期刊文献+

某2×2余度襟缝翼控制器计算机软件关键技术研究

The Research on Key Technology of the 2×2 Redundancy Flap Slat Electronics Control Unit Software
原文传递
导出
摘要 文章对2×2余度襟缝翼控制器计算机软件结构进行了介绍,根据系统构型,提出了软件容错机制要求,划分软件功能形成体系结构设计方案。对软件设计中的关键技术进行研究,重点分析了软件运行控制、双握手同步、余度管理、故障综合与申报四个方面,为实现系统容错软件提供了解决方案。 This paper introduces the structure of the 2×2 Redundancy Flap Slat Electronics Control Unit Software. According to the system configuration, the article presents the requirements of the fault tolerance software, and describes the architecture scheme by dividing the software function. The research on the key techniques of software design focus on 4 aspects, including the software running mechanism, sync shaking hands, redundancy management, and the faults synthesis declare, providing the solution for the implementations of the system fault tolerance software.
作者 马倩 王国静
出处 《电子技术(上海)》 2015年第6期19-21,5,共4页 Electronic Technology
关键词 2×2余度 余度管理 故障处理 容错软件 2×2 Redundancy Redundancy Management Faults Process Fault Tolerance Software
  • 相关文献

参考文献3

  • 1HammeR, Robert. Design by Extrapolation: An Evaluation of Fault Tolerant Avionics[C]. IEEE AESS System s Magzine, 2001(1) : 1C5/1- 12.
  • 2Algirdas Avi zienis, Jean Claude Laprie, Brian Randell, et al.Basic Concepts and Taxonomy ofDependable and Secure Computing. Kaunas: IEEE Transactionon Dependable and Secure Computing, 2004, 1(1): 11-33.
  • 3张磊,林荣超,牛文生.小型飞机航空电子系统容错技术研究[J].航空计算技术,2011,41(1):106-110. 被引量:11

二级参考文献11

  • 1伊恩.莫伊尔,阿伦.西布里奇.民用航空电子系统[M].北京:航空工业出版社,2009.
  • 2曾声奎,赵廷弟,张建国,等.系统可靠性设计分析教程[M].北京:北京航空航天大学出版社,2009:2-3.
  • 3SAE ARP4754 Certification Consideration for Highly Intergrated or Complex Aircraft Systems[S].The Engineering Society For Advancing Mobility Land Sea Air and Space,1996.
  • 4SAE ARP4761 Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and Equipment[S].The Engineering Society For Advancing Mobility Land Sea Air and Space,1996.
  • 5AC23.1309-1D System Safety Analysis and Assessment for Part 23 Airplanes[S].Federal Aviation Administration,1988.
  • 6AC25-11A Electronic Flight Deck Displays[S].Federal Aviation Administration,2007.
  • 7AC25.1309-1A System Design and Analysis[S].Federal Aviation Administration,2009.
  • 8RTCA DO-178B Software Considerations in Airborne Systems and Equipment Certification[Z].1992.
  • 9RTCA DO-254 Design Assurance Guidance for Airborne Electronic Hardware[Z].2000.
  • 10RTCA DO-297 Integrated Modular Avionics (IMA) Development Guidance and Certification Considerations[Z].2005.

共引文献10

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