PATH CONTROL AIRCRAFT OF TRAJECTORY UNDER THE INFLUENCE OF DISTURBANCES ON AN DUAL CHANNEL

Abstract

We discuss the problem of the invariance of the trajectory of the aircraft (LA) in relation to known external influences. It is shown that by splitting the optimal trajectory into segments and constructing invariant trajectory to the perturbation at each such interval, it is possible to obtain a quasi-strong invariance. The problem is solved using the algorithm with the predictive model.