The invention relates to a method for guiding the landing of an unmanned aerial vehicle in the wind disturbance environment, which solves the problem that the method for guiding the landing of the unmanned aerial vehicle in the wind disturbance environment is low in guiding precision and belongs to the field of landing control of the unmanned aerial vehicle. The method comprises the steps of S1, solving an auxiliary optimal control problem of transferring the unmanned aerial vehicle from any initial position to a final position under the control constraint condition and the windless condition,calculating to obtain a guiding movement track of the unmanned aerial vehicle, and providing the specific control constraint condition; S2, solving a problem of maximum approximation of the unmannedaerial vehicle movement track and the guiding movement track under the condition that the random component of wind is given, and determining a control law of the unmanned aerial vehicle, wherein the random component of the wind speed is a random function with given statistical properties, [sigma]W is greater than or equal to 0 and less than or equal to abs([sigma]W)M, [sigma]W represents the rootmean square of the random component of the wind speed, and abs([sigma]W)M represents the maximum allowable value of [sigma]W; and S3, realizing the landing guidance of the unmanned aerial vehicle by using the control law of the unmanned aerial vehicle. The method is applied to the landing of the unmanned aerial vehicle (UAV) on a small mobile platform in the wind disturbance environment.