Серія: Технічні науки. Випуск 18 tions of the rotational motion of a rigid body in the Rodrigues Hamilton parameters. In this paper, this approach was used to solve the main problems of controlling the angular motion of a spacecraft: stabilization problems and terminal control problems. The article may be useful to developers of spacecraft attitude control systems.

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Математичне та комп'ютерне моделювання 24 differential evolution is not worse than using much more complicated deterministic algorithms of the best uniform approximation. This testifies about the effectiveness of the differential evolution algorithm. It can be used as an alternative for known deterministic algorithms of spline approximation.