| dc.contributor.advisor | Steven R. Hall. | en_US |
| dc.contributor.author | MacMartin, Douglas G | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. | en_US |
| dc.date.accessioned | 2008-09-03T14:50:53Z | |
| dc.date.available | 2008-09-03T14:50:53Z | |
| dc.date.copyright | 1990 | en_US |
| dc.date.issued | 1990 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/42189 | |
| dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990. | en_US |
| dc.description | On t.p. "[infinity]" is the symbol. | en_US |
| dc.description | Includes bibliographical references (leaves 92-95). | en_US |
| dc.description.statementofresponsibility | by Douglas G. MacMartin. | en_US |
| dc.format.extent | 100 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 | An H [infinity] power flow approach to control of uncertain 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 | 22926400 | en_US |
