The invention relates to a petrol-electric
hybrid power
fixed wing vertical take-off and landing unmanned plane
system, which comprises a
fuselage, a wing I and a wing II. The wing I is provided with a vertical
propeller I and a wing motor I. The wing II is provided with a vertical
propeller II and a wing motor II. The front end of the
fuselage is externally connected to a
fixed wing horizontal
propeller, the
tail of the
fuselage is provided with a longitudinal balance directional propeller and a longitudinal balance directional control motor, and the fuselage is internally provided with an
autopilot for intelligently controlling the operation of the wing motor I, the wing motor II, a petrol power engine and the longitudinal balance directional control motor. The petrol-electric
hybrid power
fixed wing vertical take-off and landing unmanned plane
system provided by the invention realizes the all functions of unmanned plane take-off replying on
power battery vertical take-off, hovering to petrol power driven fixed wing fast flight, and return flight hovering to vertical landing petrol-electric
hybrid power flight, has the capability of vertical take-off and landing and hovering, and also has the characteristics of
fast speed, long voyage and long time.