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.
CONTROL DEVICE FOR ELECTRIC FLIGHT VEHICLE AND NON-TRANSITORY COMPUTER READABLE MEDIUM STORING COMPUTER PROGRAM FOR ELECTRIC FLIGHT VEHICLE
2024-08-15
Patent
Electronic Resource
English
IPC: | B64U |
FLIGHT CONTROL DEVICE AND NON-TRANSITORY COMPUTER READABLE MEDIUM STORING FLIGHT CONTROL PROGRAM
European Patent Office | 2024
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