DocumentCode
2722183
Title
Feedback linearization and VLF-techniques on the synthesis of spacecraft´s gyromoment attitude control systems
Author
Somov, Yevgeny I.
Author_Institution
Irkutsk Comput. Center, Acad. of Sci., Irkutsk, Russia
Volume
4
fYear
1996
fDate
14-17 Oct 1996
Firstpage
2522
Abstract
We present new results on optimizing and dynamic synthesis of the nonlinear gyromoment attitude control systems for a fast-manoeuvring remote sensing spacecraft with a minimum-excessive scheme of single gimbal control moment gyroscopes, achieved by the exact feedback linearization and vector Lyapunov functions (VLF)
Keywords
Lyapunov methods; aerospace control; attitude control; control system synthesis; dynamics; feedback; gyroscopes; linearisation techniques; nonlinear control systems; optimal control; space vehicles; dynamic synthesis; feedback linearization; gimbal control moment gyroscopes; gyromoment attitude control; nonlinear systems; optimal programmed control; spacecraft; vector Lyapunov functions; Aerodynamics; Ball bearings; Feedback; Gears; Gyroscopes; Mathematical model; Optical arrays; Reluctance motors; Remote sensing; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems, Man, and Cybernetics, 1996., IEEE International Conference on
Conference_Location
Beijing
ISSN
1062-922X
Print_ISBN
0-7803-3280-6
Type
conf
DOI
10.1109/ICSMC.1996.561326
Filename
561326
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