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Coupled Dynamics and Integrated Control for Position and Attitude Motions of Spacecraft:A Survey

Feng Zhang Guangren Duan

自动化学报（英文版）2023，Vol.10Issue(12)：2187-2208,22.

自动化学报（英文版）2023，Vol.10Issue(12)：2187-2208,22.DOI:10.1109/JAS.2023.123306

Coupled Dynamics and Integrated Control for Position and Attitude Motions of Spacecraft:A Survey

Feng Zhang ¹Guangren Duan²

作者信息

1. Research and Development Center,China Academy of Launch Vehicle Technology,Beijing 100076,China
2. Center for Control Science and Technology,Southern University of Science and Technology,Shenzhen 518055||Center for Control Theory and Guidance Technology,Harbin Institute of Technology,Harbin 150001,China
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摘要

关键词

Coupled position and attitude dynamic modeling/integrated position and attitude control/position and attitude cou-pling analysis/spacecraft/space missions

Key words

Coupled position and attitude dynamic modeling/integrated position and attitude control/position and attitude cou-pling analysis/spacecraft/space missions

引用本文复制引用

Feng Zhang,Guangren Duan..Coupled Dynamics and Integrated Control for Position and Attitude Motions of Spacecraft:A Survey[J].自动化学报（英文版）,2023,10(12):2187-2208,22.

基金项目

This work was supported by the National Science Foundation of China(61703437,52232014,61690210,61690212).Recommended by Associate Editor Qinglai Wei. （61703437,52232014,61690210,61690212）

自动化学报（英文版）

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