Geometrical approach-based defense-missile intercept guidance for aircraft protection against missile attack

被引：6

作者：

Yamasaki, T. ^{[1
]}

Balakrishnan, S. N. ^{[2
]}

Takano, H. ^{[1
]}

机构：

[1] Natl Def Acad Japan, Dept Aerosp Engn, Kanagawa 2398686, Japan

[2] Missouri Univ Sci & Technol, Dept Mech & Aerosp Engn, Rolla, MO USA

来源：

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | 2012年 / 226卷 / G8期

关键词：

missile guidance; geometrical approach; aircraft protection; MOVING TARGET;

D O I：

10.1177/0954410011416053

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This article develops a missile guidance technique for a 'defense missile' trying to protect a cooperative aircraft from guided munitions which have the same thrust and maneuvering capabilities as that of the defense missile. A novel guidance law for the missile-to-missile intercept is developed via a geometrical approach. Performance of the guidance law is analysed in detail and its potential is demonstrated with results from a six degrees-of-freedom simulation and comparison with a conventional guidance law.

引用

页码：1014 / 1028

页数：15