DocumentCode
1157126
Title
Attitude stabilization with actuators subject to switching restrictions: an approach via exact relay control methods
Author
Kienitz, Karl Heinz
Author_Institution
Instituto Technologico de Aeronaut., Divisao de Engenharia Eletronica, Sao Jose dos Campos
Volume
42
Issue
4
fYear
2006
fDate
10/1/2006 12:00:00 AM
Firstpage
1485
Lastpage
1492
Abstract
On-off thrusters are frequently used as actuators for attitude control. Typically these thrusters are subject to switching constraints. A limit cycle is the normal steady state operation mode of such attitude control systems. This contribution deals with controller design for precision attitude stabilization using actuators whose switching restrictions are explicitly considered. An exact approach is presented using ideas from established relay control methods. The design procedure is illustrated with an attitude controller design to attain a limit cycle with prescribed characteristics
Keywords
actuators; attitude control; relay control; actuators; attitude control systems; precision attitude stabilization; relay control methods; steady state operation; switching restrictions; Actuators; Attitude control; Control systems; Design methodology; Limit-cycles; Propellants; Relays; Space vehicles; State-space methods; Steady-state;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.2006.314588
Filename
4107990
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