Simultaneous Spacecraft Attitude Control and Vibration Suppression via Control Allocation

No AccessEngineering NotesSimultaneous Spacecraft Attitude Control and Vibration Suppression via Control AllocationYabo Hu, Yunhai Geng and James D. BiggsYabo HuHarbin Institute of Technology, 150001 Harbin, People’s Republic of China*Ph.D Candidate, Research Center of Satellite Technology; .Search for more papers by this author, Yunhai GengHarbin Institute of Technology, 150001 Harbin, People’s Republic of China†Professor, Research Center of Satellite Technology; (Corresponding Author).Search for more papers by this author and James D. BiggsPolytechnic University of Milan, 20156 Milan, Italy‡Associate Professor, Department of Aerospace Science and Technology; currently Independent Researcher, Hertfordshire, United Kingdom; .Search for more papers by this authorPublished Online:28 Jun 2021https://doi.org/10.2514/1.G005834SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Yermoldina G. 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All rights reserved. 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 ControlBeam (Structures)Computational Fluid DynamicsFinite Element MethodFlexible and Active StructuresFluid DynamicsMechanical and Structural VibrationsSpacecraft Attitude ControlStructural EngineeringStructural SystemStructures, Design and TestTrussesVibration Control KeywordsVibration SuppressionReaction WheelsControl Moment GyroscopeAdaptive Control MethodStiffness MatricesFlexible SpacecraftsFlexible StructuresElastic StructureQuaternionsActive Vibration SuppressionAcknowledgmentThe work reported in this Note is partially supported by the China Scholarship Council.PDF Received3 December 2020Accepted9 May 2021Published online28 June 2021