Optics and Precision Engineering, Volume. 17, Issue 2, 362(2009)

Design of xPC semi-physical simulation system for small-satellite attitude control

XU Kai1...2,*, CHEN Chang-qing1, GUAN Wen-cui3 and JIN Guang1 |Show fewer author(s)
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  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    References(4)

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

    [2] [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] [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] [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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    Paper Information

    Category:

    Received: Apr. 28, 2008

    Accepted: --

    Published Online: Oct. 9, 2009

    The Author Email: Kai XU (xukai118@126.com)

    DOI:

    CSTR:32186.14.

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