ekf2: fix code style

src/modules/ekf2/ekf2_main.cpp

@@ -296,6 +296,7 @@ void Ekf2::task_main()
 
 			// fetch sensor data in next loop
 			continue;
+
 		} else if (!(fds[0].revents & POLLIN)) {
 			// no new data
 			continue;
@@ -327,6 +328,7 @@ void Ekf2::task_main()
 		// Use the control model data to determine if the motors are armed as a surrogate for an on-ground vs in-air status
 		// TODO implement a global vehicle on-ground/in-air check
 		orb_check(_control_mode_sub, &control_mode_updated);
+
 		if (control_mode_updated) {
 			orb_copy(ORB_ID(vehicle_control_mode), _control_mode_sub, &vehicle_control_mode);
 			_ekf->set_arm_status(vehicle_control_mode.flag_armed);
@@ -413,8 +415,9 @@ void Ekf2::task_main()
 
 		// Position of local NED origin in GPS / WGS84 frame
 		struct map_projection_reference_s ekf_origin = {};
-                _ekf->get_ekf_origin(&lpos.ref_timestamp,&ekf_origin,&lpos.ref_alt);
-                lpos.xy_global = _ekf->position_is_valid();          // true if position (x, y) is valid and has valid global reference (ref_lat, ref_lon)
+		_ekf->get_ekf_origin(&lpos.ref_timestamp, &ekf_origin, &lpos.ref_alt);
+		lpos.xy_global =
+			_ekf->position_is_valid();          // true if position (x, y) is valid and has valid global reference (ref_lat, ref_lon)
 		lpos.z_global = true;                                // true if z is valid and has valid global reference (ref_alt)
 		lpos.ref_lat = ekf_origin.lat_rad * 180.0 / M_PI; // Reference point latitude in degrees
 		lpos.ref_lon = ekf_origin.lon_rad * 180.0 / M_PI; // Reference point longitude in degrees