本文进行了战斗机规避典型的比例导航导弹的几种机动方法的比较研究.战斗机采取持续最大过载转弯、线性加速、最佳规避机动或其组合.对于相对距离、方位角、高度等各种初始条件,计算了可能的规避区域,并进行了讨论,还研究了使导弹丢失目标的规避机动的某些特点.结果表明,每种机动都有其优越的区域.因此驾驶员应根据导弹一战斗机之间的相对几何关系、高度来改变规避策略. In this paper, a comparative study of several maneuvering methods to avoid typical typical scale-up guided missiles by fighter jets is carried out. The fighter adopts continuous maximum overload turning, linear acceleration, optimal avoidance maneuvering or its combination. For initial conditions such as relative distance, azimuth, , Calculated the possible avoidance zones and discussed them and also studied some of the features of avoidance maneuvers that made the missiles miss targets.The results showed that each maneuver had its own superior zone and therefore the pilot should base his missiles on a missile-fighter The relative geometric relationship between the height to change the avoidance strategy.