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dc.contributor.advisorRichard H. Battin.en_US
dc.contributor.authorMcCasland, William Neilen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2009-12-10T18:42:56Z
dc.date.available2009-12-10T18:42:56Z
dc.date.copyright1980en_US
dc.date.issued1981en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/49887
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1981.en_US
dc.descriptionMicrofiche copy available in Archives and Barkeren_US
dc.descriptionBibliography: leaves 108-109.en_US
dc.description.statementofresponsibilityby William Neil McCasland.en_US
dc.format.extent109 leavesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.subject.lcshArtificial satellites Attitude control systemsen_US
dc.subject.lcshKalman filteringen_US
dc.subject.lcshControl theoryen_US
dc.subject.lcshDiscrete-time systemsen_US
dc.titleAn optimal approach to computer control of a highly coupled satellite attitude loopen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc11117288en_US


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