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author | Anton Babushkin <anton.babushkin@me.com> | 2013-08-22 17:31:59 +0200 |
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committer | Anton Babushkin <anton.babushkin@me.com> | 2013-08-22 17:31:59 +0200 |
commit | b5bb20995be8c0f55bed4f2f2bd6cee9efdcf03e (patch) | |
tree | ae8bbae1c7039916af6f9f6da1245bbf2e16fb87 /src/modules/multirotor_att_control | |
parent | db950f74893a108302a167729a91765269981e7b (diff) | |
download | px4-firmware-b5bb20995be8c0f55bed4f2f2bd6cee9efdcf03e.tar.gz px4-firmware-b5bb20995be8c0f55bed4f2f2bd6cee9efdcf03e.tar.bz2 px4-firmware-b5bb20995be8c0f55bed4f2f2bd6cee9efdcf03e.zip |
multirotor_att_control: yaw setpoint reset fix
Diffstat (limited to 'src/modules/multirotor_att_control')
-rw-r--r-- | src/modules/multirotor_att_control/multirotor_att_control_main.c | 103 |
1 files changed, 53 insertions, 50 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 c057ef364..2d46bf438 100644 --- a/src/modules/multirotor_att_control/multirotor_att_control_main.c +++ b/src/modules/multirotor_att_control/multirotor_att_control_main.c @@ -81,6 +81,8 @@ __EXPORT int multirotor_att_control_main(int argc, char *argv[]); static bool thread_should_exit; static int mc_task; static bool motor_test_mode = false; +static const float min_takeoff_throttle = 0.3f; +static const float yaw_deadzone = 0.01f; static int mc_thread_main(int argc, char *argv[]) @@ -147,14 +149,14 @@ 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 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 +178,7 @@ mc_thread_main(int argc, char *argv[]) orb_copy(ORB_ID(parameter_update), param_sub, &update); /* update parameters */ - // XXX no params here yet + param_get(failsafe_throttle_handle, &failsafe_throttle); } /* only run controller if attitude changed */ @@ -208,6 +210,9 @@ 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); + /* set flag to safe value */ + control_yaw_position = true; + /* define which input is the dominating control input */ if (control_mode.flag_control_offboard_enabled) { /* offboard inputs */ @@ -225,47 +230,40 @@ mc_thread_main(int argc, char *argv[]) att_sp.yaw_body = offboard_sp.p3; att_sp.thrust = offboard_sp.p4; att_sp.timestamp = hrt_absolute_time(); - /* STEP 2: publish the result to the vehicle actuators */ + /* publish the result to the vehicle actuators */ orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp); } } else if (control_mode.flag_control_manual_enabled) { - /* direct manual input */ + /* manual input */ if (control_mode.flag_control_attitude_enabled) { /* control attitude, update attitude setpoint depending on mode */ - /* initialize to current yaw if switching to manual or att control */ - if (control_mode.flag_control_attitude_enabled != flag_control_attitude_enabled || - control_mode.flag_control_manual_enabled != flag_control_manual_enabled) { - 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 (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. */ + /* 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 > 0.2f) { // TODO use landed status instead of throttle - /* 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.thrust = failsafe_throttle; - - } else { - att_sp.thrust = 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; } } @@ -273,46 +271,48 @@ mc_thread_main(int argc, char *argv[]) * 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 = false; + if (failsafe_first_time) { + reset_yaw_sp = true; + } } else { - rc_loss_first_time = true; + failsafe_first_time = true; /* control yaw in all manual / assisted modes */ /* set yaw if arming or switching to attitude stabilized mode */ - if (!flag_control_attitude_enabled) { + if (!flag_control_manual_enabled || !flag_control_attitude_enabled || !control_mode.flag_armed) { reset_yaw_sp = true; } /* only move setpoint if manual input is != 0 */ - if ((manual.yaw < -0.01f || 0.01f < manual.yaw) && manual.throttle > 0.3f) { // TODO use landed status instead of throttle - rates_sp.yaw = manual.yaw; + // TODO review yaw restpoint reset + if ((manual.yaw < -yaw_deadzone || yaw_deadzone < manual.yaw) && manual.throttle > min_takeoff_throttle) { + /* control yaw rate */ control_yaw_position = false; - reset_yaw_sp = true; + rates_sp.yaw = manual.yaw; + reset_yaw_sp = true; // has no effect on control, just for beautiful log } else { - if (reset_yaw_sp) { - att_sp.yaw_body = att.yaw; - reset_yaw_sp = false; - } control_yaw_position = true; } if (!control_mode.flag_control_velocity_enabled) { - /* don't update attitude setpoint in position control mode */ + /* 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) { - /* don't set throttle in altitude hold modes */ + /* pass throttle directly if not in altitude control mode */ att_sp.thrust = manual.throttle; } } - att_sp.timestamp = hrt_absolute_time(); + } + + /* reset yaw setpint to current position if needed */ + if (reset_yaw_sp) { + att_sp.yaw_body = att.yaw; + reset_yaw_sp = false; } if (motor_test_mode) { @@ -321,10 +321,11 @@ mc_thread_main(int argc, char *argv[]) att_sp.pitch_body = 0.0f; att_sp.yaw_body = 0.0f; att_sp.thrust = 0.1f; - att_sp.timestamp = hrt_absolute_time(); } - /* STEP 2: publish the controller output */ + att_sp.timestamp = hrt_absolute_time(); + + /* publish the controller output */ orb_publish(ORB_ID(vehicle_attitude_setpoint), att_sp_pub, &att_sp); } else { @@ -367,6 +368,7 @@ mc_thread_main(int argc, char *argv[]) rates[1] = att.pitchspeed; rates[2] = att.yawspeed; multirotor_control_rates(&rates_sp, rates, &actuators, reset_integral); + } else { /* rates controller disabled, set actuators to zero for safety */ actuators.control[0] = 0.0f; @@ -374,6 +376,7 @@ mc_thread_main(int argc, char *argv[]) actuators.control[2] = 0.0f; actuators.control[3] = 0.0f; } + actuators.timestamp = hrt_absolute_time(); orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators); |