Chinese Journal of Lasers, Volume. 51, Issue 13, 1304007(2024)

Design and Experimental Verification of Thermal Stability for Micro Star Sensors

Yanqing Wang*, Weifeng Du, Yongkang Wu, Zhengyi Zhai, Zhongjia Zhu, and Zhaohui Cao
Author Affiliations
  • Shanghai Institute of Spaceflight Control Technology, Shanghai 201109, China
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    References(12)

    [1] Li J[M]. Research and implementation of star sensor system(2008).

    [2] Li X P, Ren P C, Gao Y et al. Distributed FOV fusion algorithm for multiple heads star tracker[J]. Flight Control & Detection, 1, 71-76(2018).

    [4] Lian D, Zhou Q, Yu L W et al. Modeling and compensation of star spot in high dynamic condition[J]. Flight Control & Detection, 3, 86-94(2020).

    [5] Wang Y Q, Wu Y K, Shen J et al. Application design and verification test of domestic components in star sensor[J]. Missiles and Space Vehicles, 59-65(2023).

    [9] Wu Y K, Hu X C, Mao X N et al. Thermal design and simulation analysis of high precision star sensor[J]. Aerospace Shanghai, 35, 123-129(2018).

    [10] Sui J, Cheng H Y, Yu C W et al. A thermal stability analysis and simulation method for boresight axis of star sensor[J]. Aerospace Control and Application, 43, 37-41(2017).

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    Yanqing Wang, Weifeng Du, Yongkang Wu, Zhengyi Zhai, Zhongjia Zhu, Zhaohui Cao. Design and Experimental Verification of Thermal Stability for Micro Star Sensors[J]. Chinese Journal of Lasers, 2024, 51(13): 1304007

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    Paper Information

    Category: Measurement and metrology

    Received: Aug. 25, 2023

    Accepted: Nov. 6, 2023

    Published Online: Jul. 2, 2024

    The Author Email: Yanqing Wang (wangyanqing803@aliyun.com)

    DOI:10.3788/CJL231140

    CSTR:32183.14.CJL231140

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