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Turbo Prop Fan Engine Identification: Practical Issues

  • Gennady G. Kulikov
  • Haydn A. Thompson
Part of the Advances in Industrial Control book series (AIC)

Abstract

In this chapter, the identification techniques considered in previous chapters are applied to a real-life power plant. Dynamic models of a turbo prop fan aero engine are identified. Practical issues of closed-loop identifiability are also demonstrated.

Keywords

Angular Position Practical Issue Proportional Integrate Controller Coherence Function Compressor Pressure 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. 1.
    Kulikov GG, Arkov VY, Breikin TV. On condition monitoring of FADEC information channels. Russian Aeronautics, 1995;4:81–85.Google Scholar
  2. 2.
    Ljung L. System Identification Toolbox for Use with MATLAB: User’s Manual. Natick, MA: Mathworks, Inc., 1991.Google Scholar
  3. 3.
    Arkov V, Kulikov G. Gas turbine engine frequency response function identification using spectral methods: Optimisation approach. In: Rahnejat H, Whalley R, editors. Multibody Dynamics: Monitoring and Simulation Techniques. London: Mechanical Engineering Publications, 1997; 123–131.Google Scholar

Copyright information

© Springer-Verlag London 2004

Authors and Affiliations

  • Gennady G. Kulikov
    • 1
  • Haydn A. Thompson
    • 2
  1. 1.Department of Automated Control SystemsUfa State Aviation Technical UniversityRussia
  2. 2.Department of Automatic Control and Systems EngineeringThe University of SheffieldSheffieldUK

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