Robust H[infinity] control of spacecraft rendezvous on elliptical orbit
This paper investigates the robust H∞H∞ control problem of spacecraft rendezvous on elliptical orbit. Based on Lyapunov theory, a sufficient condition for the existence of the robust H∞H∞ controller is given in terms of the periodic Riccati differential equation (RDE). Then, a stabilizable controlle...
| Main Authors: | , , |
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| Format: | Journal Article |
| Published: |
Elsevier Science
2012
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| Online Access: | http://hdl.handle.net/20.500.11937/37346 |
| _version_ | 1848755021531840512 |
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| author | Gao, X. Teo, Kok Lay Duan, G. |
| author_facet | Gao, X. Teo, Kok Lay Duan, G. |
| author_sort | Gao, X. |
| building | Curtin Institutional Repository |
| collection | Online Access |
| description | This paper investigates the robust H∞H∞ control problem of spacecraft rendezvous on elliptical orbit. Based on Lyapunov theory, a sufficient condition for the existence of the robust H∞H∞ controller is given in terms of the periodic Riccati differential equation (RDE). Then, a stabilizable controller design method based on a fast multi-shot algorithm is proposed. With the controller obtained, the spacecraft rendezvous mission can be accomplished. An illustrative example is provided to show the effectiveness of the proposed control design method. |
| first_indexed | 2025-11-14T08:49:41Z |
| format | Journal Article |
| id | curtin-20.500.11937-37346 |
| institution | Curtin University Malaysia |
| institution_category | Local University |
| last_indexed | 2025-11-14T08:49:41Z |
| publishDate | 2012 |
| publisher | Elsevier Science |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | curtin-20.500.11937-373462017-09-13T13:38:14Z Robust H[infinity] control of spacecraft rendezvous on elliptical orbit Gao, X. Teo, Kok Lay Duan, G. This paper investigates the robust H∞H∞ control problem of spacecraft rendezvous on elliptical orbit. Based on Lyapunov theory, a sufficient condition for the existence of the robust H∞H∞ controller is given in terms of the periodic Riccati differential equation (RDE). Then, a stabilizable controller design method based on a fast multi-shot algorithm is proposed. With the controller obtained, the spacecraft rendezvous mission can be accomplished. An illustrative example is provided to show the effectiveness of the proposed control design method. 2012 Journal Article http://hdl.handle.net/20.500.11937/37346 10.1016/j.jfranklin.2012.08.005 Elsevier Science restricted |
| spellingShingle | Gao, X. Teo, Kok Lay Duan, G. Robust H[infinity] control of spacecraft rendezvous on elliptical orbit |
| title | Robust H[infinity] control of spacecraft rendezvous on elliptical orbit |
| title_full | Robust H[infinity] control of spacecraft rendezvous on elliptical orbit |
| title_fullStr | Robust H[infinity] control of spacecraft rendezvous on elliptical orbit |
| title_full_unstemmed | Robust H[infinity] control of spacecraft rendezvous on elliptical orbit |
| title_short | Robust H[infinity] control of spacecraft rendezvous on elliptical orbit |
| title_sort | robust h[infinity] control of spacecraft rendezvous on elliptical orbit |
| url | http://hdl.handle.net/20.500.11937/37346 |