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Ensemble approaches for leveraging machine learning models in load estimation

Published online by Cambridge University Press:  03 November 2023

C. Cheung*
Affiliation:
Aerospace Research Centre, National Research Council Canada, 1200 Montreal Rd, Ottawa, ON K1A 0R6, Canada
E. Seabrook
Affiliation:
Aerospace Research Centre, National Research Council Canada, 1200 Montreal Rd, Ottawa, ON K1A 0R6, Canada
J.J. Valdés
Affiliation:
Digital Technologies Research Centre, National Research Council Canada, 1200 Montreal Rd, Ottawa, ON K1A 0R6, Canada
Z.A. Hamaimou
Affiliation:
Aerospace Research Centre, National Research Council Canada, 1200 Montreal Rd, Ottawa, ON K1A 0R6, Canada
C. Biondic
Affiliation:
Aerospace Research Centre, National Research Council Canada, 1200 Montreal Rd, Ottawa, ON K1A 0R6, Canada
*
Corresponding author: C. Cheung; Email: catherine.cheung@nrc-cnrc.gc.ca

Abstract

Helicopter component load estimation can be achieved through a variety of machine learning techniques and algorithms. A range of ensemble integration techniques were investigated in order to leverage multiple machine learning models to estimate main rotor yoke loads from flight state and control system parameters. The techniques included simple averaging, weighted averaging and forward selection. Performance of the models was evaluated using four metrics: root mean squared error, correlation coefficient and the interquartile ranges of these two metrics. When compared, every ensemble outperformed the best individual model. The ensembles using forward selection achieved the best performance. The resulting output is more robust, more highly correlated and achieves lower error values as compared to the top individual models. While individual model outputs can vary significantly, confidence in their results can be greatly increased through the use of a diverse set of models and ensemble techniques.

Type
Research Article
Copyright
© National Research Council Canada, 2023. Published by Cambridge University Press on behalf of Royal Aeronautical Society

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Footnotes

A version of this paper first appeared at The Australian International Aerospace Congress 2021 (AIAC19).

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