摘要
根据多学科设计问题系统分析的特点,提出基于系统分解的多学科集成设计过程。针对此设计过程,从支持独立的学科分析工具着手,提出了层次式多学科集成管理模型。在此基础上,采用面向对象技术和COM接口技术,开发了支持多学科集成设计的工具M DOF(M u ltid isc ip linary D es ign O ptim izationF ram ew ork)。在M DOF中,对包含四个学科的运载火箭设计问题进行集成和优化。
According to the characteristics of muhidisciplinary integrated Analysis, an integrated design process based on system decomposition was presented, which avoid entire system iteration during system analysis. An hierarchical discipline integration and management model applied during this design process was presented. After this work, a multidisciplinary integrated design tool-MDOF (Multidisciplinary Design Optimization Framework)was developed applying the Object-Oriented (OO) and Common Object Module(COM) software development technologies within Visual C++ 6. 0. At Last, a muhidisciplinary design problem of launch rocket including four disciplines was integrated and optimized in MDOF.
出处
《弹箭与制导学报》
CSCD
北大核心
2005年第3期98-101,114,共5页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
国家863计划(项目编号2004AA721052)
西北工业大学博士论文创新基金(项目编号CX200404)
关键词
多学科集成设计
系统分解
工具
优化
multidisciplinary integrated design
system decomposition
tool
optimize