Sliding Mode Attitude Control for Momentum-Biased Spacecraft

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dc.contributor.authorBang, Hyochoongko
dc.contributor.authorLoh, Young-Hwanko
dc.date.accessioned2017-12-19T03:12:27Z-
dc.date.available2017-12-19T03:12:27Z-
dc.date.created2017-01-12-
dc.date.created2017-01-12-
dc.date.created2017-01-12-
dc.date.issued2002-11-
dc.identifier.citationINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES , v.3, no.2, pp.13 - 23-
dc.identifier.issn1229-9626-
dc.identifier.urihttp://hdl.handle.net/10203/228701-
dc.languageEnglish-
dc.publisher한국항공우주학회-
dc.titleSliding Mode Attitude Control for Momentum-Biased Spacecraft-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume3-
dc.citation.issue2-
dc.citation.beginningpage13-
dc.citation.endingpage23-
dc.citation.publicationnameINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES-
dc.contributor.localauthorBang, Hyochoong-
dc.contributor.nonIdAuthorLoh, Young-Hwan-
dc.description.isOpenAccessN-
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AE-Journal Papers(저널논문)
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