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dc.contributor.advisorWallace E. Vander Velde.en_US
dc.contributor.authorSutherland, Arthur Abbotten_US
dc.date.accessioned2005-06-02T13:57:07Z
dc.date.available2005-06-02T13:57:07Z
dc.date.issued1967en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/17256
dc.descriptionMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. Sc.D.en_US
dc.descriptionSix blank pages included in paging. Vita.en_US
dc.descriptionBibliography: leaves 131-132.en_US
dc.format.extentvii, 133 p.en_US
dc.format.extent5241198 bytes
dc.format.extent5258961 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 Astronauticsen_US
dc.titleApplication of optimal linear estimation to the alignment of inertial guidance systems.en_US
dc.typeThesisen_US
dc.description.degreeSc.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc24015484en_US


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