Relative Circular Navigation Guidance for the Impact Angle Control Problem

被引：19
|
作者：
Yoon, Myung-Gon [1 ]
机构：
[1] Kangnung Natl Univ, Dept Precis Mech Engn, Kangnung 201702, Kangwon, South Korea
来源：
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2008年 / 44卷 / 04期
关键词：
D O I：
10.1109/TAES.2008.4667721
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A new homing navigation guidance law is presented for a pursuer to intercept a moving target with a prescribed impact angle: the impact angle control problem. The proposed guidance law can solve the Impact angle control problem for virtually every initial geometry of pursuer and target on a plane and any desired impact attitude angle. The impact angle error of the proposed law is presented in a closed form. In addition it is shown that the acceleration command is finite even at impact time. A comparative study with existing techniques is performed both analytically and numerically to investigate the performance and properties of the new law.
引用
收藏
页码：1449 / 1463
页数：15
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