Three-dimensional guidance law accounting for second-order dynamics of missile autopilot

被引：0

作者：

Qu, Pingping ^{[1
,2
]}

Zhou, Di ^{[1
]}

机构：

[1] Department of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, China

[2] School of Electronics and Information Engineering, Shenyang Aerospace University, Shenyang 110136, China

来源：

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2011年 / 32卷 / 11期

关键词：

404.1 Military Engineering - 431.5 Air Navigation and Traffic Control - 654.1 Rockets and Missiles - 703.2 Electric Filters;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：2096 / 2105