空空拦射导弹火控系统飞行方案建模与仿真

Modelling and Simulation of the Flight Plan for an Air-to-Air Interception Missile Fire Control System

针对空空拦射导弹火控系统的飞行试验方案建模与仿真,提出了合理的建模假设,建立了一系列关于载机、目标机及导弹在导弹发射前、发射后整个靶试过程中的运动诸元解算模型,分析了飞机运动方程与火控系统攻击需求之间的相对关系,进行了仿真计算,并将仿真计算结果与实际工程试飞应用结果进行了对比,取到了满意的效果。

Focusing on the modelling and simulation for an air-to-air interception missile fire control system, this paper puts out a reasonable modelling plan, builds a multi-elements arithmetic model of the movement concerning the carrier, target drones, and the missile before and after its launching, analyes the relative relationship between the kinematic equation of the aircraft and the attack requirements of the fire control system, and carries out the simulation calculations. Furthermore, comparisons between the calculating results of simulations and many successful flight test results have also been made, and the satisfied results have been achieved.