Hardware-in-the-loop testing technology for integrated control and condition monitoring systems of aircraft gas turbine engines-Reference-Cited by-同舟云学术

Hardware-in-the-loop testing technology for integrated control and condition monitoring systems of aircraft gas turbine engines

Published:2008-03 Issue:1 Volume:51 Page:47-52
ISSN:1068-7998
Container-title:Russian Aeronautics (Iz VUZ)
language:en
Short-container-title:Russ. Aeronaut.

Author:

Kulikov G. G.,Ar’kov V. Yu.,Abdulnagimov A. I.

Publisher

Allerton Press

Subject

Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.3103/S106879980801008X.pdf

Reference7 articles.

1. Ito, K. and Nakagawa, T., Optimal Self-Diagnosis Policy for FADEC of Gas Turbine Engines, Mathematical and Computer Modelling, 2003, vol. 38, pp. 1243–1248.

2. Rutkovskii, V.Yu., Kulikov, G.G., Kotenko, P.S., Fatikov, V.S., Ar’kov, V.Yu, and Pogorelov, G.I., Intelligent Information Technologies for Monitoring and Diagnostics of Aircraft Engines and Their Systems over the Course of Life Cycle, Trudy Instituta Problem Upravleniya RAN, Moscow, 2002, vol. 19, pp. 25–33.

3. Ar’kov, V.Yu., Kulikov, G.G., Epifanov, S.V., and Minaev, I.I., Hardware-in-the Loop Simulation of GTE Failures for Engine Monitoring and Diagnostics System Tests, Aviatsionno-Kosmicheskaya Tekhnika i Tekhnologiya, 2004, no. 7 (15), pp. 167–173.

4. Shannon, R.E., Systems Simulation: the Art and Science, Prentice Hall, Englewood Cliffs, 1975.

5. Dynamic Modeling of Gas Turbines: Identification, Simulation, Condition Monitoring and Optimal Control, Kulikov, G.G. and Thompson, H.A., Eds., London: Springer-Verlag, 2004.

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