Разработка алгоритма создания нейросетевой модели малоразмерного газотурбинного двигателя

Abstract

The study covers the development of recurrent neural network mathematical model of micro gas turbine (MGTE) under transient conditions. In order to verify the developed model we have used thermodynamic mathematical dynamic MGTE model based on per-unit description. The engine face temperature and pressure via aircraft height and speed have been taken into account explicitly.