| Title | Optimal Control of Fully-Actuated Systems for Spacecraft Rendezvous |
| Author | |
| DOI | |
| Publication Years | 2022
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| Conference Name | 41st Chinese Control Conference (CCC)
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| ISSN | 1934-1768
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| ISBN | 978-1-6654-8256-1
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| Source Title | |
| Pages | 1690-1695
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| Conference Date | 25-27 July 2022
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| Conference Place | Hefei, China
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| Publication Place | 345 E 47TH ST, NEW YORK, NY 10017 USA
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| Publisher | |
| Abstract | In this paper, the rigid spacecraft rendezvous problem is studied in the sense of fully-actuated system. According to the attitude and orbit dynamics, the fully-actuated system model is established. And the linear quadratic optimal controller of the fully-actuated system is designed for spacecraft rendezvous task. Finally, numerical simulation and physical experiment are considered. Both simulation and experiment results indicate the effectiveness and practicability of the optimal controller. |
| Keywords | |
| SUSTech Authorship | Others
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| Language | English
|
| URL | [Source Record] |
| Indexed By | |
| Funding Project | National Natural Science Foundation of China["62173255","62188101"]
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| WOS Research Area | Automation & Control Systems
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| WOS Subject | Automation & Control Systems
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| WOS Accession No | WOS:000932071601138
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| Data Source | IEEE
|
| PDF url | https://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=9902246 |
| Citation statistics |
Cited Times [WOS]:0
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| Document Type | Conference paper |
| Identifier | http://kc.sustech.edu.cn/handle/2SGJ60CL/406492 |
| Department | Department of Electrical and Electronic Engineering |
| Affiliation | 1.Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin, P. R. China 2.Department of Electronic and Electrical Engineering, Southern University of Science and Technology, Shenzhen, P. R. China |
| Recommended Citation GB/T 7714 |
Guang-Quan Duan,Guo-Ping Liu. Optimal Control of Fully-Actuated Systems for Spacecraft Rendezvous[C]. 345 E 47TH ST, NEW YORK, NY 10017 USA:IEEE,2022:1690-1695.
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| Files in This Item: | There are no files associated with this item. | |||||
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