Journal of Theoretical
and Applied Mechanics

30, 1, pp. 51-69, Warsaw 1992

Identyfikacja modelu dynamiki lotu poddźwiękowego samolotu

Jerzy Manerowski

A mathematical model of a subsonic jet aircraft was described with the aid of identification method by means of regression. Measurement results for some linked acrobatic figures were used for the identification. These flight measurement results and the time history of control as in the real flight, obtained for the described model, were presented. Some flight results, not used for the identification, were shown as well.