OPTICS & OPTOELECTRONIC TECHNOLOGY, Volume. 18, Issue 2, 87(2020)

Star Map Simulation of Star Tracker Based on Inertial Platform

LI De-biao*
Author Affiliations
  • [in Chinese]
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    References(10)

    [1] [1] HE Ju. Survey of overseas celestial navigation technology development[J]. Ship Science and Technology, 2005, 27(5): 91-96.

    [2] [2] ZHANG Jin-liang. Key techniques for inertial stellar integrated navigation system[D]. Xi′an: Northwestern Polytechnical University, 2015.

    [3] [3] ZHAO Ming-bo, LIU Yu, TAO Zheng-yu. One method on star image simulation of airborne astronomical navigation [J]. Optoeletronic Technology, 2008, 28(3): 184-192.

    [4] [4] ZHANG Qian-cheng. Inertial /multiple celestial integrated navigation for nearspace vehicle[D]. Xi′an: Northwestern Polytechnical University, 2015.

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    [6] [6] XIE Lun-zhi. Horizontal attitude and heading determination based on star sensor[J]. Optics and Optoelectronic Technology, 2012, 10(3): 172-175.

    [7] [7] YUE Ya-zhou, Tian Yu, ZHANG Xiao-dong. Investigation on airborne inertial / celestial integrated navigation[J]. Optics and Optoelectronic Technology, 2008, 6(4): 90-92.

    [8] [8] YUAN Hong-wei. Inertial /celestial integrated navigation technology and application on airborne[J]. Optics and Optoelectronic Technology, 2012, 10(3): 194-198.

    [9] [9] WANG An-guo. Modern celestial navigation and the key techniques[J]. Chinese J. of Electronics, 2007, 35(12): 2347-2353.

    [10] [10] FANG Jian-cheng. Celestial navigation principle and aplication[M]. Beijing: Beihang University Press, 2006.

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    LI De-biao. Star Map Simulation of Star Tracker Based on Inertial Platform[J]. OPTICS & OPTOELECTRONIC TECHNOLOGY, 2020, 18(2): 87

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    Paper Information

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    Received: Jul. 22, 2019

    Accepted: --

    Published Online: Jun. 18, 2020

    The Author Email: De-biao LI (lidbcn@sina.com)

    DOI:

    CSTR:32186.14.

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