| 基于侧向推力矢量控制的防空导弹抗击TBM问题的研究 |
| |
| 引用本文： | 程彦杰,王学奎,覃天. 基于侧向推力矢量控制的防空导弹抗击TBM问题的研究[J]. 舰船电子工程, 2011, 31(1): 41-42,82 |
| |
| 作者姓名： | 程彦杰 王学奎 覃天 |
| |
| 作者单位： | 防空兵指挥学院,郑州,450052 |
| |
| 摘 要： | 针对战术弹道导弹对防空侦察预警系统的合理部署进行了分析，计算出了反TBM防御系统拦截过程中的弹道预测及预定拦截点，为防空导弹火力单元提供较精确的TBM弹道诸元及落点预测值，基于侧向推力矢量控制对TBM实施拦截，达到末端有效抗击TBM的目的。
|
| 关 键 词： | 战术弹道导弹 侧向推力矢量 弹道 防空导弹 |
Study of Resisting TBM Problem for Antiaircraft Missile Based on the Thrust Vector Control of Side Direction |
| |
| Cheng Yanjie,Wang Xuekui,Qin Tian. Study of Resisting TBM Problem for Antiaircraft Missile Based on the Thrust Vector Control of Side Direction[J]. Ship Electronic Engineering, 2011, 31(1): 41-42,82 |
| |
| Authors: | Cheng Yanjie Wang Xuekui Qin Tian |
| |
| Affiliation: | Cheng Yanjie Wang Xuekui Qin Tian(Air Defense Forces Command Academy,Zhengzhou 450052) |
| |
| Abstract: | Aimming at tactical ballistic missile,the reasonable disposition for air defence reconnoiter of early warning system is analysed.In order to offer more accurate TBM trajectory various points and placement forecast value,the defence systematic course of intercepting and the ballistic forecast are calculated.Then based on the thrust vector control of side direction,reach the purpose of resisting TBM efficiently at the end. |
| |
| Keywords: | tactical ballistic missile thrust vector of side direction trajectory antiaircraft missile |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
