• DocumentCode
    711461
  • Title

    An adaptive middleware approach for fault-tolerant avionic systems

  • Author

    Marquardt, Oliver ; Riedlinger, Marc ; Ahmadi, Reza ; Reichel, Reinhard

  • Author_Institution
    Inst. of Aircraft Syst., Univ. of Stuttgart, Stuttgart, Germany
  • fYear
    2015
  • fDate
    7-14 March 2015
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    The distributed nature of avionic systems is hidden by the system architecture, containing a middleware which abstracts the communication and the system management. To introduce scalability and modifiability in future fault-tolerant avionic systems, adaptive mechanisms have to replace the still common manual configuration and parameterization of the middleware. This requires a fundamentally new middleware approach, which is presented in this paper. Adaptivity refers to the autonomous adaption during the initial middleware configuration and has to take domain specific requirements into account, e.g. deterministic communication paths. This is why known concepts from congeneric domains cannot be transferred directly, e.g. PnP from computer science. The publish/subscribe communication paradigm (pub/sub paradigm), with its inherent loose-coupling property serves the ability to interconnect an arbitrary unconfigured system autonomously. The concept of the pub/sub paradigm is applied to the adaptive communication middleware. Alongside the conceptual consideration, the concept is validated on a laboratory demonstrator. The results are promising and the adaptive middleware approach aims to push future avionic systems further towards adaptivity. Further validations should iteratively close the gap towards authorized avionics hardware and for aerospace certified protocols.
  • Keywords
    aerospace computing; avionics; fault tolerant computing; middleware; adaptive communication middleware; adaptive middleware approach; aerospace certified protocol; arbitrary unconfigured system interconnection; authorized avionics hardware; autonomous adaption; domain specific requirement; fault tolerant avionic system; laboratory demonstrator; loose coupling property; modifiability; publish-subscribe communication paradigm; scalability; Actuators; Aerospace electronics; Biographies; Fault tolerance; Fault tolerant systems; Middleware;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2015 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4799-5379-0
  • Type

    conf

  • DOI
    10.1109/AERO.2015.7119303
  • Filename
    7119303