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dc.contributor.advisorPaul J. Cefola.en_US
dc.contributor.authorWagner, Elaine Annen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2006-11-06T15:59:51Z
dc.date.available2006-11-06T15:59:51Z
dc.date.copyright1983en_US
dc.date.issued1983en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/34298
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1983.en_US
dc.descriptionMICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO.en_US
dc.descriptionIncludes bibliographical references.en_US
dc.description.statementofresponsibilityby Elaine Ann Wagner.en_US
dc.format.extent157 leavesen_US
dc.format.extent6013566 bytes
dc.format.extent6020156 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
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/1721.1/7582
dc.subjectAeronautics and Astronautics.en_US
dc.titleApplication of the extended semianalytical Kalman filter to synchronous orbitsen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc11363142en_US


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