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作 者:胡涛[1] 金雪松[2] 申立群[1] 刘磊[1] HU Tao;JIN Xuesong;SHEN Liqun;LIU Lei(School of Instrumentation Science and Engineering,Harbin Institute of Technology,Harbin 150001,China;School of Computer and Information Engineering,Harbin University of Commerce,Harbin 150028,China)
机构地区:[1]哈尔滨工业大学仪器科学与工程学院,黑龙江哈尔滨150001 [2]哈尔滨商业大学计算机与信息工程学院,黑龙江哈尔滨150028
出 处:《计算机集成制造系统》2021年第5期1422-1428,共7页Computer Integrated Manufacturing Systems
摘 要:为了提高高层体系结构仿真联邦的开发效率,将Simulink模型接入运行支撑系统,以在高层体系结构分布式仿真中充分利用Simulink强大的数值计算功能,对搭建高层体系结构分布式仿真系统具有很强的实用价值。对现有的3种接入方法进行分析,针对其不足,结合插件技术对基于插件的接入方法进行研究,与现有方法相比,该方法具有更高的模型接入效率。对该方法进行方案设计,并阐述了关键流程,包括接口适配包装、仿真数据绑定与仿真数据更新。采用该方法将Simulink模型接入运行支撑系统,构建了小型固体火箭分布式飞行仿真系统应用实例,证明该方法不但可行,而且高效、易用。To improve the development efficiency of High Level Architecture(HLA)simulation,the Simulink model was connected with Run-Time Infrastructure(RTI)to make full use of powerful calculation ability of Simulink,which was of great benefit for building HLA distributed simulation.Combining plug-in technology with connecting method,the shortcomings of three current methods were analyzed.The connecting method based on plug-in technology was designed,and the critical implementation process including making interfaces adapted,binding and updating simulation data was described.Simulink model was connected with RTI successfully with the proposed connecting method,and a small solid rocket flight distributed simulation system was constructed.The simplicity of connecting process showed that the plug-in technology based method had superiority in efficiency and usability.
关 键 词:SIMULINK模型 运行支撑系统 插件技术 高层体系结构 分布式仿真
分 类 号:TP391.9[自动化与计算机技术—计算机应用技术]
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