vtol attitude control: fixed code style

Signed-off-by: tumbili <roman@px4.io>

src/modules/vtol_att_control/standard.cpp

@@ -188,7 +188,7 @@ void Standard::update_vtol_state()
 		} else if (_vtol_schedule.flight_mode == TRANSITION_TO_FW) {
 			// continue the transition to fw mode while monitoring airspeed for a final switch to fw mode
 			if (((_params_standard.airspeed_mode == control_state_s::AIRSPD_MODE_DISABLED ||
-				_airspeed->indicated_airspeed_m_s >= _params_standard.airspeed_trans) &&
+			      _airspeed->indicated_airspeed_m_s >= _params_standard.airspeed_trans) &&
 			     (float)hrt_elapsed_time(&_vtol_schedule.transition_start)
 			     > (_params_standard.front_trans_time_min * 1000000.0f)) ||
 			    can_transition_on_ground()) {
@@ -250,11 +250,13 @@ void Standard::update_transition_state()
 			_mc_yaw_weight = weight;
 			_mc_throttle_weight = weight;
 
-		// time based blending when no airspeed sensor is set
+			// time based blending when no airspeed sensor is set
+
 		} else if (_params_standard.airspeed_mode == control_state_s::AIRSPD_MODE_DISABLED &&
-				  (float)hrt_elapsed_time(&_vtol_schedule.transition_start) < (_params_standard.front_trans_time_min * 1000000.0f)
-				  ) {
-			float weight = 1.0f - (float)(hrt_elapsed_time(&_vtol_schedule.transition_start) / (_params_standard.front_trans_time_min * 1000000.0f));
+			   (float)hrt_elapsed_time(&_vtol_schedule.transition_start) < (_params_standard.front_trans_time_min * 1000000.0f)
+			  ) {
+			float weight = 1.0f - (float)(hrt_elapsed_time(&_vtol_schedule.transition_start) /
+						      (_params_standard.front_trans_time_min * 1000000.0f));
 			_mc_roll_weight = weight;
 			_mc_pitch_weight = weight;
 			_mc_yaw_weight = weight;