Metoda syntezy algorytmu adaptacji układu stabilizacji samolotu

In the paper we have proposed a general method of syntesis of adaptation algorithms on the example of the oblong channel of the supersonic aircraft. The method consists in, firstly, defining the transient criterion of information about the values of parameters of the mathematical model and secondly, determining the changes of the values of the parameters of stabilization system in the function the values of which have been approximated by an analytic function i.e., the algorithm of adaptation of stabilization system of aircraft. The criterion of information is defined for a given mathematical model of aircraft from the condition that the appropriate quality of transient process of stabilization system has been achieved.