机械与电子Issue(2)：14-18,5.
LabWindows/CVI和PLC技术下的飞机电负载系统设计
Design of Airplane Electric- load System Based on LabWindows/CVI and PLC
孙新川 1仲秦 1范蟠果1
作者信息
- 1. 中国飞行试验研究院改装部,陕西西安710089
- 折叠
摘要
Abstract
Old electrical systems have such problems like low load or low automation. Designing proposal of virtual instruments is forwarded for electrical loading uploading and emergency control. The whole system is a combination of sub -control system,makes up water draining water sub - system, load sub - system, heat exchange sub -system. The control sub - system of upper computer adopting LabWindows/CVI virtual instruments technology to develop human - machine interface, communication and control. Lower computer, of which the receiving and carry - on control instruction is processed by PLC.关键词
虚拟仪器/LabWindows/CVI/电负载/多线程Key words
virtual instrument/ labWindows/ CVI/ electrical load/multi - thread分类
信息技术与安全科学引用本文复制引用
孙新川,仲秦,范蟠果..LabWindows/CVI和PLC技术下的飞机电负载系统设计[J].机械与电子,2012,(2):14-18,5.
