Journal of Aerospace System Engineering (항공우주시스템공학회지)

The Society for Aerospace System Engineering (항공우주시스템공학회)
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Dynamic Characteristics Analysis of Landing Gear that Consider 6-Degree of Freedom of Helicopter

6자유도를 고려한 회전익 항공기 착륙장치의 동특성 해석

  • 박완수 (한국항공대학교 기계공학과 대학원) ;
  • 황재업 (한국항공대학교 기계공학과 대학원) ;
  • 현영오 (한국항공대학교 기계공학과 대학원) ;
  • 황재혁 (한국항공대학교) ;
  • 배재성 (한국항공대학교) ;
  • 김태욱 (한국항공우주연구원)
  • Published : 2008.03.31
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Abstract

In this paper, full body modeling and analysis of nose and main landing gear's characteristics of a helicopter are performed using the dynamics analysis program ADAMS. Also, when land limiting about helicopter body's degree-of-freedom, compared the characteristics. In the case of helicopter, because there are a lot of dangerous missions under flight condition that is disadvantageous than fixed wing airplane, need more detailed research for a helicopter.

Keywords