Temperature-stabilized star sensor thermal design method
作者： Yu Chengwu , Sun Jianbo , Du Wei , Wu Yanpeng , Dai Shuying
DOI:
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摘要: The invention relates to a temperature-stabilized star sensor thermal design method and particularly with the temperature highly stable, which belongs tothe technical field of spacecraft attitude control. According high stability body is realized, in both sunshine area shadow area, range 19 DEG C 21 C. Temperature decoupling between baffle assembly anda structure difference about 30 front section rear at least 15 also effects on are greatly reduced.
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