Wyznaczanie modelu sterowania samolotem zapewniającego ścisłą realizację ruchu programowego

In the paper the problem of exact realization of a program motion by an airplane has been considered. The program of motion was meant as a set of conditions imposed on the motion, or in other words a set of program constraints. The model of airplane control ensuring the simulated motion be consistent with the program constraint equations was determined. The problem was solved for a rigid airplane controlled by parameters. The criteria of control realizability in a certain program motion were also formulated. The program constraint conditions imposed on the system were transformed into the equivalent set of differential equations determining functions of control parameters.