反向设计方法在防空导弹中的应用研究  

Research on the Application of Reverse Design Method in Antiaircraft Missile

作　　者：郑咏岚[1] 王友进[1] 邹忠望 杨存富[1] 

机构地区：[1]北京电子工程总体研究所,北京100854

出　　处：《现代防御技术》2011年第1期1-11,28,共12页Modern Defence Technology

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。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.

关 键 词：反向设计方法 防空导弹 弹道仿真 

分 类 号：TJ761.13[兵器科学与技术—武器系统与运用工程]