Identification of a gas turbine engine mathematical model by the ressults of testing

Abstract

The paper deals with the identification of a linear mathematical model of gas turbine engines by the results of testing using the simplest Huber method with regard to additional information on engine parameter measurement error and possible magnitudes of parameter variations characterizing unit operation.

About the authors

S. K. Botchkaryov

Samara State Aerospace University

Author for correspondence.
Email: bochkar@ssau.ru
Russian Federation

A. Ya. Dmitriyev

Samara State Aerospace University

Email: bochkar@ssau.ru
Russian Federation

References

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