Research on Optimization Strategy of Missile Preliminary Design

作     者：SUZi-jian ZHONGYi-fang 

作者机构：SchoolofMechanicalScience＆EngineeringHuazhongUniversityofScienceandTechnologyWuhan430074.China 

基　　金：Supported by National Doctoral Foundation of china (20010487024) 

出 版 物：《Computer Aided Drafting,Design and Manufacturing》 (计算机辅助绘图设计与制造（英文版）)

年 卷 期：2004年第14卷第1期

页      码：1-6页

摘      要：Two system optimization architectures are proposed for missile system preliminary design, taking into account aerodynamics, weights and sizing, propulsion and trajectory. Approximation methods are investigated in order to reduce problem dimensionality and to improve the efficiency of optimization process.

主 题 词：system optimization missile design approximation missile analysis 

学科分类：08[工学] 082601[082601] 082501[082501] 0826[工学-生物医学工程类] 082602[082602] 0825[工学-环境科学与工程类] 

D　O　I：10.19583/j.1003-4951.2004.01.001

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