Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.13087/3301
Title: Thrust modelling of a target drone engine with nonlinear least - squares estimation based on series expansions
Authors: Kaba, Aziz
Yurdusevimli Metin, Ece
Turan, Önder
Keywords: Aircraft
Nonlinear least squares
Turbojet
Microturbo target drone
Series expansion
Thrust modeling
Issue Date: 2022
Publisher: Emerald Group Publishing Ltd
Abstract: Purpose The purpose of this study is to build a high accuracy thrust model under various small turbojet engine shaft speeds by using robust, ordinary, linear and nonlinear least squares estimation methods for target drone applications. Design/methodology/approach The dynamic shaft speeds from the test experiment of a target drone engine is conducted. Then, thrust values are calculated. Based on these, the engine thrust is modeled by robust linear and nonlinear equations. The models are benefited from quadratic, power and various series expansion functions with several coefficients to optimize the model parameters. Findings The error terms and accuracy of the model are given using sum of squared errors, root mean square error (RMSE) and R-squared (R-2) error definitions. Based on the multiple analyses, it is seen that the RMSE values are no more than 17.7539 and the best obtained result for robust least squares estimation is 15.0086 for linear at all cases. Furthermore, the R-2 value is found to be 0.9996 as the highest with the nonlinear Fourier series expansion model. Originality/value The motivation behind this paper is to propose robust nonlinear thrust models based on power, Fourier and various series expansion functions for dynamic shaft speeds from the test experiments.
URI: https://doi.org/10.1108/AEAT-08-2021-0236
https://hdl.handle.net/20.500.13087/3301
ISSN: 1748-8842
1758-4213
Appears in Collections:Pilotaj Bölümü Koleksiyonu
Scopus İndeksli Yayınlar Koleksiyonu
WoS İndeksli Yayınlar Koleksiyonu

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