Abstract
The conclusion of the aircraft to a given track line is considered. The possibility of using for this purpose a nonlinear roll control algorithm with functions of functions is analyzed. The results of modeling of the guidance process are given, showing that the investigated nonlinear algorithm ensures the withdrawal of an aircraft from any points in space on a given path for any initial course in a calm atmosphere and in the presence of wind. Key words: line of a given path, roll control, trajectory control algorithm, motion control of the center of mass, lateral deviation.
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