期刊文献+

综合核心处理系统评价工具设计 被引量:1

Design of a Performance Evaluation Tool for Integrity Core Processor
下载PDF
导出
摘要 综合核心处理系统是航空电子综合化模块化的关键支撑技术。如何对其性能指标进行评价是一个非常重要的理论和工程问题。首先建立了综合核心处理器模型、任务模型。然后基于ARINC 653标准建立了双层分区调度模型,该模型实现了不同安全关键级别应用软件之间的隔离。根据离散事件仿真方法,建立了系统仿真模型。在此基础上编制了基于Visual C++平台的系统仿真程序,最后提取ICD接口控制文件进行了实例仿真,分析了任务的可调度性及系统的实时性,其结果对指导新一代航电系统设计具有重要意义。 The Integrity Core Processor(ICP) system is the key technology in integrity modular avionics.How to evaluate its performance index is an important theoretical and practical problem.The ICP model and task model were established at first.Then,a hierarchical partition scheduling model was determined based on ARINC653 criterion,which implement partitioning between applications of different safety critical levels.In addition,the system simulation model was established with the method of discrete event system simulation,and the system simulation program was developed by using the Visual C++ platform.Finally,with the supposed ICD,the schedulable problem of tasks and real-time performance of the system were analyzed,which result has great significance for the design of integrated modular avionic system.
出处 《电光与控制》 北大核心 2012年第2期59-62,共4页 Electronics Optics & Control
基金 国家自然科学基金(60879024)
关键词 航电系统 综合核心处理系统 分区调度 离散事件系统仿真 avionics Integrity Core Processor(ICP) partition scheduling discrete event simulation
  • 相关文献

参考文献10

  • 1熊华钢.先进综合航空电子技术[M].北京:国防工业出版社,2009.
  • 2袁晓晗.航空电子综合核心处理技术研究[J].航空电子技术,2004,35(3):6-10. 被引量:12
  • 3CASSANDRAS C G,LAFORTUNE S. Introduction to discrete event systems[ M]. 2nd ed. Springer,2008.
  • 4LI Xinying,XIONG Huagang. Modelling and simulation of intergated modular avionics [ C ]//Proceedings of 28th Digital Avionics Systems Conference ,2009 : 1-8.
  • 5ASSAC phase II stage 2 second draft of proposed standards for architecture[ Z ]. UK Defence Procurement Agency,2004.
  • 6Airlines electronic engineering committee, avionics appli- cation software standard interface [ Z ]. ARINC Specifica- tion 653, Aeronautical Radio Inc. , Annapolis, MD, 1997.
  • 7Airlines electronic engineering committee, avionics applica- tion software standard interface [ Z ]. ARINC Specification 653-1-2JX13,Aeronautical Radio Inc. ,Annapohs,MD,21XI3.
  • 8张凤鸣,褚文奎,樊晓光,万明.综合模块化航空电子体系结构研究[J].电光与控制,2009,16(9):47-51. 被引量:58
  • 9宋丽茹,何锋,熊华钢.航空电子蓝图系统实时性设计[J].电光与控制,2010,17(6):5-8. 被引量:6
  • 10李昕颖,顾健,何锋,熊华钢.硬实时系统在强分区约束下的双层分区调度[J].计算机学报,2010,33(6):1032-1039. 被引量:16

二级参考文献49

  • 1霍曼,邓中卫.国外军用飞机航空电子系统发展趋势[J].航空电子技术,2004,35(4):5-10. 被引量:65
  • 2罗巧云,高勇强.美军第四代战斗机F-35“联合攻击战斗机”最卓越的航空电子系统[J].电子科学技术评论,2005(4):5-8. 被引量:11
  • 3Joint Advanced Strike Technology Program. Avionics architecture definition [ M ]. Arlington (USA) : JAST Avionics Lead, 1994.
  • 4EUROCONTROL. Study report on avionics systems for 2011 -2020 [R]. Proposed Issue, OATA - P2 - D4. 2. 11 - 03 - 01, Brussels : EATMP Infocentre,2007.
  • 5PRISAZNUK P J. Integrated modular avionics [ C ]//Proceedings of the IEEE International Aerospace and Electronics Conference, 1992:39-45.
  • 6MORI I, SEABRIDGE A G. Military avionics systems [ M ]. Chichester (England) : John Wiley & Sons, 2006.
  • 7NATO. STANAG 4626--2005 modular and open avionics architecture ( part II: software) [ S ].
  • 8ARINC. Design guidance for integrated modular avionics [ R ]. Technical Report, 651-1, Annapolis (USA) : Aeronautical Radio, Inc,2003.
  • 9RTCA DO -255--2000. Requirements specification for Avionics Computer Resource (ACR) [ S].
  • 10SPITZER C R. The avionics handbook [ M ]. Boca Raton (USA) :CRC Press LLC, 2001.

共引文献88

同被引文献4

引证文献1

二级引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部