The invention provides a single-man manual-control rotorcraft which is composed of a rotorcraft body, a rotor shaft cantilever tilt structure, a full-manual-control mechanism and a rotor head mechanism having an internal variable distance function. The rotorcraft body has a high-gravity center normal-three-point undercarriage structure, wherein the main rotorcraft body consists of a vertical column, a front beam, a back beam, an engine bracket and a front support beam. A steering wheel is arranged right ahead and empennages are arranged at the back. A driver seat and an engine are respectively at the front and the back of the vertical column. In the rotorcraft, a push-type propeller provides power and a three-point frame-type individual damping support mechanism having a rotor reactive force balancing device is used for balancing the reactive force generated to the rotorcraft body by air during operation of the rotor, so that the rotorcraft is improved in takeoff and landing stability. By means of the full-manual-control mechanism having a steering linking function, a driver can complete the operations comprising distance change of the rotor, rotor shaft tilt, flying direction turning and braking just like driving a motorbike.