Dynamic Modeling of Satellite with Deployable Solar Arrays

인공위성 태양전지판 전개 시스템 동적 모델링

  • 허석 (동국대학교 기계공학과 대학원) ;
  • 곽문규 (동국대학교 기계공학과) ;
  • 김홍배 (한국항공우주연구원 우주시험그룹) ;
  • 문상무 (한국항공우주연구원 우주시험그룹) ;
  • 우성현 (한국항공우주연구원 우주시험그룹) ;
  • 이상설 (한국항공우주연구원 우주시험그룹)
  • Published : 2002.11.01

Abstract

This reaserch is concern with dynamic modeling of satellite with deployable solar arrays equipped with strain energy hinges(SEH). It is found from experiments that the SEH has the nonlinear dynamic characteristics and complex buckling behavior which is difficult to explain theoretically. In this paper, we use an equivalent one dimensional nonlinear torsional spring for the SEH. Lagrangian equations of motion are used for the derivations.

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