.rc_map_auto_mode_sw = param_find("RC_MAP_MODE_SW"); + _parameter_handles.rc_map_mode_sw = param_find("RC_MAP_MODE_SW"); + _parameter_handles.rc_map_return_sw = param_find("RC_MAP_RETURN_SW"); _parameter_handles.rc_map_flaps = param_find("RC_MAP_FLAPS"); /* optional mode switches, not mapped per default */ - _parameter_handles.rc_map_manual_mode_sw = param_find("RC_MAP_MAN_SW"); - _parameter_handles.rc_map_sas_mode_sw = param_find("RC_MAP_SAS_SW"); - _parameter_handles.rc_map_rtl_sw = param_find("RC_MAP_RTL_SW"); - _parameter_handles.rc_map_offboard_ctrl_mode_sw = param_find("RC_MAP_OFFB_SW"); + _parameter_handles.rc_map_mission_sw = param_find("RC_MAP_MISSIO_SW"); + +// _parameter_handles.rc_map_offboard_ctrl_mode_sw = param_find("RC_MAP_OFFB_SW"); _parameter_handles.rc_map_aux1 = param_find("RC_MAP_AUX1"); _parameter_handles.rc_map_aux2 = param_find("RC_MAP_AUX2"); @@ -611,33 +606,25 @@ Sensors::parameters_update() warnx("Failed getting throttle chan index"); } - if (param_get(_parameter_handles.rc_map_manual_override_sw, &(_parameters.rc_map_manual_override_sw)) != OK) { - warnx("Failed getting override sw chan index"); - } - - if (param_get(_parameter_handles.rc_map_auto_mode_sw, &(_parameters.rc_map_auto_mode_sw)) != OK) { - warnx("Failed getting auto mode sw chan index"); - } - - if (param_get(_parameter_handles.rc_map_flaps, &(_parameters.rc_map_flaps)) != OK) { - warnx("Failed getting flaps chan index"); + if (param_get(_parameter_handles.rc_map_mode_sw, &(_parameters.rc_map_mode_sw)) != OK) { + warnx("Failed getting mode sw chan index"); } - if (param_get(_parameter_handles.rc_map_manual_mode_sw, &(_parameters.rc_map_manual_mode_sw)) != OK) { - warnx("Failed getting manual mode sw chan index"); + if (param_get(_parameter_handles.rc_map_return_sw, &(_parameters.rc_map_return_sw)) != OK) { + warnx("Failed getting return sw chan index"); } - if (param_get(_parameter_handles.rc_map_rtl_sw, &(_parameters.rc_map_rtl_sw)) != OK) { - warnx("Failed getting rtl sw chan index"); + if (param_get(_parameter_handles.rc_map_mission_sw, &(_parameters.rc_map_mission_sw)) != OK) { + warnx("Failed getting mission sw chan index"); } - if (param_get(_parameter_handles.rc_map_sas_mode_sw, &(_parameters.rc_map_sas_mode_sw)) != OK) { - warnx("Failed getting sas mode sw chan index"); + if (param_get(_parameter_handles.rc_map_flaps, &(_parameters.rc_map_flaps)) != OK) { + warnx("Failed getting flaps chan index"); } - if (param_get(_parameter_handles.rc_map_offboard_ctrl_mode_sw, &(_parameters.rc_map_offboard_ctrl_mode_sw)) != OK) { - warnx("Failed getting offboard control mode sw chan index"); - } +// if (param_get(_parameter_handles.rc_map_offboard_ctrl_mode_sw, &(_parameters.rc_map_offboard_ctrl_mode_sw)) != OK) { +// warnx("Failed getting offboard control mode sw chan index"); +// } if (param_get(_parameter_handles.rc_map_aux1, &(_parameters.rc_map_aux1)) != OK) { warnx("Failed getting mode aux 1 index"); @@ -681,15 +668,13 @@ Sensors::parameters_update() _rc.function[PITCH] = _parameters.rc_map_pitch - 1; _rc.function[YAW] = _parameters.rc_map_yaw - 1; - _rc.function[OVERRIDE] = _parameters.rc_map_manual_override_sw - 1; - _rc.function[AUTO_MODE] = _parameters.rc_map_auto_mode_sw - 1; + _rc.function[MODE] = _parameters.rc_map_mode_sw - 1; + _rc.function[RETURN] = _parameters.rc_map_return_sw - 1; + _rc.function[MISSION] = _parameters.rc_map_mission_sw - 1; _rc.function[FLAPS] = _parameters.rc_map_flaps - 1; - _rc.function[MANUAL_MODE] = _parameters.rc_map_manual_mode_sw - 1; - _rc.function[RTL] = _parameters.rc_map_rtl_sw - 1; - _rc.function[SAS_MODE] = _parameters.rc_map_sas_mode_sw - 1; - _rc.function[OFFBOARD_MODE] = _parameters.rc_map_offboard_ctrl_mode_sw - 1; +// _rc.function[OFFBOARD_MODE] = _parameters.rc_map_offboard_ctrl_mode_sw - 1; _rc.function[AUX_1] = _parameters.rc_map_aux1 - 1; _rc.function[AUX_2] = _parameters.rc_map_aux2 - 1; @@ -1145,10 +1130,10 @@ Sensors::ppm_poll() manual_control.yaw = NAN; manual_control.throttle = NAN; - manual_control.manual_mode_switch = NAN; - manual_control.manual_sas_switch = NAN; - manual_control.return_to_launch_switch = NAN; - manual_control.auto_offboard_input_switch = NAN; + manual_control.mode_switch = NAN; + manual_control.return_switch = NAN; + manual_control.mission_switch = NAN; +// manual_control.auto_offboard_input_switch = NAN; manual_control.flaps = NAN; manual_control.aux1 = NAN; @@ -1248,11 +1233,14 @@ Sensors::ppm_poll() manual_control.yaw *= _parameters.rc_scale_yaw; } - /* override switch input */ - manual_control.manual_override_switch = limit_minus_one_to_one(_rc.chan[_rc.function[OVERRIDE]].scaled); - /* mode switch input */ - manual_control.auto_mode_switch = limit_minus_one_to_one(_rc.chan[_rc.function[AUTO_MODE]].scaled); + manual_control.mode_switch = limit_minus_one_to_one(_rc.chan[_rc.function[MODE]].scaled); + + /* land switch input */ + manual_control.return_switch = limit_minus_one_to_one(_rc.chan[_rc.function[RETURN]].scaled); + + /* land switch input */ + manual_control.mission_switch = limit_minus_one_to_one(_rc.chan[_rc.function[MISSION]].scaled); /* flaps */ if (_rc.function[FLAPS] >= 0) { @@ -1264,21 +1252,17 @@ Sensors::ppm_poll() } } - if (_rc.function[MANUAL_MODE] >= 0) { - manual_control.manual_mode_switch = limit_minus_one_to_one(_rc.chan[_rc.function[MANUAL_MODE]].scaled); - } - - if (_rc.function[SAS_MODE] >= 0) { - manual_control.manual_sas_switch = limit_minus_one_to_one(_rc.chan[_rc.function[SAS_MODE]].scaled); + if (_rc.function[MODE] >= 0) { + manual_control.mode_switch = limit_minus_one_to_one(_rc.chan[_rc.function[MODE]].scaled); } - if (_rc.function[RTL] >= 0) { - manual_control.return_to_launch_switch = limit_minus_one_to_one(_rc.chan[_rc.function[RTL]].scaled); + if (_rc.function[MISSION] >= 0) { + manual_control.mission_switch = limit_minus_one_to_one(_rc.chan[_rc.function[MISSION]].scaled); } - if (_rc.function[OFFBOARD_MODE] >= 0) { - manual_control.auto_offboard_input_switch = limit_minus_one_to_one(_rc.chan[_rc.function[OFFBOARD_MODE]].scaled); - } +// if (_rc.function[OFFBOARD_MODE] >= 0) { +// manual_control.auto_offboard_input_switch = limit_minus_one_to_one(_rc.chan[_rc.function[OFFBOARD_MODE]].scaled); +// } /* aux functions, only assign if valid mapping is present */ if (_rc.function[AUX_1] >= 0) { diff --git a/src/modules/systemlib/pid/pid.c b/src/modules/systemlib/pid/pid.c index 4996a8f66..9308100b0 100644 --- a/src/modules/systemlib/pid/pid.c +++ b/src/modules/systemlib/pid/pid.c @@ -124,7 +124,7 @@ __EXPORT int pid_set_parameters(PID_t *pid, float kp, float ki, float kd, float * @param dt * @return */ -__EXPORT float pid_calculate(PID_t *pid, float sp, float val, float val_dot, float dt) +__EXPORT float pid_calculate(PID_t *pid, float sp, float val, float val_dot, float dt, float *ctrl_p, float *ctrl_i, float *ctrl_d) { /* error = setpoint - actual_position integral = integral + (error*dt) @@ -196,6 +196,10 @@ __EXPORT float pid_calculate(PID_t *pid, float sp, float val, float val_dot, flo pid->last_output = output; } + *ctrl_p = (error * pid->kp); + *ctrl_i = (i * pid->ki); + *ctrl_d = (d * pid->kd); + return pid->last_output; } diff --git a/src/modules/systemlib/pid/pid.h b/src/modules/systemlib/pid/pid.h index eca228464..5f2650f69 100644 --- a/src/modules/systemlib/pid/pid.h +++ b/src/modules/systemlib/pid/pid.h @@ -85,7 +85,7 @@ typedef struct { __EXPORT void pid_init(PID_t *pid, float kp, float ki, float kd, float intmax, float limit, uint8_t mode, float dt_min); __EXPORT int pid_set_parameters(PID_t *pid, float kp, float ki, float kd, float intmax, float limit); //void pid_set(PID_t *pid, float sp); -__EXPORT float pid_calculate(PID_t *pid, float sp, float val, float val_dot, float dt); +__EXPORT float pid_calculate(PID_t *pid, float sp, float val, float val_dot, float dt, float *ctrl_p, float *ctrl_i, float *ctrl_d); __EXPORT void pid_reset_integral(PID_t *pid); diff --git a/src/modules/uORB/objects_common.cpp b/src/modules/uORB/objects_common.cpp index e7d7e7bca..8ae47ba8b 100644 --- a/src/modules/uORB/objects_common.cpp +++ b/src/modules/uORB/objects_common.cpp @@ -98,6 +98,9 @@ ORB_DEFINE(rc_channels, struct rc_channels_s); #include "topics/vehicle_command.h" ORB_DEFINE(vehicle_command, struct vehicle_command_s); +#include "topics/vehicle_control_mode.h" +ORB_DEFINE(vehicle_control_mode, struct vehicle_control_mode_s); + #include "topics/vehicle_local_position_setpoint.h" ORB_DEFINE(vehicle_local_position_setpoint, struct vehicle_local_position_setpoint_s); @@ -119,6 +122,9 @@ ORB_DEFINE(vehicle_attitude_setpoint, struct vehicle_attitude_setpoint_s); #include "topics/manual_control_setpoint.h" ORB_DEFINE(manual_control_setpoint, struct manual_control_setpoint_s); +#include "topics/vehicle_control_debug.h" +ORB_DEFINE(vehicle_control_debug, struct vehicle_control_debug_s); + #include "topics/offboard_control_setpoint.h" ORB_DEFINE(offboard_control_setpoint, struct offboard_control_setpoint_s); @@ -146,7 +152,9 @@ ORB_DEFINE(actuator_controls_0, struct actuator_controls_s); ORB_DEFINE(actuator_controls_1, struct actuator_controls_s); ORB_DEFINE(actuator_controls_2, struct actuator_controls_s); ORB_DEFINE(actuator_controls_3, struct