dc.contributor.author | Wan, Neng | |
dc.contributor.author | Liu, Ming | |
dc.contributor.author | Karimi, Hamid Reza | |
dc.date.accessioned | 2014-12-18T11:34:48Z | |
dc.date.available | 2014-12-18T11:34:48Z | |
dc.date.issued | 2014 | |
dc.identifier.citation | Wan, 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: 10.1155/2014/710850 | nb_NO |
dc.identifier.issn | 1687-0409 | |
dc.identifier.uri | http://hdl.handle.net/11250/227783 | |
dc.description | Published 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 Access | nb_NO |
dc.description.abstract | This 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.iso | eng | nb_NO |
dc.publisher | Hindawi Publishing Corporation | nb_NO |
dc.title | Observer-based robust control for spacecraft rendezvous with thrust saturation | nb_NO |
dc.type | Journal article | nb_NO |
dc.type | Peer reviewed | nb_NO |
dc.subject.nsi | VDP::Mathematics and natural science: 400::Mathematics: 410::Analysis: 411 | nb_NO |
dc.source.pagenumber | 1-10 | nb_NO |
dc.source.journal | Abstract and Applied Analysis | nb_NO |
dc.identifier.doi | 10.1155/2014/710850 | |