N. V. Sukhanov, A. V. Zajtsev, A. N. Nikishov, L. L. Talimanchuk, A. A. Oleynik

This article describes the results of modelling intellectual pitch stabilization system of an aircraft on an extra-atmospheric phase of flight. The practical possibility of constructing intellectual aircraft control systems on the basis of the neural networks theory is proved. The authors suggest the method to modernize the observed algorithm for the inverse-adaptive control diagram of the composite dynamic object.