A method for design and verification of autonomous flight controller of a flight vehicle by utilizing magnetic forces

The present invention in designing the automatic flight control apparatus for controlling, more specifically, the vehicle automatic flight relates to a method for design and verification of the performance of the vehicle automatic flight control devices, such as aircraft or missiles, the magnetic force replacing the flight test in a wind tunnel test utilization and at the same time, one, one vehicle automatic flight control utilizing magnetic force by a wind tunnel tests take advantage of this magnetic force, designing an aircraft automatic flight control system more effective and to verify its performance It relates to the design and verification method of the device. According to the present invention, the design and performance verification of an automatic flight control system, instead of the air vehicle flight test, since this is performed by utilizing the magnetic force wind tunnel test, it is possible to ensure the safety of the vehicle. This may be in the safety state of the vehicle is guaranteed, grasp the flight dynamic properties of various types of vehicle, or design a vehicle automatic flight control system and to verify its performance.