DocumentCode
2387901
Title
Adaptive control of wing rock system in uncertain environment using contraction theory
Author
Sharma, B.B. ; Kar, I.N.
Author_Institution
Dept. of Electr. Eng., Indian Inst. of Technol., New Delhi
fYear
2008
fDate
11-13 June 2008
Firstpage
2963
Lastpage
2968
Abstract
Contraction theory is used to study stability based on differential and incremental behaviour of trajectories of a system with respect to each other. Application of contraction theory provides a platform to analyze the exponential stability of nonlinear systems. This paper considers the design of a control law for wing rock system using contraction theory principles. An adaptive control design approach based on contraction theory is proposed for controlling the dynamics of such systems for the cases with and without uncertainty in parameters. An adaptive control law along with parameter updation law is derived for uncertain wing rock system to achieve convergence of trajectories of actual system to that of desired system. The analysis made in the paper leads to quite simple results avoiding complexities involved with Lyapunov method. Finally numerical simulations are presented to justify the effectiveness of the proposed controller.
Keywords
Lyapunov methods; adaptive control; aerospace components; asymptotic stability; nonlinear control systems; numerical analysis; adaptive control design approach; contraction theory; differential-incremental behaviour; exponential stability; nonlinear systems; uncertain environment; wing rock system; Adaptive control; Aerodynamics; Aircraft; Control systems; Convergence; Lyapunov method; Nonlinear dynamical systems; Nonlinear systems; Stability analysis; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2008
Conference_Location
Seattle, WA
ISSN
0743-1619
Print_ISBN
978-1-4244-2078-0
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2008.4586946
Filename
4586946
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