摘要
简要分析了反辐射武器攻击多点源诱偏系统飞行轨迹,判断其最终落点只与空间分离点位置及反辐射武器自身运动参数有关,提出了利用飞艇搭载反辐射导引头模拟反辐射武器攻击的试验方法,给出了空间分离点位置计算公式以及影响空间分离点位置的参数,对如何确定诱骗系统的诱骗能力或是反辐射武器抗诱偏能力的试验方法具有一定的借鉴作用。
It is briefly analyzed that the track of the anti-radiation weapons attacking the muhi - point decoying system. And the conclusion is deduced that the final impact point of the anti-radiation weapon is decided only by the position of the critical point and the motion parameters of the anti-radi- ation weapon itself. And the test method of using airship carrying a passive radar seeker （PRS） is proposed to simulate the anti-radiation weapon attacking. Then the calculation formula and the effect- ing factors of the critical point are given. And the research result could be a help for the determination of the test method of checking the anti-decoying capability of the anti-radiation weapons and the decoying capability of the decoying system.
出处
《电子信息对抗技术》
2010年第1期56-59,共4页
Electronic Information Warfare Technology
关键词
飞艇
反辐射武器
试验方法
airship
anti-radiation weapons
test method
