基于虚拟仪器的直升机电源综合测试系统  

Design and Implementation of Integrated Test System for Helicopter Electrical Power Based on Virtual Instrument

作　　者：梁虹[1] 吴瑞金[1] 果占治[1] 吴立勋[1] 

机构地区：[1]陆军航空兵学院机载设备系,北京101123

出　　处：《信息与电子工程》2007年第1期26-30,共5页information and electronic engineering

摘　　要：介绍了一种直升机电源特性综合测试系统的设计方法,该系统采用现场总线测试技术,使用虚拟仪器编程语言LabWindows/CVI6.0设计了直升机各种供电特性参数的测试算法,实现了数据的多通道同时快速采集以及并行同步采集。虚拟仪器面板的交互式使用,使界面操作简单、便捷。实践证明该电源综合测试系统设计先进,稳定可靠,测试结果达到了要求的精度,可对被测对象的电气特性是否达到国军标要求进行评估。In this paper, the design and implementation of the test system for characteristic parameters of helicopter power is introduced. Different algorithms for testing the characteristic parameters of helicopter power in the field is designed by LabWindows/CV16.0, which is a programming language of virtual instrument. By the method, the multi-channel quick data acquisition and high performance parallel data acquisition are realized. The use of the virtual instrument panel makes the graphical user interface very clear and simple. Experiment in the helicopter electrical power system indicates that the system has reliable performance for the measurement of steady and transient parameters. It also has good prospects for extensive application to other measurements.

关 键 词：直升机电源 虚拟仪器 性能试验 参数 

分 类 号：TP274[自动化与计算机技术—检测技术与自动化装置]