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DOI:
飞控与探测:2021,(2):66-72
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基于光星模拟器的星敏感器安装极性测试方法
叶立军1,王新萌2,朱 虹3,刘付成4,宝音贺西5
(1.清华大学 航天航空学院 上海航天控制技术研究所 上海市空间智能控制技术重点实验室;2.上海新跃联汇电子科技有限公司;3.上海航天技术研究院;4.上海航天控制技术研究所 上海市空间智能控制技术重点实验室;5.清华大学 航天航空学院)
Polarity Test Method of Star Sensor Installation Based on Optical Star Simulator
YE Lijun1, WANG Xinmeng2, ZHU Hong3, LIU Fucheng4, BAOYIN Hexi5
(1.School of Aerospace Engineering, Tsinghua University Shanghai Aerospace Control Technology Institute Shanghai Key Laboratory of Aerospace Intelligent Control Technology;2.Shanghai Xinyuelianhui Electronic Technology Co.LTD,;3.Shanghai Academy of Spaceflight Technology;4.Shanghai Aerospace Control Technology Institute Shanghai Key Laboratory of Aerospace Intelligent Control Technology;5.School of Aerospace Engineering, Tsinghua University)
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中文摘要: 针对目前星敏感器在整星上的安装极性无法被直接测试的问题,提出了基于光星模拟器的星敏感器安装极性测试方法,从物理和数学两方面阐述了该测试方法的原理,设计了星敏感器安装极性的操作方法和相应的判据。提出了可测性指标的概念,并通过对星敏感器极性和星敏感器安装极性分别进行可测性分析,证明了该方法的有效性。整星电测试结果表明,该方法操作简单,效果直观,可广泛应用。
中文关键词: 星敏感器;极性测试;光星模拟器;安装极性;在回路测试
Abstract:Aiming at the problem that the polarity of star sensor installation cannot be directly tested at present, the polarity test method of star sensor installation based on star simulator is proposed. The principle of this test method is explained from two aspects of physics and mathematics, and the operation and criterion of the test method are designed. The concept of testability is proposed, and the validity of this method is proved by the testability analysis of the star sensor polarity and the star sensor installation polarity. The test results of star sensor in loop on satellite show that the method is easy to operate with the intuitive effect, and can be widely used.
keywords: star sensor; polarity test; optical star simulator; polarity of installation; in loop test
文章编号:20210208     中图分类号:V448    文献标志码:A
基金项目:国家重点研发计划;国家自然科学基金重大项目
作者单位
叶立军 清华大学 航天航空学院 上海航天控制技术研究所 上海市空间智能控制技术重点实验室 
王新萌 上海新跃联汇电子科技有限公司 
朱 虹 上海航天技术研究院 
刘付成 上海航天控制技术研究所 上海市空间智能控制技术重点实验室 
宝音贺西 清华大学 航天航空学院 
Author NameAffiliation
YE Lijun School of Aerospace Engineering, Tsinghua University Shanghai Aerospace Control Technology Institute Shanghai Key Laboratory of Aerospace Intelligent Control Technology 
WANG Xinmeng Shanghai Xinyuelianhui Electronic Technology Co.LTD, 
ZHU Hong Shanghai Academy of Spaceflight Technology 
LIU Fucheng Shanghai Aerospace Control Technology Institute Shanghai Key Laboratory of Aerospace Intelligent Control Technology 
BAOYIN Hexi School of Aerospace Engineering, Tsinghua University 
引用文本:
叶立军,王新萌,朱 虹,刘付成,宝音贺西.基于光星模拟器的星敏感器安装极性测试方法[J].飞控与探测,2021,(2):66-72.

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