The invention discloses a power-operated
tail-sitting type mixed
layout vertical take-off and landing aircraft. The power-operated
tail-sitting type mixed
layout vertical take-off and landing aircraft is composed of a
fuselage, airfoils, motors, propellers and landing gears; the
fuselage axis coincides with the OX axis of a body axial
system, the projections of the
fuselage axis and the OX axis in an XOY plane of the body axial
system are distributed in an X shape; each airfoil on the fuselage is divided into several sections, sweepback angles and dihedral angles of all the sections are different from one another, and excellent pneumatic performance and maneuvering performance are achieved through positively-curved airfoil profiles and negatively-curved airfoil profiles; four sets of
propeller-
motor power systems are installed on the four airfoils correspondingly, and the distances between the positions where the
propeller-
motor power systems are located and the OX axis of the body axial
system are the same; and four power devices take off in an X-shaped quad-rotor mode in the vertical take-off and landing processes and complete conversion operation to enter a cruising state through different tensile forces of the motors or by being matched with maneuvering surfaces, and required maneuvering is completed through tensile force changing of the motors in the whole process. The power devices of the aircraft are simple, the
control mode is reliable,
propeller slipstreams can be effectively utilized, and the aircraft is suitable for serving as flying platforms of a
tail-sitting type vertical take-off and landing unmanned aerial vehicle.