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mc pos ctrl: do not publish att sp in offboard && no position/velocity control

sbg
Thomas Gubler 10 years ago
parent
commit
0dec33526b
  1. 25
      src/modules/mc_pos_control/mc_pos_control_main.cpp

25
src/modules/mc_pos_control/mc_pos_control_main.cpp

@ -761,8 +761,8 @@ void MulticopterPositionControl::control_auto(float dt) @@ -761,8 +761,8 @@ void MulticopterPositionControl::control_auto(float dt)
orb_copy(ORB_ID(position_setpoint_triplet), _pos_sp_triplet_sub, &_pos_sp_triplet);
//Make sure that the position setpoint is valid
if (!isfinite(_pos_sp_triplet.current.lat) ||
!isfinite(_pos_sp_triplet.current.lon) ||
if (!isfinite(_pos_sp_triplet.current.lat) ||
!isfinite(_pos_sp_triplet.current.lon) ||
!isfinite(_pos_sp_triplet.current.alt)) {
_pos_sp_triplet.current.valid = false;
}
@ -1367,7 +1367,7 @@ MulticopterPositionControl::task_main() @@ -1367,7 +1367,7 @@ MulticopterPositionControl::task_main()
} else if (yaw_offs > YAW_OFFSET_MAX) {
_att_sp.yaw_body = _wrap_pi(_att.yaw + YAW_OFFSET_MAX);
}
}
}
//Control roll and pitch directly if we no aiding velocity controller is active
@ -1388,15 +1388,22 @@ MulticopterPositionControl::task_main() @@ -1388,15 +1388,22 @@ MulticopterPositionControl::task_main()
_att_sp.timestamp = hrt_absolute_time();
}
else {
reset_yaw_sp = true;
reset_yaw_sp = true;
}
// publish attitude setpoint
if (_att_sp_pub > 0) {
orb_publish(ORB_ID(vehicle_attitude_setpoint), _att_sp_pub, &_att_sp);
/* publish attitude setpoint
* Do not publish if offboard is enabled but position/velocity control is disabled,
* in this case the attitude setpoint is published by the mavlink app
*/
if (!(_control_mode.flag_control_offboard_enabled &&
!(_control_mode.flag_control_position_enabled ||
_control_mode.flag_control_velocity_enabled))) {
if (_att_sp_pub > 0) {
orb_publish(ORB_ID(vehicle_attitude_setpoint), _att_sp_pub, &_att_sp);
} else {
_att_sp_pub = orb_advertise(ORB_ID(vehicle_attitude_setpoint), &_att_sp);
} else {
_att_sp_pub = orb_advertise(ORB_ID(vehicle_attitude_setpoint), &_att_sp);
}
}
/* reset altitude controller integral (hovering throttle) to manual throttle after manual throttle control */

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