actuator_controls_s); -ORB_DEFINE(actuator_armed, struct actuator_armed_s); + +#include "topics/actuator_safety.h" +ORB_DEFINE(actuator_safety, struct actuator_safety_s); /* actuator controls, as set by actuators / mixers after limiting */ #include "topics/actuator_controls_effective.h" diff --git a/src/modules/uORB/topics/actuator_controls.h b/src/modules/uORB/topics/actuator_controls.h index b7c4196c0..26b967237 100644 --- a/src/modules/uORB/topics/actuator_controls.h +++ b/src/modules/uORB/topics/actuator_controls.h @@ -52,6 +52,9 @@ #define NUM_ACTUATOR_CONTROLS 8 #define NUM_ACTUATOR_CONTROL_GROUPS 4 /**< for sanity checking */ +/* control sets with pre-defined applications */ +#define ORB_ID_VEHICLE_ATTITUDE_CONTROLS ORB_ID(actuator_controls_0) + struct actuator_controls_s { uint64_t timestamp; float control[NUM_ACTUATOR_CONTROLS]; @@ -63,16 +66,4 @@ ORB_DECLARE(actuator_controls_1); ORB_DECLARE(actuator_controls_2); ORB_DECLARE(actuator_controls_3); -/* control sets with pre-defined applications */ -#define ORB_ID_VEHICLE_ATTITUDE_CONTROLS ORB_ID(actuator_controls_0) - -/** global 'actuator output is live' control. */ -struct actuator_armed_s { - bool armed; /**< Set to true if system is armed */ - bool ready_to_arm; /**< Set to true if system is ready to be armed */ - bool lockdown; /**< Set to true if actuators are forced to being disabled (due to emergency or HIL) */ -}; - -ORB_DECLARE(actuator_armed); - #endif
\ No newline at end of file diff --git a/src/modules/uORB/topics/actuator_safety.h b/src/modules/uORB/topics/actuator_safety.h new file mode 100644 index 000000000..c431217ab --- /dev/null +++ b/src/modules/uORB/topics/actuator_safety.h @@ -0,0 +1,66 @@ +/**************************************************************************** + * + * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file actuator_controls.h + * + * Actuator control topics - mixer inputs. + * + * Values published to these topics are the outputs of the vehicle control + * system, and are expected to be mixed and used to drive the actuators + * (servos, speed controls, etc.) that operate the vehicle. + * + * Each topic can be published by a single controller + */ + +#ifndef TOPIC_ACTUATOR_SAFETY_H +#define TOPIC_ACTUATOR_SAFETY_H + +#include <stdint.h> +#include "../uORB.h" + +/** global 'actuator output is live' control. */ +struct actuator_safety_s { + + uint64_t timestamp; + bool safety_switch_available; /**< Set to true if a safety switch is connected */ + bool safety_off; /**< Set to true if safety is off */ + bool armed; /**< Set to true if system is armed */ + bool ready_to_arm; /**< Set to true if system is ready to be armed */ + bool lockdown; /**< Set to true if actuators are forced to being disabled (due to emergency or HIL) */ + bool hil_enabled; /**< Set to true if hardware-in-the-loop (HIL) is enabled */ +}; + +ORB_DECLARE(actuator_safety); + +#endif
\ No newline at end of file diff --git a/src/modules/uORB/topics/manual_control_setpoint.h b/src/modules/uORB/topics/manual_control_setpoint.h index 261a8a4ad..cfee81ea2 100644 --- a/src/modules/uORB/topics/manual_control_setpoint.h +++ b/src/modules/uORB/topics/manual_control_setpoint.h @@ -56,17 +56,17 @@ struct manual_control_setpoint_s { float yaw; /**< rudder / yaw rate / yaw */ float throttle; /**< throttle / collective thrust / altitude */ - float manual_override_switch; /**< manual override mode (mandatory) */ - float auto_mode_switch; /**< auto mode switch (mandatory) */ + float mode_switch; /**< mode 3 position switch (mandatory): manual, assisted, auto */ + float return_switch; /**< land 2 position switch (mandatory): land, no effect */ + float mission_switch; /**< mission 2 position switch (optional): mission, loiter */ /** * Any of the channels below may not be available and be set to NaN * to indicate that it does not contain valid data. */ - float manual_mode_switch; /**< manual mode (man, sas, alt) switch (optional) */ - float manual_sas_switch; /**< sas mode (rates / attitude) switch (optional) */ - float return_to_launch_switch; /**< return to launch switch (0 = disabled, 1 = enabled) */ - float auto_offboard_input_switch; /**< controller setpoint source (0 = onboard, 1 = offboard) */ + + // XXX needed or parameter? + //float auto_offboard_input_switch; /**< controller setpoint source (0 = onboard, 1 = offboard) */ float flaps; /**< flap position */ diff --git a/src/modules/uORB/topics/rc_channels.h b/src/modules/uORB/topics/rc_channels.h index 9dd54df91..a0bb25af4 100644 --- a/src/modules/uORB/topics/rc_channels.h +++ b/src/modules/uORB/topics/rc_channels.h @@ -68,18 +68,16 @@ enum RC_CHANNELS_FUNCTION ROLL = 1, PITCH = 2, YAW = 3, - OVERRIDE = 4, - AUTO_MODE = 5, - MANUAL_MODE = 6, - SAS_MODE = 7, - RTL = 8, - OFFBOARD_MODE = 9, - FLAPS = 10, - AUX_1 = 11, - AUX_2 = 12, - AUX_3 = 13, - AUX_4 = 14, - AUX_5 = 15, + MODE = 4, + RETURN = 5, + MISSION = 6, + OFFBOARD_MODE = 7, + FLAPS = 8, + AUX_1 = 9, + AUX_2 = 10, + AUX_3 = 11, + AUX_4 = 12, + AUX_5 = 13, RC_CHANNELS_FUNCTION_MAX /**< indicates the number of functions. There can be more functions than RC channels. */ }; diff --git a/src/modules/uORB/topics/vehicle_control_debug.h b/src/modules/uORB/topics/vehicle_control_debug.h new file mode 100644 index 000000000..6184284a4 --- /dev/null +++ b/src/modules/uORB/topics/vehicle_control_debug.h @@ -0,0 +1,87 @@ +/**************************************************************************** + * + * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Author: @author Lorenz Meier <lm@inf.ethz.ch> + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * 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 vehicle_control_debug.h + * For debugging purposes to log PID parts of controller + */ + +#ifndef TOPIC_VEHICLE_CONTROL_DEBUG_H_ +#define TOPIC_VEHICLE_CONTROL_DEBUG_H_ + +#include <stdint.h> +#include "../uORB.h" + +/** + * @addtogroup topics + * @{ + */ +struct vehicle_control_debug_s +{ + uint64_t timestamp; /**< in microseconds since system start */ + + float roll_p; /**< roll P control part */ + float roll_i; /**< roll I control part */ + float roll_d; /**< roll D control part */ + + float roll_rate_p; /**< roll rate P control part */ + float roll_rate_i; /**< roll rate I control part */ + float roll_rate_d; /**< roll rate D control part */ + + float pitch_p; /**< pitch P control part */ + float pitch_i; /**< pitch I control part */ + float pitch_d; /**< pitch D control part */ + + float pitch_rate_p; /**< pitch rate P control part */ + float pitch_rate_i; /**< pitch rate I control part */ + float pitch_rate_d; /**< pitch rate D control part */ + + float yaw_p; /**< yaw P control part */ + float yaw_i; /**< yaw I control part */ + float yaw_d; /**< yaw D control part */ + + float yaw_rate_p; /**< yaw rate P control part */ + float yaw_rate_i; /**< yaw rate I control part */ + float yaw_rate_d; /**< yaw rate D control part */ + +}; /**< vehicle_control_debug */ + + /** + * @} + */ + +/* register this as object request broker structure */ +ORB_DECLARE(vehicle_control_debug); + +#endif diff --git a/src/modules/uORB/topics/vehicle_control_mode.h b/src/modules/uORB/topics/vehicle_control_mode.h new file mode 100644 index 000000000..177e30898 --- /dev/null +++ b/src/modules/uORB/topics/vehicle_control_mode.h @@ -0,0 +1,91 @@ +/**************************************************************************** + * + * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Author: @author Lorenz Meier <lm@inf.ethz.ch> + * @author Petri Tanskanen <petri.tanskanen@inf.ethz.ch> + * @author Thomas Gubler <thomasgubler@student.ethz.ch> + * @author Julian Oes <joes@student.ethz.ch> + * + * 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 vehicle_control_mode.h + * Definition of the vehicle_control_mode uORB topic. + * + * All control apps should depend their actions based on the flags set here. + */ + +#ifndef VEHICLE_CONTROL_MODE +#define VEHICLE_CONTROL_MODE + +#include <stdint.h> +#include <stdbool.h> +#include "../uORB.h" + +/** + * @addtogroup topics @{ + */ + + +/** + * state machine / state of vehicle. + * + * Encodes the complete system state and is set by the commander app. + */ +struct vehicle_control_mode_s +{ + uint16_t counter; /**< incremented by the writing thread everytime new data is stored */ + uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */ + + bool flag_external_manual_override_ok; /**< external override non-fatal for system. Only true for fixed wing */ + + bool flag_system_emergency; + bool flag_preflight_calibration; + + bool flag_control_manual_enabled; /**< true if manual input is mixed in */ + bool flag_control_offboard_enabled; /**< true if offboard control input is on */ + bool flag_auto_enabled; + bool flag_control_rates_enabled; /**< true if rates are stabilized */ + bool flag_control_attitude_enabled; /**< true if attitude stabilization is mixed in */ + bool flag_control_velocity_enabled; /**< true if speed (implies direction) is controlled */ + bool flag_control_position_enabled; /**< true if position is controlled */ + + bool failsave_lowlevel; /**< Set to true if low-level failsafe mode is enabled */ + bool