diff --git a/UAV-ControlSystem/src/drivers/accel_gyro.c b/UAV-ControlSystem/src/drivers/accel_gyro.c
index f0b87cc..00be629 100644
--- a/UAV-ControlSystem/src/drivers/accel_gyro.c
+++ b/UAV-ControlSystem/src/drivers/accel_gyro.c
@@ -588,8 +588,10 @@ void mpu6000_read_angle(accel_t* accel, gyro_t* gyro)
 		float a_PitchAngle	 = atan2( accelConv[1], sqrt(accelConv[2]*accelConv[2] + accelConv[0]*accelConv[0]))*180/M_PI;
 
 		//Check how much the accelerometer angle differs from the current calculated ange with the gyro. Add calculated factor to the real angle value
+
 		accel->rollAngle 	 += (a_RollAngle - accel->rollAngle) / GYRO_ACC_DIV_FACTOR;
 		accel->pitchAngle	 += (a_PitchAngle - accel->pitchAngle) / GYRO_ACC_DIV_FACTOR;
+
 	}
 
 }