摘要
详细介绍了在研究某型航空发动机电子控制器工作原理的基础上,利用虚拟仪器技术设计该控制器压气机静子调节通道的自动测试系统,以及应用工控机和研华数据采集卡PCL-818L实现该系统的过程。
Based on the research of test method of electronic controller's control channel of compressor inlet guide vanes of a certain type of aeroengine,the design of it's automatic test system by Virtual Instrument Technology is introduced in the paper in details and the using of Industrial Control Computer,Advantech Company's DAQ card PCL818L to implement the system is also presented.
出处
《航空计算技术》
2003年第2期116-119,共4页
Aeronautical Computing Technique