An aircraft monitoring system includes an avionics communication bus structure, at least one network member user device that transmits a broadcast message onto the avionics communication bus structure, and at least one non-member user device that receives the broadcast message transmitted onto the avionics communication bus, processes the received broadcast message, and transmits output data to a monitoring device. The at least one non-member user device includes a bus interface, and a field programmable gate array (FPGA) that communicates with the bus interface. The FPGA is programmed to function as a main finite state machine that processes the broadcast message from the bus interface, and a transfer finite state machine that generates output data and transfers the generated output data to an output processor that communicates with the monitoring device. The monitoring device outputs a monitored data report.


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    Titel :

    AIRCRAFT MONITORING SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    03.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H04L TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION , Übertragung digitaler Information, z.B. Telegrafieverkehr / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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