퍼지 동조 PID 제어기를 이용한 모형 헬리콥터의 개선된 3자유도 자세제어

Improved 3-DOF Attitude Control of a Model Helicopter using Fuzzy-Tuning PID Controller

  • 박문수 (아주대학교 전자공학과) ;
  • 박덕기 (아주대학교 전자공학과) ;
  • 정원재 (아주대학교 전자공학과) ;
  • 김병두 (아주대학교 전자공학과) ;
  • 홍석교 (아주대학교 전자공학부)
  • 발행 : 2001.07.18

초록

This paper describes the application of a fuzzy-tuning PID controller to a 3-DOF attitude control of a small model helicopter in hover for the compensation of coupling effects between each axis and system uncertainties due to the variation of engine RPM. A Low-level PID controller is designed by Ziegler-Nichols method and its gains are tuned by a high-level fuzzy system based on error states and its time derivatives. The experimental results show that the attitude control performance of fuzzy-tuning PID controller is improved comparing with that of a Ziegler-Nichols PID controller and fuzzy controller.

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