항공기 Anti-Braking System을 위한 적응 슬라이딩 모드 제어기 설계

Design Of Adaptive Sliding Mode Control For Aircraft Anti-Braking System

  • 최형섭 (연세대학교 전기전자공학과) ;
  • 이원주 (연세대학교 전기전자공학과) ;
  • 박민용 (연세대학교 전기전자공학과) ;
  • 김은태 (연세대학교 전기전자공학과)
  • Choi, Hyung-Sup (School of Electrical & Electronic Engineering Yonsei University) ;
  • Lee, Won-Ju (School of Electrical & Electronic Engineering Yonsei University) ;
  • Park, Mig-Non (School of Electrical & Electronic Engineering Yonsei University) ;
  • Kim, Eun-Tai (School of Electrical & Electronic Engineering Yonsei University)
  • 발행 : 2008.06.18

초록

This paper proposes the design of anti-braking system on aircraft and wheel slip ratio control using adaptive slide mode control. By maintaining the desired wheel slip ratio under runway conditions, we can obtain the maximal frictional force and reduce the braking range. In this paper, we apply an adaptive sliding mode control to aircraft brake system and it can guarantee the robustness under variations in brake characteristics. The performance of proposed controller is verified in simulations.

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