Browse Source

Fix attitude yaw generation, store last acceleration setpoint for all non-velocity / position flight modes.

sbg
Lorenz Meier 9 years ago
parent
commit
bc3f5daeec
  1. 10
      src/modules/mc_pos_control/mc_pos_control_main.cpp

10
src/modules/mc_pos_control/mc_pos_control_main.cpp

@ -1652,9 +1652,10 @@ MulticopterPositionControl::task_main() @@ -1652,9 +1652,10 @@ MulticopterPositionControl::task_main()
_vel_sp_prev = _vel;
}
math::Matrix<3, 3> R_sp;
/* generate attitude setpoint from manual controls */
if (_control_mode.flag_control_manual_enabled && _control_mode.flag_control_attitude_enabled
&& !_control_mode.flag_control_velocity_enabled) {
if (_control_mode.flag_control_manual_enabled && _control_mode.flag_control_attitude_enabled) {
/* reset yaw setpoint to current position if needed */
if (reset_yaw_sp) {
@ -1694,7 +1695,6 @@ MulticopterPositionControl::task_main() @@ -1694,7 +1695,6 @@ MulticopterPositionControl::task_main()
}
/* construct attitude setpoint rotation matrix */
math::Matrix<3, 3> R_sp;
R_sp.from_euler(_att_sp.roll_body, _att_sp.pitch_body, _att_sp.yaw_body);
memcpy(&_att_sp.R_body[0], R_sp.data, sizeof(_att_sp.R_body));
@ -1704,8 +1704,6 @@ MulticopterPositionControl::task_main() @@ -1704,8 +1704,6 @@ MulticopterPositionControl::task_main()
memcpy(&_att_sp.q_d[0], &q_sp.data[0], sizeof(_att_sp.q_d));
_att_sp.timestamp = hrt_absolute_time();
_thrust_sp_prev = R_sp * math::Vector<3>(0, 0, -_att_sp.thrust);
} else {
reset_yaw_sp = true;
}
@ -1723,6 +1721,8 @@ MulticopterPositionControl::task_main() @@ -1723,6 +1721,8 @@ MulticopterPositionControl::task_main()
!(_control_mode.flag_control_position_enabled ||
_control_mode.flag_control_velocity_enabled))) {
_thrust_sp_prev = R_sp * math::Vector<3>(0, 0, -_att_sp.thrust);
if (_att_sp_pub != nullptr) {
orb_publish(_attitude_setpoint_id, _att_sp_pub, &_att_sp);

Loading…
Cancel
Save