摘要
高速导弹采用红外成像末制导技术实现直接碰撞目标是精确制导武器发展的主要方向。从高速导弹采用红外成像末制导技术所面临的新问题出发，研究了气动光学效应规律，进行气动光学效应的校正对高速导弹光学头罩的设计、提高导引头对目标探测的信噪比以及提高末制导精度和抗干扰能力具有重要作用。
It is one of the main methods relating to guidance on the missile guide header for a high altitude hypersonic endoatmospheric missile to kill a target directly with the infrared image guide tech- nology. In this paper, it is introduced firstly that same new problems are resulted from hypersonic missile to be employed infrared image guide technology . Then the importance to research aero-optical effect properties is analysed and illustrated and aero-optical effects rectified is of great significance .
出处
《红外与激光工程》
EI
CSCD
1998年第1期42-43,51,共3页
Infrared and Laser Engineering
关键词
精确制导
红外成像
气动光学
导弹
Precision guidance Infrared image Aero-optical effects
