The present invention relates to an unmanned aerial vehicle (100), an unmanned aerial vehicle control system, an unmanned aerial vehicle control method, and an unmanned aerial vehicle landing control method. The unmanned aerial vehicle includes a fuselage (12), a power device (32) connected onto the fuselage, and a control device and a takeoff and landing device (50) disposed on the fuselage. The power device (32) and the takeoff and landing device are electrically connected with the control device respectively. The control device includes a landing surface detection assembly. The control device is used for controlling operating modes of the power device and the takeoff and landing device when the landing surface detection assembly detects that a landing destination of the unmanned aerial vehicle is a water surface. It may enable the unmanned aerial vehicle to land on the water surface and navigate. The unmanned aerial vehicle can fly in the air and can also navigate in water.
UNMANNED AERIAL VEHICLE, CONTROL SYSTEM AND METHOD THEREFOR, AND LANDING CONTROL METHOD FOR UNMANNED AERIAL VEHICLE
UNBEMANNTES LUFTFAHRZEUG, STEUERUNGSSYSTEM UND VERFAHREN DAFÜR SOWIE LANDUNGSSTEUERUNGSVERFAHREN FÜR UNBEMANNTES LUFTFAHRZEUG
VÉHICULE AÉRIEN SANS PILOTE, SYSTÈME DE COMMANDE ET SON PROCÉDÉ , ET PROCÉDÉ DE COMMANDE D'ATTERRISSAGE DE VÉHICULE AÉRIEN SANS PILOTE
2021-09-08
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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