Invariant Aircraft Control Under Wind Disturbances

A method is developed for compensating the effect of wind disturbances on the flight path of an aircraft. Computer modeling of the method is performed. An approach is considered based on methods of the theory of absolute nonlinear invariance. The results of computer modeling of the method developed for compensating the influence of turbulent atmosphere on the flight of an aircraft are presented with a view to comparing its efficiency with that of an existing 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 safety of flights.