| 机动弹头弹道导弹六自由度建模与仿真 |
| |
| 引用本文： | 郭杨,王仕成,蒲源. 机动弹头弹道导弹六自由度建模与仿真[J]. 制导与引信, 2007, 28(2): 13-15,41 |
| |
| 作者姓名： | 郭杨 王仕成 蒲源 |
| |
| 作者单位： | 第二炮兵工程学院301教研室,陕西,西安,710025 |
| |
| 摘 要： | 针对机动弹头弹道导弹飞行的特点,应用六自由度一体化建模理论建立了较为精确的数学模型,并对其进行了仿真,给出了部分仿真结果。结果表明,所建立的六自由度运动模型能够充分表征其飞行特点,可在此基础上进一步进行系统分析、质量评估等工作。
|
| 关 键 词： | 机动弹头 导弹 仿真 |
| 文章编号： | 1671-0576（2007）02-0013-03 |
| 修稿时间： | 2007-04-14 |
Six Degree Modeling and Simulation of the Ballistic Missile with Maneucvering Reentry Vehicle |
| |
| GUO Fang,WANG Shi-cheng,PU Yuan. Six Degree Modeling and Simulation of the Ballistic Missile with Maneucvering Reentry Vehicle[J]. Guidance & Fuze, 2007, 28(2): 13-15,41 |
| |
| Authors: | GUO Fang WANG Shi-cheng PU Yuan |
| |
| Abstract: | Considering flying characteristic of the ballistic missile maneucvering reentry vehicle,applies the integrated modeling theory of six degree and simulates.It is can be infered by consequence that the model represent the characteristic of missile flying sufficiently,system analysis,quality evluation and some other work can be gone along next. |
| |
| Keywords: | maneuvering reentry vehicle missile simulation |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
|
