DocumentCode
1294996
Title
Optimal Discrete-Time Design of Three-Axis Magnetic Attitude Control Laws
Author
Pulecchi, Tiziano ; Lovera, Marco ; Varga, Andras
Author_Institution
Dipt. di Elettron. e Inf., Politec. di Milano, Milan, Italy
Volume
18
Issue
3
fYear
2010
fDate
5/1/2010 12:00:00 AM
Firstpage
714
Lastpage
722
Abstract
The problem of designing discrete-time attitude controllers for three-axis stabilization of magnetically actuated spacecraft is considered. Several methods are discussed and an approach to the tuning of various classes of projection-based controllers is proposed relying on periodic optimal output feedback control techniques. The main advantages of the proposed methods are discussed and illustrated in a simulation study.
Keywords
attitude control; control system synthesis; discrete time systems; electromagnetic actuators; feedback; optimal control; space vehicles; attitude control; magnetically actuated spacecraft; optimal discrete-time design; output feedback; projection-based controllers; three-axis stabilization; Attitude control; magnetic actuators; periodic optimal control; periodic systems; spacecraft control; static output feedback;
fLanguage
English
Journal_Title
Control Systems Technology, IEEE Transactions on
Publisher
ieee
ISSN
1063-6536
Type
jour
DOI
10.1109/TCST.2009.2024757
Filename
5200344
Link To Document