Research on a backstepping flight control method improved by STFT in atmospheric disturbance applications

Ruichen Ming, Xiaoxiong Liu, Yu Li, WeiGuo Zhang
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Abstract

The adaptive backstepping method has strong performance in handling control problems with disturbances in previous research. However, it exhibits limitations when applied to time-varying disturbances. This paper proposes an improved adaptive backstepping method based on Discrete Fourier Transform (DFT). By estimating the frequency spectrum of the disturbance and indirectly obtaining its time-domain estimate, the proposed method effectively overcomes the shortcomings of traditional adaptive backstepping. To address the issue of frequency leakage caused by discontinuities in window data, the idea of DFT is improved by using STFT with the addition of the window function and window-shifting operation. Additionally, a projection operator and adaptive reduction of the control objective are employed to mitigate the effects of actuator saturation. Finally, in simulations involving an aircraft subjected to gusts and turbulence, the proposed method is compared with traditional adaptive backstepping and radial basis function (RBF) neural network control methods. Simulation results demonstrate that the proposed method outperforms the others in these experimental scenarios.
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大气扰动应用中 STFT 改进的反步态飞行控制方法研究
在以往的研究中,自适应反步法在处理有扰动的控制问题时表现出色。然而,当它应用于时变扰动时,却表现出了局限性。本文提出了一种基于离散傅立叶变换(DFT)的改进型自适应反步法。通过估计干扰的频谱并间接获得其时域估计值,该方法有效地克服了传统自适应反步法的缺点。为了解决窗口数据不连续造成的频率泄漏问题,利用 STFT 改进了 DFT 的思想,增加了窗口函数和窗口移动操作。此外,还采用了投影算子和自适应降低控制目标的方法,以减轻致动器饱和的影响。最后,在对遭受阵风和湍流的飞机进行模拟时,将所提出的方法与传统的自适应反步进和径向基函数(RBF)神经网络控制方法进行了比较。仿真结果表明,在这些实验场景中,所提出的方法优于其他方法。
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来源期刊
CiteScore
2.40
自引率
18.20%
发文量
212
审稿时长
5.7 months
期刊介绍: The Journal of Aerospace Engineering is dedicated to the publication of high quality research in all branches of applied sciences and technology dealing with aircraft and spacecraft, and their support systems. "Our authorship is truly international and all efforts are made to ensure that each paper is presented in the best possible way and reaches a wide audience. "The Editorial Board is composed of recognized experts representing the technical communities of fifteen countries. The Board Members work in close cooperation with the editors, reviewers, and authors to achieve a consistent standard of well written and presented papers."Professor Rodrigo Martinez-Val, Universidad Politécnica de Madrid, Spain This journal is a member of the Committee on Publication Ethics (COPE).
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Fatigue life analysis of a composite materials structure using allowable strain criteria Feasibility study of carbon-fiber reinforced polymer linerless pressure vessel tank Testability modeling of aeroengine and analysis optimization method based on improved correlation matrix Research on a backstepping flight control method improved by STFT in atmospheric disturbance applications Evaluating the effect of frigate hangar shape modifications on helicopter recovery using piloted flight simulation
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