Kriging and Radial Basis Function Models for Optimized Design of UAV Wing Fences to Reduce Rolling Moment

IF 5 2区 计算机科学 Q1 COMPUTER SCIENCE, ARTIFICIAL INTELLIGENCE International Journal of Intelligent Systems Pub Date : 2024-02-27 DOI:10.1155/2024/4108121
Mohammad Hossein Moghimi Esfand-Abadi, Mohammad Hassan Djavareshkian, Afshin Madani
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Abstract

In the present study, the effects of the wing fence on the wing tip vortices and control surfaces located at the tip of the wing in a flying wing aircraft have been investigated using a numerical method. For the size of the fences, the average dimensions extracted from the wing tip vortices at different angles of attack are used. The basic determining parameter is the rolling torque coefficient, which is tried to be shown by employing a parametric study of the flow behavior in different situations of fence placement. These effects on the rolling torque of the aircraft are measured due to the presence of the split drag rudder control system. In this study, the fences were installed at three different heights and three different positions along the length of the wing, which were investigated at angles of attack of 7 to 16 degrees. The next stage of the research is to design the dimensions of the fence using the single-objective optimization method (a method to find the best solution for a problem with a specific goal). The designing of the fences at three points based on the dimensions of the wing tip vortex is carried out with the computational fluid dynamics (CFD) method (CFD is a computational method that uses physical laws to predict the behavior of fluids.). The aim of this research is to achieve the best design that converges to an optimal solution with minimum time and cost (CFD solution is long). However, CFD analysis requires a lot of computational time. To address this challenge, we employed a hybrid learning model comprising the radial basis function (RBF), a type of artificial neural network, and Kriging, a Gaussian process-based interpolation technique. The dataset for training the hybrid model was obtained from numerical solutions of CFD simulations involving a fence placed at various locations on the wing. Additionally, a genetic algorithm was employed as the optimization method in all instances where it was required. Using the power of machine learning techniques helped us identify the optimal placement of the fence to prevent it from being engulfed by the vortex and to optimize the utilization of the split drag system, yielding significant improvements.

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用于优化设计无人机机翼围栏以减少滚动力矩的克里金法和径向基函数模型
本研究采用数值方法研究了机翼栅栏对飞翼飞机翼尖涡流和翼尖控制面的影响。对于栅栏的尺寸,采用了从不同攻角下的翼尖涡流中提取的平均尺寸。基本决定参数是滚动扭矩系数,通过对不同栅栏放置情况下的流动行为进行参数化研究,试图显示出这一系数。这些对飞机滚动扭矩的影响是在分拖舵控制系统存在的情况下测量的。在这项研究中,栅栏被安装在机翼长度方向上的三个不同高度和三个不同位置,研究的攻角为 7 至 16 度。研究的下一阶段是使用单目标优化法(一种为具有特定目标的问题寻找最佳解决方案的方法)设计栅栏的尺寸。根据翼尖涡流的尺寸,利用计算流体动力学(CFD)方法(CFD 是一种利用物理规律预测流体行为的计算方法)设计三点栅栏。这项研究的目的是以最少的时间和成本(CFD 解决方案耗时较长)实现收敛到最优解的最佳设计。然而,CFD 分析需要大量的计算时间。为了应对这一挑战,我们采用了一种混合学习模型,包括径向基函数(一种人工神经网络)和克里金(一种基于高斯过程的插值技术)。用于训练混合模型的数据集来自 CFD 模拟的数值解,涉及机翼上不同位置的栅栏。此外,在所有需要优化的情况下,都采用了遗传算法作为优化方法。利用机器学习技术的强大功能,我们确定了栅栏的最佳位置,以防止其被涡流吞噬,并优化了分体式阻力系统的利用,取得了显著的改进。
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来源期刊
International Journal of Intelligent Systems
International Journal of Intelligent Systems 工程技术-计算机:人工智能
CiteScore
11.30
自引率
14.30%
发文量
304
审稿时长
9 months
期刊介绍: The International Journal of Intelligent Systems serves as a forum for individuals interested in tapping into the vast theories based on intelligent systems construction. With its peer-reviewed format, the journal explores several fascinating editorials written by today''s experts in the field. Because new developments are being introduced each day, there''s much to be learned — examination, analysis creation, information retrieval, man–computer interactions, and more. The International Journal of Intelligent Systems uses charts and illustrations to demonstrate these ground-breaking issues, and encourages readers to share their thoughts and experiences.
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