| 航空电动机构综合测试系统设计 |
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| 引用本文： | 廖永涛,朱名铨,张光磊.航空电动机构综合测试系统设计[J].航空计测技术,2006,26(3):17-19,51. |
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| 作者姓名： | 廖永涛 朱名铨 张光磊 |
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| 作者单位： | [1]西北工业大学机电学院,陕西西安710072 [2]西安飞机工业（集团）有限责任公司特设处,陕西西安710089 [3]西北工业大学自动化学院,陕西西安710072 |
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| 摘 要： | 对航空电动机构综合测试系统设计开发的背景及意义作了简单介绍,并阐述了系统的测试原理与方法;详细论述了测试系统的硬件组成及各部分功能,最后对测试系统的软件设计环境、软件系统功能和关键算法作了介绍.
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| 关 键 词： | 航空电动机构 计算机测试 负荷控制 |
| 文章编号： | 1002-6061（2006）03-0017-03 |
| 收稿时间： | 2005-10-24 |
| 修稿时间： | 2005-10-242005-12-05 |
Design of Computer Integrated Test System for Aviation Electromotor |
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| LIAO Yong-tao,ZHU Ming-quan,ZHANG Guang-lei.Design of Computer Integrated Test System for Aviation Electromotor[J].Aviation Metrology & Measurement Technology,2006,26(3):17-19,51. |
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| Authors: | LIAO Yong-tao ZHU Ming-quan ZHANG Guang-lei |
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| Abstract: | This paper introduces the background and significance of the computer integrated test system for aviation electromotor, then presents its testing parameters, testing principles and methods. The hardware composition and function of every part of the testing system has been presented in detail. At last, it discourses upon the hardware makeup and function as well as the software environment, function and significant arithmetic of the testing system. |
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| Keywords: | aviation electromotor computer testing load control hardware system software system |
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