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


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Abstract

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.

About the authors

A. V. Ivanov

Moscow Aviation Institute (National Research University)

Email: vint@aerosila.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993

A. M. Danilikhin

OAO Aerosila, Research and Production Enterprise

Email: vint@aerosila.ru
Russian Federation, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800

V. V. Baranov

OAO Aerosila, Research and Production Enterprise

Author for correspondence.
Email: vint@aerosila.ru
Russian Federation, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800

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