Journal of Aerospace System Engineering (항공우주시스템공학회지)

The Society for Aerospace System Engineering (항공우주시스템공학회)
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Drop Test Simulation of semi-active Landing Gear using Commercial Magneto-Rheological Damper

상용 MR 댐퍼를 이용한 반능동형 착륙장치 낙하실험

  • 황재업 (한국대학교 항공우주공학과) ;
  • 황재혁 (한국대학교 항공우주공학부) ;
  • 배재성 (한국대학교 항공우주공학부) ;
  • 임경호 (한국대학교 항공우주공학부)
  • Published : 2010.12.31
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Abstract

This paper is used the commercial magneto-rheological(MR) damper for landing gear. The damping characteristics of Commercial MR damper by changing the intensity of the magnetic field are investigated and the dynamic responses of the landing gear. it is set up tset equipment, the landing gear drop test system. The landing gear involved drop testing the gear. The landing gear is tested by implementing sky-hook control algorithm and its performance is evaluated comparing to the result.

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