基于KBE的导弹结构快速设计系统的研究与开发  

Research and Development of Rapid Design System for Missile Based on KBE Method

作　　者：陈鑫[1] 刘献伟[1] 偏晓鹏[1] 

机构地区：[1]中国空空导弹研究院,洛阳471009

出　　处：《航空制造技术》2016年第6期76-79,共4页Aeronautical Manufacturing Technology

摘　　要：武器装备的快速性设计和优化是提升自主创新的重要手段。导弹结构快速设计系统是针对导弹结构设计复杂性和反复性的特点,基于KBE的理念,借助UG平台,融入设计规则和经验教训的设计平台。通过该平台的开发,实现了导弹结构的自动式建模和自导式建模,以及对模型的分析计算,生成可脱离该系统进行单独修改设计的导弹各舱段的知识特征模型,从而满足了快速性和重复优化设计的需要,大大提高了设计的效率。The rapid design and optimizing method for weapons is an important means to enhance independent inno- vation competence. This rapid design system of missile structure is a very useful tool which makes use of UG software and aims at the complicacy and repeat of design experience. This system can complete automatic modeling and model analysis, and then can create knowledge characteristic model which can disengage from system and be modified for each cabin of missile. The system can meet the needs of rapid and repeat design so that can improve design efficiency.

关 键 词：KBE 快速设计 导弹结构 知识特征模型 

分 类 号：TP311.52[自动化与计算机技术—计算机软件与理论]