航空装备典型软件可靠性与性能一体化设计流程与验证
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  • 英文篇名:Aeronautical Equipment Software Reliability and Performance Integrated Design Workflow and Verification
  • 作者:陈阳 ; 刘俊荣
  • 英文作者:CHEN Yang;LIU Jun-rong;China Academy of Electronics and Information Technology;
  • 关键词:软件可靠性 ; 一体化设计 ; 监控点
  • 英文关键词:software reliability;;integrated design;;supervision point
  • 中文刊名:HJJJ
  • 英文刊名:Environmental Technology
  • 机构:中国电子科技集团公司电子科学研究院;
  • 出版日期:2019-06-25
  • 出版单位:环境技术
  • 年:2019
  • 期:v.37;No.219
  • 语种:中文;
  • 页:HJJJ201903010
  • 页数:6
  • CN:03
  • ISSN:44-1325/X
  • 分类号:44-49
摘要
航空装备软件系统可靠性工作未形成长效机制,影响任务成功。本文将软件可靠性流程进行固化与优化,实现软件可靠性工作与其整个寿命周期的融合,同时提升监控能力,并将流程应用于典型软件产品进行验证。
        Long-term mechanism of software reliability has not been established in aeronautical equipment manufacturing, which has an extremely bad influence on mission completion success probability and consumer satisfaction. Software reliability workflow is solidified and optimized in this paper. Simultaneously, software reliability and performance design are integrated through the whole life cycle and more effectively supervised by consumer representative. The workflow chart is applied and verified in a typical aeronautical equipment software engineering process lastly.
引文
[1]Michael R.Lyu,ed.Handbook of Software Reliability Engineering[M].New York:McGraw Hill and IEEE Computer Society Press,1996.
    [2]夏青,钱山,张士峰,等.飞行器可靠性与性能一体化设计初步研究[J].弹箭与制导学报,2009.01(29):257-259+263.
    [3]GJB 450A-2004,中华人民共和国国家军用标准--装备可靠性工作通用要求[S].
    [4]GJB 2786A-2009,中华人民共和国国家军用标准--军用软件开发通用要求[S].

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