The invention relates to an aircraft capable of taking off and landing vertically, belonging to the technical field of aircraft, comprising a fuselage, a wing, a lifting device, a power device and a movable wing surface. The fuselage has a streamlined rhombus structure. The wings are inverted triangles, extending from the forward end of the fuselage to the rear end of the fuselage; a main controlis arranged in that fuselage, and the main controller is connected with a lifting device. The lifting device provides vertical lift for the aircraft. The lifting device comprises eight motors providedwith paddles, eight motors are fixed on both sides of the fuselage 1 through a support frame and eight motors are symmetrically arranged on the left and right sides of the wing. The movable airfoil comprises a left rudder surface and a right rudder surface, and the left rudder surface and the right rudder surface are symmetrically movably connected with the wing ends on the left and right sides of the fuselage tail. The power unit is arranged at the front end of the fuselage. The invention can carry out vertical lifting and lowering, has two ways of providing lifting force, a plurality of batteries supply power to motors at different positions respectively, and has high safety factor. Ideal for air patrols, surveillance, logistics and transportation.