The avionic calculator is suitable for being carried on-board an aircraft and comprises a multi-core processor configured for executing avionic software applications. The processor includes at least one primary core for communicating with at least one avionic equipment distinct from the calculator, each avionic equipment being carried on-board the aircraft and belonging to an avionic domain; at least one secondary core for communicating with at least one electronic device external to the avionic domain; and a tertiary core for performing at least one filtering of a data message received from a respective device external to the avionic domain and intended for a respective avionic equipment of the avionic domain. Each avionic software application being executable by the at least one primary core or the at least one secondary core.


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    Titel :

    Avionic calculator comprising a multicore processor, with a filtering core between open and avionic domains


    Beteiligte:

    Erscheinungsdatum :

    07.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



    Filtering techniques in avionic transmitters

    Grabowiecki, A. / Kazmierski, A.J. / Kunachewicz, K. | Tema Archiv | 1977


    Avionic Corrosion

    I. S. Shaffer | NTIS | 1987


    Avionic Corrosion

    I. S. Shaffer | NTIS | 1987


    Filtering Techniques in Avionic Transmitters

    Grabowiecki, A. / Kazmierski, A. J. / Kunachowicz, K. | IEEE | 1977


    Avionic Systems

    Middleton, Donald H. | TIBKAT | 1989