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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

  • Aircraft and Rocket Engine Theory
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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.

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References

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Authors and Affiliations

  1. Moscow Aviation Institute (National Research University), Volokolamskoe sh. 4, Moscow, 125993, Russia

    A. V. Ivanov

  2. OAO Aerosila, Research and Production Enterprise, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800, Russia

    A. M. Danilikhin & V. V. Baranov

Authors
  1. A. V. Ivanov
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  2. A. M. Danilikhin
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  3. V. V. Baranov
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Corresponding author

Correspondence to V. V. Baranov.

Additional information

Original Russian Text© A.V. Ivanov, A.M. Danilikhin, V.V. Baranov, published in Izvestiya Vysshikh Uchebnykh Zavedenii. Aviatsionnaya Tekhnika, 2018, No. 1, pp. 131–136.

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Ivanov, A.V., Danilikhin, A.M. & Baranov, V.V. 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. Russ. Aeronaut. 61, 138–144 (2018). https://doi.org/10.3103/S1068799818010221

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  • DOI: https://doi.org/10.3103/S1068799818010221

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