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旋转导弹掠飞击顶弹道控制研究
Research on the Trajectory Control of Hedgehopping Upper Armor Attack of a Spinning Missile
【摘要】 文中以某改型反坦克导弹为例,针对攻击坦克顶部装甲,探讨掠飞击顶弹道控制有关问题。采用脉冲发动机推力矢量控制实现导弹弹体转弯,研究推力矢量控制力与弹体姿态转动角速度、落角及过载的关系,并对旋转反坦克导弹的控制力工作时间及掠飞高度选择等方面进行了分析和研究。
【Abstract】 In this paper,for the attacking on the tank upper armor,as an example of a revised antitank missile,some key questions for the trajectory control of hedgehopping upper armor attack are studied. The thrust vector control(TVC)is used by means of the small engines to control the missile turning. The relations between the thrust vector control forces and an angular speed of a body attitude,an impact angle and a load are discussed. Also the working time of the control forces and the selection of the hedgehopping height of the spinning missile are researched.
【关键词】 反坦克导弹;
击顶弹道;
推力矢量控制;
【Key words】 antitank missiles; trajectory for attacking on upper armor; TVC;
【Key words】 antitank missiles; trajectory for attacking on upper armor; TVC;
- 【文献出处】 弹箭与制导学报 ,Journal of Projectiles.Rockets.Missiles and Guidance , 编辑部邮箱 ,2004年03期
- 【分类号】TJ761.12
- 【被引频次】3
- 【下载频次】292