末段修正弹对脉冲修正力的角运动响应分析

The Analysis on the Angle Motion of Terminal Correct Projectile Responsing to Impulse Corective Force

建立了末段脉冲修正弹在脉冲修正力作用下的角运动数学模型 ,分析了末段修正弹对脉冲修正力的动态响应特性和响应谱 ,给出了对尾翼稳定脉冲修正弹设计有普遍指导意义的结果。

On the basis of setting up the angle motion mathematic model of the terminal correct projectile forced by impulse corrective force, this paper discusses the dynamic response of the terminal correct projectile and response spectrum. The general conclusion that profit to design impulse correct projectile stabilized by taiFl wing is given.