飞航导弹部位的安排设计研究  

Research on Parts-layout for Winged Missile

作　　者：张涛[1] 常伯浚[1] 董正卫[1] 王江元[1] 

机构地区：[1]中国航天科工集团公司第三研究院,北京100074

出　　处：《战术导弹技术》2005年第1期1-4,共4页Tactical Missile Technology

摘　　要：针对飞航导弹部位安排的手段与方法的现状,提出了-种基于人机交互的智能化布局设计方法.该方法利用三维计算机辅助设计软件,在三维可视化环境下模拟部位安排的全过程,并使用启发式算法优化布局方案以提高工作效率.A visualized intelligent method is presented to resolve the parts layout problem of missile. The 3-D CAD software is used by this method to simulate the progress of layout under 3-D visualization environment , and mathematic model which describes the layout progress is also established. Furthermore, heuristic algorithm is used to optimize the parts layout scheme in order to improve working efficency.

关 键 词：部位安排 布局 启发式算法 三维 

分 类 号：TJ760.2[兵器科学与技术—武器系统与运用工程]