DocumentCode :
83417
Title :
H_\\infty Fuzzy Control for a Class of Nonlinear Coupled ODE-PDE Systems With Input Constraint
Author :
Huai-Ning Wu ; Huan-Yu Zhu ; Jun-Wei Wang
Author_Institution :
Sci. & Technol. on Aircraft Control Lab., Beihang Univ. (formerly Beijing Univ. of Aeronaut. & Astronaut.), Beijing, China
Volume :
23
Issue :
3
fYear :
2015
fDate :
Jun-15
Firstpage :
593
Lastpage :
604
Abstract :
This paper deals with the problem of H fuzzy control design with an input constraint for a class of coupled systems, which consist of an n-dimensional nonlinear subsystem of ordinary differential equations (ODEs) and a scalar linear parabolic subsystem of partial differential equation (PDE) connected in feedback. Initially, the nonlinear coupled system is represented by a Takagi-Sugeno (T-S) fuzzy-coupled ODE-PDE model. Then, based on the fuzzy model and parallel distributed compensation scheme, a fuzzy state feedback control design is developed via Lyapunov´s direct method, such that the resulting closed-loop fuzzy-coupled system is exponentially stable, and a prescribed H performance of disturbance attenuation is satisfied. The existing condition of the proposed H∞ fuzzy controllers is given in terms of linear matrix inequalities (LMIs). Moreover, in order to make the attenuation level as small as possible while the input constraint is respected to avoid the high magnitude, a suboptimal H-constrained fuzzy control problem is also addressed, which is formulated as an LMI optimization problem. Finally, the proposed method is applied to the control of a hypersonic rocket car to illustrate its effectiveness.
Keywords :
H control; Lyapunov methods; aircraft control; asymptotic stability; closed loop systems; control system synthesis; distributed control; fuzzy control; linear matrix inequalities; linear systems; nonlinear control systems; parabolic equations; partial differential equations; rockets; state feedback; H fuzzy control design; H performance; LMI optimization problem; Lyapunov direct method; Takagi-Sugeno fuzzy-coupled ODE-PDE model; closed-loop fuzzy-coupled system; coupled systems; exponentially stable system; fuzzy state feedback control design; hypersonic rocket control; input constraint; linear matrix inequalities; n-dimensional nonlinear subsystem; ordinary differential equations; parallel distributed compensation scheme; partial differential equation; scalar linear parabolic subsystem; suboptimal H-constrained fuzzy control problem; Aerospace electronics; Attenuation; Boundary conditions; Control design; Fuzzy control; State feedback; Symmetric matrices; $H_infty$ control; Coupled ordinary differential equation and partial differential equation (ODE-PDE) systems; Takagi???Sugeno (T???S) fuzzy model; exponential stability;
fLanguage :
English
Journal_Title :
Fuzzy Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
1063-6706
Type :
jour
DOI :
10.1109/TFUZZ.2014.2318180
Filename :
6800027
Link To Document :
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