| 垂直发射低空超低空防空导弹杀伤区近界研究 |
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| 引用本文： | 陈久生,李向林.垂直发射低空超低空防空导弹杀伤区近界研究[J].现代防御技术,2004,32(5):21-24. |
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| 作者姓名： | 陈久生 李向林 |
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| 作者单位： | 中国航天科工集团公司,二院二部,北京,100854 |
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| 摘 要： | 以低空超低空防空导弹为研究对象,分析了影响其杀伤区近界的主要因素,并针对其采取垂直冷发射的特殊发射方式,应用快速姿态调转的方法,保证了导弹由姿态调转段到制导段的动态误差小。提出了有效的控制方式,进行了大量的典型弹道的数学仿真,从结果来看,这种设计可以将低空超低空防空导弹的杀伤区近界压至接近最小。
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| 关 键 词： | 低空超低空防空导弹 垂直冷发射 侧向直接推力控制 快速控制 |
| 文章编号： | 1009-086X(2004)05-0021-04 |
| 修稿时间： | 2003年8月30日 |
The research of near boundary of damage zone of vertical launching low altitude and zero feet antiaircraft missile |
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| CHEN Jiu-sheng,LI Xiang-lin.The research of near boundary of damage zone of vertical launching low altitude and zero feet antiaircraft missile[J].Modern Defence Technology,2004,32(5):21-24. |
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| Authors: | CHEN Jiu-sheng LI Xiang-lin |
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| Abstract: | The low altitude missile is investigated by considering its special launch mode and the major factors affecting the near boundary of damage zone of missile, small dynamic error attitude maneuver is ensured by applying fast attitude maneuver.An effective controlling method is put forward,and many typical trajectories are calculated.The results show that the near killing range can be compressed to the minimum. |
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| Keywords: | Low altitude and zero feet antiaircraft missile Vertical cold launching Lateral direct thrust control Rapid control |
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