Numeryczna symulacja programowej realizacji figur akrobacji lotniczej

Examples of numerical simulation of some aerobatic maneouvres are presented. The program flights are modelled using some constraints imposed on an aircraft trajectory, a aircraft angular orientation in the space and a speed history. Histories of the state parameter variations and the demanded control are obtained. An emphasis is laid on the trajectory path description by means of a succesion-of-points. A spline function smoothing is applied for interpolation and approximation formulas.