Redesign of morphing UAV's winglet using DS algorithm based ANFIS model

Mehmet Konar (Department of Aircraft Electrical and Electronics, Faculty of Aeronautics and Astronautics, Erciyes University, Kayseri, Turkey)

Aircraft Engineering and Aerospace Technology

ISSN: 1748-8842

Publication date: 19 June 2019

Abstract

Purpose

The purpose of this paper is to present a novel approach based on the differential search (DS) algorithm integrated with the adaptive network-based fuzzy inference system (ANFIS) for unmanned aerial vehicle (UAV) winglet design.

Design/methodology/approach

The winglet design of UAV, which was produced at Faculty of Aeronautics and Astronautics in Erciyes University, was redesigned using artificial intelligence techniques. This approach proposed for winglet redesign is based on the integration of ANFIS into the DS algorithm. For this purpose, the cant angle (c), the twist angle (t) and taper ratio (λ) of winglet are selected as input parameters; the maximum value of lift/drag ratio (Emax) is selected as the output parameter for ANFIS. For the selected input and output parameters, the optimum ANFIS parameters are determined by the DS algorithm. Then the objective function based on optimum ANFIS structure is integrated with the DS algorithm. With this integration, the input parameters for the Emax value are obtained by the DS algorithm. That is, the DS algorithm is used to obtain both the optimization of the ANFIS structure and the necessary parameters for the winglet design. Thus, the UAV was reshaped and the maximum value of lift/drag ratio was calculated based on new design.

Findings

Considerable improvements on the max E are obtained through winglet redesign on morphing UAVs with artificial intelligence techniques.

Research limitations/implications

It takes a long time to obtain the optimum Emax value by the computational fluid dynamics method.

Practical implications

Using artificial intelligence techniques saves time and reduces cost in maximizing Emax value. The simulation results showed that satisfactory Emax values were obtained, and an optimum winglet design was achieved. Thus, the presented method based on ANFIS and DS algorithm is faster and simpler.

Social implications

The application of artificial intelligence methods could be used in designing more efficient aircrafts.

Originality/value

The study provides a new and efficient method that saves time and reduces cost in redesigning UAV winglets.

Keywords

Citation

Konar, M. (2019), "Redesign of morphing UAV's winglet using DS algorithm based ANFIS model", Aircraft Engineering and Aerospace Technology, Vol. ahead-of-print No. ahead-of-print. https://doi.org/10.1108/AEAT-09-2018-0255

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Publisher

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Emerald Publishing Limited

Copyright © 2019, Emerald Publishing Limited

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