某型推力矢量控制空空导弹攻击区仿真研究

Research on the Attack Zone Simulation of a Kind of Air-to-air Missile with Thrust Vector Control

在分析某型导弹机械扰流板式推力矢量控制基本原理的基础上,建立了推力矢量/气动力复合控制的数学模型。利用Matlab/Simulink工具对某型空空导弹攻击区进行仿真解算,绘制出几种不同作战条件下的导弹攻击区,并将带推力矢量控制与不带推力矢量控制的导弹攻击区进行对比,分析确定了推力矢量控制对导弹攻击区的影响。

Firstly, this paper analyses the working principles of mechanical spoiler which is a kind of thrust vector control. and rhea establishes the mathematical simulation model of a kind of TVC/ADC（thruster vector control/air dynamic control）missile. Secondly. using matlab/simulink, it simulates the air-to-air missile and calculates it＇s attack zone. and draws auack zones in some different conditions.Lastly. by contrasting two kind of air-to-air missiles＇ attack zones, with and will,out thrust vector, it analyses the effects of thrust vectoring control on air-to-air missile＇s attack zone.