The study of flight machine functions, modes dependencies and mathematical modeling of onboard control systems data flows

Abstract

This work is devoted to mathematical determination of the amount of data required to implement the functions of an automatic unmanned aircraft. A comparison of the characteristics of the investigated practical implementation of the aircraft with the declared functions was carried out. We calculate the percentage of the volume of technological data exchange and the calculator's reserve for the realization of automatic control functions. The work has the practical nature of introducing a new methodology, the stages of aircraft design to reduce subsequent revisions.