A flight control arrangement for a hybrid aircraft includes a fixed-wing flight (F/W) control module and vertical takeoff/landing flight (VTOL) control module. The F/W control module is an integrated component having a respective network interface connected to an aircraft data network via which it provides fixed-wing control output to network-connected fixed-wing flight components including one or more horizontal-thrust components. The VTOL control module is also an integrated component having a respective network interface to the aircraft data network via which the VTOL control module (1) observes flight status as reflected in network messages originated by the fixed-wing flight control module, and (2) based on the observed flight status, generates VTOL control output to network-connected VTOL flight components including one or more vertical-thrust components, to control VTOL flight as well as transitions to and from fixed-wing flight.


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    Titel :

    FLIGHT CONTROL ARRANGEMENT USING SEPARATE FIXED-WING AND VTOL CONTROL MODULES


    Weitere Titelangaben:

    FLUGSTEUERUNGSANORDNUNG MIT SEPARATEN STARRFLÜGEL- UND VTOL-STEUERUNGSMODULEN
    AGENCEMENT DE COMMANDE DE VOL FAISANT INTERVENIR DES MODULES DE COMMANDE SÉPARÉS DE VOILURE FIXE ET DE VOL À DÉCOLLAGE/ATTERRISSAGE VERTICAL


    Beteiligte:

    Erscheinungsdatum :

    05.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



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