摘要
通过对机载拖曳式诱饵干扰的原理及使用拖曳式诱饵干扰前后飞机被击毁概率的计算模型进行了仿真计算及分析,指出了有源拖曳式诱饵干扰存在的圆锥模糊区,提出了针对机载拖曳式诱饵干扰进行反干扰的建议。
On the basis of the principle of airborne towed decoys jamming,this paper compute the missile hitting proba- bility when enemy fighter using the airborne towed decoys and when airborne towed decoys is not used,point out the ta- per inefficacy area when enemy aircraft using the airborne towed decoys,propose some suggestions on the opposing air- borne towed decoys jamming.
出处
《弹箭与制导学报》
CSCD
北大核心
2006年第S8期876-878,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
机载拖曳式诱饵
击毁概率
圆锥模糊区
airborne towed decoys
hitting probability
taper inefficacy area