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
Link To Document :
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