| 基于LabWindows/CVI的无人机燃油组件测试系统的开发 |
| |
| 引用本文： | 王锐,雷金奎. 基于LabWindows/CVI的无人机燃油组件测试系统的开发[J]. 测控技术, 2008, 27(2): 41-44 |
| |
| 作者姓名： | 王锐 雷金奎 |
| |
| 作者单位： | 西北工业大学,电子信息学院,陕西,西安,710072;西北工业大学,第365研究所,陕西,西安,710072 |
| |
| 摘 要： | 在虚拟仪器技术的基础上,对无人机燃油组件测试系统进行了设计和研究.阐述了该测试系统搭建的全过程和工作原理.采用LabWindows/CVI7.0作为该测试系统的软件开发平台,选定CompactPCI结构为本系统的硬件构成方案.试验结果表明基于虚拟仪器开发的无人机燃油组件测试系统能够满足工程和测试技术的要求.
|
| 关 键 词： | 虚拟仪器 燃油组件 LabWindows/CVI IIR滤波器 |
| 文章编号： | 1000-8829（2008）02-0041-04 |
| 收稿时间： | 2007-03-28 |
| 修稿时间： | 2007-03-28 |
Lab Windows/CVI-Based UAV Fuel Assembly Test System Development |
| |
| WANG Rui,LEI Jin-kui. Lab Windows/CVI-Based UAV Fuel Assembly Test System Development[J]. Measurement & Control Technology, 2008, 27(2): 41-44 |
| |
| Authors: | WANG Rui LEI Jin-kui |
| |
| Abstract: | The UAV fuel assembly system for the design and test research which is based on the virtual instrument technology is stated, and the entire process of the test system structure and working principle is also described. LabWindows/CVI7. 0 is used as the test system software development platform, and CompactPCI system structure is selected as a hardware-based program. The result of test shows that the UAV fuel assembly system which is based on the virtual instrument technology can meet the requirements of engineering and test technology. |
| |
| Keywords: | virtual instrument fuel assembly LabWindows/CVI IIR filter |
| 本文献已被 维普 万方数据 等数据库收录！ |
