DocumentCode
1976663
Title
Adaptive robust attitude tracking control of spacecraft
Author
Motlagh, Reza Banirazi ; Motlagh, M. R Jahed
Author_Institution
Dept. of Electr. Eng., Iran Univ. of Sci. & Technol., Tehran
fYear
2005
fDate
28-31 Aug. 2005
Firstpage
498
Lastpage
503
Abstract
A nonlinear adaptive-robust scheme is presented to control a class of nonlinear systems. It effectively combines the design techniques of adaptive and robust control to improve performance by retaining the advantages of both techniques. It enhances transient performance and eliminates robustness problems compared to a parameter adaptive control. It also improves tracking performance by reducing modeling uncertainty and optimizes control effort by estimating bound uncertainty compared to a deterministic robust control. The controller is applied to a spacecraft making the body frame track a reference orientation, when there are parametric uncertainty, modeling errors, and external disturbances
Keywords
adaptive control; attitude control; control system synthesis; nonlinear control systems; robust control; space vehicles; tracking; uncertain systems; deterministic robust control; external disturbance; modeling error; nonlinear adaptive-robust scheme; nonlinear system control; optimal control; parametric uncertainty; reference orientation; spacecraft adaptive robust attitude tracking control; transient performance; uncertainty modeling; Adaptive control; Attitude control; Control systems; Error correction; Nonlinear control systems; Nonlinear systems; Programmable control; Robust control; Space vehicles; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 2005. CCA 2005. Proceedings of 2005 IEEE Conference on
Conference_Location
Toronto, Ont.
Print_ISBN
0-7803-9354-6
Type
conf
DOI
10.1109/CCA.2005.1507175
Filename
1507175
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