中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Modeling and analysis of the influence caused by micro-vibration on satellite attitude control system

文献类型:期刊论文

作者L. Li; Y. Yu; L. Wang; L. Yuan; L. Zhang; X. Gong; Y. Wu and R. Zheng
刊名Acta Astronautica
出版日期2023
卷号213页码:71-80
ISSN号00945765
DOI10.1016/j.actaastro.2023.08.047
英文摘要A closed-loop integrated model including micro-vibration disturbance, dynamic characteristics of satellite, optical system of star sensor and attitude control algorithm is established. The control torque error caused by additional disturbance torque and the star sensor imaging error caused by structural resonance is fully integrated analyzed, which are firstly presented into the attitude control system (ACS). Steady-state and transient response analyses are completed to evaluate the impact of such two errors on performances of (ACS). Steady-state response results show that the effect of control torque error appears in lower frequency band with a peak of 6.784E-8″ at 53 Hz, while influence of star sensor imaging error on attitude determination mainly concentrates in high frequency band with maximum response of 0.4101″ at 315 Hz. Transient response results show that the two errors will not significantly affect control indicators such as rise time, overshoot and peak time. The results indicate that the influence of star sensor imaging error is non-negligible for satellite ACS which required milli-arc-second attitude control accuracy. According to the analytical results, traditional analysis only on payload optical axis cannot reveal the whole impact of micro vibration on LOS error, the two errors of micro-vibration introduced to ACS in this work must be considered for the development of spacecraft with 0.1″ pointing accuracy. © 2023
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源URL[http://ir.ciomp.ac.cn/handle/181722/67622]  
专题中国科学院长春光学精密机械与物理研究所
推荐引用方式
GB/T 7714
L. Li,Y. Yu,L. Wang,et al. Modeling and analysis of the influence caused by micro-vibration on satellite attitude control system[J]. Acta Astronautica,2023,213:71-80.
APA L. Li.,Y. Yu.,L. Wang.,L. Yuan.,L. Zhang.,...&Y. Wu and R. Zheng.(2023).Modeling and analysis of the influence caused by micro-vibration on satellite attitude control system.Acta Astronautica,213,71-80.
MLA L. Li,et al."Modeling and analysis of the influence caused by micro-vibration on satellite attitude control system".Acta Astronautica 213(2023):71-80.

入库方式: OAI收割

来源:长春光学精密机械与物理研究所

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