관성모멘트 분포특성을 이용한 피치 바이어스 모멘텀 위성의 자세제어기 특성 해석Analysis on the Attitude Controller for Pitch Bias Momentum Satellite Using Moment of Inertia Distribution

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dc.contributor.author방효충ko
dc.contributor.author김정아ko
dc.contributor.author황보한ko
dc.date.accessioned2013-02-27T22:10:51Z-
dc.date.available2013-02-27T22:10:51Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued1998-04-
dc.identifier.citation한국항공우주학회지, v.26, no.8, pp.74 - 82-
dc.identifier.issn1225-1348-
dc.identifier.urihttp://hdl.handle.net/10203/71128-
dc.languageKorean-
dc.publisher한국항공우주학회-
dc.title관성모멘트 분포특성을 이용한 피치 바이어스 모멘텀 위성의 자세제어기 특성 해석-
dc.title.alternativeAnalysis on the Attitude Controller for Pitch Bias Momentum Satellite Using Moment of Inertia Distribution-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume26-
dc.citation.issue8-
dc.citation.beginningpage74-
dc.citation.endingpage82-
dc.citation.publicationname한국항공우주학회지-
dc.contributor.localauthor방효충-
dc.contributor.nonIdAuthor김정아-
dc.contributor.nonIdAuthor황보한-
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AE-Journal Papers(저널논문)
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