DocumentCode :
700498
Title :
Control of flexible space vehicles using an adjustable model and alternate control laws
Author :
Rutkovsky, V.Yu. ; Sukhanov, V.M. ; Dodds, S.J.
Author_Institution :
Inst. of Control Sci., Moscow, Russia
fYear :
1997
fDate :
1-7 July 1997
Firstpage :
405
Lastpage :
410
Abstract :
The problem of model uncertainty is discussed and an attitude control system is proposed utilising a new onboard identification algorithm updating an adjustable model whose state estimate feeds two control laws, one for active flexure mode damping and the other for basic orientation. An onboard expert monitors the state estimate and automatically switches between the two alternate control laws according to the relative degrees of excitation of the rigid body and flexure modes. The present study is restricted to single-axis control and would be applicable for three-axis control in cases where the inter-axis coupling is negligible. The effectiveness of the control system is demonstrated by means of computer simulations.
Keywords :
attitude control; flexible structures; nonlinear control systems; space vehicles; state estimation; uncertain systems; active flexure mode damping; adjustable model; alternate control laws; attitude control system; computer simulations; excitation relative degrees; flexible space vehicles control; flexible structure; flexure modes; inter-axis coupling; model uncertainty; nonlinear control; onboard expert; onboard identification algorithm; rigid body; single-axis control; state estimation; three-axis control; Attitude control; Control systems; Damping; Mathematical model; Parameter estimation; Space vehicles; Torque; Adaptive; Flexible structures; Nonlinear control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (ECC), 1997 European
Conference_Location :
Brussels
Print_ISBN :
978-3-9524269-0-6
Type :
conf
Filename :
7082128
Link To Document :
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