dc.contributor.advisor | David W. Miller. | en_US |
dc.contributor.author | Masuda, Kazumi | en_US |
dc.date.accessioned | 2009-12-10T18:51:38Z | |
dc.date.available | 2009-12-10T18:51:38Z | |
dc.date.copyright | 1995 | en_US |
dc.date.issued | 1995 | en_US |
dc.identifier.uri | http://hdl.handle.net/1721.1/49949 | |
dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995. | en_US |
dc.description | Includes bibliographical references (p. 169-172). | en_US |
dc.description.statementofresponsibility | by Kazumi Masuda. | en_US |
dc.format.extent | 172 p. | 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 | Application of multiple model control to space structure systems with nonlinear inertial properties | 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 | 33945884 | en_US |