The present invention relates to a multipurpose and long endurance Hybrid Unmanned Aerial Vehicle (HUAV) with the combined functions of a Vertical Take-off and Landing (VTOL) and a fixed wing operation. The HUAV may take-off and land vertically on both land and water, and perform a mid-air transition from a VTOL mode to a fixed wing mode. The HUAV includes an airframe, a fixed wing unit having at least one forward thrust motor, one or more VTOL units mounted on a tail boom, and a fuselage of the airframe. Each of the one or more VTOL units includes at least one VTOL motor, and a control unit configured to control on-board transition of the HUAV between the VTOL mode and the fixed wing mode by controlling at least one forward thrust motor and at least one VTOL motor.
MULTIPURPOSE AND LONG ENDURANCE HYBRID UNMANNED AERIAL VEHICLE
2023-08-24
Patent
Electronic Resource
English
MULTIPURPOSE AND LONG ENDURANCE HYBRID UNMANNED AERIAL VEHICLE
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