空空导弹可攻击区的递推算法研究

A Improving Recursive Method of Fitting A/A Missile Launch Envelops

文中提出了一种具有可信度的递推拟合算法。该方法先对标准弹道表进行多元插值扩充,并且根据扩充后各条弹道与标准弹道表距离赋予其可信度的值,然后运用文中提出的递推算法进行计算,得到导弹可攻击区计算式。仿真计算表明文中提出的方法是可行的并能够有效的改善标准弹道表外数据病态现象。

This paper presents a missile launch envelops fitting method.Firstly.the method widen the given trajectory table.Secondly.It gives a reliability to trajectory.Lastly,It fits missile launch envelops with taking into account relia- bility.The emulation shows that this method is feasible.The result have been applied to the fire control design of one aircraft.