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
Link To Document :
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