飞控FTI系统状态监测与数据分析系统设计与实现  

Design and Implementation of FCS-FTI System Status Monitoring and Data Analysis

作　　者：张娟[1] 吕鹏涛[1] 

机构地区：[1]中国飞行试验研究院,西安710089

出　　处：《计算机测量与控制》2015年第9期3174-3177,共4页Computer Measurement &Control

基　　金："十二五"航空支撑预研项目(61901090304)

摘　　要：在飞行试验工程中,机载测试系统完成对飞控数据的采集、封装和输出;为了实现基于USB的PCM数据解调及其与计算机之间的数据通信,实现实时的状态监测和数据事后分析处理,设计并实现了基于.NET框架的FCS-FTI系统状态监测与数据分析系统;该系统包括数据实时捕获、状态监测、数据事后处理等模块;测试表明,系统各功能模块运行稳定,能对FCS-FTI进行状态监测并能进行数据事后分析处理,具有高效的实时性和良好的可靠性。In flight test engineering,the flight test instruments system implements data acquisition,packaging and output.In order to achieve data communication between PCM data demodulation and computer,realize the real-time status monitoring,data post-analysis and processing,a FCS-FTI system status monitoring and data analysis system is designed and implemented based on.NET framework.The system functions include data capturing,real-time condition monitoring,data post-processing module.The testing results show that the system each function module running stability,and can realize the real-time status monitoring,data post-analysis and processing with efficient real-time and good reliability.

关 键 词：飞行试验 FLIGHT CONTROLLER system FLIGHT test INSTRUMENTS 状态监测 数据分析 

分 类 号：TP31[自动化与计算机技术—计算机软件与理论]