Predefined-Time Hybrid Tracking Control of Flexible Satellites with Conditional Anti-Unwinding

No AccessEngineering NotesPredefined-Time Hybrid Tracking Control of Flexible Satellites with Conditional Anti-UnwindingGargi Das and Manoranjan SinhaGargi DasIndian Institute of Technology Kharagpur, West Bengal 721 302, India and Manoranjan SinhaIndian Institute of Technology Kharagpur, West Bengal 721 302, IndiaPublished Online:23 Aug 2024https://doi.org/10.2514/1.G008286SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About References [1] Bhat S. P. and Bernstein D. S., "A Topological Obstruction to Continuous Global Stabilization of Rotational Motion and the Unwinding Phenomenon," Systems & Control Letters, Vol. 39, No. 1, 2000, pp. 63–70. https://doi.org/10.1016/S0167-6911(99)00090-0 CrossrefGoogle Scholar[2] Schaub H. and Junkins J. L., "Stereographic Orientation Parameters for Attitude Dynamics: A Generalization of the Rodrigues Parameters," Journal of the Astronautical Sciences, Vol. 44, No. 1, 1996, pp. 1–19. 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All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerospace SciencesAstrodynamicsAstronauticsAttitude ControlControl TheoryEnergyEnergy ConsumptionEnergy EconomicsGuidance, Navigation, and Control SystemsOrbital ManeuversSatellite GuidanceSatellitesSpace OrbitSpace Systems and VehiclesSpacecraft Guidance and ControlSpacecrafts KeywordsSatellite BusTerminal Sliding ModeAttitude Control SystemEnergy ConsumptionPassive Vibration ControlSatellite Attitude ControlLarge Angle ManeuverAnti-unwindingpredefined-time controlDigital Received20 February 2024Accepted5 July 2024Published online23 August 2024