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College of Engineering(공과대학)School of Mechanical and Aerospace Engineering(기계항공공학부)Dept. of Aerospace Engineering(항공우주공학과)AE-Journal Papers(저널논문)

Satellite attitude stabilization using solar radiation pressure and magnetotorquer

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dc.contributor.authorKumar, K. D.ko
dc.contributor.authorTahk, Min-Jeako
dc.contributor.authorBang, Hyochoongko
dc.date.accessioned2009-11-10T06:20:22Z-
dc.date.available2009-11-10T06:20:22Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued2009-02-
dc.identifier.citationCONTROL ENGINEERING PRACTICE, v.17, no.2, pp.267 - 279-
dc.identifier.issn0967-0661-
dc.identifier.urihttp://hdl.handle.net/10203/12353-
dc.description.abstractThe paper presents three-dimensional (3-D) attitude stabilization of a geosynchronous satellite. The solar radiation pressure is considered for the satellite pitch and roll stabilization while the yaw attitude is stabilized by a magnetotorquer. The general formulation of the system comprised of a satellite body, two solar flaps, and a magnetotorquer is obtained through Euler's equations. The linearized system model is derived and then the control laws are developed for suitable rotations of solar flaps and variations in magnetic moment. The numerical simulation of the governing nonlinear system equations of motion establishes the feasibility of achieving the desired 3-D satellite attitude. The controllers are successful in stabilizing the satellite attitude even in the presence of orbital eccentricity and variations in system parameters. (C) 2008 Elsevier Ltd. All rights reserved.-
dc.description.sponsorshipThe authors wish to acknowledge the financial support for this study provided by Canada Research Chair Program and National Research Laboratory Program (2002, M1-0203-00-006) of the Ministry of Science and Technology, Korea. The authors would also like to thank all reviewers for providing valuable suggestions and comments.en
dc.languageEnglish-
dc.language.isoen_USen
dc.publisherPERGAMON-ELSEVIER SCIENCE LTD-
dc.subjectSPINNING SPACECRAFT-
dc.subjectMAGNETIC TORQUER-
dc.subjectEARTH SATELLITES-
dc.subjectCONTROL SYSTEM-
dc.subjectVEHICLES-
dc.subjectFIELDS-
dc.subjectORBITS-
dc.titleSatellite attitude stabilization using solar radiation pressure and magnetotorquer-
dc.typeArticle-
dc.identifier.wosid000262606300004-
dc.identifier.scopusid2-s2.0-57649102178-
dc.type.rimsART-
dc.citation.volume17-
dc.citation.issue2-
dc.citation.beginningpage267-
dc.citation.endingpage279-
dc.citation.publicationnameCONTROL ENGINEERING PRACTICE-
dc.identifier.doi10.1016/j.conengprac.2008.07.006-
dc.embargo.liftdate9999-12-31-
dc.embargo.terms9999-12-31-
dc.contributor.localauthorTahk, Min-Jea-
dc.contributor.localauthorBang, Hyochoong-
dc.contributor.nonIdAuthorKumar, K. D.-
dc.type.journalArticleArticle-
dc.subject.keywordAuthorSatellite attitude-
dc.subject.keywordAuthorAttitude stabilization-
dc.subject.keywordAuthorSolar radiation pressure-
dc.subject.keywordAuthorMagnetotorquer-
dc.subject.keywordAuthorGeosynchronous satellite-
dc.subject.keywordPlusSPINNING SPACECRAFT-
dc.subject.keywordPlusMAGNETIC TORQUER-
dc.subject.keywordPlusEARTH SATELLITES-
dc.subject.keywordPlusCONTROL SYSTEM-
dc.subject.keywordPlusVEHICLES-
dc.subject.keywordPlusFIELDS-
dc.subject.keywordPlusORBITS-
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AE-Journal Papers(저널논문)
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