• Optics and Precision Engineering
  • Vol. 17, Issue 2, 362 (2009)
XU Kai1,2,*, CHEN Chang-qing1, GUAN Wen-cui3, and JIN Guang1
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    DOI: Cite this Article
    XU Kai, CHEN Chang-qing, GUAN Wen-cui, JIN Guang. Design of xPC semi-physical simulation system for small-satellite attitude control[J]. Optics and Precision Engineering, 2009, 17(2): 362 Copy Citation Text show less
    References

    [1] LIU L D. Satellite Control System Simulation Technic[M].Beijing:Space Navigation Press,2003.(in Chinese)

    [2] ZHANG SH J,CAO X B,WANG F. Design of semi-physical system for micro-satellite attitude control[J].Chinese Space Science and Technology,2005,12(6):43-50.(in Chinese)

    [3] YANG D,LI L T. The Development Environment and Application of the Real -Time Simulation System [M].Beijing:Tsinghua University Press,2002.(in Chinese)

    [4] SCHWARTZ J L,PECK M P,HALL C D.Historical review of spacecraft simulators[J].American Astronautical Society,2003,AAS Paper 03-125,(1-48)

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    XU Kai, CHEN Chang-qing, GUAN Wen-cui, JIN Guang. Design of xPC semi-physical simulation system for small-satellite attitude control[J]. Optics and Precision Engineering, 2009, 17(2): 362
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