One embodiment is an aircraft (100) including at least one propulsion assembly (115); a cargo area (102) for receiving payload to be transported by the aircraft 9100); and a control system (20) for determining characteristics of the received payload; automatically determining optimal control gains for operating the aircraft (100) including the payload based on the determined payload characteristics; and providing control signals to at least one of the at least one propulsion assembly (115)and a control assembly of the aircraft (100)to control operation of the at least one propulsion assembly (115) in accordance with the determined optimal control gains.


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    Titel :

    ADAPTIVE FLIGHT CONTROLS


    Weitere Titelangaben:

    ADAPTIVE FLUGSTEUERUNGEN
    COMMANDES DE VOL ADAPTATIVES


    Beteiligte:

    Erscheinungsdatum :

    2023-10-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U



    ADAPTIVE FLIGHT CONTROLS

    WITTMAAK JR JOHN ROBERT / PETERS RUSSELL C / LOUIS ANDREW VINCENT | Europäisches Patentamt | 2020

    Freier Zugriff

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