| 遭毁伤导弹弹道特性仿真分析 |
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| 引用本文： | 李向荣,童睆,贺金丽.遭毁伤导弹弹道特性仿真分析[J].战术导弹技术,2009(3):33-36,59. |
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| 作者姓名： | 李向荣 童睆 贺金丽 |
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| 作者单位： | [1]装甲兵工程学院,北京100072 [2]中国兵器工业第208研究所,北京102202 |
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| 摘 要： | 针对结构毁伤引起导弹偏航问题,进行了遭毁伤导弹六自由度全弹道数字仿真分析.建立了导弹六自由度运动方程组,在Matlab/Simulink实时仿真平台下开发了导弹全弹道数字仿真系统,进行了遭毁伤导弹终点状态和飞行轨迹特性分析,研究结果对新型反导技术发展具有一定参考价值.
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| 关 键 词： | 遭毁伤导弹 弹道特性 六自由度运动方程组 |
Simulation Analysis of Ballistic Characteristic of Damaged Missile |
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| Affiliation: | Li Xiangrong, Tong Huan , He Jinli (1. Academy of Armored Force Engineering, Beijing 100072, China; 2. No. 208 Institute of China Ordnance Industry, Beijing 102202, China) |
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| Abstract: | Aiming listic simulation of at the problem of construct damage resulting in the yaw of missile, six-free-degree baldamaged missile is carried out. Six-free-degree movement equations for the missile are established, and ballistic simulation system for the missile is developed by real-time simulation platform of Matlab/Simulink. Based on the simulation results, terminal state and flight track of damaged missile are analyzed. This is significant to new anti-missile technology development. |
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| Keywords: | damaged missile ballistic characteristic six-free-degree movement equations |
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