| 便携式防空导弹拦截巡航导弹效能仿真研究 |
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| 引用本文： | 迟刚,王树宗. 便携式防空导弹拦截巡航导弹效能仿真研究[J]. 系统工程与电子技术, 2004, 26(2): 261-263 |
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| 作者姓名： | 迟刚 王树宗 |
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| 作者单位： | 海军工程大学研究生4队,湖北,武汉,430033 |
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| 摘 要： | 制定了拦截规则,部署了火力分配方案,对某型便携式防空导弹武器系统在其作战空域内拦截巡航导弹的实战环境进行了仿真研究,并得出了较为可信的结论:只有增加系统的快速反应能力,提高防空导弹的飞行速度,并尽可能地减小其拦截巡航导弹时的高度差和航路捷径,系统的作战效能才能得到最大限度的提高。
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| 关 键 词： | 防空导弹 巡航导弹 数学模型 仿真 |
| 文章编号： | 1001-506X(2004)02-0261-03 |
| 修稿时间： | 2002-09-06 |
Research of anti-cruise missile efficiency simulations of the man-portable air defense missile |
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| CHI Gang,WANG Shu-zong. Research of anti-cruise missile efficiency simulations of the man-portable air defense missile[J]. System Engineering and Electronics, 2004, 26(2): 261-263 |
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| Authors: | CHI Gang WANG Shu-zong |
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| Abstract: | The defence problem of cruise missile is becoming more and more important. After establishing the interception rules and deploying the fire distribution scheme one certain weapon system of man-portable air defence missile has carried out simulation research under the real environment of anticruise missile in air fight area. The obtained comparable credible couclusions are the following: only if the fast-reaction ability of this system is increased and the flying speed of air defence missile is enhanced, and when the cruisue missile is intercepted the height differences and fairway crossout are decreased as possible, then the system operational efficiency can be euhanced to maximum limitation. |
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| Keywords: | air defense missile cruise missile mathematical models simulations |
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