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

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

Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S. === Bibliography: leaf v. === M.S.

Bibliographic Details
Main Author: Smuck, Jerry Patrick
Other Authors: Arthur E. Bryson, Jr.
Format: Others
Language:English
Published: Massachusetts Institute of Technology 2015
Subjects:
Aeronautics and Astronautics
Online Access:http://hdl.handle.net/1721.1/97949

Internet

http://hdl.handle.net/1721.1/97949

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