dc.contributor.advisor | Edward F. Crawley. | en_US |
dc.contributor.author | Fleming, Farla Mindy | en_US |
dc.date.accessioned | 2008-09-03T15:46:35Z | |
dc.date.available | 2008-09-03T15:46:35Z | |
dc.date.copyright | 1990 | en_US |
dc.date.issued | 1991 | en_US |
dc.identifier.uri | http://hdl.handle.net/1721.1/42475 | |
dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991. | en_US |
dc.description | Includes bibliographical references (leaves 131-135). | en_US |
dc.description.statementofresponsibility | by Farla Mindy Fleming. | en_US |
dc.format.extent | 135 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 | The effect of structure, actuator, and sensor on the zeroes of controlled structures | 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 | 24571873 | en_US |