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Small unmanned helicopter system identification based on the weighted least square method and improved grey wolf optimisation algorithm

Published online by Cambridge University Press:  03 February 2025

SY. Liu
Affiliation:
School of Electronics and Information, Xi’an Polytechnic University, Xi’an, Shanxi, China
J. Zhou*
Affiliation:
School of Electronics and Information, Xi’an Polytechnic University, Xi’an, Shanxi, China
JY. Shi
Affiliation:
School of Electronics and Information, Xi’an Polytechnic University, Xi’an, Shanxi, China
J. Lu
Affiliation:
School of Electronics and Information, Xi’an Polytechnic University, Xi’an, Shanxi, China
*
Corresponding author: J. Zhou; Email: zhoujian0627@163.com

Abstract

Aiming to address the issue of low accuracy in model predictions obtained from fitting frequency domain response curves for small unmanned helicopters during the process of modeling their flight dynamics, this study proposes a system identification algorithm based on the combination of weighted least squares and improved grey wolf optimisation algorithm. The algorithm utilises the weighted least squares method to obtain the initial model structure, optimises the initial model parameters using the improved grey wolf optimisation algorithm, and enhances the local search and global optimisation ability of the grey wolf optimisation algorithm by introducing an improved grey wolf subgrouping rule, nonlinear convergence factor and dynamic cooperative rule. Ultimately, this approach establishes a dynamic model for small, unmanned helicopters. The identified model is validated using flight test data, with findings demonstrating that this method achieves higher accuracy in model identification and better fits to frequency domain response curves, thus providing a more accurate reflection of the flight dynamics of small unmanned helicopters.

Information

Type
Research Article
Copyright
© The Author(s), 2025. Published by Cambridge University Press on behalf of Royal Aeronautical Society

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