Identyfikacja parametryczna modelu matematycznego samolotu

Tlie present paper deals with the problem of parametric identification of discrete mathematical mode of aircraft in the oblong channel solved by means of the method of least squares. It is shown that identification of parameters of non-stationary mathematical model is possible in the real time basing upon passive experiment consisting of measurement of input signal as well as one or all variables of the state of the model. The convergence of the identification algorithms being obtained and the problem of determining of continuous mathematical model on the basis of discrete model resulting from parametric identification has been analysed.