dc.contributor.advisor | David W. Wallace. | en_US |
dc.contributor.author | Elias, Laila Mireille, 1977- | en_US |
dc.contributor.other | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. | en_US |
dc.date.accessioned | 2013-10-24T17:29:03Z | |
dc.date.available | 2013-10-24T17:29:03Z | |
dc.date.copyright | 2001 | en_US |
dc.date.issued | 2001 | en_US |
dc.identifier.uri | http://hdl.handle.net/1721.1/81563 | |
dc.description | Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001. | en_US |
dc.description | Includes bibliographical references (leaves 113-114). | en_US |
dc.description.statementofresponsibility | by Laila Mireille Elias. | en_US |
dc.format.extent | 114 leaves | en_US |
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 | en_US |
dc.subject | Aeronautics and Astronautics. | en_US |
dc.title | A structurally coupled disturbance analysis method using dynamic mass measurement techniques, with application to spacecraft-reaction wheel systems | en_US |
dc.title.alternative | Coupled reaction wheel and spacecraft structural modeling via impedance measurement techniques | en_US |
dc.type | Thesis | en_US |
dc.description.degree | S.M. | en_US |
dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
dc.identifier.oclc | 49870926 | en_US |