| 基于脉冲点火弹头平面机动的被动段弹道设计 |
| |
| 引用本文： | 张广明,高普云,冯志刚,唐乾刚.基于脉冲点火弹头平面机动的被动段弹道设计[J].弹道学报,2009,21(2). |
| |
| 作者姓名： | 张广明 高普云 冯志刚 唐乾刚 |
| |
| 作者单位： | 1. 国防科学技术大学,航天与材料工程学院,长沙,410073;二炮装备部,北京,100083
2. 国防科学技术大学,航天与材料工程学院,长沙,410073 |
| |
| 摘 要： | 机动突防是提高弹道导弹生存能力的重要手段之一.提出了一种基于脉冲点火的弹头平面机动的被动段弹道设计一般方法,该方法不同于经典方法和其他弹头机动弹道设计方法.由这种方法设计出来的弹道是由几条曲线段拼接而成.推出了限制点火约束方程的一种更简单形式,描述了解限制点火约束方程的方法,给出了2个仿真实例.仿真结果显示基于脉冲点火的弹头平面机动可提高导弹抵御反导系统的能力,证明了该方法的可行性.
|
| 关 键 词： | 弹道导弹 弹道 被动段 突防 脉冲点火 |
Design of Trajectory of the Maneuver of Warhead in a Plane Based on Impulse Firing in the Passive Curve |
| |
| ZHANG Guang-ming,GAO Pu-yun,FENG Zhi-gang,TANG Qian-gang.Design of Trajectory of the Maneuver of Warhead in a Plane Based on Impulse Firing in the Passive Curve[J].Journal of Ballistics,2009,21(2). |
| |
| Authors: | ZHANG Guang-ming GAO Pu-yun FENG Zhi-gang TANG Qian-gang |
| |
| Affiliation: | ZHANG Guang-ming1,2,GAO Pu-yun1,FENG Zhi-gang1,TANG Qian-gang1(1.School of Astronautical , Materials Engineering,NUDT,Changsha 410073,China,2.The Equipment Department of the Second Artillery,Beijing 10083,China) |
| |
| Abstract: | The missile maneuver is an important method to increase survivability of missile.A general method of the trajectory design of the maneuver of warhead in a plane based on the impulse firing in the passive curve was presented,which is different from the classical method and other methods of maneuver trajectory design of the missile.The trajectory designed by the method consists of several curves.The simpler constraint equations of restricting impulse firing were found.The method of solving the constraint equa... |
| |
| Keywords: | ballistic missiles trajectory passive curve penetration impulse firing |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
|
