DocumentCode
313160
Title
Nonlinear singular H∞ suboptimal control for a rigid spacecraft with actuator dynamics
Author
Dalsmo, Morten ; Mass, W.C.A.
Author_Institution
ABB Corp. Res., Vasteras, Sweden
Volume
3
fYear
1997
fDate
4-6 Jun 1997
Firstpage
1879
Abstract
We address a nonlinear singular H∞ suboptimal control problem for a rigid spacecraft with actuator dynamics. Using results from nonlinear H∞ control theory, we find an explicit feedback solution involving the Euler parameters. Our solution is based on a solution to a corresponding nonlinear regular H∞ suboptimal control problem for a rigid spacecraft with three control torques and disturbances
Keywords
H∞ control; aerospace control; dynamics; feedback; nonlinear control systems; space vehicles; suboptimal control; Euler parameters; actuator dynamics; control torques; disturbances; explicit feedback solution; nonlinear singular H∞ suboptimal control; rigid spacecraft; Actuators; Control systems; Earth; Nonlinear systems; Optimal control; Orbits; Space vehicles; State feedback; State-space methods; Torque control;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1997. Proceedings of the 1997
Conference_Location
Albuquerque, NM
ISSN
0743-1619
Print_ISBN
0-7803-3832-4
Type
conf
DOI
10.1109/ACC.1997.610911
Filename
610911
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