发射空对空导弹时目标进入角的确定

Determination of the Target Approaching Angle while Launching Air-to-Air Missiles

提出了一种确定目标进入角的原理和方法 ,这种原理和方法具有较高的计算精度和实时性 ,易于工程实现 ,可用于机载火力控制系统完成空对空导弹允许发射区计算。

This paper puts forward a method to determine the approaching angle of the target.This method are with a high accuracy and real time application,and can be applied in the calculation of allowable launching area of air to air missile in air borne fire control system.