| 可控翼伞导航控制系统的设计 |
| |
| 引用本文： | 李哲,顾正铭.可控翼伞导航控制系统的设计[J].航天返回与遥感,2000(2). |
| |
| 作者姓名： | 李哲 顾正铭 |
| |
| 作者单位： | 北京空间机电研究所，北京空间机电研究所 北京 100076，北京 100076 |
| |
| 摘 要： | 文章详细介绍了翼伞自动导航控制系统采用的导航算法、系统构成、硬件电路及导航控制软件的设计。并且结合空投试验的数据及对比国外类似系统的设计,对系统存在的不足及改进方法提出了自己的意见。
|
| 关 键 词： | 翼伞 GPS 嵌入式工控机 导航算法 |
DESIGN OF NAVIGATION CONTROL SYSTEM FOR PARAFOIL |
| |
| Li Zhe Gu Zhengming.DESIGN OF NAVIGATION CONTROL SYSTEM FOR PARAFOIL[J].Spacecraft Recovery & Remote Sensing,2000(2). |
| |
| Authors: | Li Zhe Gu Zhengming |
| |
| Abstract: | The paper introduces the design of navigation control system for parafoil, which includes thd navigarion arithmetic, system structure, hardware circuit and navigation control software. According to the data from airdrop test and comparing with the similar systems of foreign countries, it brings out some advice on improving thd system. |
| |
| Keywords: | Parafoil GPS Inbuilt engingeering control machine Navigation arithmetic |
| 本文献已被 CNKI 等数据库收录！ |
