An optimal approach to computer control of a highly coupled satellite attitude loop

Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1981.

Библиографические подробности
Главный автор: McCasland, William Neil
Другие авторы: Richard H. Battin.
Формат: Диссертация
Язык:eng
Опубликовано: Massachusetts Institute of Technology 2009
Предметы:
Online-ссылка:http://hdl.handle.net/1721.1/49887
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author McCasland, William Neil
author2 Richard H. Battin.
author_facet Richard H. Battin.
McCasland, William Neil
author_sort McCasland, William Neil
collection MIT
description Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1981.
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spelling mit-1721.1/498872019-04-11T11:09:15Z An optimal approach to computer control of a highly coupled satellite attitude loop McCasland, William Neil Richard H. Battin. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Artificial satellites Attitude control systems Kalman filtering Control theory Discrete-time systems Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1981. Microfiche copy available in Archives and Barker Bibliography: leaves 108-109. by William Neil McCasland. M.S. 2009-12-10T18:42:56Z 2009-12-10T18:42:56Z 1980 1981 Thesis http://hdl.handle.net/1721.1/49887 11117288 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 109 leaves application/pdf Massachusetts Institute of Technology
spellingShingle Aeronautics and Astronautics.
Artificial satellites Attitude control systems
Kalman filtering
Control theory
Discrete-time systems
McCasland, William Neil
An optimal approach to computer control of a highly coupled satellite attitude loop
title An optimal approach to computer control of a highly coupled satellite attitude loop
title_full An optimal approach to computer control of a highly coupled satellite attitude loop
title_fullStr An optimal approach to computer control of a highly coupled satellite attitude loop
title_full_unstemmed An optimal approach to computer control of a highly coupled satellite attitude loop
title_short An optimal approach to computer control of a highly coupled satellite attitude loop
title_sort optimal approach to computer control of a highly coupled satellite attitude loop
topic Aeronautics and Astronautics.
Artificial satellites Attitude control systems
Kalman filtering
Control theory
Discrete-time systems
url http://hdl.handle.net/1721.1/49887
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