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dc.contributor.advisorWalter M. Hollister...et al.en_US
dc.contributor.authorCollins, Sean Kevinen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2012-09-13T18:47:17Z
dc.date.available2012-09-13T18:47:17Z
dc.date.copyright1981en_US
dc.date.issued1981en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/72742
dc.descriptionThesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1981.en_US
dc.descriptionMICROFICHE COPY AVAILABLE IN ARCHIVES AND AERONAUTICS.en_US
dc.descriptionIncludes bibliographical references.en_US
dc.description.statementofresponsibilityby Sean Kevin Collins.en_US
dc.format.extent341 p.en_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 Astronautics.en_US
dc.subject.lcshArtificial satellites Orbitsen_US
dc.subject.lcshAveraging method (Differential equations)en_US
dc.subject.lcshRecursive functionsen_US
dc.subject.lcshPerturbation (Astronomy)en_US
dc.subject.lcshThree-body problemen_US
dc.titleLong term prediction of high altitude orbitsen_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc08121567en_US


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