The invention relates to an unmanned aerial vehicle which takes off and lands down vertically. The unmanned aerial vehicle has pneumatic arrangement of double bodies and remote duck wings, a power system of the unmanned aerial vehicle is composed of four propellers with tilting mechanisms, which are arranged in a 'Y'-shaped manner, variable wings based on flexible structures are adopted as wings of the unmanned aerial vehicle, and a control surface of the unmanned aerial vehicle is of a flexible seamless control surface structure. The unmanned aerial vehicle has the beneficial effects that dueto adoption of a tiltable multi-rotor wing system, vertical lifting and landing down are achieved, and a 'waste weight' caused by a useless power system is avoided in level flight; due to adoption ofthe power system between the two bodies, air flow interference between the propellers and the bodies is avoided; due to adoption of the double bodies, the body rigidity can be improved, and the bodyweight can be reduced; due to adoption of the remote duck wings, the lift coefficient of the whole vehicle is increased, the position of a pneumatic center is adjusted, the rigidity of the vehicle isimproved, and the weight of the vehicle is reduced; due to adoption of the self-adaptive wings based on flexible structures, the pneumatic appearances of the wings are at optimal states constantly; and due to adoption of the flexible seamless control surface, the wings and the control surface are in seamless connection, so that interference resistance is reduced.