제어로봇시스템학회:학술대회논문집

Institute of Control, Robotics and Systems (제어로봇시스템학회)
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Structural analysis of satellite bus

위성체본체의 구조해석

  • 이장무 (서울대학교 기계설계학과) ;
  • 김승조 (서울대학교 항공공학과) ;
  • 김기욱 (서울대학교 기계설계학과) ;
  • 유정열 (서울대학교 항공공학과)
  • Published : 1989.10.01
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Abstract

Structural analysis of a satellite bus is carried out by using a finite element program NISA II. It is assumed that the bus is composed of bars, plates and shells made of CFRP composite materials and aluminum alloys. Displacements and stresses are calculated as static analysis under accelerated motion and frequencies and mode shapes are computed as dynamic analysis.

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