一种新型弹体结构导弹动力学方程的建立

Foundation of Kinetic Equations for Missile with A New Type of Body Structure

文中提出了一种新型导弹弹体结构,该种结构的弹体一部分保持滚转稳定,另一部分可绕弹体纵轴自由旋转;并推导了该种弹体结构的动力学方程。该种弹体结构可充分结合滚转导弹和非滚转导弹各自的优点,在某些应用场合可解决传统导弹的一些固有难题。

A new type of missile body structure was brought forward,which consisted of two parts:one with roll control and the other with free spin.Then kinetic equations for missile with it were founded.This type of missile body structure can com- bine perfectly respective advantages of rolling missiles and non-rolling missiles.In some case,it can be used to solve some inher- ent difficult problems with regard to traditional missiles.