AUTOMATIC TAKEOFF APPARATUS FOR AIRCRAFT, AUTOMATIC LANDING APPARATUS FOR AIRCRAFT, AUTOMATIC TAKEOFF AND LANDING APPARATUS FOR AIRCRAFT, AUTOMATIC TAKEOFF METHOD FOR AIRCRAFT, AUTOMATIC LANDING METHOD FOR AIRCRAFT AND AUTOMATIC TAKEOFF AND LANDING METHOD FOR AIRCRAFT

摘要

An automatic takeoff apparatus for an aircraft includes: an altitude sensor; an airspeed sensor; an attitude angle sensor; a direction sensor; a takeoff command inputting section; and a control device for controlling a propulsion device and an control surface of the aircraft, wherein the control device includes: a takeoff run control section for realizing a takeoff run by controlling the propulsion device to provide a maximum output and by controlling the control surface to maintain the attitude angle and the traveling direction constant, in response to the takeoff command; a rotation control section for controlling the control surface to rotate when the airspeed exceeds a predetermined speed; and an ascending flight control section for controlling the propulsion device and the control surface to perform an ascending flight up to a target altitude with a predetermined speed maintained, when the altitude exceeds a predetermined altitude.