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dc.contributor.advisorH. Philip Whitaker.en_US
dc.contributor.authorBonnice, William Fentonen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2010-09-03T18:46:15Z
dc.date.available2010-09-03T18:46:15Z
dc.date.copyright1983en_US
dc.date.issued1983en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/58415
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1983.en_US
dc.descriptionMicrofiche copy available in Archives and Barkeren_US
dc.description.statementofresponsibilityby William Fenton Bonnice.en_US
dc.format.extent197 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/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleSteering of a boost vehicle to a desired flight path angle trajectory using angle of attack controlen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc11130481en_US


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