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dc.contributor.advisorWallace E. Vander Velde.en_US
dc.contributor.authorLupi, Victor D. (Victor Dominick)en_US
dc.date.accessioned2008-11-07T19:21:04Z
dc.date.available2008-11-07T19:21:04Z
dc.date.copyright1992en_US
dc.date.issued1992en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/43252
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1992.en_US
dc.descriptionIncludes bibliographical references (leaves 219-225).en_US
dc.description.statementofresponsibilityby Victor D. Lupi.en_US
dc.format.extent225 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 Astronauticsen_US
dc.titleThe use of mathematically exact solutions of structural dynamics models for structural control designen_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Dept. of Aeronautics and Astronauticsen_US
dc.identifier.oclc26622967en_US


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