Robust H[infinity] control of spacecraft rendezvous on elliptical orbit
dc.contributor.author | Gao, X. | |
dc.contributor.author | Teo, Kok Lay | |
dc.contributor.author | Duan, G. | |
dc.date.accessioned | 2017-01-30T14:02:06Z | |
dc.date.available | 2017-01-30T14:02:06Z | |
dc.date.created | 2015-03-03T20:17:29Z | |
dc.date.issued | 2012 | |
dc.identifier.citation | Gao, X. and Teo, K.L. and Duan, G. 2012. Robust H[infinity] control of spacecraft rendezvous on elliptical orbit. Journal of the Franklin Institute. 349 (8): pp. 2515-2529. | |
dc.identifier.uri | http://hdl.handle.net/20.500.11937/37346 | |
dc.identifier.doi | 10.1016/j.jfranklin.2012.08.005 | |
dc.description.abstract |
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. | |
dc.publisher | Elsevier Science | |
dc.title | Robust H[infinity] control of spacecraft rendezvous on elliptical orbit | |
dc.type | Journal Article | |
dcterms.source.volume | 349 | |
dcterms.source.startPage | 2515 | |
dcterms.source.endPage | 2529 | |
dcterms.source.issn | 00160032 | |
dcterms.source.title | Journal of the Franklin Institute | |
curtin.department | Department of Mathematics and Statistics | |
curtin.accessStatus | Fulltext not available |