| 导弹姿态控制系统动态测试设计 |
| |
| 引用本文： | 黄金峰,许化龙,蒲源,张斌.导弹姿态控制系统动态测试设计[J].国外电子测量技术,2007,26(7):42-44,54. |
| |
| 作者姓名： | 黄金峰 许化龙 蒲源 张斌 |
| |
| 作者单位： | 1. 第二炮兵工程学院,西安,710025
2. 79106部队60分队,淮安,223311 |
| |
| 摘 要： | 为进行导弹的动态测试,利用PC/104总线组建了高可靠性、高精度的导弹动态测试系统,本文对该系统的软硬件结构与设计方法进行了介绍.该系统能够自行产生测试所需的激励信号,并能够自动完成数据采集、结果处理等任务,极大地提高了动态测试的自动化程度.
|
| 关 键 词： | 导弹姿态控制系统 动态测试 PC/104总线 |
Design of dynamic measurement of missile-attitude-control-system |
| |
| Huang Jinfeng,Xu Hualong,Pu Yuan,Zhang Bin.Design of dynamic measurement of missile-attitude-control-system[J].Foreign Electronic Measurement Technology,2007,26(7):42-44,54. |
| |
| Authors: | Huang Jinfeng Xu Hualong Pu Yuan Zhang Bin |
| |
| Abstract: | In order to test the dynamic performance of missile, a dynamic testing system with high credibility, high precision,which is based on PC/104 bus, is built up. The paper mainly describes the soft-hardware design of the testing system. The testing system can generate actuating signals in time, collect and process the data automatically. Therefore, the automation degree of dynamic measuring is highly increased. |
| |
| Keywords: | missile-attitude-control-system dynamic measurement PC/104 Bus |
| 本文献已被 维普 万方数据 等数据库收录！ |
|
