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dc.contributor.advisorWallace E. Vander Velde.en_US
dc.contributor.authorHanawa, Yujien_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2009-12-10T18:42:50Z
dc.date.available2009-12-10T18:42:50Z
dc.date.copyright1979en_US
dc.date.issued1979en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/49886
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1979.en_US
dc.descriptionMICROFICHE COPY AVAILABLE IN ARCHIVES AND AERONAUTICS.en_US
dc.descriptionBibliography: leaf 72.en_US
dc.description.statementofresponsibilityby Yuji Hanawa.en_US
dc.format.extent72 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.lcshSpace vehicles Attitude control systemsen_US
dc.subject.lcshSpace vehicles Fuel consumptionen_US
dc.subject.lcshKalman filteringen_US
dc.subject.lcshSpace trajectoriesen_US
dc.titleFuel efficient attitude control of spacecraften_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc07493711en_US


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