Disclosed herein is a system and method for effector reboot on an electric aircraft during flight. An effector controller may perform a power on built-in test on boot. An effector controller may selective perform an additional built-in test (ABIT) on boot based on instructions from a flight controller. The flight controller may use flags to indicate the necessity of an ABIT on boot. The effector controller may not perform an ABIT during flight. A backup controller may be used to send standard commands to an effector controller but may not sent an ABIT command.


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    Titel :

    SYSTEM AND METHOD FOR EFFECTOR REBOOT ON AN ELECTRIC AIRCRAFT DURING FLIGHT


    Beteiligte:
    WOODALL CHRIS (Autor:in) / RICHTER TIMOTHY GERARD (Autor:in) / SHAW MIKE (Autor:in)

    Erscheinungsdatum :

    2024-04-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    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 / B64C AEROPLANES , Flugzeuge



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    Dexterous End Effector Flight Demonstration

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    Dexterous End Effector Flight Demonstration

    United States; National Aeronautics and Space Administration / United States; Air Force | British Library Conference Proceedings | 1993