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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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.

作者简介

A. Ivanov

Moscow Aviation Institute (National Research University)

Email: vint@aerosila.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

A. Danilikhin

OAO Aerosila, Research and Production Enterprise

Email: vint@aerosila.ru
俄罗斯联邦, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800

V. Baranov

OAO Aerosila, Research and Production Enterprise

编辑信件的主要联系方式.
Email: vint@aerosila.ru
俄罗斯联邦, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800

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