| 反向设计方法在防空导弹中的应用研究 |
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| 引用本文： | 郑咏岚,王友进,邹忠望,杨存富.反向设计方法在防空导弹中的应用研究[J].现代防御技术,2011,39(1):1-11,28. |
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| 作者姓名： | 郑咏岚 王友进 邹忠望 杨存富 |
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| 作者单位： | 北京电子工程总体研究所,北京,100854 |
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| 摘 要： | 对反向设计方法在防空导弹中的应用进行初步探讨。重点讨论了导弹总体、气动以及动力系统之间的关系。针对国外典型防空导弹,建立了反向设计模型,结合弹道仿真研究了国外典型防空导弹的战技指标、关键技术以及发展趋势。
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| 关 键 词： | 反向设计方法 防空导弹 弹道仿真 |
Research on the Application of Reverse Design Method in Antiaircraft Missile |
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| ZHENG Yong-lan,WANG You-jin,ZOU Zhong-wang,YANG Cun-fu.Research on the Application of Reverse Design Method in Antiaircraft Missile[J].Modern Defence Technology,2011,39(1):1-11,28. |
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| Authors: | ZHENG Yong-lan WANG You-jin ZOU Zhong-wang YANG Cun-fu |
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| Institution: | ZHENG Yong-lan,WANG You-jin,ZOU Zhong-wang,YANG Cun-fu (Beijing Inst.of Electronic System Engineering,Beijing 100854,China) |
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| Abstract: | The application technique of reverse design method in antiaircraft missile was researched.The relationship between missile system and aerodynamics and engine system was discussed.Model of reverse design for foreign representative antiaircraft missiles was modeled.Tactical and technical performance and key technology and development trend of foreign representative antiaircraft missile was researched by simulation. |
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| Keywords: | reverse design method antiaircraft missile trajectory simulation |
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