本文进行了歼击机对付典型的比例导引导弹的几种躲避机动的比较研究。飞机采取了持续的最大 G 转弯、线性加速及最佳躲避机动或其组合。计算和讨论了与相对距离、方位角及高度有关的各种初始条件下的可能躲避距离。还研究了试图摆脱导弹锁定的一些躲避机动特性。结果表明,每种机动都有它的有利区域,因此,驾驶员应按飞机一导弹的相对几何位置和高度来变化躲避战术。 This article has carried on the fighter to deal with the typical proportion guided missile’s several kinds to evade the maneuver comparative research. The aircraft took a sustained maximum G-turn, linear acceleration and optimal avoidance maneuver or combination thereof. The possible evasion distances for various initial conditions related to relative distance, azimuth and altitude are calculated and discussed. Some evasion maneuvers trying to get out of the missile lock were also studied. The results show that each maneuver has its own favorable area, so pilots should change avoidance tactics in terms of the relative geometric position and altitude of the aircraft-to-missile.