Device fixed wing vertical takeoff and landing capable of providing a transition in level flight and move in space without the assistance of rudders

Device fixed wing aircraft with vertical take off and landing capable of providing a transition in level flight and move in space without the assistance of rudders. The device consists of a cell (1), a fixed wing (2) intended to ensure the buoyancy of the aircraft in horizontal flight portion, a tail unit (3), a set of thrusters ( 4), (5), (6) and (7) the minimum number of three but more usually 4, whose individual command steering the aircraft in space without the use of traditional mobile plans surfaces. The device of the invention is particularly suited for UAV type of aircraft to take off and land in limited dimensions of places, fixed or mobile, while having good distance passable performance between takeoff and landing points.