The utility model discloses a vertical lift rotor unmanned aerial vehicle that verts belongs to the unmanned air vehicle technique field, vertical lift rotor unmanned aerial vehicle that verts includes fuselage, wing, fin and verts the mechanism, the wing is installed at the forward position in the upper end of fuselage, and perpendicular with the fuselage, it includes to vert the mechanism: it isfirst to fourth connecting rod, first and second steering wheels, first to fourth execution unit, firstly all include electronic governor, DC Brushless motor and screw to fourth execution unit, firstly install respectively at first tip to the fourth connecting rod to fourth execution unit, first and second steering wheels are installed inside the fuselage respectively to link to each other with first and second universal driving shafts of being connected in the connecting rod. The utility model discloses easy and simple to handle, autonomic take off and land and need not the to take off characteristics in place, greatly reduced just can be familiar with the operation to unmanned aerial vehicle operating personnel's technical requirement in the zero -base plinth short time, break through the short restriction of unmanned aerial vehicle operation hand, breaks the bottleneck of unmanned aerial vehicle industry development.