基于侧向推力矢量控制的防空导弹抗击TBM问题的研究  

Study of Resisting TBM Problem for Antiaircraft Missile Based on the Thrust Vector Control of Side Direction

作　　者：程彦杰[1] 王学奎[1] 覃天[1] 

机构地区：[1]防空兵指挥学院,郑州450052

出　　处：《舰船电子工程》2011年第1期41-42,82,共3页Ship Electronic Engineering

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。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 defenee systematic course of intercepting and the ballistic forecast are calculated. Then based on the thrust vector control of side di- rection, reach the purpose of resisting TBM efficiently at the end.

关 键 词：战术弹道导弹 侧向推力矢量 弹道 防空导弹 

分 类 号：E927[军事—军事装备学]