基于FMI仿真系统的参数注入技术研究  

Research on Parameter Injection Based on FMI Simulation System

作　　者：国一兵[1] 玉少康 GUO Yibing;YU Shaokang(Shenyang Ligong University,Shenyang,Liaoning Province,110159 China)

机构地区：[1]沈阳理工大学,辽宁沈阳110159

出　　处：《科技资讯》2021年第6期23-25,共3页Science & Technology Information

摘　　要：随着对飞行器的研究以及开发水平的不断提高,飞行器地面仿真系统的研究已成为必然。为了完善仿真飞行器的飞行过程及实验,该文在分析立即注入和定时注入两种技术的基础上,在仿真过程中设计了参数注入功能,并应用在FMI联合仿真系统中。利用Redis通信中间件实现控制参数注入过程,并在仿真系统进行测试与结果分析,成功验证了参数注入技术的有效性与实用性。With the continuous improvement of aircraft,the research of aircraft ground simulation system has become inevitable.In order to simulate the flight process of aircraft completely,the parameter injection function is designed and applied in FMI simulation system based on the analysis of the two techniques of immediate injection and timing injection.Using Redis communication middleware to realize the process of control parameter injection,the simulation system is tested and the results are analyzed,which successfully verifies the effectiveness and practicability of parameter injection technology.

关 键 词：FMI仿真系统 参数注入 REDIS FMU 

分 类 号：G64[文化科学—高等教育学]