GA-PID 제어기를 이용한 헬리콥터 시스템의 자세 제어

Attitude Control of Helicopter Simulator System Using GA-PID Controller

  • 성상규 ((주)한국항공우주산업) ;
  • 이준탁 (동아대학교 전기전자컴퓨터공학) ;
  • 박두환 (동아대학교 대학원 전기공학과)
  • 발행 : 2004.05.01

초록

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.

키워드

참고문헌

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