论文部分内容阅读
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。
In this paper, a civil aircraft as a background, elaborated on the verification of flight control system for the purpose of the ground simulation test of importance. On this basis, combined with the semi-physical simulation technology, this paper introduces and designs the flight control avionics interface control system which can replace the real avionics system in the ground simulation test for the purpose of verifying the function of the flight control system. The system uses the core advantages of VC ++ 6.0 and Access databases, while using VMIC real-time network communication to ensure real-time simulation data transmission and instrument display. Through the ground simulation test for the purpose of verifying the function of the flight control system, the real-time and reliability of the flight control avionics interface control system are verified, which can meet the test requirements.