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dc.contributor.advisorEdward F. Crawley.en_US
dc.contributor.authorFleming, Farla Mindyen_US
dc.date.accessioned2008-09-03T15:46:35Z
dc.date.available2008-09-03T15:46:35Z
dc.date.copyright1990en_US
dc.date.issued1991en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/42475
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.en_US
dc.descriptionIncludes bibliographical references (leaves 131-135).en_US
dc.description.statementofresponsibilityby Farla Mindy Fleming.en_US
dc.format.extent135 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 effect of structure, actuator, and sensor on the zeroes of controlled structuresen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc24571873en_US


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