diff --git a/src/modules/navigator/mission_block.cpp b/src/modules/navigator/mission_block.cpp
index bb3caf2628..13ecf30acc 100644
--- a/src/modules/navigator/mission_block.cpp
+++ b/src/modules/navigator/mission_block.cpp
@@ -66,23 +66,23 @@ orb_advert_t actuator_pub_fd;
 
 MissionBlock::MissionBlock(Navigator *navigator, const char *name) :
 	NavigatorMode(navigator, name),
-	_mission_item({0}),
-	_waypoint_position_reached(false),
-	_waypoint_yaw_reached(false),
-	_time_first_inside_orbit(0),
-	_action_start(0),
-	_time_wp_reached(0),
-	_actuators{},
-	_actuator_pub(nullptr),
-	_cmd_pub(nullptr),
-	_param_loiter_min_alt(this, "MIS_LTRMIN_ALT", false),
-	_param_yaw_timeout(this, "MIS_YAW_TMT", false),
-	_param_yaw_err(this, "MIS_YAW_ERR", false),
-	_param_vtol_wv_land(this, "VT_WV_LND_EN", false),
-	_param_vtol_wv_takeoff(this, "VT_WV_TKO_EN", false),
-	_param_vtol_wv_loiter(this, "VT_WV_LTR_EN", false),
-	_param_force_vtol(this, "NAV_FORCE_VT", false),
-	_param_back_trans_dur(this, "VT_B_TRANS_DUR", false)
+	_mission_item( {0}),
+	       _waypoint_position_reached(false),
+	       _waypoint_yaw_reached(false),
+	       _time_first_inside_orbit(0),
+	       _action_start(0),
+	       _time_wp_reached(0),
+	       _actuators{},
+	       _actuator_pub(nullptr),
+	       _cmd_pub(nullptr),
+	       _param_loiter_min_alt(this, "MIS_LTRMIN_ALT", false),
+	       _param_yaw_timeout(this, "MIS_YAW_TMT", false),
+	       _param_yaw_err(this, "MIS_YAW_ERR", false),
+	       _param_vtol_wv_land(this, "VT_WV_LND_EN", false),
+	       _param_vtol_wv_takeoff(this, "VT_WV_TKO_EN", false),
+	       _param_vtol_wv_loiter(this, "VT_WV_LTR_EN", false),
+	       _param_force_vtol(this, "NAV_FORCE_VT", false),
+	       _param_back_trans_dur(this, "VT_B_TRANS_DUR", false)
 {
 }
 
@@ -309,13 +309,13 @@ MissionBlock::is_mission_item_reached()
 			/* for vtol back transition calculate acceptance radius based on time and ground speed */
 			if (_mission_item.vtol_back_transition) {
 
-			    float groundspeed = sqrtf(_navigator->get_global_position()->vel_n * _navigator->get_global_position()->vel_n +
-						      _navigator->get_global_position()->vel_e * _navigator->get_global_position()->vel_e);
+				float groundspeed = sqrtf(_navigator->get_global_position()->vel_n * _navigator->get_global_position()->vel_n +
+							  _navigator->get_global_position()->vel_e * _navigator->get_global_position()->vel_e);
 
-			    if (_param_back_trans_dur.get() > FLT_EPSILON && groundspeed > FLT_EPSILON
+				if (_param_back_trans_dur.get() > FLT_EPSILON && groundspeed > FLT_EPSILON
 				    && groundspeed * _param_back_trans_dur.get() > mission_acceptance_radius) {
-				mission_acceptance_radius = groundspeed * _param_back_trans_dur.get();
-			    }
+					mission_acceptance_radius = groundspeed * _param_back_trans_dur.get();
+				}
 
 			}