• DocumentCode
    2901280
  • Title

    Research on Distributed Integrated Modular Avionics system architecture design and implementation

  • Author

    Guoqing Wang ; Qingfan Gu

  • Author_Institution
    China Nat. Aeronaut. Radio Electron. Res. Inst., Shanghai, China
  • fYear
    2013
  • fDate
    5-10 Oct. 2013
  • Abstract
    A well-designed Distributed Integrated Modular Avionics (DIMA) should keep the complexity of system interconnections to a minimum with the constraints set by communication links, LRM size, and fault tolerance requirements. In this paper, a basic DIMA model is put forward and the design philosophy is detailed for constructing DIMA system framework which enhanced capabilities with improved reliability and lower cost. The paper analyzes the system framework model, ability and effectiveness, discusses the organization mode, management mode and process scheduling management mode of DIAM system, and created an organization and management mode for DIMA system architecture. Furthermore, the key enable technologies for DIMA system implementation are analyzed which can guide implementing DIMA system.
  • Keywords
    avionics; fault tolerance; reliability; DIMA system architecture; DIMA system framework model; LRM size; communication links; distributed integrated modular avionics system architecture design; fault tolerance; management mode; organization mode; process scheduling management mode; reliability; Aerospace electronics; Aircraft; Complexity theory; Computer architecture; Organizations; Organizing; Resource management;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference (DASC), 2013 IEEE/AIAA 32nd
  • Conference_Location
    East Syracuse, NY
  • ISSN
    2155-7195
  • Print_ISBN
    978-1-4799-1536-1
  • Type

    conf

  • DOI
    10.1109/DASC.2013.6712647
  • Filename
    6712647