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dc.contributor.advisorRichard Battin.en_US
dc.contributor.authorHart, Andrew Markland Stanleyen_US
dc.date.accessioned2008-09-03T15:51:17Z
dc.date.available2008-09-03T15:51:17Z
dc.date.copyright1991en_US
dc.date.issued1991en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/42500
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.en_US
dc.descriptionIncludes bibliographical references (leaves 205).en_US
dc.description.statementofresponsibilityby Andrew Markland Stanley Hart.en_US
dc.format.extent205 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.titleApplication of the homotopy continuation method to low-eccentricity preliminary orbit determinationen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc25601236en_US


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