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  5. Attitude control system for the high energy transient experiment small satellite

Attitude control system for the high energy transient experiment small satellite

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Author(s)
Chang, Daniel H
Advisor(s)
Andreas von Flotow.
Date Issued
1991
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.
Includes bibliographical references (p. 207-208).
Subjects
Aeronautics and Astronautics
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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M.I.T. theses are protected by
copyright. They may be viewed from this source for any purpose, but
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permission. See provided URL for inquiries about permission.
http://dspace.mit.edu/handle/1721.1/7582
Persistent DSpace Link
http://hdl.handle.net/1721.1/42493
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