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VTOL standard - Remove pitch trim
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@@ -498,7 +498,7 @@ void Standard::fill_actuator_outputs()
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// pitch
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_actuators_out_1->control[actuator_controls_s::INDEX_PITCH] =
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_actuators_fw_in->control[actuator_controls_s::INDEX_PITCH] + _params->fw_pitch_trim;
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_actuators_fw_in->control[actuator_controls_s::INDEX_PITCH];
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// yaw
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_actuators_out_1->control[actuator_controls_s::INDEX_YAW] =
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_actuators_fw_in->control[actuator_controls_s::INDEX_YAW];
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@@ -510,7 +510,7 @@ void Standard::fill_actuator_outputs()
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if (_params->elevons_mc_lock) {
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// zero outputs when inactive
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_actuators_out_1->control[actuator_controls_s::INDEX_ROLL] = 0.0f;
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_actuators_out_1->control[actuator_controls_s::INDEX_PITCH] = _params->fw_pitch_trim;
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_actuators_out_1->control[actuator_controls_s::INDEX_PITCH] = 0.0f;
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_actuators_out_1->control[actuator_controls_s::INDEX_YAW] = 0.0f;
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_actuators_out_1->control[actuator_controls_s::INDEX_AIRBRAKES] = 0.0f;
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@@ -521,7 +521,7 @@ void Standard::fill_actuator_outputs()
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// pitch
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_actuators_out_1->control[actuator_controls_s::INDEX_PITCH] =
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_actuators_fw_in->control[actuator_controls_s::INDEX_PITCH] + _params->fw_pitch_trim;
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_actuators_fw_in->control[actuator_controls_s::INDEX_PITCH];
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_actuators_out_1->control[actuator_controls_s::INDEX_YAW] = 0.0f;
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_actuators_out_1->control[actuator_controls_s::INDEX_AIRBRAKES] = 0.0f;
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