气动力与推力矢量控制近距击顶弹道研究

针对某型反坦克导弹从顶部攻击近距离目标存在的空气动力控制不足的问题，探讨了在导弹初始飞行段采用推力矢量控制的可行性，并对有推力矢量控制的近距击顶飞行弹道进行了分析研究，最，通过计算机数字仿真，进行了弹道飞行仿真计算。结果表明，所提方法改善了导弹飞行弹道特性，提出了导弹机动性能和对近距离目标攻击的效果，并有利于减少最小射程。

The Research on the Short-Range Upper Armor Attack Trajectory by Using Both Atmospheric Force and Thrust Vector Control

To solve the problem of insufficient aerodynamic control on an antitank missile attacking the short range upper armor, the practicability by using thrust vector control (TVC) at the initial stage of the trajectory is researched. The analysis on the trajectory with TVC attacking the short range upper armor is also studied. By means of the computer digital simulation, the characteristics of the flight trajectory are improved. And the missile maneuverability is raised. The effect on the attack on the short range targets is improved. As well as it is good for decreasing the minimum range of the missile.