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

Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S.

Bibliographic Details
Main Author: Smuck, Jerry Patrick
Other Authors: Arthur E. Bryson, Jr.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2015
Subjects:
Online Access:http://hdl.handle.net/1721.1/97949
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author Smuck, Jerry Patrick
author2 Arthur E. Bryson, Jr.
author_facet Arthur E. Bryson, Jr.
Smuck, Jerry Patrick
author_sort Smuck, Jerry Patrick
collection MIT
description Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S.
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institution Massachusetts Institute of Technology
language eng
last_indexed 2024-09-23T10:31:35Z
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publisher Massachusetts Institute of Technology
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spelling mit-1721.1/979492019-04-11T12:36:43Z Nonlinear feedback solution for minimum-time intercept with constant thrust acceleration. Smuck, Jerry Patrick Arthur E. Bryson, Jr. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics Aeronautics and Astronautics Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S. Bibliography: leaf v. M.S. 2015-07-31T19:07:06Z 2015-07-31T19:07:06Z 1966 Thesis http://hdl.handle.net/1721.1/97949 26025067 eng 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 11, [13] leaves application/pdf Massachusetts Institute of Technology
spellingShingle Aeronautics and Astronautics
Smuck, Jerry Patrick
Nonlinear feedback solution for minimum-time intercept with constant thrust acceleration.
title Nonlinear feedback solution for minimum-time intercept with constant thrust acceleration.
title_full Nonlinear feedback solution for minimum-time intercept with constant thrust acceleration.
title_fullStr Nonlinear feedback solution for minimum-time intercept with constant thrust acceleration.
title_full_unstemmed Nonlinear feedback solution for minimum-time intercept with constant thrust acceleration.
title_short Nonlinear feedback solution for minimum-time intercept with constant thrust acceleration.
title_sort nonlinear feedback solution for minimum time intercept with constant thrust acceleration
topic Aeronautics and Astronautics
url http://hdl.handle.net/1721.1/97949
work_keys_str_mv AT smuckjerrypatrick nonlinearfeedbacksolutionforminimumtimeinterceptwithconstantthrustacceleration