Non-fragile robust H[infinity] control for uncertain spacecraft rendezvous system with pole and input constraints
This article investigates the robust H1 control problem for a class of spacecraft rendezvous systems with parameter uncertainties and subject to input constraint, pole constraint and external and controllerperturbations. Based on the Lyapunov theory, a sufficient condition for the existence of the n...
| Main Authors: | , , |
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| Format: | Journal Article |
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Taylor & Francis
2012
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| Online Access: | http://hdl.handle.net/20.500.11937/49246 |
| _version_ | 1848758197760819200 |
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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 article investigates the robust H1 control problem for a class of spacecraft rendezvous systems with parameter uncertainties and subject to input constraint, pole constraint and external and controllerperturbations. Based on the Lyapunov theory, a sufficient condition for the existence of the non-fragile robust state-feedback controller is given in terms of linear matrix inequalities (LMIs). Then, proper non-fragile controller design can be cast as a convex optimisation problem subject to LMI constraints. With the obtained controller, the spacecraft rendezvous mission can be accomplished. An illustrative example is provided to show the effectiveness of the proposed control design method. |
| first_indexed | 2025-11-14T09:40:10Z |
| format | Journal Article |
| id | curtin-20.500.11937-49246 |
| institution | Curtin University Malaysia |
| institution_category | Local University |
| last_indexed | 2025-11-14T09:40:10Z |
| publishDate | 2012 |
| publisher | Taylor & Francis |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | curtin-20.500.11937-492462017-03-15T22:55:44Z Non-fragile robust H[infinity] control for uncertain spacecraft rendezvous system with pole and input constraints Gao, X. Teo, Kok Lay Duan, G. LMIs spacecraft rendezvous system poles constraint non-fragile H control input constraint This article investigates the robust H1 control problem for a class of spacecraft rendezvous systems with parameter uncertainties and subject to input constraint, pole constraint and external and controllerperturbations. Based on the Lyapunov theory, a sufficient condition for the existence of the non-fragile robust state-feedback controller is given in terms of linear matrix inequalities (LMIs). Then, proper non-fragile controller design can be cast as a convex optimisation problem subject to LMI constraints. With the obtained controller, 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/20.500.11937/49246 Taylor & Francis restricted |
| spellingShingle | LMIs spacecraft rendezvous system poles constraint non-fragile H control input constraint Gao, X. Teo, Kok Lay Duan, G. Non-fragile robust H[infinity] control for uncertain spacecraft rendezvous system with pole and input constraints |
| title | Non-fragile robust H[infinity] control for uncertain spacecraft rendezvous system with pole and input constraints |
| title_full | Non-fragile robust H[infinity] control for uncertain spacecraft rendezvous system with pole and input constraints |
| title_fullStr | Non-fragile robust H[infinity] control for uncertain spacecraft rendezvous system with pole and input constraints |
| title_full_unstemmed | Non-fragile robust H[infinity] control for uncertain spacecraft rendezvous system with pole and input constraints |
| title_short | Non-fragile robust H[infinity] control for uncertain spacecraft rendezvous system with pole and input constraints |
| title_sort | non-fragile robust h[infinity] control for uncertain spacecraft rendezvous system with pole and input constraints |
| topic | LMIs spacecraft rendezvous system poles constraint non-fragile H control input constraint |
| url | http://hdl.handle.net/20.500.11937/49246 |