The disclosure relates to hybrid unmanned aerial vehicle (UAV) having vertical take-off and landing (VTOL) capabilities. Specifically, the disclosure relates to a stable hybrid fixed angle rotor arrays UAV having VTOL capabilities with hovering capabilities using rotors and cruising using fixed wing.
HYBRID FIXED ANGLE ROTOR UNMANNED AERIAL VEHICLE WITH VERTICAL TAKEOFF AND LANDING CAPABILITIES
29.08.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64U |
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