The utility model discloses a kind of unmanned aerial vehicle for realizing vertical take-off and
attitude control using small
turbojet engine, small
turbojet engine is installed at wing tip of wing, small
turbojet engine is installed at the back of
fuselage (or in front of
fuselage) two sides;Small
turbojet engine is made to produce upward thrust by vertical rotation 90 ° using
turbine worm drive mechanism or motor with self-locking holding torque, and unmanned aerial vehicle vertical take-off is realized;Unmanned aerial vehicle has
aileron installed at the
trailing edge of left and right wing tips, and the differential deflection of
aileron makes unmanned aerial vehicle tilt rotation around longitudinal axis, and the direction of thrust of small
turbojet engine is deflected using
turbine worm drive mechanism, to realize the flight state stabilization and flight
attitude control of unmanned aerial vehicle, so that unmanned aerial vehicle has good maneuverability;Horizontal stabilizer and
elevator are omitted,
vertical stabilizer and
rudder are omitted, so as to reduce flight resistance, which is conducive to improving the
flight speed and effective load of unmanned aerial vehicle.