Use of a Nonlinear Mathematical Model of Turboprop Engine on a Semi-Full-Scale Simulation Test Bench for Testing Propellers in Conjunction with Their Automatic Control System

摘要

This paper considers an issue of increasing reliability of turboprop engine simulation on a semi-full-scale simulation test bench. A detailed mathematical model (subassembly model) of a turboprop engine is used for improving simulation quality and optimizing the algorithms of turboprop automatic control system in the operation conditions being expected.