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
Link To Document :
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