Development of a Power Supply System for a Single-engine Aircraft

This article discusses options for power supply systems for use on a single-engine aircraft, as well as the choice of the type of electricity used and the structure of the power supply system. This choice is made based on the totality of requirements imposed by standards, specified operating modes, as well as the need to provide consumers with electricity at any given time in accordance with their functional purpose. Formalization is carried out on the basis of a structural and functional approach.