vtol_att_control astyle

Tools/check_code_style_all.sh

@@ -37,6 +37,7 @@ find \
     src/modules/systemlib \
     src/modules/unit_test \
     src/modules/uORB \
+    src/modules/vtol_att_control \
     src/platforms \
     src/systemcmds \
     -type f \( -name "*.c" -o -name "*.h" -o -name "*.cpp" -o -name "*.hpp" \) \

src/modules/vtol_att_control/standard.cpp

@@ -311,7 +311,8 @@ void Standard::update_mc_state()
 	_pusher_throttle = body_x_zero_tilt * thrust_sp_axis * _v_att_sp->thrust * _params_standard.forward_thurst_scale;
 	_pusher_throttle = _pusher_throttle < 0.0f ? 0.0f : _pusher_throttle;
 
-	float pitch_sp_corrected = _v_att_sp->pitch_body < -_params_standard.down_pitch_max ? -_params_standard.down_pitch_max : _v_att_sp->pitch_body;
+	float pitch_sp_corrected = _v_att_sp->pitch_body < -_params_standard.down_pitch_max ? -_params_standard.down_pitch_max :
+				   _v_att_sp->pitch_body;
 
 	// compute new desired rotation matrix with corrected pitch angle
 	// and copy data to attitude setpoint topic

src/modules/vtol_att_control/vtol_att_control_main.cpp

@@ -491,6 +491,7 @@ VtolAttitudeControl::is_fixed_wing_requested()
 	if (_abort_front_transition) {
 		if (to_fw) {
 			to_fw = false;
+
 		} else {
 			// the state changed to mc mode, reset the abort request
 			_abort_front_transition = false;

src/modules/vtol_att_control/vtol_type.cpp

@@ -128,6 +128,7 @@ void VtolType::set_idle_fw()
 	}
 
 	struct pwm_output_values pwm_values;
+
 	memset(&pwm_values, 0, sizeof(pwm_values));
 
 	for (int i = 0; i < _params->vtol_motor_count; i++) {