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dc.contributor.advisorPhilip Whitaker.en_US
dc.contributor.authorStofko, David Michaelen_US
dc.date.accessioned2013-07-10T14:45:34Z
dc.date.available2013-07-10T14:45:34Z
dc.date.issued1976en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/79444
dc.descriptionThesis. 1976. M.S.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.descriptionMICROFICHE COPY AVAILABLE IN ARCHIVES AND AERONAUTICS.en_US
dc.descriptionIncludes bibliographical references.en_US
dc.description.statementofresponsibilityby David M. Stofko.en_US
dc.format.extent154 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.subject.lcshLaunch vehicles (Astronautics) Control systemsen_US
dc.subject.lcshAutomatic pilot (Space vehicles)en_US
dc.subject.lcshDigital electronicsen_US
dc.subject.lcshGyroscopes Reliabilityen_US
dc.titleEffects of multirate compensation on a digital autopilot for thrust vector control of a launch vehicleen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc06079683en_US


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