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Velocity-Free Attitude Reorientation of a Flexible Spacecraft with Attitude Constraints

2017; American Institute of Aeronautics and Astronautics; Volume: 40; Issue: 5 Linguagem: Inglês

10.2514/1.g002129

1533-3884

Qiang Shen, Chengfei Yue, Cher Hiang Goh,

Dynamics and Control of Mechanical Systems

No AccessEngineering NoteVelocity-Free Attitude Reorientation of a Flexible Spacecraft with Attitude ConstraintsQiang Shen, Chengfei Yue and Cher Hiang GohQiang ShenNational University of Singapore, Singapore 119077, Republic of Singapore*Associate Scientist, Temasek Laboratories; (Corresponding Author).Search for more papers by this author, Chengfei YueNational University of Singapore, Singapore 119077, Republic of Singapore†Ph.D. Student, Department of Electrical and Computer Engineering; .Search for more papers by this author and Cher Hiang GohNational University of Singapore, Singapore 119077, Republic of Singapore‡Adjunct Professor, Department of Electrical and Computer Engineering; .Search for more papers by this authorPublished Online:3 Apr 2017https://doi.org/10.2514/1.G002129SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] McInnes C. 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All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAvionicsControl TheoryFeedback ControlGuidance, Navigation, and Control SystemsIntegrated CircuitsOptimal Control TheorySatellitesSemiconductor DevicesSpace Systems and VehiclesSpacecraft DesignSpacecraft InstrumentsSpacecraft SystemSpacecrafts KeywordsFlexible SpacecraftsQuaternionsAttitude ControlBackstepping ControlMotion PlanningSpacecraft MissionsControl AlgorithmEuler AnglesCharge Coupled DeviceInfrared TelescopesPDF Received24 March 2016Accepted5 January 2017Published online3 April 2017