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dc.contributor.advisorAndreas H. von Flotow.en_US
dc.contributor.authorQuadrelli, Bruno Marcoen_US
dc.date.accessioned2007-11-16T14:31:57Z
dc.date.available2007-11-16T14:31:57Z
dc.date.copyright1992en_US
dc.date.issued1992en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/39603
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1992.en_US
dc.descriptionIncludes bibliographical references (p. 134-137).en_US
dc.description.statementofresponsibilityby Bruno Marco Quadrelli.en_US
dc.format.extent143, [154] p.en_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/1721.1/7582
dc.subjectAeronautics and Astronauticsen_US
dc.titleModelling, dynamics analysis and control of a multi-body space platformen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc27472124en_US


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