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dc.contributor.authorGao, Xiangyu
dc.contributor.authorTeo, Kok Lay
dc.contributor.authorDuan, Guang-Ren
dc.date.accessioned2017-01-30T14:33:14Z
dc.date.available2017-01-30T14:33:14Z
dc.date.created2014-03-16T20:01:16Z
dc.date.issued2014
dc.identifier.citationGao, Xiangyu and Teo, Kok Lay and Duan, Guang-Ren. 2014. An optimal control approach to spacecraft rendezvous on elliptical orbit. Optimal Control Applications and Methods. 36 (2): pp. 158-178.
dc.identifier.urihttp://hdl.handle.net/20.500.11937/39357
dc.identifier.doi10.1002/oca.2108
dc.description.abstract

In this paper, we consider a linear quadratic regulator control problem for spacecraft rendezvous in an elliptical orbit. A new spacecraft rendezvous model is established. On the basis of this model, a linear quadratic regulator control problem is formulated. A parametric Lyapunov differential equation approach is used to design a state feedback controller such that the resulting closed-loop system is asymptotically stable, and the performance index is minimized. By an appropriate choice of the value of a parameter, an approximate state feedback controller is obtained from a solution to the periodic Lyapunov differential equation,where the periodic Lyapunov differential equation is solved on the basis of a new numerical algorithm. The spacecraft rendezvous mission under the controller obtained will be accomplished successfully. Several illustrative examples are provided to show the effectiveness of the proposed control design method.

dc.publisherJohn Wiley and Sons, Ltd.
dc.subjectLQR
dc.subjectPLDE
dc.subjectspacecraft rendezvous
dc.subjectnumerical algorithm
dc.titleAn optimal control approach to spacecraft rendezvous on elliptical orbit
dc.typeJournal Article
dcterms.source.volume-
dcterms.source.startPage1
dcterms.source.endPage21
dcterms.source.issn0143-2087
dcterms.source.titleOptimal Control Applications and Methods
curtin.department
curtin.accessStatusFulltext not available


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