PreflightCheck trivial astyle fix

src/modules/commander/PreflightCheck.cpp

@@ -576,10 +576,12 @@ static bool ekf2Check(orb_advert_t *mavlink_log_pub, vehicle_status_s &vehicle_s
 
 	// check accelerometer delta velocity bias estimates
 	param_get(param_find("COM_ARM_EKF_AB"), &test_limit);
-	for (uint8_t index=13; index<16; index++) {
+
+	for (uint8_t index = 13; index < 16; index++) {
 		// allow for higher uncertainty in estimates for axes that are less observable to prevent false positives
 		// adjust test threshold by 3-sigma
-		float test_uncertainty = 3.0f * sqrtf(fmaxf(status.covariances[index],0.0f));
+		float test_uncertainty = 3.0f * sqrtf(fmaxf(status.covariances[index], 0.0f));
+
 		if (fabsf(status.states[index]) > test_limit + test_uncertainty) {
 			if (report_fail) {
 				mavlink_log_critical(mavlink_log_pub, "Preflight Fail: High Accelerometer Bias");