[KSCI] Korea Science Citation Index Service

Attitude Control of Helicopter Simulator System Using GA-PID Controller

성상규 ((주)한국항공우주산업)
이준탁 (동아대학교 전기전자컴퓨터공학)
박두환 (동아대학교 대학원 전기공학과)

Publication Information

Journal of Advanced Marine Engineering and Technology / v.28, no.4, 2004 , pp. 675-684 More about this Journal

Abstract

The Helicopter system has a non-linearity and complexity. Futhermore, because of absence of its correct mathematical model. it is difficult to control accurately its attitudes for elevation angle and azimuth one. Therefore, we proposed a GA-PID control technique to control these angles efficiently. The proposed GA-PID controller can systematically generate optimal PID parameters by applying GA theory to a helicopter attitude control system. Through the computer simulation, the GA-PID technique shows better attitude control characteristic than traditional PID control technique.

Keywords

Helicopter Simulator; System Identification; Genetic Algorithm(GA ); GA-PID controller; Attitude control;

Citations & Related Records

Reference

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KSCI

Attitude Control of Helicopter Simulator System Using GA-PID Controller GA-PID 제어기를 이용한 헬리콥터 시스템의 자세 제어

Attitude Control of Helicopter Simulator System Using GA-PID Controller