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.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Research on Distributed Integrated Modular Avionics system architecture design and implementation


    Beteiligte:
    Guoqing Wang (Autor:in) / Qingfan Gu (Autor:in)


    Erscheinungsdatum :

    01.10.2013


    Format / Umfang :

    1219025 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Integrated Modular Spacecraft Avionics. Architecture and SpaceWire-Based Implementation

    Sheynin, Y. / Gorbachev, S. / International Federation of Automatic Control | British Library Conference Proceedings | 2004



    Integrated Modular Avionics Architecture Concepts Demonstration

    Potthaus, J. / Kloeckner, W. / Sprang, I. et al. | British Library Conference Proceedings | 1997


    Distributed flight control system implemented according to an integrated modular avionics architecture

    FERVEL MARC / LECANU ARNAUD / MAUSSION ANTOINE et al. | Europäisches Patentamt | 2015

    Freier Zugriff