failsave_highlevel; /**< Set to true if high-level failsafe mode is enabled */ +}; + +/** + * @} + */ + +/* register this as object request broker structure */ +ORB_DECLARE(vehicle_control_mode); + +#endif diff --git a/src/modules/uORB/topics/vehicle_status.h b/src/modules/uORB/topics/vehicle_status.h index c7c1048f6..2bcd57f4b 100644 --- a/src/modules/uORB/topics/vehicle_status.h +++ b/src/modules/uORB/topics/vehicle_status.h @@ -59,21 +59,58 @@ */ /* State Machine */ -typedef enum -{ - SYSTEM_STATE_PREFLIGHT = 0, - SYSTEM_STATE_STANDBY = 1, - SYSTEM_STATE_GROUND_READY = 2, - SYSTEM_STATE_MANUAL = 3, - SYSTEM_STATE_STABILIZED = 4, - SYSTEM_STATE_AUTO = 5, - SYSTEM_STATE_MISSION_ABORT = 6, - SYSTEM_STATE_EMCY_LANDING = 7, - SYSTEM_STATE_EMCY_CUTOFF = 8, - SYSTEM_STATE_GROUND_ERROR = 9, - SYSTEM_STATE_REBOOT= 10, - -} commander_state_machine_t; +typedef enum { + NAVIGATION_STATE_INIT=0, + NAVIGATION_STATE_MANUAL_STANDBY, + NAVIGATION_STATE_MANUAL, + NAVIGATION_STATE_SEATBELT_STANDBY, + NAVIGATION_STATE_SEATBELT, + NAVIGATION_STATE_SEATBELT_DESCENT, + NAVIGATION_STATE_AUTO_STANDBY, + NAVIGATION_STATE_AUTO_READY, + NAVIGATION_STATE_AUTO_TAKEOFF, + NAVIGATION_STATE_AUTO_LOITER, + NAVIGATION_STATE_AUTO_MISSION, + NAVIGATION_STATE_AUTO_RTL, + NAVIGATION_STATE_AUTO_LAND +} navigation_state_t; + +typedef enum { + MANUAL_STANDBY = 0, + MANUAL_READY, + MANUAL_IN_AIR +} manual_state_t; + +typedef enum { + ARMING_STATE_INIT = 0, + ARMING_STATE_STANDBY, + ARMING_STATE_ARMED, + ARMING_STATE_ARMED_ERROR, + ARMING_STATE_STANDBY_ERROR, + ARMING_STATE_REBOOT, + ARMING_STATE_IN_AIR_RESTORE +} arming_state_t; + +typedef enum { + HIL_STATE_OFF = 0, + HIL_STATE_ON +} hil_state_t; + +typedef enum { + MODE_SWITCH_MANUAL = 0, + MODE_SWITCH_SEATBELT, + MODE_SWITCH_AUTO +} mode_switch_pos_t; + +typedef enum { + RETURN_SWITCH_NONE = 0, + RETURN_SWITCH_RETURN +} return_switch_pos_t; + +typedef enum { + MISSION_SWITCH_NONE = 0, + MISSION_SWITCH_MISSION +} mission_switch_pos_t; enum VEHICLE_MODE_FLAG { VEHICLE_MODE_FLAG_SAFETY_ARMED = 128, @@ -86,26 +123,6 @@ enum VEHICLE_MODE_FLAG { VEHICLE_MODE_FLAG_CUSTOM_MODE_ENABLED = 1 }; /**< Same as MAV_MODE_FLAG of MAVLink 1.0 protocol */ -enum VEHICLE_FLIGHT_MODE { - VEHICLE_FLIGHT_MODE_MANUAL = 0, /**< direct manual control, exact mode determined by VEHICLE_MANUAL_CONTROL_MODE */ - VEHICLE_FLIGHT_MODE_STAB, /**< attitude or rate stabilization plus velocity or position stabilization */ - VEHICLE_FLIGHT_MODE_HOLD, /**< hold current position (hover or loiter around position when switched) */ - VEHICLE_FLIGHT_MODE_AUTO /**< attitude or rate stabilization plus absolute position control and waypoints */ -}; - -enum VEHICLE_MANUAL_CONTROL_MODE { - VEHICLE_MANUAL_CONTROL_MODE_DIRECT = 0, /**< no attitude control, direct stick input mixing (only fixed wing) */ - VEHICLE_MANUAL_CONTROL_MODE_RATES, /**< body rates control mode */ - VEHICLE_MANUAL_CONTROL_MODE_SAS /**< stability augmented system (SAS) mode */ -}; - -enum VEHICLE_MANUAL_SAS_MODE { - VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_ABS = 0, /**< roll, pitch and yaw absolute */ - VEHICLE_MANUAL_SAS_MODE_ROLL_PITCH_ABS_YAW_RATE, /**< roll and pitch absolute, yaw rate */ - VEHICLE_MANUAL_SAS_MODE_SIMPLE, /**< simple mode (includes altitude hold) */ - VEHICLE_MANUAL_SAS_MODE_ALTITUDE /**< altitude hold */ -}; - /** * Should match 1:1 MAVLink's MAV_TYPE ENUM */ @@ -134,7 +151,7 @@ enum VEHICLE_TYPE { enum VEHICLE_BATTERY_WARNING { VEHICLE_BATTERY_WARNING_NONE = 0, /**< no battery low voltage warning active */ VEHICLE_BATTERY_WARNING_WARNING, /**< warning of low voltage 1. stage */ - VEHICLE_BATTERY_WARNING_ALERT /**< aleting of low voltage 2. stage */ + VEHICLE_BATTERY_WARNING_ALERT /**< alerting of low voltage 2. stage */ }; @@ -150,32 +167,55 @@ struct vehicle_status_s uint16_t counter; /**< incremented by the writing thread everytime new data is stored */ uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */ uint64_t failsave_lowlevel_start_time; /**< time when the lowlevel failsafe flag was set */ - //uint64_t failsave_highlevel_begin; TO BE COMPLETED +// uint64_t failsave_highlevel_begin; TO BE COMPLETED + + navigation_state_t navigation_state; /**< current system state */ + arming_state_t arming_state; /**< current arming state */ + hil_state_t hil_state; /**< current hil state */ - commander_state_machine_t state_machine; /**< current flight state, main state machine */ - enum VEHICLE_FLIGHT_MODE flight_mode; /**< current flight mode, as defined by mode switch */ - enum VEHICLE_MANUAL_CONTROL_MODE manual_control_mode; /**< current