The disclosure relates to a technique for controlling an electric flight vehicle having a rotary wing driven by electric power of a battery. In the technique, a temperature of the battery is acquired as a battery temperature. Restriction is placed on take-off of the electric flight vehicle when the battery temperature is lower than a take-off permitting temperature that is a temperature for permitting take-off of the electric flight vehicle. The restriction placed on take-off of the electric flight vehicle may be terminated when the battery temperature exceeds a restriction terminating temperature and the battery temperature raising processing is performed. The restriction terminating temperature is higher than the take-off permitting temperature.


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    Titel :

    CONTROL DEVICE FOR ELECTRIC FLIGHT VEHICLE AND NON-TRANSITORY COMPUTER READABLE MEDIUM STORING COMPUTER PROGRAM FOR ELECTRIC FLIGHT VEHICLE


    Beteiligte:
    TAKEMURA YUICHI (Autor:in) / FUKUSHI MASATO (Autor:in)

    Erscheinungsdatum :

    15.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U




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