| 战术弹飞行力学软件系统设计 |
| |
| 引用本文： | 唐胜景,袁子怀.战术弹飞行力学软件系统设计[J].飞行力学,1997,15(2):81-85. |
| |
| 作者姓名： | 唐胜景 袁子怀 |
| |
| 作者单位： | 北京理工大学!北京，100081 |
| |
| 摘 要： | 从战术弹飞行力学软件系统的设计开发角度，提出了软件系统的设计指导思想，对软件系统基本运行流程进行了分析研究，完成导弹设计不同阶段有关飞行力学问题研究的应用软件设计开发。编制了系统的符号词典和软件文档。在软件系统设计时考虑多种语言程序之间的接口设计及运行环境，并就软件系统进一步开发研究进行了探讨。完成了战术弹飞行力学软件系统的设计。
|
| 关 键 词： | 飞行力学 软件设计 战术导弹 基本结构 |
Design of Flight Mechanics Software System of Tactical Missiles |
| |
| Tang Shengjing, Yuan Zihuai.Design of Flight Mechanics Software System of Tactical Missiles[J].Flight Dynamics,1997,15(2):81-85. |
| |
| Authors: | Tang Shengjing Yuan Zihuai |
| |
| Institution: | Beijing Institute of Technology |
| |
| Abstract: | In this paper, from the angle of the development of the flight mechanics software system of tactical missiles, the design idea is presented. And the basic construction and run flow process of the software system are studied. Some applications programmes in flight mechanics are designed. The software text and signs dictionary of the software system are complied. Interface design and run environment and further development of the software system are researched. Finally, the flight mechanics software system of tactical missiles has been designed. |
| |
| Keywords: | Flight mechanics Software design Tactical missile |
| 本文献已被 CNKI 维普 等数据库收录！ |
