Komputerowy model dynamiki lotu samolotu zweryfikowany próbami w locie

The paper presents a computer model of a subsonic aircraft flight dynamics. The equations of model presented in works [1-3] have been applied. Aerodynamic characteristics of an aircraft that had previously been obtained by means of wind tunnel tests as wellas analytic methods have been improved due to test flights of a real aircraft. The comparative results of flight tests of a real aircraft and its computer model have been shown.