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dc.contributor.authorGao, X.
dc.contributor.authorTeo, Kok Lay
dc.contributor.authorDuan, G.
dc.date.accessioned2017-01-30T11:29:43Z
dc.date.available2017-01-30T11:29:43Z
dc.date.created2013-11-12T20:00:47Z
dc.date.issued2013
dc.identifier.citationGao, Xiangyu and Teo, Kok Lay and Duan, Guang ren. 2013. An optimal control approach to robust control of nonlinear spacecraft rendezvous system with θ-D technique. International Journal of Innovative Computing, Information and Control. 9 (5): pp. 2099-2110.
dc.identifier.urihttp://hdl.handle.net/20.500.11937/12266
dc.description.abstract

In this paper, a new optimal robust control design approach is proposed for the task of spacecraft rendezvous such that both the stabilization and optimal performance are achieved. An approximate closed-form solution to the nonlinear optimal control problem is obtained by employing the θ-D technique, which is derived based on an approximate solution to the Hamilton-Jacobi-Bellman equation obtained via a perturbation technique. This approach provides a simple design procedure, and the feedback control law obtained is easy for on-board implementation. The effectiveness of the proposed approach is demonstrated through simulation studies.

dc.publisherICIC International
dc.subjectrobust control
dc.subjectuncertainties
dc.subjectspacecraft rendezvous
dc.subjectoptimal control
dc.titleAn optimal control approach to robust control of nonlinear spacecraft rendezvous system with θ-D technique
dc.typeJournal Article
dcterms.source.volume9
dcterms.source.number5
dcterms.source.startPage2099
dcterms.source.endPage2110
dcterms.source.issn1349-4198
dcterms.source.titleInternational Journal of Innovative Computing, Information and Control
curtin.department
curtin.accessStatusFulltext not available


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