基于物理规划的拦截弹反设计优化方法

王祖尧; 李晓斌; 张为华

基于物理规划的拦截弹反设计优化方法

1.
国防科技大学航天与材料工程学院, 长沙 410073
2.
92941部队葫芦岛 125000

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出版历程
- 收稿日期: 2006-12-01
- 修回日期: 2007-04-29
- 刊出日期: 2007-12-28

Optimization of inverse design of antimissile interceptor based on physical programming

1.
College of Aerospace and Material Engineering, National University ofDefense Technology, Changsha 410073, China
2.
92941 Unit, Huludao 125000, China

摘要

摘要: 提出了基于物理规划的拦截弹反设计优化方法,建立了拦截弹多学科系统分析模型,依据文献报道的拦截弹技术参数,通过技术分析,将拦截弹作为"灰箱"系统处理,通过反设计优化研究,得到了合理的拦截弹性能参数.
- 航空、航天推进系统 /
- 拦截弹 /
- 反设计优化 /
- 物理规划
Abstract: The optimization method for inverse design of antimissile interceptor was put forward based on physical programming,and a multidisciplinary system analysis model was established.According to the performance parameters of antimissile interceptor in the literature,the antimissile interceptor was disposed as a "greybox" system.The performance parameters of antimissile interceptor were gained through research of inverse design optimization.
- aerospace propulsion system /
- antimissile interceptor /
- inverse design optimization /
- physical programming

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参考文献(8)

[1]	周睿.反设计的运用及现实意义[J].包装工程,2006,27(1):206-208.ZHOU Rui.Application of inverse design and its practical meaning[J].Packaging Engineering,2006,27(1):206-208.
[2]	Wang X,Damodaran M,Lee S L.Inverse transonic airfoil design using parallel simulated annealing and computational fluid dynamics[J].AIAA Journal,2002,40(4):791-794.
[3]	魏志军,张平,方蜀州."爱国者PAC23"型导弹主发动机装药药型反设计[J].固体火箭技术,2004,27(2):114-116.WEI Zhijun,ZHANG Ping,FANG Shuzhou.Analysis on the grain design of the solid rocket motor for PATRIOT PAC-3 missile[J].Journal of Solid Rocket Technology,2004,27(2):114-116.
[4]	胡泽保,张振鹏."标准-3"拦截弹发动机参数复原设计[R].上海:中国宇航学会固体火箭推进专业委员会第21届年会,2004.
[5]	Messac A.Physical programming:effective optimization for computational design[J].AIAA Journal,1996,34(1):149-158.
[6]	李晓斌,张为华,王中伟.基于物理规划的固体火箭发动机不确定性优化设计[J].固体火箭技术,2006,29(3):165-168,173.LI Xiaobin,ZHANG Weihua,WANG Zhongwei.Uncertainty optimization design of solid rocket motor based on physical programming[J].Journal of Solid Rocket Technology,2006,29(3):165-168,173.
[7]	杨维维,陈小前,李晓斌,等.通用导弹气动力计算软件DATCOM的开发与校验[J].固体火箭技术,2006,29(3):161-164.YANG Weiwei,CHEN Xiaoqian,LI Xiaobin,et al.Development and verification of a common software DATCOM for missile aerodynamic force calculation[J].Journal of Solid Rocket Technology,2006,29(3):161-164.
[8]	温羡峤,郑慧敏.美国战区高空防御系统(THAAD)分析[J].现代防御技术,2006,34(4):1-15.WEN Xianqiao,ZHENG Huimin.Theater high altitude area defense analysis[J].Modern Defence Technology,2006,34(4):1-15.