attitude control mode, as defined by VEHICLE_ATTITUDE_MODE enum */ - enum VEHICLE_MANUAL_SAS_MODE manual_sas_mode; /**< current stabilization mode */ int32_t system_type; /**< system type, inspired by MAVLink's VEHICLE_TYPE enum */ int32_t system_id; /**< system id, inspired by MAVLink's system ID field */ int32_t component_id; /**< subsystem / component id, inspired by MAVLink's component ID field */ /* system flags - these represent the state predicates */ - bool flag_system_armed; /**< true is motors / actuators are armed */ - bool flag_control_manual_enabled; /**< true if manual input is mixed in */ - bool flag_control_offboard_enabled; /**< true if offboard control input is on */ + mode_switch_pos_t mode_switch; + return_switch_pos_t return_switch; + mission_switch_pos_t mission_switch; + + + bool condition_system_emergency; + bool condition_system_in_air_restore; /**< true if we can restore in mid air */ + bool condition_system_sensors_initialized; + bool condition_system_returned_to_home; + bool condition_auto_mission_available; + bool condition_global_position_valid; /**< set to true by the commander app if the quality of the gps signal is good enough to use it in the position estimator */ + bool condition_launch_position_valid; /**< indicates a valid launch position */ + bool condition_home_position_valid; /**< indicates a valid home position (a valid home position is not always a valid launch) */ + bool condition_local_position_valid; + bool condition_airspeed_valid; /**< set to true by the commander app if there is a valid airspeed measurement available */ + + // bool condition_auto_flight_mode_ok; /**< conditions of auto flight mode apply plus a valid takeoff position lock has been aquired */ + bool flag_external_manual_override_ok; /**< external override non-fatal for system. Only true for fixed wing */ + bool flag_hil_enabled; /**< true if hardware in the loop simulation is enabled */ + //bool flag_armed; /**< true is motors / actuators are armed */ + //bool flag_safety_off; /**< true if safety is off */ + bool flag_system_emergency; + bool flag_preflight_calibration; - bool flag_control_rates_enabled; /**< true if rates are stabilized */ - bool flag_control_attitude_enabled; /**< true if attitude stabilization is mixed in */ - bool flag_control_velocity_enabled; /**< true if speed (implies direction) is controlled */ - bool flag_control_position_enabled; /**< true if position is controlled */ + // bool flag_control_manual_enabled; /**< true if manual input is mixed in */ + // bool flag_control_offboard_enabled; /**< true if offboard control input is on */ + // bool flag_auto_enabled; + // bool flag_control_rates_enabled; /**< true if rates are stabilized */ + // bool flag_control_attitude_enabled; /**< true if attitude stabilization is mixed in */ + // bool flag_control_velocity_enabled; /**< true if speed (implies direction) is controlled */ + // bool flag_control_position_enabled; /**< true if position is controlled */ - bool flag_preflight_gyro_calibration; /**< true if gyro calibration is requested */ - bool flag_preflight_mag_calibration; /**< true if mag calibration is requested */ - bool flag_preflight_accel_calibration; - bool flag_preflight_airspeed_calibration; + // bool flag_preflight_gyro_calibration; /**< true if gyro calibration is requested */ + // bool flag_preflight_mag_calibration; /**< true if mag calibration is requested */ + // bool flag_preflight_accel_calibration; + // bool flag_preflight_airspeed_calibration; bool rc_signal_found_once; bool rc_signal_lost; /**< true if RC reception is terminally lost */ @@ -188,7 +228,7 @@ struct vehicle_status_s uint64_t offboard_control_signal_lost_interval; /**< interval in microseconds without an offboard control message */ bool failsave_lowlevel; /**< Set to true if low-level failsafe mode is enabled */ - //bool failsave_highlevel; + bool failsave_highlevel; /* see SYS_STATUS mavlink message for the following */ uint32_t onboard_control_sensors_present; @@ -205,15 +245,6 @@ struct vehicle_status_s uint16_t errors_count2; uint16_t errors_count3; uint16_t errors_count4; - - bool flag_global_position_valid; /**< set to true by the commander app if the quality of the gps signal is good enough to use it in the position estimator */ - bool flag_local_position_valid; - bool flag_vector_flight_mode_ok; /**< position estimation, battery voltage and other critical subsystems are good for autonomous flight */ - bool flag_auto_flight_mode_ok; /**< conditions of vector flight mode apply plus a valid takeoff position lock has been aquired */ - bool