Research of integrated robust high order sliding mode guidance and control for missiles

被引：0
|
作者：
Dong, Feiyao [1 ]
Lei, Humin [1 ]
Zhou, Chijun [1 ]
Li, Jiong [1 ]
Shao, Lei [1 ]
机构：
[1] School of Air and Missile Defense, Air Force Engineering University, Xi'an 710051, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2013年 / 34卷 / 09期
关键词：
15;
D O I：
10.7527/S1000-6893.2013.0054
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：2212 / 2218
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