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dc.contributor.advisorWinston R. Markey.en_US
dc.contributor.authorKillingsworth, William Roberten_US
dc.date.accessioned2005-08-10T20:12:15Z
dc.date.available2005-08-10T20:12:15Z
dc.date.issued1968en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/14163
dc.descriptionMassachusetts Institute of Technology, Dept. of Aeronautics and Astronautics. Thesis. 1968. M.S.en_US
dc.descriptionMICROFICHE COPY ALSO AVAILABLE IN AERO LIBRARY.en_US
dc.descriptionBibliography: p. 59-60.en_US
dc.format.extent[4], 73 p.en_US
dc.format.extent7767963 bytes
dc.format.extent7767719 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.titleComputation frames for strapdown inertial systems.en_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc23964526en_US


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