中远距空空导弹不可逃逸发射区远界的一种计算方法

A Calculation Method for the Far Boundary of Non-escaped Zone of Medium-range and Long-range Air-to-Air Missile

给出一种中远距空空导弹动力射程不可逃逸发射区远界的计算方法,运用这种方法,不可逃逸发射区远界用解析表达式表示,不用搜索不可逃逸发射区边界,只需知道导弹最大飞行距离、飞行时间、目标速度和目标最大机动过载。该方法可推广到考虑目标截获概率的不可逃逸发射区远界的计算。

This paper gives a calculation method for the far boundary of non-escaped zone of medium-range and long-range air-to-air missile. By this method needs only missile maximum flight range, flight time, target speed, target maximum maneuvering overload, and the far boundary of the non-escaped zone can be formulated, the far boundary of the non-escaped zone needs not be searched. The method can be extended to calculate the boundary of non-escaped zone in the condition of considering probability of target acquisition.