The utility model relates to unmanned aerial vehicles. It finds application in remote sensing of ground objects, search and rescue operations, activities related to ecology, combating disasters and accidents, reconnaissance operations, etc. The vertical takeoff and landing aircraft consists of a fuselage (1), to which a right half-wing (2I) and a left half-wing (2II) are respectively connected. Engine nacelles with electric motors (3I and 3III) are attached directly to the right half-wing (2I), and an engine nacelle with an electric motor (3II) is mounted between them via a console (5I) to the half-wing (2I). Similarly, engine nacelles with electric motors (3IV and 3VI) are directly mounted to the left half-wing (2II), and an engine nacelle with an electric motor (3V) is attached via a console (5II). Propellers (4I, 4II, 4III, 4IV, 4V, and 4VI) are respectively mounted on the axes of all electric motors. 1 claim, 2 figures.
