Invention Title: A Quadrotor-Autorotor Combined with a Vertical Take-Off and Landing Variant Aircraft and Control Method This specification discloses a quadrotor-autorotor combined with a vertical take-off and landing (VTOL) variant aircraft and its control method, belonging to the field of aircraft technology. The aircraft includes: a power
system, a flight
control system, a quadrotor
system, an autorotor
system, and a
variator system. The power system provides power to the aircraft; the flight
control system is responsible for regulating the parameters of the quadrotor system and the
variator system; the quadrotor system provides lift when the aircraft is in a
stable state (VTOL or hovering), and provides forward and steering power when the aircraft is in
cruise mode; the autorotor system provides lift when the aircraft is in
cruise mode; the
variator system rotates the quadrotor variator spindle via a driver, thereby rotating the quadrotor motors' planar angle. Combined with the flight
control system's regulation of the quadrotor motor's planar angle and the speed of the four motors, a reasonable distribution of
horizontal and vertical forces is achieved, enabling a smooth transition between stable and
cruise states. Compared to traditional autogyros, this aircraft can take off and land vertically and hover. Its control is simple and efficient. Compared to traditional quadcopters, it is more energy-efficient and
safer. This invention combines the advantages of both quadcopters and autogyros, resulting in an economical, easy-to-
handle, safe, and reliable vertical
takeoff and landing flight platform.