| 基于SIMICS的ICP系统模块仿真技术研究 |
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| 引用本文： | 戴小氐,王婷,崔西宁.基于SIMICS的ICP系统模块仿真技术研究[J].航空计算技术,2017,47(2). |
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| 作者姓名： | 戴小氐 王婷 崔西宁 |
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| 作者单位： | 1. 中航工业西安航空计算技术研究所,陕西 西安,710068;2. 中航工业西安航空计算技术研究所,陕西 西安 710068;西安电子科技大学 计算机学院,陕西 西安 710071 |
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| 摘 要： | 随着机载综合化航电系统的日益复杂,航电系统中软件的开发和验证也日益困难.通过研究基于SIMICS的仿真平台及二次建模技术,建立了综合核心处理机(ICP)中几种通用功能模块(CFM)的仿真模型,为系统软件和应用软件的开发、调试、测试、综合等提供了一套虚拟仿真环境,实现了软硬件协同开发,缩短了项目研制周期,提高了工作效率和软件质量,较大地提升了复杂机载软件产品的研制能力.
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| 关 键 词： | 综合核心处理机 SIMICS 仿真 故障注入 |
Research on Simulation Technology of ICP Module Based on SIMICS |
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| DAI Xiao-di,WANG Ting,CUI Xi-ning.Research on Simulation Technology of ICP Module Based on SIMICS[J].Aeronautical Computer Technique,2017,47(2). |
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| Authors: | DAI Xiao-di WANG Ting CUI Xi-ning |
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| Abstract: | With airborne integrated avionics system is becoming more complex,it becomes more and more difficult to develop and validate software in avionics system.Through studies of the simulation platform and secondary modeling technique based on SIMICS,this paper established models for several kinds of common function module(CFM) in the integrated core processor(ICP),provided a set of virtual simulation environment for developing,debugging,testing and integrating of system software and application,realized the collaborative development of software and hardware,shortened project development cycle,improved the working efficiency and software quality,significantly improved development of complex airborne software. |
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| Keywords: | ICP SIMICS simulation fault injection |
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