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@ -1192,7 +1192,8 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi
@@ -1192,7 +1192,8 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi
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} |
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/* Copy thrust and pitch values from tecs
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* making sure again that the correct thrust is used, without depending on library calls */ |
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* making sure again that the correct thrust is used, |
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* without depending on library calls */ |
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if (pos_sp_triplet.current.type == SETPOINT_TYPE_TAKEOFF && |
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launch_detection_state != LAUNCHDETECTION_RES_DETECTED_ENABLEMOTORS) { |
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_att_sp.thrust = launchDetector.getThrottlePreTakeoff(); |
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@ -1200,7 +1201,12 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi
@@ -1200,7 +1201,12 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi
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else { |
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_att_sp.thrust = math::min(_mTecs.getEnabled() ? _mTecs.getThrottleSetpoint() : _tecs.get_throttle_demand(), throttle_max); |
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} |
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_att_sp.pitch_body = _mTecs.getEnabled() ? _mTecs.getPitchSetpoint() : _tecs.get_pitch_demand(); |
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/* During a takeoff waypoint while waiting for launch the pitch sp is set
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* already (not by tecs) */ |
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if (!(pos_sp_triplet.current.type == SETPOINT_TYPE_TAKEOFF && |
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launch_detection_state == LAUNCHDETECTION_RES_NONE)) { |
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_att_sp.pitch_body = _mTecs.getEnabled() ? _mTecs.getPitchSetpoint() : _tecs.get_pitch_demand(); |
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} |
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if (_control_mode.flag_control_position_enabled) { |
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last_manual = false; |
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