Problem stabilizacji samolotu z zastosowaniem identyfikacji parametrycznej

The problem of stabilization of an aircraft in the oblong channel with regard to changes of its static and dynamic parameters is analysed. The changes are determined by means of parametric identification of discrete mathematical model of aircraft by the method of least squares. The results of identification provide the basis for correcting the values of the parameters of stabilization system provided proper algorithms of adaptation during changeable conditions of the flight are used. The problems of identification, stabilization and adaptation are presented on the assumption that small changes of the parameters of the mathematical model of aircraft take place during the transient process of identification and adaptation.