dc.contributor.advisor | Wallace E. Vander Velde. | en_US |
dc.contributor.author | Lupi, Victor D. (Victor Dominick) | en_US |
dc.date.accessioned | 2008-11-07T19:21:04Z | |
dc.date.available | 2008-11-07T19:21:04Z | |
dc.date.copyright | 1992 | en_US |
dc.date.issued | 1992 | en_US |
dc.identifier.uri | http://hdl.handle.net/1721.1/43252 | |
dc.description | Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1992. | en_US |
dc.description | Includes bibliographical references (leaves 219-225). | en_US |
dc.description.statementofresponsibility | by Victor D. Lupi. | en_US |
dc.format.extent | 225 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 use of mathematically exact solutions of structural dynamics models for structural control design | en_US |
dc.type | Thesis | en_US |
dc.description.degree | Ph.D. | en_US |
dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
dc.identifier.oclc | 26622967 | en_US |