DocumentCode
1129850
Title
Nonsaturating Satellite Open-Loop Feedback Controls
Author
Guibord, A. ; Ahmed, N.U.
Author_Institution
University of Ottawa
Issue
2
fYear
1979
fDate
3/1/1979 12:00:00 AM
Firstpage
199
Lastpage
203
Abstract
The dynamics of a zero-momentum three-axis attitude controlled satellite is used to formulate an optimal control problem, which is then solved for the special case where the flywheels operate in a nonsaturating mode. The results then serve as guidelines in the design of simple open-loop and feedback controllers.
Keywords
Acceleration; Aerodynamics; Angular velocity; Attitude control; Control systems; Feedback control; Flywheels; Open loop systems; Optimal control; Satellites;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1979.308705
Filename
4102135
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