Journal of Projectiles, Rockets, Missiles and Guidance >
Missile Configuration Parameters Design Based on Multidisciplinary Design Optimization
Received date: 2009-10-20
Online published: 2025-05-28
In order to improve the performance of hypervelocity antitank missile, the method of overall parameter analysis and optimization using multidisciplinary design optimization (MDO) technology was studied, the MDO model and integrated simulating system was founded, and overall parameter was optimized. The results show that missile performance can be effectively improved based on the application of MDO in overall design.
Key words： hypervelocity; antitank missile; overall design; parameter optimization; MDO
ZHOU Jian , ZHOU Yuhong , QIANG Jinhui , WANG Zhuping . Missile Configuration Parameters Design Based on Multidisciplinary Design Optimization[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(4) : 19 -22 . DOI: 10.15892/j.cnki.djzdxb.2010.04.042
| [1] | 王振国, 陈小前, 罗文彩, 等. 飞行器多学科设计优化理论与应用研究[M]. 北京: 国防工业出版社, 2006: 27- 45. |
| [2] | 钟毅芳, 陈柏鸿, 王周宏. 多学科综合优化设计原理与方法[M]. 武汉: 华中科技大学出版社, 2006: 17- 25. |
| [3] | 龚春林, 谷良贤, 袁建平. 基于系统分解的多学科集成设计过程与工具[J]. 计算机集成制造系统, 2006, 12(3): 334- 338. |
| [4] | 谷良贤, 温炳恒. 导弹总体设计原理[M]. 西安: 西北工业大学出版社, 2004: 279- 323. |
| [5] | 周健, 姜晓菡, 周喻虹. 基于 OPTIMUS 的控制系统参数优化计算[J]. 弹箭与制导学报, 2008, 28(3): 13- 14. |
/
| 〈 |
|
〉 |