Badanie wpływu praw sterowania kursem samolotu na jakość automatycznego sterowania lotem

In this paper the velocity, height and course control laws have been described. For investigations, as an example maneuver, the coordinated turn of 15 deg with stabilised velocity and height has been chosen. The influence of coefficients of course control laws on the dynamics of flight and transition processes has been described. The results of an example of computer simulation of the chosen phase of flight have been shown.