flag_external_manual_override_ok; /**< external override non-fatal for system. Only true for fixed wing */ - bool flag_valid_launch_position; /**< indicates a valid launch position */ - bool flag_valid_home_position; /**< indicates a valid home position (a valid home position is not always a valid launch) */ - bool flag_airspeed_valid; /**< set to true by the commander app if there is a valid airspeed measurement available */ }; /** diff --git a/src/systemcmds/esc_calib/esc_calib.c b/src/systemcmds/esc_calib/esc_calib.c new file mode 100644 index 000000000..188fa4e37 --- /dev/null +++ b/src/systemcmds/esc_calib/esc_calib.c @@ -0,0 +1,250 @@ +/**************************************************************************** + * + * Copyright (C) 2013 PX4 Development Team. All rights reserved. + * + * Redistribution and use in source and binary forms, with or without + * modification, are permitted provided that the following conditions + * are met: + * + * 1. Redistributions of source code must retain the above copyright + * notice, this list of conditions and the following disclaimer. + * 2. Redistributions in binary form must reproduce the above copyright + * notice, this list of conditions and the following disclaimer in + * the documentation and/or other materials provided with the + * distribution. + * 3. Neither the name PX4 nor the names of its contributors may be + * used to endorse or promote products derived from this software + * without specific prior written permission. + * + * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS + * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT + * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS + * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE + * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, + * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, + * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS + * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED + * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT + * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN + * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE + * POSSIBILITY OF SUCH DAMAGE. + * + ****************************************************************************/ + +/** + * @file esc_calib.c + * + * Tool for ESC calibration + */ + +#include <nuttx/config.h> + +#include <stdio.h> +#include <stdlib.h> +#include <string.h> +#include <stdbool.h> +#include <unistd.h> +#include <fcntl.h> +#include <sys/mount.h> +#include <sys/ioctl.h> +#include <sys/stat.h> + +#include <nuttx/i2c.h> +#include <nuttx/mtd.h> +#include <nuttx/fs/nxffs.h> +#include <nuttx/fs/ioctl.h> + +#include <arch/board/board.h> + +#include "systemlib/systemlib.h" +#include "systemlib/err.h" +#include "drivers/drv_pwm_output.h" + +static void usage(const char *reason); +__EXPORT int esc_calib_main(int argc, char *argv[]); + +#define MAX_CHANNELS 8 + +static void +usage(const char *reason) +{ + if (reason != NULL) + warnx("%s", reason); + errx(1, + "usage:\n" + "esc_calib [-d <device>] <channels>\n" + " <device> PWM output device (defaults to " PWM_OUTPUT_DEVICE_PATH ")\n" + " <channels> Provide channels (e.g.: 1 2 3 4)\n" + ); + +} + +int +esc_calib_main(int argc, char *argv[]) +{ + const char *dev = PWM_OUTPUT_DEVICE_PATH; + char *ep; + bool channels_selected[MAX_CHANNELS] = {false}; + int ch; + int ret; + char c; + + if (argc < 2) + usage(NULL); + + while ((ch = getopt(argc, argv, "d:")) != EOF) { + switch (ch) { + + case 'd': + dev = optarg; + argc--; + break; + + default: + usage(NULL); + } + } + + if(argc < 1) { + usage("no channels provided"); + } + + while (--argc) { + const char *arg = argv[argc]; + unsigned channel_number = strtol(arg, &ep, 0); + + if (*ep == '\0') { + if (channel_number > MAX_CHANNELS || channel_number <= 0) { + err(1, "invalid channel number: %d", channel_number); + } else { + channels_selected[channel_number-1] = true; + + } + } + } + + /* Wait for confirmation */ + int console = open("/dev/console", O_NONBLOCK | O_RDONLY | O_NOCTTY); + if (!console) + err(1, "failed opening console"); + + warnx("ATTENTION, please remove or fix props before starting calibration!\n" + "\n" + "Also press the arming switch first for safety off\n" + "\n" + "Do you really want to start calibration: y or n?