Several models of artificial intelligence elements for airctaft control

It is made an attempt to find some optimal measure for the coefficient of a proportional governor augmentation in the aircraft navigation and motion linear model inertness-less object control system as continuous alternatives individual preferences densities distributions, using the preferences subjective entropy maximum principle, proposed by Professor V.A. Kasianov (National Aviation University, Kyiv, Ukraine) in case of one and two-dimensions. It is obtained the continuous alternative preferences distribution densities; this together with the preferences distributions for the predetermined time points allows making the optimal choice of the available aircraft navigation. Theoretical speculations are illustrated with the example calculation experiments. The necessary diagrams are plotted.