Adaptive critic-based neural networks for agile missile control

被引：13

作者：

Han, DC ^{[1
]}

Balakrishnan, SN ^{[1
]}

机构：

[1] Univ Missouri, Dept Mech & Aerosp Engn & Engn Mech, Rolla, MO 65409 USA

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2002年 / 25卷 / 02期

关键词：

Aircraft - Equations of motion - Feedback control - Neural networks - Nonlinear systems - Optimization;

D O I：

10.2514/2.4895

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Adaptive critic-based neural networks were discussed for agile missile control. The neural network solutions were obtained by using a pair of action and critic networks at each stage. The computational effort associated with the adaptive critic-based solutions is not prohibitive. It was observed that this computational technique is fairly general and applicable to a wide variety of problems.

引用

页码：404 / 407

页数：4

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