Coupled Dynamics and Integrated Control for Position and Attitude Motions of Spacecraft: A Survey
文献类型：期刊论文
| 作者 | Feng Zhang; Guangren Duan |
| 刊名 | IEEE/CAA Journal of Automatica Sinica
 |
| 出版日期 | 2023 |
| 卷号 | 10期号:12页码:2187-2208 |
| 关键词 | Coupled position and attitude dynamic modeling integrated position and attitude control position and attitude coupling analysis spacecraft space missions |
| ISSN号 | 2329-9266 |
| DOI | 10.1109/JAS.2023.123306 |
| 英文摘要 | Inspired by the integrated guidance and control design for endo-atmospheric aircraft, the integrated position and attitude control of spacecraft has attracted increasing attention and gradually induced a wide variety of study results in last over two decades, fully incorporating control requirements and actuator characteristics of space missions. This paper presents a novel and comprehensive survey to the coupled position and attitude motions of spacecraft from the perspective of dynamics and control. To this end, a systematic analysis is firstly conducted in details to show the position and attitude mutual couplings of spacecraft. Particularly, in terms of the time discrepancy between spacecraft position and attitude motions, space missions can be categorized into two types: space proximity operation and space orbital maneuver. Based on this classification, the studies on the coupled dynamic modeling and the integrated control design for position and attitude motions of spacecraft are sequentially summarized and analyzed. On the one hand, various coupled position and dynamic formulations of spacecraft based on various mathematical tools are reviewed and compared from five aspects, including mission applicability, modeling simplicity, physical clearance, information matching and expansibility. On the other hand, the development of the integrated position and attitude control of spacecraft is analyzed for two space missions, and especially, five distinctive development trends are captured for space operation missions. Finally, insightful prospects on future development of the integrated position and attitude control technology of spacecraft are proposed, pointing out current primary technical issues and possible feasible solutions. |
| 源URL | [http://ir.ia.ac.cn/handle/173211/52464]  |
| 专题 | 自动化研究所_学术期刊_IEEE/CAA Journal of Automatica Sinica |
| 推荐引用方式 GB/T 7714 | Feng Zhang,Guangren Duan. Coupled Dynamics and Integrated Control for Position and Attitude Motions of Spacecraft: A Survey[J]. IEEE/CAA Journal of Automatica Sinica,2023,10(12):2187-2208. |
| APA | Feng Zhang,&Guangren Duan.(2023).Coupled Dynamics and Integrated Control for Position and Attitude Motions of Spacecraft: A Survey.IEEE/CAA Journal of Automatica Sinica,10(12),2187-2208. |
| MLA | Feng Zhang,et al."Coupled Dynamics and Integrated Control for Position and Attitude Motions of Spacecraft: A Survey".IEEE/CAA Journal of Automatica Sinica 10.12(2023):2187-2208. |
入库方式： OAI收割
来源：自动化研究所
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