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Off-line Models

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

Abstract

The level of complexity of aero gas turbine engine modelling in terms of dynamic and static accuracy can vary dramatically depending on the model’s intended usage: research, analysis or synthesis of control systems. In this chapter the development of models for off-line use is discussed. Typically these models would be used in simulation exercises during engine design and development of the control system to establish performance criteria. For example, the stability study of a system for a given operating point can be conducted using classical control theory methods [1, 2] on a linear model of a turbine engine. However, the same problem can be solved with the use of a detailed thermodynamic model in the time domain.

Keywords

Operating Point Control System Design Flight Condition Fuel Flow Shaft Speed 
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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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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