Predictor-Based Model Reference Adaptive Control

被引：52

作者：

Lavretsky, Eugene ^{[1
]}

Gadient, Ross ^{[1
]}

Gregory, Irene M. ^{[2
]}

机构：

[1] Boeing Co, Huntington Beach, CA 92647 USA

[2] NASA, Langley Res Ctr, Hampton, VA 23681 USA

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2010年 / 33卷 / 04期

基金：

美国国家航空航天局;

关键词：

DYNAMIC INVERSION;

D O I：

10.2514/1.46849

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper is devoted to the design and analysis of a predictor-based model reference adaptive control. Stable adaptive laws are derived using Lyapunov framework. The proposed architecture is compared with the now-classical model reference adaptive control. A simulation example is presented in which numerical evidence indicates that the proposed controller yields improved transient characteristics.

引用

页码：1195 / 1201

页数：7

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