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  5. Nonlinear feedback solution for minimum-time intercept with constant thrust acceleration.

Nonlinear feedback solution for minimum-time intercept with constant thrust acceleration.

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Author(s)
Smuck, Jerry Patrick
Advisor(s)
Arthur E. Bryson, Jr.
Date Issued
1966
Publisher
Massachusetts Institute of Technology
Description
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S.
Bibliography: leaf v.
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 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/1721.1/97949
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