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The design of a control system for the terminal phase of a satellite rendezvous

dc.contributor.authorHollister, Walter M., 1930-en_US
dc.date.accessioned2026-01-06T20:23:36Z
dc.date.available2026-01-06T20:23:36Z
dc.date.copyright1959en_US
dc.date.issued1959en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/164454
dc.descriptionThesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1959en_US
dc.descriptionIncludes bibliographical references (leaf 47).en_US
dc.description.statementofresponsibilityby Walter M. Hollister.en_US
dc.format.extent52 leavesen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses may be protected by copyright. Please reuse MIT thesis content according to the MIT Libraries Permissions Policy, which is available through the URL provided.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronauticsen_US
dc.titleThe design of a control system for the terminal phase of a satellite rendezvousen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc32586070en_US
dc.description.collectionM.S. Massachusetts Institute of Technology, Department of Aeronautics and Astronauticsen_US
dspace.imported2026-01-06T20:23:36Zen_US
mit.thesis.degreeMasteren_US


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