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
收藏
页码：1195 / 1201
页数：7
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