DocumentCode
1174616
Title
On the Optimum Stabilization of a Satellite
Author
Kumar, K.S.P.
Author_Institution
Department of Electrical Engineering University of Minnesota Minneapolis, Minn.
Issue
2
fYear
1965
Firstpage
82
Lastpage
83
Abstract
The problem of stabilizing a tumbling satellite prior to attitude control is discussed. The method of Hamilton-Jacobi theory is used to derive an explicit closed-loop control law for the problem.
Keywords
Angular velocity; Application software; Calculus; Dynamic programming; Feedback; Motion control; Optimal control; Partial differential equations; Satellites; Torque control; Attitude; Hamilton-Jacobi; closed loop; control; stabilization; tumbling;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1965.4501667
Filename
4501667
Link To Document