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dc.contributor.advisorRudrapatna V. Ramnath.en_US
dc.contributor.authorAubin, Pierre-Etienneen_US
dc.date.accessioned2009-08-26T16:22:36Z
dc.date.available2009-08-26T16:22:36Z
dc.date.copyright1993en_US
dc.date.issued1993en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/46417
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.en_US
dc.descriptionIncludes bibliographical references (leaves 105-107).en_US
dc.description.statementofresponsibilityby Pierre-Etienne Aubin.en_US
dc.format.extent107 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.titleBifurcation analysis and control of a fighter aircraften_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc28469425en_US


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