dc.contributor.advisor | Walter Wrigley. | en_US |
dc.contributor.author | Graham, David Bruce | en_US |
dc.date.accessioned | 2006-03-24T17:58:03Z | |
dc.date.available | 2006-03-24T17:58:03Z | |
dc.date.issued | 1972 | en_US |
dc.identifier.uri | http://hdl.handle.net/1721.1/29863 | |
dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1972. | en_US |
dc.description | Includes bibliographical references. | en_US |
dc.format.extent | 71 leaves | en_US |
dc.format.extent | 2368283 bytes | |
dc.format.extent | 2375359 bytes | |
dc.format.mimetype | application/pdf | |
dc.format.mimetype | application/pdf | |
dc.language.iso | eng | en_US |
dc.publisher | Massachusetts Institute of Technology | en_US |
dc.rights | M.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.uri | http://dspace.mit.edu/handle/1721.1/7582 | |
dc.subject | Aeronautics and Astronautics | en_US |
dc.title | Analysis and error model for a two-degrees-of-freedom elastically supported tuned gyro. | en_US |
dc.type | Thesis | en_US |
dc.description.degree | M.S. | en_US |
dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
dc.identifier.oclc | 29060720 | en_US |