On the Approximate Solution of Aircraft Landing Gear under Nonstationary Random Excitations

비정상 랜덤 가진력을 받는 항공기 착륙장치의 응답해석 기법연구

  • 황재혁 (한국항공대학교, 항공기계공학과) ;
  • 유병성 (한국항공대학교 대학원) ;
  • 공병식 (한국항공대학교 대학원)
  • Published : 1997.10.01

Abstract

The motion of an aircraft landing gear over rough runway at variable speed is nonstationary. hi this paper, a method for the computation of nonstationary response variance is presented which uses a state space form for the combination of landing gear and runway excitation. The dynamic characteristics of the landing gear under nonstationazy random excitations has also been analyzed using the proposed method. The formulation is for linear systems of arbitrary order and allows any deterministic velocity history.

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