The invention relates to the field of unmanned aerial vehicles, in particular to a rotor unmanned aerial vehicle landing auxiliary balancing device which comprises a vehicle body, blades arranged on the periphery of the vehicle body, supporting rods mounted at the bottoms of the blades and a driving mechanism, a fluted disc is arranged in the center of the bottom of the vehicle body, and a sliding groove, an inserting groove and a transmission part are arranged at the bottom of the vehicle body. A base is arranged in the sliding groove. The follow-up mechanism comprises a fixing block and a T-shaped block which are arranged in the sliding groove, a pulling part and a locking part are arranged on the T-shaped block, and an unlocking part is arranged on the base; the adjusting mechanism comprises a tooth groove in the T-shaped block, an overturning rod is arranged on the base, a tooth block is arranged on the arc-shaped side wall of the overturning rod and meshed with the tooth groove, one end of the overturning rod is connected with a telescopic part, and a reset part, a limiting part and an adjusting part are arranged on the telescopic part. And through the arrangement of the driving mechanism, the follow-up mechanism and the adjusting mechanism, the unmanned aerial vehicle can be adjusted according to the supporting surface of the ground.