Provided are a control device for unmanned aerial vehicle and an unmanned aerial vehicle. The control device for unmanned aerial vehicle includes a shell, an inertial measurement device fixed in the shell, a main flight control circuit board electrically connected to the inertial measurement device, and a flexible interface board electrically connected to the main flight control circuit board and appressed against the inwall of the shell. At least one external device is connected to two opposite sides of the flexible interface board through the shell.
CONTROL APPARATUS FOR UNMANNED AERIAL VEHICLE, AND UNMANNED AERIAL VEHICLE
STEUERUNGSVORRICHTUNG FÜR UNBEMANNTES LUFTFAHRZEUG SOWIE UNBEMANNTES LUFTFAHRZEUG
DISPOSITIF DE COMMANDE POUR UN DRONE ET DRONE
2021-08-25
Patent
Electronic Resource
English
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