The invention belongs to the technical field of helicopter dynamics, and relates to a method for adjusting vibration in a rotating surface of a rotor hub of a helicopter. The method comprises two parts, specially, the adjustment of a hub shimmy damper and the adjustment of a hub weight stack are carried out, when the vibration eccentric force in the rotating surface of the rotor hub reaches 60-100kg or the speed value of the vertical vibration in a cabin reaches 0.6-1 IPS, and the hub shimmy damper is adopted to adjust; when the vibration eccentric force in the rotating surface of the rotor hub is less than 60 kg or the speed value of the vertical vibration in the cabin is less than 0. 6g IPS, and the hub weight stack is adopted to adjust. According to the method, the defects of a currentsingle adjustment mode can be overcome, and the vibration environment of the helicopter is ensured to be kept at a comfortable level.