An aerial vehicle having more basic structure and safety measures. The aerial vehicle according to the present invention includes a thrust unit having a plurality of rotary vanes for generating thrust, a tail, a fuselage that connects the thrust unit and the tail, a main wing provided in a substantially center of the fuselage, and a control unit for controlling at least the main wing. When the aerial vehicle makes a landing, the control unit controls the main wing so that a part of the main wing becomes a lower end.
AERIAL VEHICLE AND FLYING METHOD OF AERIAL VEHICLE
2022-09-01
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
UNMANNED AERIAL VEHICLE FLYING METHOD AND UNMANNED AERIAL VEHICLE FLYING SYSTEM
Europäisches Patentamt | 2017
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