An Experimental Study on Attitude Control of Spacecraft using Two-axis Rotational Simulator with a Flexible Arm

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dc.contributor.authorOh, Choongsuk-
dc.contributor.authorMyung, Hyunsam-
dc.contributor.authorBang, Hyochoong-
dc.contributor.authorTahk, Min-Jea-
dc.date.accessioned2010-02-09T01:52:43Z-
dc.date.available2010-02-09T01:52:43Z-
dc.date.created2012-02-06-
dc.date.issued2002-09-25-
dc.identifier.citation4th Asian Control Conference, v., no., pp.2051 - 2056-
dc.identifier.urihttp://hdl.handle.net/10203/16526-
dc.description.sponsorshipKorea Research Foundation Granten
dc.languageENG-
dc.language.isoen_USen
dc.publisherASCC-
dc.titleAn Experimental Study on Attitude Control of Spacecraft using Two-axis Rotational Simulator with a Flexible Arm-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.beginningpage2051-
dc.citation.endingpage2056-
dc.citation.publicationname4th Asian Control Conference-
dc.identifier.conferencecountrySingapore-
dc.identifier.conferencecountrySingapore-
dc.contributor.localauthorBang, Hyochoong-
dc.contributor.localauthorTahk, Min-Jea-
dc.contributor.nonIdAuthorOh, Choongsuk-
dc.contributor.nonIdAuthorMyung, Hyunsam-

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