Capturing Aerodynamic Characteristics of ATTAS Aircraft with Evolving Intelligent System

• URL: http://arxiv.org/abs/2504.19949v1
• Date: Mon, 28 Apr 2025 16:21:20 GMT
• Title: Capturing Aerodynamic Characteristics of ATTAS Aircraft with Evolving Intelligent System
• Authors: Aydoğan Soylu, Tufan Kumbasar,
• Abstract summary: This paper presents the novel deployment of an Evolving Type-2 Quantum Fuzzy Neural Network (eT2QFNN) for modeling the aerodynamic coefficients of the ATTAS aircraft.<n>eT2QFNN can represent the nonlinear aircraft model by creating multiple linear submodels with its rule-based structure.<n>It enhances robustness to uncertainties and data noise through its quantum membership functions.
• Score: 2.8391355909797644
• License: http://creativecommons.org/licenses/by-nc-sa/4.0/
• Abstract: Accurate modeling of aerodynamic coefficients is crucial for understanding and optimizing the performance of modern aircraft systems. This paper presents the novel deployment of an Evolving Type-2 Quantum Fuzzy Neural Network (eT2QFNN) for modeling the aerodynamic coefficients of the ATTAS aircraft to express the aerodynamic characteristics. eT2QFNN can represent the nonlinear aircraft model by creating multiple linear submodels with its rule-based structure through an incremental learning strategy rather than a traditional batch learning approach. Moreover, it enhances robustness to uncertainties and data noise through its quantum membership functions, as well as its automatic rule-learning and parameter-tuning capabilities. During the estimation of the aerodynamic coefficients via the flight data of the ATTAS, two different studies are conducted in the training phase: one with a large amount of data and the other with a limited amount of data. The results show that the modeling performance of the eT2QFNN is superior in comparison to baseline counterparts. Furthermore, eT2QFNN estimated the aerodynamic model with fewer rules compared to Type-1 fuzzy counterparts. In addition, by applying the Delta method to the proposed approach, the stability and control derivatives of the aircraft are analyzed. The results prove the superiority of the proposed eT2QFNN in representing aerodynamic coefficients.

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