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MC pos control: Comment style fixes
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@@ -1380,16 +1380,16 @@ MulticopterPositionControl::task_main()
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reset_int_xy = true;
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}
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// generate attitude setpoint from manual controls
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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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/* 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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/* 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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@@ -1405,19 +1405,19 @@ MulticopterPositionControl::task_main()
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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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/* 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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}
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//Control climb rate directly if no aiding altitude controller is active
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/* control throttle directly if no climb rate controller is active */
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if (!_control_mode.flag_control_climb_rate_enabled) {
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_att_sp.thrust = math::min(_manual.z, _params.thr_max);
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_att_sp.thrust = math::max(_att_sp.thrust, _params.thr_min);
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}
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//Construct attitude setpoint rotation matrix
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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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