OUTPUT FEEDBACK SLEWING CONTROL OF FLEXIBLE SPACECRAFT BY LYAPUNOV STABILITY THEORY

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dc.contributor.author김대식ko
dc.contributor.author김천휘ko
dc.contributor.author방효충ko
dc.date.accessioned2013-02-27T15:06:59Z-
dc.date.available2013-02-27T15:06:59Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued1997-12-
dc.identifier.citationJOURNAL OF ASTRONOMY AND SPACE SCIENCES, v.14, no.2, pp.367 - 374-
dc.identifier.issn1598-5601-
dc.identifier.urihttp://hdl.handle.net/10203/69246-
dc.languageKorean-
dc.publisher한국우주과학회-
dc.titleOUTPUT FEEDBACK SLEWING CONTROL OF FLEXIBLE SPACECRAFT BY LYAPUNOV STABILITY THEORY-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume14-
dc.citation.issue2-
dc.citation.beginningpage367-
dc.citation.endingpage374-
dc.citation.publicationnameJOURNAL OF ASTRONOMY AND SPACE SCIENCES-
dc.contributor.localauthor방효충-
dc.contributor.nonIdAuthor김대식-
dc.contributor.nonIdAuthor김천휘-
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AE-Journal Papers(저널논문)
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