diff options
Diffstat (limited to 'src/modules/multirotor_att_control')
-rw-r--r-- | src/modules/multirotor_att_control/multirotor_att_control_main.c | 98 |
1 files changed, 41 insertions, 57 deletions
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 b3669d9ff..04582f2a4 100644 --- a/src/modules/multirotor_att_control/multirotor_att_control_main.c +++ b/src/modules/multirotor_att_control/multirotor_att_control_main.c @@ -2,6 +2,7 @@ * * Copyright (C) 2012 PX4 Development Team. All rights reserved. * Author: Lorenz Meier <lm@inf.ethz.ch> + * Anton Babushkin <anton.babushkin@me.com> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -38,6 +39,7 @@ * Implementation of multirotor attitude control main loop. * * @author Lorenz Meier <lm@inf.ethz.ch> + * @author Anton Babushkin <anton.babushkin@me.com> */ #include <nuttx/config.h> @@ -63,6 +65,7 @@ #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_status.h> #include <uORB/topics/sensor_combined.h> #include <uORB/topics/actuator_controls.h> #include <uORB/topics/parameter_update.h> @@ -74,8 +77,6 @@ #include "multirotor_attitude_control.h" #include "multirotor_rate_control.h" -PARAM_DEFINE_FLOAT(MC_RCLOSS_THR, 0.0f); // This defines the throttle when the RC signal is lost. - __EXPORT int multirotor_att_control_main(int argc, char *argv[]); static bool thread_should_exit; @@ -102,7 +103,8 @@ mc_thread_main(int argc, char *argv[]) memset(&offboard_sp, 0, sizeof(offboard_sp)); struct vehicle_rates_setpoint_s rates_sp; memset(&rates_sp, 0, sizeof(rates_sp)); - + struct vehicle_status_s status; + memset(&status, 0, sizeof(status)); struct actuator_controls_s actuators; memset(&actuators, 0, sizeof(actuators)); @@ -114,6 +116,8 @@ mc_thread_main(int argc, char *argv[]) int control_mode_sub = orb_subscribe(ORB_ID(vehicle_control_mode)); int manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); int sensor_sub = orb_subscribe(ORB_ID(sensor_combined)); + int rates_sp_sub = orb_subscribe(ORB_ID(vehicle_rates_setpoint)); + int status_sub = orb_subscribe(ORB_ID(vehicle_status)); /* * Do not rate-limit the loop to prevent aliasing @@ -136,7 +140,6 @@ mc_thread_main(int argc, char *argv[]) orb_advert_t 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); orb_advert_t rates_sp_pub = orb_advertise(ORB_ID(vehicle_rates_setpoint), &rates_sp); - int rates_sp_sub = orb_subscribe(ORB_ID(vehicle_rates_setpoint)); /* register the perf counter */ perf_counter_t mc_loop_perf = perf_alloc(PC_ELAPSED, "multirotor_att_control_runtime"); @@ -149,12 +152,6 @@ mc_thread_main(int argc, char *argv[]) /* store last control mode to detect mode switches */ bool control_yaw_position = true; bool reset_yaw_sp = true; - bool failsafe_first_time = true; - - /* prepare the handle for the failsafe throttle */ - param_t failsafe_throttle_handle = param_find("MC_RCLOSS_THR"); - float failsafe_throttle = 0.0f; - param_get(failsafe_throttle_handle, &failsafe_throttle); while (!thread_should_exit) { @@ -176,7 +173,6 @@ mc_thread_main(int argc, char *argv[]) orb_copy(ORB_ID(parameter_update), param_sub, &update); /* update parameters */ - param_get(failsafe_throttle_handle, &failsafe_throttle); } /* only run controller if attitude changed */ @@ -205,6 +201,13 @@ mc_thread_main(int argc, char *argv[]) orb_copy(ORB_ID(offboard_control_setpoint), setpoint_sub, &offboard_sp); } + /* get a local copy of status */ + orb_check(status_sub, &updated); + + if (updated) { + orb_copy(ORB_ID(vehicle_status), status_sub, &status); + } + /* get a local copy of the current sensor values */ orb_copy(ORB_ID(sensor_combined), sensor_sub, &raw); @@ -244,47 +247,18 @@ mc_thread_main(int argc, char *argv[]) /* manual input */ if (control_mode.flag_control_attitude_enabled) { /* control attitude, update attitude setpoint depending on mode */ - /* if the RC signal is lost, try to stay level and go slowly back down to ground */ - if (control_mode.failsave_highlevel) { - failsafe_first_time = false; - - if (!control_mode.flag_control_velocity_enabled) { - /* don't reset attitude setpoint in position control mode, it's handled by position controller. */ - att_sp.roll_body = 0.0f; - att_sp.pitch_body = 0.0f; - } - - if (!control_mode.flag_control_climb_rate_enabled) { - /* don't touch throttle in modes with altitude hold, it's handled by position controller. - * - * 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 > min_takeoff_throttle) { // TODO use landed status instead of throttle - /* the failsafe throttle is stored as a parameter, as it depends on the copter and the payload */ - att_sp.thrust = failsafe_throttle; - - } else { - att_sp.thrust = 0.0f; - } - } + if (att_sp.thrust < 0.1f) { + /* no thrust, don't try to control yaw */ + rates_sp.yaw = 0.0f; + control_yaw_position = false; - /* 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 (failsafe_first_time) { + if (status.condition_landed) { + /* reset yaw setpoint if on ground */ reset_yaw_sp = true; } } else { - failsafe_first_time = true; - - /* only move yaw setpoint if manual input is != 0 and not landed */ + /* only move yaw setpoint if manual input is != 0 */ if (manual.yaw < -yaw_deadzone || yaw_deadzone < manual.yaw) { /* control yaw rate */ control_yaw_position = false; @@ -294,18 +268,17 @@ mc_thread_main(int argc, char *argv[]) } else { control_yaw_position = true; } + } - if (!control_mode.flag_control_velocity_enabled) { - /* update attitude setpoint if not in position control mode */ - att_sp.roll_body = manual.roll; - att_sp.pitch_body = manual.pitch; + if (!control_mode.flag_control_velocity_enabled) { + /* update attitude setpoint if not in position control mode */ + att_sp.roll_body = manual.roll; + att_sp.pitch_body = manual.pitch; - if (!control_mode.flag_control_climb_rate_enabled) { - /* pass throttle directly if not in altitude control mode */ - att_sp.thrust = manual.throttle; - } + if (!control_mode.flag_control_climb_rate_enabled) { + /* pass throttle directly if not in altitude control mode */ + att_sp.thrust = manual.throttle; } - } /* reset yaw setpint to current position if needed */ @@ -324,7 +297,7 @@ mc_thread_main(int argc, char *argv[]) att_sp.timestamp = hrt_absolute_time(); - /* publish the controller output */ + /* publish the attitude setpoint */ orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp); } else { @@ -342,6 +315,17 @@ mc_thread_main(int argc, char *argv[]) } } else { + if (!control_mode.flag_control_auto_enabled) { + /* no control, try to stay on place */ + if (!control_mode.flag_control_velocity_enabled) { + /* no velocity control, reset attitude setpoint */ + att_sp.roll_body = 0.0f; + att_sp.pitch_body = 0.0f; + att_sp.timestamp = hrt_absolute_time(); + orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp); + } + } + /* reset yaw setpoint after non-manual control */ reset_yaw_sp = true; } |