| 摘要 |
The technical purpose of the present invention is to solve conventional problems, and to provide a system and a method for alleviating limitation of a center gravity of an aircraft and optimizing aviation characteristics. In order to achieve the above-described objectives, the present invention provides a system for controlling aviation of an aircraft including an aviation control unit for controlling aviation of the aircraft by applying a control law to a manipulation surface of the aircraft, and the system for controlling the control gain according to the change of the center of the gravity for an aircraft further includes a center of gravity calculation unit for receiving information on the weight and location of an object mounted to the aircraft, and calculating the center of the gravity changed during aviation of the aircraft using the information on weight and location; and a control gain scheduler for setting a control gain determined according to the center of the gravity calculated by the center of gravity calculation unit using the preset control gain schedule to the aviation control unit. According to the system and method for adjusting a control gain according to a change in the center of gravity of an aircraft according to the present invention, dynamic stability of the aircraft can be improved, limitation in the center of gravity of the aircraft can be alleviated, and aviation characteristics can be optimized by reflecting the change in the center of gravity during aviation of the aircraft and controlling aviation of the aircraft according to a new control gain. |
