Abstract. A method is developed for compensating the effect of wind disturbances on the flight path of an aircraft. Computer simulation of the method is performed. An approach is considered based on methods of the theory of absolute nonlinear invariance. The results of computer simulation of the developed method for compensating the influence of turbulent atmosphere on the flight of an aircraft are presented with a view to comparing its efficiency with an available method for compensating the influence of turbulent atmosphere. The use of the conception of aircraft control based on the theory of absolute nonlinear invariance in designing automatic control systems will make it possible to implement an efficient method for flight control under uncertainty and external disturbances that has advantages over existing methods and will provide the comfort of passengers and safeness of flights.

Keywords: disturbance, compensation, control, aircraft, invariance.