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  5. An asymptotic approach in the preliminary design of a launch vehicle control system

An asymptotic approach in the preliminary design of a launch vehicle control system

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Author(s)
Le Fur, Philippe
Advisor(s)
Rudrapatna V. Ramnath.
Date Issued
1989
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.
Includes bibliographical references (leaves 96-97).
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
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.
http://dspace.mit.edu/handle/1721.1/7582
Persistent DSpace Link
http://hdl.handle.net/1721.1/40134
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