针对多脉冲固体火箭发动机在空空导弹上的应用,以扩大空空导弹的不可逃逸攻击距离作为主要优化目标,同时考虑导弹的最远射程和末端速度,借用遗传优化算法,对双脉冲和三脉冲发动机的综合性能参数进行了优化,得到了导弹综合性能最优的发动机能量分配方案,为空空导弹多脉冲发动机的设计提供了理论依据。

Aiming at the application of multi-pulse solid rocket motor on airborne missile, energy allocation and controlling parameters of double and treble-pulse motor are optimized with the goal of amplifying no escape attack distance, as well as given attention to most far-distance and terminal velocity. According to the optimization, the superb energy allocation object has been acquired. These results offer theoretical evidence for the design of multi-pulse solid rocket motor in airborne missile.