Output-based disturbance rejection control for non-linear uncertain systems with unknown frequency disturbances using an observer backstepping approach

被引:36
作者
Yang, Jun [1 ]
Ding, Zhengtao [2 ]
Chen, Wen-Hua [3 ]
Li, Shihua [1 ]
机构
[1] Southeast Univ, Sch Automat, Key Lab Measurement & Control Complex Syst Engn, Minist Educ, Nanjing 210096, Jiangsu, Peoples R China
[2] Univ Manchester, Sch Elect & Elect Engn, Control Syst Ctr, Sackville St Bldg, Manchester M13 9PL, Lancs, England
[3] Univ Loughborough, Dept Aeronaut & Automot Engn, Loughborough LE11 3TU, Leics, England
基金
中国国家自然科学基金;
关键词
feedback; nonlinear control systems; control nonlinearities; observers; uncertain systems; control system synthesis; adaptive control; Lyapunov methods; closed loop systems; output-based disturbance rejection control; nonlinear uncertain system; unknown frequency disturbance; output feedback control design; compact exogenous model; adaptive internal model principle; dynamic estimator; composite output feedback controller; state estimation; closed-loop system; Lyapunov stability criterion; missile roll stabilisation; harmonic disturbance; unknown constant disturbance; observer backstepping; ASYMPTOTIC REJECTION; FEEDBACK-CONTROL; STABILIZATION;
D O I
10.1049/iet-cta.2015.1160
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This study is concerned with the output feedback control design for a class of non-linear uncertain systems subject to multiple sources of disturbances including model uncertainties, unknown constant disturbances, harmonic disturbances with unknown frequency and amplitude. The total disturbances and uncertainties are delicately represented by a compact exogenous model first. By incorporating the adaptive internal model principle, a set of dynamic estimators are developed for both state and disturbance observations. By means of observer backstepping technique, a composite output feedback controller is constructed based on the disturbance and state estimations. The stability of the closed-loop system is rigorously established based on Lyapunov stability criterion. A missile roll stabilisation example is finally investigated to validate the effectiveness of the proposed control approach.
引用
收藏
页码:1052 / 1060
页数:9
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