| 基于多学科设计优化技术的导弹方案设计 |
| |
| 引用本文： | 龚春林,谷良贤,孙建勋,陈建江,于红艳. 基于多学科设计优化技术的导弹方案设计[J]. 计算机集成制造系统, 2009, 15(5) |
| |
| 作者姓名： | 龚春林 谷良贤 孙建勋 陈建江 于红艳 |
| |
| 作者单位： | 西北工业大学航天学院,陕西,西安,710072;中国航天科工集团三院三部,北京,100074 |
| |
| 基金项目： | 国家自然科学基金，航天支撑基金 |
| |
| 摘 要： | 多学科设计优化技术当前主要作为传统设计过程的补充,存在较大的局限性.为此,在导弹方案设计全过程引入了多学科并行设计思想,建立了包含两阶段的多学科设计优化流程,在多学科设计阶段形成基准方案,在多学科优化阶段完成基准方案的可行化与最佳化.建立了支持两个设计阶段的五种模型,并分析了基于这些模型描述多学科设计和多学科优化问题的方法.根据所研究的设计流程和建模方法,提出了建立四层体系结构的总体设计软件框架的思想.最后,在Visual C++开发环境下,开发了面向导弹总体设计的多学科设计优化原型系统.
|
| 关 键 词： | 多学科设计优化 导弹 方案设计 设计流程 建模 |
Multidisciplinary design optimization based missile conceptual design |
| |
| GONG Chun-lin,GU Liang-xian,SUN Jian-xun,CHEN Jian-jiang,YU Hong-yan. Multidisciplinary design optimization based missile conceptual design[J]. Computer Integrated Manufacturing Systems, 2009, 15(5) |
| |
| Authors: | GONG Chun-lin GU Liang-xian SUN Jian-xun CHEN Jian-jiang YU Hong-yan |
| |
| Affiliation: | 1.College of Astronautics;Northwestern Polytechnical University;Xi'an 710072;China;2.The Third Research Academy;China Aerospace Science & Industry Corporation;Beijing 100074;China |
| |
| Abstract: | Currently,Multidisciplinary Design Optimization(MDO)technology was served as complement to traditional design,which limited the potential of MDO.To deal with this problem,the concepts of multidisciplinary concurrent design was introduced to the entire process of missile design,and a two-phase design process,including Multidisciplinary Design(MD)and Multidisciplinary Optimization(MO)was presented.The benchmark of missile could be designed in MD phase and optimized in MO phase.Five data models were constructe... |
| |
| Keywords: | multidisciplinary design optimization missile conceptual design design process modeling |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
|
