某型空地电视制导导弹可发射域研究

The Research of a Certain TV-Guided Missile's Launcn Area

分析了某型空地电视制导导弹的制导原理,建立了该型电视制导导弹空间六自由度运动方程组,给出了该型导弹控制系统数学模型和控制信号的形成模型。用最小二乘法拟合技术建立了空地电视制导导弹的气动力参数模型,对该型空地电视制导导弹的可发射域进行仿真计算,分析了影响可发射域的因素。

The guidance principle of a certain air-to-ground TV-guidance missile is analysed.The missile's six- freedom space movement differential equations is established,and the control system mathematical model and control signal formation model are presented.The lease twain-multiplication approach technology is taken use of to get the model of pneumatic force.The missile's launch area is provided by calculation and simulation,at the same time.the impact factors are analysed.