Research on Optimization Strategy of Missile Preliminary Design

作     者：SUZi-jian ZHONGYi-fang 

作者机构：SchoolofMechanicalScience＆EngineeringHuazhongUniversityofScienceandTechnologyWuhan430074.China 

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      面：1-6页

学科分类：082601[工学-武器系统与运用工程] 08[工学] 082501[工学-飞行器设计] 0826[工学-兵器科学与技术] 082602[工学-兵器发射理论与技术] 0825[工学-航空宇航科学与技术] 

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

主　　题：system optimization missile design approximation missile analysis 

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.