A neural-metaheuristic kalman filter for moving microburst wind shear identification

IF 3.7 3区 计算机科学 Q2 AUTOMATION & CONTROL SYSTEMS
E. Mohajeri , Seid H. Pourtakdoust , F. Pazooki
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引用次数: 0

Abstract

Microburst wind shears (MB) are powerful localized three dimensional (3D) columns of wind that occur when cooled air drops from the base of thunderstorms at high speeds. They eventually hit the ground and spread out in all directions. As such MBs are considered a major atmospheric hazard for aircrafts (ACs), especially in terminal flight phases. Though pilots train regularly to survive it, yet the most recommended practice within the aviation community is to avoid its encounter upon detection. Some modern aircrafts have predictive wind shear warning systems, but they have limited short range capability and do not provide quantitative data for engineering application. In this sense, accurate onboard detection and identification of MBs and its characteristics is of importance for flight safety, whose success can lead to design of automatic flight control systems (FCSs) that reduce the risk of aircraft crash landings and accidents. Even though there are some studies on FCS designs for MB encounter, research on MB identification is rare but ongoing. To this aim, the present study is among the firsts that focuses on online identification of multiple and moving MB parameters using onboard aircraft air data and inertial sensors. The identification task is initially performed using the aircraft six degrees of freedom (6DoF) equations of motion (EOM) integrated with a 3D MB model via the utility of nonlinear Kalman filtering (KF) algorithms. Subsequently, an enhanced neural metaheuristic Kalman filter (NMKF) is proposed that improves the estimation accuracy of the MB model parameters. The results demonstrate the efficacy of the proposed NMKF in comparison with previous studies.
用于移动微爆风切变识别的神经-元启发式卡尔曼滤波器
微爆风切变(MB)是一种强大的局部三维(3D)风柱,当冷却空气从雷暴底部高速下降时就会产生这种风柱。它们最终撞击地面并向四面八方扩散。因此,雷暴气流被认为是飞机(AC)的主要大气危害,尤其是在终端飞行阶段。尽管飞行员定期接受培训以应对这种飞行物,但航空界最推荐的做法是在发现飞行物时避免与其相遇。一些现代飞机拥有预测性风切变预警系统,但其短程能力有限,无法提供工程应用所需的定量数据。从这个意义上说,准确的机载检测和识别 MBs 及其特征对飞行安全非常重要,其成功可促进自动飞行控制系统(FCS)的设计,从而降低飞机迫降和事故的风险。尽管有一些关于遇到 MB 的飞行控制系统设计的研究,但关于 MB 识别的研究还很少,而且仍在进行中。为此,本研究是首批利用机载航空数据和惯性传感器对多个移动 MB 参数进行在线识别的研究之一。识别任务最初使用飞机六自由度(6DoF)运动方程(EOM),并通过非线性卡尔曼滤波(KF)算法与三维 MB 模型集成。随后,提出了一种增强型神经元启发式卡尔曼滤波器(NMKF),可提高 MB 模型参数的估计精度。结果表明,与之前的研究相比,所提出的 NMKF 非常有效。
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来源期刊
CiteScore
7.30
自引率
14.60%
发文量
586
审稿时长
6.9 months
期刊介绍: The Journal of The Franklin Institute has an established reputation for publishing high-quality papers in the field of engineering and applied mathematics. Its current focus is on control systems, complex networks and dynamic systems, signal processing and communications and their applications. All submitted papers are peer-reviewed. The Journal will publish original research papers and research review papers of substance. Papers and special focus issues are judged upon possible lasting value, which has been and continues to be the strength of the Journal of The Franklin Institute.
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