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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    Title :

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


    Contributors:

    Publication date :

    2024-08-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U




    VEHICLE CONTROL DEVICE, VEHICLE CONTROL METHOD, AND NON-TRANSITORY COMPUTER READABLE MEDIUM STORING VEHICLE CONTROL PROGRAM

    KOBAYASHI HIDEKI / MUGURUMA AKIHIRO / SUGIYAMA YUKIYA et al. | European Patent Office | 2019

    Free access

    Vehicle control device, vehicle control method, and non-transitory computer readable medium storing vehicle control program

    KOBAYASHI HIDEKI / MUGURUMA AKIHIRO / SUGIYAMA YUKIYA et al. | European Patent Office | 2024

    Free access