飞控航电接口控制系统设计  

The Design of Flight Control and Avionics Interface Control System

作　　者：匡群[1] 张京津[1] 

机构地区：[1]上海飞机设计研究院,中国上海200436

出　　处：《科技视界》2017年第1期186-186,203,共2页Science & Technology Vision

摘　　要：本文以某型民用飞机为背景,阐述了以验证飞控系统功能为目的的地面模拟试验的重要性。在此基础上,结合半物理仿真技术,介绍并设计了在以验证飞控系统功能为目的的地面模拟试验中可以替代真实航电系统进行试验的飞控航电接口控制系统。此系统利用VC++6.0和Access数据库的核心优势,同时采用VMIC实时网通讯保证仿真数据传输和仪表显示的实时性。通过以验证飞控系统功能为目的的地面模拟试验,验证了飞控航电接口控制系统的实时性和可靠性,能够满足试验的需求。Based on a certain civil aircraft, the significance of on-ground simulation tests＇ verification function of flight control system function is depicted.Based on this,integrated with semi-physical simulation technology,flight control and avionics interface control system which acts as a substitute of real avionics system and used in on-ground Simulation tests aiming at flight control system function verification is introduced and designed.Flight control and avionics interface control system utilizes the key predominance of VC＋＋ and Access database and adopts VMIC real-time network communication to ensure the real-time performance of simulated data transfer and cockpit simulated instrument display.Moreover,through the on-ground simulation tests which aim at flight Control system function verification,the system＇s real-time performance and reliability are verified,it can satisfy the requirements of tests.

关 键 词：飞控系统功能验证 飞控航电接口控制系统 地面模拟试验 

分 类 号：TP273[自动化与计算机技术—检测技术与自动化装置]