Chinese Journal of Lasers, Volume. 47, Issue 4, 404002(2020)

Method for Experimental Analysis of Thermostability of Star Sensors

Jin He*, Zhai Zhengyi, Du Weifeng, Wu Yongkang, and Gao Yuan
Author Affiliations
  • Shanghai key Laboratory of Aerospace Intelligent Control Technology, Shanghai Institute of Spaceflight Control Technology, Shanghai 201109, China
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    Figures & Tables(10)
    Typical structure of star sensor
    Design of thermostability experiment
    Details in vacuum tank
    Thermal control with multilayer cladding
    Auto-collimation outside vacuum tank
    Error analysis. (a) x axis or y axis error; (b) z axis error
    Distribution of temperature measurement point
    Changes of measuring coordinate system caused by baffle heating. (a) Thermal deformation removing frock part; (b) temperature of each measurement point
    Change of measuring coordinate system caused by mounting support heating. (a) Thermal deformation removing frock part; (b) temperature of each measurement point
    Optical axis drift with mounting surface temperature ranging from 17 ℃ to 23 ℃
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    Jin He, Zhai Zhengyi, Du Weifeng, Wu Yongkang, Gao Yuan. Method for Experimental Analysis of Thermostability of Star Sensors[J]. Chinese Journal of Lasers, 2020, 47(4): 404002

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    Paper Information

    Category: Measurement and metrology

    Received: Aug. 1, 2019

    Accepted: --

    Published Online: Apr. 8, 2020

    The Author Email: He Jin (13621946541@163.com)

    DOI:10.3788/CJL202047.0404002

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