Guidance and Control for Missiles with a Strapdown Seeker

被引:0
作者
Kim, Dowan [1 ]
Ryoo, Chang-Kyung [1 ]
Kim, Yongho [2 ]
Kim, Jongju [2 ]
机构
[1] Inha Univ, Dept Aerosp Engn, Inchon 402751, South Korea
[2] Hanwha Corp, R&D Ctr, Taejon, South Korea
来源
2011 11TH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND SYSTEMS (ICCAS) | 2011年
关键词
Strapdown Seeker; Look Angle; Guidance Law;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The strapdown seeker is not commonly used despite of many advantages, because of some weaknesses. This paper suggests the guidance law, the look angle control guidance, that controls the look angle measured by strapdown seeker directly. In this paper, we explain briefly the problem using proportional guidance law with the strapdown seeker and introduce the concept of suggested guidance law. And finally we verify the performance of suggested guidance law by simple simulation.
引用
收藏
页码:969 / 972
页数:4
相关论文
共 3 条
[1]  
Blakelock John H., AIRCRAFT MISSILES
[2]  
Park C. B., 2004, UNDERSTANDING AERODY
[3]  
Zarchan P., 2002, TACTICAL STRATEGIC M