Design of H∞ control based nonlinear terminal guidance law

被引：0
|
作者：
Guo, Jianguo [1 ]
Zhou, Jun [1 ]
机构：
[1] Institute of Precision Guidance and Control, Northwestern Polytechnical University, Xi'an 710072, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2009年 / 30卷 / 12期
关键词：
Compilation and indexing terms; Copyright 2025 Elsevier Inc;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Electronic guidance systems - Guided missiles - Asymptotic stability
引用
收藏
页码：2423 / 2427
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