\n"); + + /* wait for user input */ + while (1) { + + if (read(console, &c, 1) == 1) { + if (c == 'y' || c == 'Y') { + + break; + } else if (c == 0x03 || c == 0x63 || c == 'q') { + warnx("ESC calibration exited"); + close(console); + exit(0); + } else if (c == 'n' || c == 'N') { + warnx("ESC calibration aborted"); + close(console); + exit(0); + } else { + warnx("Unknown input, ESC calibration aborted"); + close(console); + exit(0); + } + } + /* rate limit to ~ 20 Hz */ + usleep(50000); + } + + /* open for ioctl only */ + int fd = open(dev, 0); + if (fd < 0) + err(1, "can't open %s", dev); + + // XXX arming not necessaire at the moment + // /* Then arm */ + // ret = ioctl(fd, PWM_SERVO_SET_ARM_OK, 0); + // if (ret != OK) + // err(1, "PWM_SERVO_SET_ARM_OK"); + + // ret = ioctl(fd, PWM_SERVO_ARM, 0); + // if (ret != OK) + // err(1, "PWM_SERVO_ARM"); + + + + + /* Wait for user confirmation */ + warnx("Set high PWM\n" + "Connect battery now and hit ENTER after the ESCs confirm the first calibration step"); + + while (1) { + + /* First set high PWM */ + for (unsigned i = 0; i<MAX_CHANNELS; i++) { + if(channels_selected[i]) { + ret = ioctl(fd, PWM_SERVO_SET(i), 2100); + if (ret != OK) + err(1, "PWM_SERVO_SET(%d)", i); + } + } + + if (read(console, &c, 1) == 1) { + if (c == 13) { + + break; + } else if (c == 0x03 || c == 0x63 || c == 'q') { + warnx("ESC calibration exited"); + close(console); + exit(0); + } + } + /* rate limit to ~ 20 Hz */ + usleep(50000); + } + + /* we don't need any more user input */ + + + warnx("Set low PWM, hit ENTER when finished"); + + while (1) { + + /* Then set low PWM */ + for (unsigned i = 0; i<MAX_CHANNELS; i++) { + if(channels_selected[i]) { + ret = ioctl(fd, PWM_SERVO_SET(i), 900); + if (ret != OK) + err(1, "PWM_SERVO_SET(%d)", i); + } + } + + if (read(console, &c, 1) == 1) { + if (c == 13) { + + break; + } else if (c == 0x03 || c == 0x63 || c == 'q') { + warnx("ESC calibration exited"); + close(console); + exit(0); + } + } + /* rate limit to ~ 20 Hz */ + usleep(50000); + } + + + warnx("ESC calibration finished"); + close(console); + + // XXX disarming not necessaire at the moment + /* Now disarm again */ + // ret = ioctl(fd, PWM_SERVO_DISARM, 0); + + + + exit(0); +}
\ No newline at end of file diff --git a/src/systemcmds/esc_calib/module.mk b/src/systemcmds/esc_calib/module.mk new file mode 100644 index 000000000..990c56768 --- /dev/null +++ b/src/systemcmds/esc_calib/module.mk @@ -0,0 +1,41 @@ +############################################################################ +# +# 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. +# +############################################################################ + +# +# Build the esc_calib tool. +# + +MODULE_COMMAND = esc_calib +SRCS = esc_calib.c + +MODULE_STACKSIZE = 4096 diff --git a/src/systemcmds/pwm/pwm.c b/src/systemcmds/pwm/pwm.c index e150b5a74..c42a36c7f 100644 --- a/src/systemcmds/pwm/pwm.c +++ b/src/systemcmds/pwm/pwm.c @@ -180,7 +180,8 @@ pwm_main(int argc, char *argv[]) } /* iterate remaining arguments */ - unsigned channel = 0; + unsigned nchannels = 0; + unsigned channel[8] = {0}; while (argc--) { const char *arg = argv[0]; argv++; @@ -204,13 +205,15 @@ pwm_main(int argc, char *argv[]) } unsigned pwm_value = strtol(arg, &ep, 0); if (*ep == '\0') { - ret = ioctl(fd, PWM_SERVO_SET(channel), pwm_value); - if (ret != OK) - err(1, "PWM_SERVO_SET(%d)", channel); - channel++; + if (nchannels > sizeof(channel) / sizeof(channel[0])) + err(1, "too many pwm values (max %d)", sizeof(channel) / sizeof(channel[0])); + + channel[nchannels] = pwm_value; + nchannels++; + continue; } - usage("unrecognised option"); + usage("unrecognized option"); } /* print verbose info */ @@ -250,5 +253,38 @@ pwm_main(int argc, char *argv[]) } fflush(stdout); } + + /* perform PWM output */ + if (nchannels) { + + /* Open console directly to grab CTRL-C signal */ + int console = open("/dev/console", O_NONBLOCK | O_RDONLY | O_NOCTTY); + if (!console) + err(1, "failed opening console"); + + warnx("Press CTRL-C or 'c' to abort."); + + while (1) { + for (int i = 0; i < nchannels; i++) { + ret = ioctl(fd, PWM_SERVO_SET(i), channel[i]); + if (ret != OK) + err(1, "PWM_SERVO_SET(%d)", i); + } + + /* abort on user request */ + char c; + if (read(console, &c, 1) == 1) { + if (c == 0x03 || c == 0x63 || c == 'q') { + warnx("User abort\n"); + close(console); + exit(0); + } + } + + /* rate limit to ~ 20 Hz */ + usleep(50000); + } + } + exit(0); }
\ No newline at end of file diff --git a/src/systemcmds/reboot/reboot.c b/src/systemcmds/reboot/reboot.c index 47d3cd948..cc380f94b 100644 --- a/src/systemcmds/reboot/reboot.c +++ b/src/systemcmds/reboot/reboot.c @@ -47,6 +47,9 @@ __EXPORT int reboot_main(int argc, char *argv[]); int reboot_main(int argc, char *argv[]) { + printf("Rebooting now...\n"); + fflush(stdout); + usleep(5000); up_systemreset(); } |