Parametrical Excitation Model for Rigid–Flexible Coupling System of Solar Power Satellite
2017; American Institute of Aeronautics and Astronautics; Volume: 40; Issue: 10 Linguagem: Inglês
10.2514/1.g002739
ISSN1533-3884
AutoresYuliang Liu, Shunan Wu, Kaiming Zhang, Zhigang Wu,
Tópico(s)Space Satellite Systems and Control
ResumoNo AccessEngineering NoteParametrical Excitation Model for Rigid–Flexible Coupling System of Solar Power SatelliteYuliang Liu, Shunan Wu, Kaiming Zhang and Zhigang WuYuliang LiuDalian University of Technology, 116024 Dalian, People's Republic of China, Shunan WuDalian University of Technology, 116024 Dalian, People's Republic of China, Kaiming ZhangDalian University of Technology, 116024 Dalian, People's Republic of China and Zhigang WuDalian University of Technology, 116024 Dalian, People's Republic of ChinaPublished Online:27 Apr 2017https://doi.org/10.2514/1.G002739SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Glaser P. 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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 ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsPlanetary AtmospheresPlanetary Science and ExplorationPlanetsSatellitesSolar PhysicsSpace AgenciesSpace Science and TechnologySpace SystemsSpace Systems and VehiclesSpacecrafts KeywordsSolar Power SatelliteFinite Element ModelingVibration SuppressionDynamic ResponseAttitude Control SystemControl System DesignJapan Aerospace Exploration AgencyLinear Time InvariantNumerical SimulationFlexible StructuresAcknowledgmentsThis work is supported by the National Natural Science Foundation of China under grant numbers 11502040 and 11432010 and the Fundamental Research Funds for the Central Universities (grant number DUT15LK31).PDF Received8 January 2017Accepted9 February 2017Published online27 April 2017
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