Anti-disturbance tracking control for systems with nonlinear disturbances using T–S fuzzy modeling

This paper addresses a novel anti-disturbance dynamical tracking problem for a class of MIMO systems subject to unknown disturbances and nonlinear dynamics. Different from some traditional anti-disturbance results, T–S fuzzy models are firstly employed to describe the nonlinear disturbances, in whic...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Neurocomputing (Amsterdam) Jg. 171; S. 1027 - 1037
Hauptverfasser: Yi, Yang, Fan, Xiang Xiang, Zhang, Tian Ping
Format: Journal Article
Sprache:Englisch
Veröffentlicht: Elsevier B.V 01.01.2016
Schlagworte:
Anti-disturbance control
Convex optimization algorithm
Disturbance observer (DO)
T–S disturbance modeling
T–S fuzzy models
Convex optimization algorithm
Anti-disturbance control
T–S disturbance modeling
T–S fuzzy models
Disturbance observer (DO)
ISSN:0925-2312, 1872-8286
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:This paper addresses a novel anti-disturbance dynamical tracking problem for a class of MIMO systems subject to unknown disturbances and nonlinear dynamics. Different from some traditional anti-disturbance results, T–S fuzzy models are firstly employed to describe the nonlinear disturbances, in which a disturbance observer based on T–S exogenous models is designed under different conditions to estimate the unknown nonlinear disturbances for the plants with known and unknown nonlinearities, respectively. By integrating the estimates of disturbance with PI-type control input, a composite controller based on convex optimization theory is proposed to ensure the system stability and convergence of the tracking error to zero. Meanwhile, the favorable disturbance estimation and attenuation performance can also be achieved by the designed convex optimization algorithm. Finally, the effectiveness of the proposed control schemes is verified by simulations for flight control systems with three different types of nonlinear disturbances.
ISSN:0925-2312
1872-8286
DOI:10.1016/j.neucom.2015.07.039