Chinese Journal of Lasers, Volume. 44, Issue 6, 604003(2017)

Orbit-Dynamics Model of Spacecrafts and Error Analysis of Ahead-Point

Ye Xiaowei1,2,3、* and Shen Feng1,2
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    Ye Xiaowei, Shen Feng. Orbit-Dynamics Model of Spacecrafts and Error Analysis of Ahead-Point[J]. Chinese Journal of Lasers, 2017, 44(6): 604003

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    Paper Information

    Category: measurement and metrology

    Received: Dec. 27, 2017

    Accepted: --

    Published Online: Jun. 8, 2017

    The Author Email: Xiaowei Ye (13882208919@163.com)

    DOI:10.3788/cjl201744.0604003

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