Research On Missile System With Strapdown Guidance Technology

被引：1

作者：

Feng, Delong ^{[1
]}

Yang, Suochang ^{[1
]}

Liu, Yingxi ^{[2
]}

机构：

[1] Shijiazhuang Mech Engn Coll, Dept Missilery Engn, Shijiazhuang, Peoples R China

[2] Xidian Univ, Natl Key Lab Sci & Technol Radar Signal Proc, Xian, Peoples R China

来源：

CURRENT TRENDS IN THE DEVELOPMENT OF INDUSTRY, PTS 1 AND 2 | 2013年 / 785-786卷

关键词：

proportional guidance law; guided missile; strapdown; seeker;

D O I：

10.4028/www.scientific.net/AMR.785-786.1560

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

This paper presents a project of missile guidance system based on the strapdown guidance technology. The project is composed of strapdown seeker and inertial measurement unit. The integrated guidance and control technology have been adopted. The project raise accuracy of missiles on the premise that the low cost should be guaranteed. According to simulation experiment, this paper proves the feasiblity of the scheme, and it has good ballistic missile.

引用

页码：1560 / +

页数：2

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