Attitude control system for the high energy transient experiment small satellite

Author(s)
Chang, Daniel H
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Advisor
Andreas von Flotow.
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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
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Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.
 
Includes bibliographical references (p. 207-208).
 
Date issued
1991
URI
http://hdl.handle.net/1721.1/42493
Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Publisher
Massachusetts Institute of Technology
Keywords
Aeronautics and Astronautics
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