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计算机工程 ›› 2009, Vol. 35 ›› Issue (23): 272-273,. doi: 10.3969/j.issn.1000-3428.2009.23.095

• 开发研究与设计技术 • 上一篇    下一篇

综合模块化航空电子系统的可靠性设计

郑朝辉1,陈新中2,张晓先1   

  1. (1. 华东计算技术研究所,上海 200233;2. 中国电子科学研究院,北京 100041)
  • 收稿日期:1900-01-01 修回日期:1900-01-01 出版日期:2009-12-05 发布日期:2009-12-05

Reliability Design of Integrated Modular Avionics System

ZHENG Chao-hui1, CHEN Xin-zhong2, ZHANG Xiao-xian1   

  1. (1. East China Institute of Computer Technology, Shanghai 200233; 2. China Academy of Electronics and Information Technology, Beijing 100041)
  • Received:1900-01-01 Revised:1900-01-01 Online:2009-12-05 Published:2009-12-05

摘要: ASAAC软件体系结构侧重于整个系统的模块化、可扩展性,其节点使用普通操作系统导致系统可靠性不够。针对该问题,将符合ARINC653标准的高可靠性分区操作系统作为ASAAC软件体系结构的节点操作系统,设计新的ASAAC通用系统管理并将其植入ARINC653的核心软件层,使两者充分融合以提高综合模块化航空电子系统的可靠性。

关键词: 综合模块化航空电子, 分区操作系统, 通用系统管理, 可靠性

Abstract: The software architecture of ASAAC standard emphasizes on the modular and scalability of the whole system, but its safety is not enough because of using normal operating system as node system. Aiming at this problem, this paper uses ARINC653 partition operating system as ASAAC node system, designs a new ASAAC generic system management and puts it into the core software layer of ARINC653 operating system to improve the safety of integrated modular avionics system.

Key words: Integrated Modular Avionics(IMA), partition operating system, general system management, reliability

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