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文章重点介绍飞行器控制系统全功能等效与故障检测系统的研制目标、设计思想、硬件结构、测试软件的构成以及各种测试应用界面等。利用PC总线和VI技术使该系统具备对飞行器地面测试发射设备的智能化在线监测能力 ,同时对地面测试发射设备在工作中出现的问题能够进行故障检测。
This article focuses on the research objectives, design concepts, hardware structure, composition of test software and various test application interfaces of full-function equivalent and fault detection system of aircraft control system. Utilizing PC bus and VI technology, the system is capable of intelligentizing on-line monitoring of aircraft ground testing and transmitting equipment and capable of performing fault detection on the ground testing and transmitting equipment during operation.