Unmanned aerial systems including an unmanned aerial vehicle and a command device. The unmanned aerial vehicle includes a propulsion system, a vehicle power source, a vehicle electronic controller, and a vehicle coupling mechanism. The command device includes a command power source, a command electronic controller, and a command coupling mechanism. The vehicle electronic controller is without power from the vehicle power source when the vehicle coupling mechanism is connected to the command coupling mechanism. The command electronic controller is without power from the command power source when the vehicle coupling mechanism is connected to the command coupling mechanism. The vehicle electronic controller receives power from the vehicle power source when the vehicle coupling mechanism is separate from the command coupling mechanism. The command electronic controller receives power from the command power source when the vehicle coupling mechanism is separate from the command coupling mechanism.
CONTROL SYSTEMS FOR UNMANNED AERIAL VEHICLES
2019-07-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |