摘要
为了攻击武装直升机，一般要求导弹的速度和过载上应远高于直升机，特别是在速度方面。由于图像制导导引头的最大识别距离一般远小于导弹的最大射程，因此需要通过在飞行过程中导引头的扫描搜索来发现目标。但飞行速度太高对搜索目标不利。为此，本文提出了一种速度和动力方案，较好地满足了这两方面的要求。
To attack armed helicopter, the speed
and overload of missile,especially the former,should be far higher than those of helicopter should.
Since the image seeker's maximum distance for target identification is far short than the maximum
range of the missile,the seeker should search targets during flight.But high speed of missile is
disadvantageous to searching target.This paper gives a velocity and power program to meet the
needs of these two aspects. [
出处
《弹箭与制导学报》
CSCD
北大核心
1999年第2期26-30,共5页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
图像制导
反直升机导弹
设计
Image guidance
Anti-Helicopoter Missile,Missile Design
