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@ -73,8 +73,7 @@
@@ -73,8 +73,7 @@
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#include <uORB/topics/position_setpoint_triplet.h> |
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#include <uORB/topics/vehicle_global_velocity_setpoint.h> |
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#include <uORB/topics/vehicle_local_position_setpoint.h> |
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// #include <systemlib/param/param.h>
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// #include <systemlib/err.h>
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#include <systemlib/systemlib.h> |
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#include <mathlib/mathlib.h> |
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#include <lib/geo/geo.h> |
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@ -746,8 +745,7 @@ MulticopterPositionControl::cross_sphere_line(const math::Vector<3>& sphere_c, f
@@ -746,8 +745,7 @@ MulticopterPositionControl::cross_sphere_line(const math::Vector<3>& sphere_c, f
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} |
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} |
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void |
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MulticopterPositionControl::control_auto(float dt) |
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void MulticopterPositionControl::control_auto(float dt) |
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{ |
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if (!_mode_auto) { |
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_mode_auto = true; |
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@ -924,7 +922,7 @@ MulticopterPositionControl::task_main()
@@ -924,7 +922,7 @@ MulticopterPositionControl::task_main()
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bool reset_int_z = true; |
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bool reset_int_z_manual = false; |
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bool reset_int_xy = true; |
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bool reset_yaw_sp = false; |
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bool reset_yaw_sp = true; |
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bool was_armed = false; |
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hrt_abstime t_prev = 0; |
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@ -968,15 +966,12 @@ MulticopterPositionControl::task_main()
@@ -968,15 +966,12 @@ MulticopterPositionControl::task_main()
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_reset_alt_sp = true; |
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reset_int_z = true; |
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reset_int_xy = true; |
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reset_yaw_sp = true; |
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} |
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//Update previous arming state
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was_armed = _control_mode.flag_armed; |
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/* check if should reset yaw setpoint for manual attitude control */ |
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if(!_arming.armed || !_control_mode.flag_control_manual_enabled || (!_control_mode.flag_control_altitude_enabled && _control_mode.flag_control_manual_enabled)) { |
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reset_yaw_sp = true; |
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} |
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update_ref(); |
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if (_control_mode.flag_control_altitude_enabled || |
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@ -1137,7 +1132,7 @@ MulticopterPositionControl::task_main()
@@ -1137,7 +1132,7 @@ MulticopterPositionControl::task_main()
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/* adjust limits for landing mode */ |
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if (!_control_mode.flag_control_manual_enabled && _pos_sp_triplet.current.valid && |
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_pos_sp_triplet.current.type == position_setpoint_s::SETPOINT_TYPE_LAND) { |
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_pos_sp_triplet.current.type == position_setpoint_s::SETPOINT_TYPE_LAND) { |
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/* limit max tilt and min lift when landing */ |
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tilt_max = _params.tilt_max_land; |
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@ -1350,40 +1345,53 @@ MulticopterPositionControl::task_main()
@@ -1350,40 +1345,53 @@ MulticopterPositionControl::task_main()
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reset_int_xy = true; |
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} |
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if(!_control_mode.flag_control_velocity_enabled) { |
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/* generate attitude setpoint from manual controls */ |
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if(_control_mode.flag_control_manual_enabled) { |
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/* move yaw setpoint */ |
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float yaw_sp_move_rate = _manual.r * _params.man_yaw_max; |
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_att_sp.yaw_body = _wrap_pi(_att_sp.yaw_body + yaw_sp_move_rate * dt); |
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float yaw_offs_max = _params.man_yaw_max / _params.mc_att_yaw_p; |
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// generate attitude setpoint from manual controls
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if(_control_mode.flag_control_manual_enabled && _control_mode.flag_control_attitude_enabled) { |
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// reset yaw setpoint to current position if needed
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if (reset_yaw_sp) { |
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reset_yaw_sp = false; |
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_att_sp.yaw_body = _att.yaw; |
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} |
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// do not move yaw while arming
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else if (_manual.z > 0.1f) |
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{ |
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const float YAW_OFFSET_MAX = _params.man_yaw_max / _params.mc_att_yaw_p; |
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_att_sp.yaw_sp_move_rate = _manual.r * _params.man_yaw_max; |
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_att_sp.yaw_body = _wrap_pi(_att_sp.yaw_body + _att_sp.yaw_sp_move_rate * dt); |
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float yaw_offs = _wrap_pi(_att_sp.yaw_body - _att.yaw); |
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if (yaw_offs < - yaw_offs_max) { |
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_att_sp.yaw_body = _wrap_pi(_att.yaw - yaw_offs_max); |
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if (yaw_offs < - YAW_OFFSET_MAX) { |
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_att_sp.yaw_body = _wrap_pi(_att.yaw - YAW_OFFSET_MAX); |
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} else if (yaw_offs > yaw_offs_max) { |
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_att_sp.yaw_body = _wrap_pi(_att.yaw + yaw_offs_max); |
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} |
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} else if (yaw_offs > YAW_OFFSET_MAX) { |
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_att_sp.yaw_body = _wrap_pi(_att.yaw + YAW_OFFSET_MAX); |
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}
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} |
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//Control roll and pitch directly if we no aiding velocity controller is active
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if(!_control_mode.flag_control_velocity_enabled) { |
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_att_sp.roll_body = _manual.y * _params.man_roll_max; |
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_att_sp.pitch_body = -_manual.x * _params.man_pitch_max; |
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_att_sp.yaw_sp_move_rate = yaw_sp_move_rate; |
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_att_sp.thrust = _control_mode.flag_control_altitude_enabled ? _att_sp.thrust : _manual.z; |
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} |
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/* reset yaw setpoint to current position if needed */ |
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if (reset_yaw_sp) { |
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reset_yaw_sp = false; |
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_att_sp.yaw_body = _att.yaw; |
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//Control climb rate directly if no aiding altitude controller is active
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if(!_control_mode.flag_control_climb_rate_enabled) { |
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_att_sp.thrust = _manual.z; |
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} |
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//Construct attitude setpoint rotation matrix
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math::Matrix<3,3> R_sp; |
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R_sp.from_euler(_att_sp.roll_body,_att_sp.pitch_body,_att_sp.yaw_body); |
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memcpy(&_att_sp.R_body[0], R_sp.data, sizeof(_att_sp.R_body)); |
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_att_sp.timestamp = hrt_absolute_time(); |
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} |
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/* publish attitude setpoint */ |
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else { |
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reset_yaw_sp = true;
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} |
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// publish attitude setpoint
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if (_att_sp_pub > 0) { |
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orb_publish(ORB_ID(vehicle_attitude_setpoint), _att_sp_pub, &_att_sp); |
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