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基于在线加载分区机制的重构方案的设计与实现 被引量:2

Design and Implementation of A Reconfiguration Blueprint Based on Online-Loaded Partition Mechanism
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摘要 随着综合模块化航空电子系统(IMA)结构技术的发展,对航电系统的安全性和可靠性的要求也进一步提高。本文提出的IMA重构方案基于Vx Works653系统中的在线加载分区(Online-Loaded)机制,可以做到对应用程序的动态加载,使得IMA系统在发生故障时能按预设的配置进行功能迁移,从而实现IMA系统的重构。在该重构方案的基础上还同时设计了分步加载技术。测试验证表明,分步加载技术明显减少了重构的耗时,提高了重构的效率。 With the further development of Integrated Modular Avionics (IMA), it requires much more security and reliability of the Avionics system. This paper proposes a reconfiguration blueprint of IMA based on the mechanism of Online-Loaded partition in VxWorks653 system. The blueprint can load applications dynamically, so that IMA system can do the function migration according to the default configuration when a failure occurs, which will implement the reconfiguration of IMA system. Based on this blueprint, this paper also designs a fractional steps loading technology, which will reduce the time of the reconfiguration obviously and improve the efficiency of the reconfiguration through testing.
作者 王震 朱剑锋
出处 《航空电子技术》 2016年第1期25-30,共6页 Avionics Technology
关键词 综合模块化航空电子系统(IMA) 在线加载分区 重构 分步加载 integrated modular avionics (IMA) online-loaded reconfiguration fractional steps loading
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参考文献4

  • 1Wind River System INC..Wind River:VxWorks 653Configuration and Build Guide2.2[M]. Wind River System INC.,2007.
  • 2Wind River System INC..Wind River:VxWorks 653 Programmer's Guide 2.2[M]. Wind River System INC.,2007.
  • 3宋晗,陈宗基.民用航空电子系统结构研究[C].中国航空学会2007年学术年会,2007.
  • 4郭莎莎,王巍,朱晓飞.IMA平台重构中的人素和安全性研究[J].航空电子技术,2014,45(2):8-13. 被引量:3

二级参考文献5

  • 1Giuseppe Montano, John McDermid. Human Involvement in Dynamic Reconfiguration of Integrated Modular Avionics[C].Digital Avionics Systems Conference(DASC), 2008. IEEE/AIAA 27^th.
  • 2Dajiang Suo, Jinxia An, Jihong Zhu. A New Approach to Improve Safety of Reconfiguration in Integrated Modular Avionics[C]. Digital Avionics Systems Conference(DASC), 2008. IEEE/AIAA,30^th.
  • 3Rudolf Fuchsen. How to Address Certification for Multi-core Based IMA Platforms: Current Status and Potential Solutions[C].Digital Avionics Systems Conference(DASC), 2008. IEEE/AIAA,29^th.
  • 4Dajiang Suo, Jinxia An, Jihong Zhu. AADL-based Modeling and TPN-based verification of reconfiguration in Integrated Modular Avionics[C]. 2011 18th Asia-Pacifc Software Engineering Conference.
  • 5Victor Lpez-Jaquero, Francisco Montero. Supporting AR1NC 653-based Dynamic Reconfiguration[C].2012 Joint Working Conference on Software Architecture & 6th European Conference on Software Architecture.

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