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dc.contributor.authorAxelrad, Penina.en_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2005-08-08T16:57:13Z
dc.date.available2005-08-08T16:57:13Z
dc.date.copyright1986en_US
dc.date.issued1986en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/15034en_US
dc.descriptionThesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1986en_US
dc.descriptionBibliography: leaves 144-148.en_US
dc.description.statementofresponsibilityby Penina Axelrad.en_US
dc.format.extent148 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 Astronautics.en_US
dc.titleNear Earth orbit determination and rendezvous navigation using GPSen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc15368532en_US
dc.description.collectionM.S. Massachusetts Institute of Technology, Department of Aeronautics and Astronauticsen_US
dspace.imported2022-10-07T15:47:01Zen_US


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