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