摘要
简要介绍了弹道导弹的发展历史 ,说明了经典弹道导弹的设计方法以及增加附加约束条件后的解决途径 .以此为基础编制了弹道导弹总体参数的计算机辅助设计软件 ,并针对一个选定的设计实例 ,计算了优化设计参数和增加附加约束条件后的设计结果 。
Traditional methods of ballistic missile design are introduced following a brief introduction of its development history,and an approach to meet extra constrains in the draft design process is selected.Based on theoretical analysis,a computer aided design software package is coded and an example ballistic missile is designed.Comparing the primary parameters of different designs with and without extra constrains,its impact in draft ballistic missile design is analyzed.
出处
《战术导弹技术》
2003年第6期42-47,共6页
Tactical Missile Technology
关键词
飞行器设计
弹道导弹
约束条件
计算机辅助设计
flight vehicle design
ballistic missile
constrains
computer aided design
