飞行器控制系统全功能等效与故障检测系统设计与实现

Design and Implementation of Aerocraft Control System All-function Equivalent and Fault Diagnosis System

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。

The main design idea, hardware structure, software structure and main test interfaces are discussed. In this paper, the advanced VI and IPC technology is used to develop the intelligentized system. And the new instrument has the ability of on-line testing and real-time malfunction diagnosis in the course of checking the ground test and launch equipments.