A new design of adaptive model following control system for lateral motion of aircraft

被引:2
|
作者
Maddi A. [1 ]
Guessoum A. [1 ]
Berkani D. [2 ]
机构
[1] Electronics Department, Faculty of Technology, Saad Dahlab University of Blida
[2] Department of Electrical Engineering, National Polytechnic School of Algiers
关键词
Adaptive control; Aircraft model; Hyperstability criteria; Lyapunov function; Model following;
D O I
10.1504/IJSCC.2020.110849
中图分类号
学科分类号
摘要
In this paper, a new design of an adaptive model following control (AMFC) system is proposed and analysed for a class of multi-input multi-output (MIMO) linear time-varying plants with unknown bounded parameters, and sufficiently slowly varying with time. We then show that the new approach based on combined Lyapunov method and hyper-stability criteria tries to overcome the problems of stability and zero tracking error. The main difficulty of Lyapunov methods is in finding an appropriate Lyapunov control function for the closed-loop system, therefore different choices of Lyapunov functions may result in different control structures and control performance. We show that the design of AMFC for the class of linear time-varying systems could be composed of a stable linear block in the feed forward path which turns out to be easily solvable by Lyapunov equation and a nonlinear time-varying block in the feedback path can be handled with using adaptive control techniques, such that the closed-loop dynamics of the system approaches the reference model. This structure results in greater flexibility in the choice of the adaptive laws. Finally, a typical numerical example to an aircraft control problem is analysed. Copyright © 2020 Inderscience Enterprises Ltd.
引用
收藏
页码:364 / 380
页数:16
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