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Identification of a gas turbine engine mathematical model by the ressults of testing
- Authors: Botchkaryov S.K.1, Dmitriyev A.Y.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 7, No 1 (2008)
- Pages: 37-39
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/542
- DOI: https://doi.org/10.18287/2541-7533-2008-0-1(14)-37-39
- ID: 542
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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
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