Vibration control of flexible spacecraft under attitude maneuver using adaptive controller

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dc.contributor.authorOh, C.-
dc.contributor.authorBang, Hyochoong-
dc.contributor.authorPark, J.-O.-
dc.date.accessioned2010-02-09T07:07:44Z-
dc.date.available2010-02-09T07:07:44Z-
dc.date.created2012-02-06-
dc.date.issued2006-08-21-
dc.identifier.citationAIAA Guidance, Navigation, and Control Conference 2006, v., no., pp.957 - 976-
dc.identifier.urihttp://hdl.handle.net/10203/16552-
dc.description.sponsorshipNational Research Lab.(NRL) Program(M1-0203-00-0006) by the Ministry of Science Technology, Korea.en
dc.languageENG-
dc.language.isoen_USen
dc.publisherAmerican Institute of Aeronautics and Astronautics-
dc.titleVibration control of flexible spacecraft under attitude maneuver using adaptive controller-
dc.typeConference-
dc.identifier.scopusid2-s2.0-33845725662-
dc.type.rimsCONF-
dc.citation.beginningpage957-
dc.citation.endingpage976-
dc.citation.publicationnameAIAA Guidance, Navigation, and Control Conference 2006-
dc.identifier.conferencecountryUnited States-
dc.identifier.conferencecountryUnited States-
dc.contributor.localauthorBang, Hyochoong-
dc.contributor.nonIdAuthorOh, C.-
dc.contributor.nonIdAuthorPark, J.-O.-

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