Structural Dynamic Analysis of the Low Earth Orbit Satellite

저궤도 인공위성의 구조 동해석

  • 김경원 (한국항공우주연구원 위성기술사업단 위성구조팀) ;
  • 이주훈 (한국항공우주연구원 위성기술사업단 위성구조팀) ;
  • 황도순 (한국항공우주연구원 위성기술사업단 위성구조팀)
  • Published : 2008.09.30

Abstract

Keywords

References

  1. T. P. Sarafin (1995), "Spacecraft Structures and Mechanisms", Space Technology Library
  2. R. R. Craig and M. C Bampton (1968), "Coupling of Substructures for Dynamic Analysis" AIAA Journal, Vol. 6, No.8, pp.1313-1319 https://doi.org/10.2514/3.4741
  3. W. A Benfield and R. F. Hruda (1971), "Vibration Analysis of Structures by Component Model Substitution", AlAA Journal, Vol. 9, No.7, pp.1255-1261
  4. D. S. Hwang (1998), "CLA Model and Assessment of Satellite", Journal of the Korean Society of Aeronautical and Space Sciences, Vol. 26, No.7, pp.108-115
  5. K. W. Kim (2003), "Notching Analysis for Sinusoidal Vibration Test of Satellite", The Proceeding of the Korean Society of Aeronautical and Space Sciences, pp.76-79
  6. MSC/Nastran Quick Reference Guide (2005), MSC Software
  7. S. H. Kim (2001), "Deployment Analysis of a Satellite Solar Array", LMS User's Conference, pp.257-267
  8. Recurdyn Basic Tutorials (2006), FunctionBay, Inc
  9. K. W. Kim (2008), "Solar Array Deployment Analysis of a Satellite", The journal of the Korea Society of Space Technology, Vol. 3, No.3, pp.29-34