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dc.contributor.authorWan, Neng
dc.contributor.authorLiu, Ming
dc.contributor.authorKarimi, Hamid Reza
dc.date.accessioned2014-12-18T11:34:48Z
dc.date.available2014-12-18T11:34:48Z
dc.date.issued2014
dc.identifier.citationWan, N., Liu, M., & Karimi, H. R. (2014). Observer-based robust control for spacecraft rendezvous with thrust saturation. Abstract and Applied Analysis, 2014, 1-10. doi: 10.1155/2014/710850nb_NO
dc.identifier.issn1687-0409
dc.identifier.urihttp://hdl.handle.net/11250/227783
dc.descriptionPublished version of an article in the journal: Abstract and Applied Analysis. Also available from the publisher at: http://dx.doi.org/10.1155/2014/710850 Open Accessnb_NO
dc.description.abstractThis paper proposes an observer-based robust guaranteed cost control method for thrust-limited rendezvous in near-circular orbits. Treating the noncircularity of the target orbit as a parametric uncertainty, a linearized motion model derived from the two-body problem is adopted as the controlled plant. Based on this model, a robust guaranteed cost observer-controller is synthesized with a less conservative saturation control law, and sufficient condition for the existence of this observer-based rendezvous controller is derived. Finally, an illustrative example with immeasurable velocity states is presented to demonstrate the advantages and effectiveness of the control scheme.nb_NO
dc.language.isoengnb_NO
dc.publisherHindawi Publishing Corporationnb_NO
dc.titleObserver-based robust control for spacecraft rendezvous with thrust saturationnb_NO
dc.typeJournal articlenb_NO
dc.typePeer reviewednb_NO
dc.subject.nsiVDP::Mathematics and natural science: 400::Mathematics: 410::Analysis: 411nb_NO
dc.source.pagenumber1-10nb_NO
dc.source.journalAbstract and Applied Analysisnb_NO
dc.identifier.doi10.1155/2014/710850


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