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插件式可重配导弹总体设计集成优化框架研究
引用本文:梅珊,赵雯,朱一凡,王维平. 插件式可重配导弹总体设计集成优化框架研究[J]. 系统仿真学报, 2006, 18(12): 3564-3567,3569
作者姓名:梅珊  赵雯  朱一凡  王维平
作者单位:国防科技大学信息系统与管理学院系统工程系,湖南长沙,410073
摘    要:导弹武器系统总体设计过程的复杂性,对于模型和应用集成、方案优化提出了更高要求。在虚拟样机、多学科设计优化、应用集成等技术的基础上,提出一种插件式可量配导弹总体设计集成优化框架,并对其中一些关键技术进行探讨,最后实现了一个原型系统。

关 键 词:虚拟样机  多学科设计优化  集成优化框架  导弹总体设计
文章编号:1004-731X(2006)12-3564-04
收稿时间:2005-12-18
修稿时间:2005-12-182006-04-18

Research of Plug-in based Configurable Missile Design, Integration and Optimization Framework
MEI Shan,ZHAO Wen,ZHU Yi-fan,WANG Wei-ping. Research of Plug-in based Configurable Missile Design, Integration and Optimization Framework[J]. Journal of System Simulation, 2006, 18(12): 3564-3567,3569
Authors:MEI Shan  ZHAO Wen  ZHU Yi-fan  WANG Wei-ping
Affiliation:National University of Defense Technology. Changsha 410073, China
Abstract:The integrated design of missile weapon system is quite complicated, which calls for more powerful model integration, application integration and plan optimization. On the basis of the technology of Virtual Prototype, Multidisciplinary Design Optimization and application integration etc, a Plug-in based Configurable Missile Design, Integration and Optimization Framework is brought forward, and some key problems of the Framework are discussed. Finally, a prototype system is implemented.
Keywords:virtual prototype   multidisciplinary design optimization   integration and optimization framework   the integrated design of missile weapon system
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