A new parallel multi-harmonic neural network adaptive filtering hybrid control algorithm for helicopter active vibration control under variable working conditions

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Jiangtao Deng , Chenxi Wang , Xingwu Zhang , Tian Chen , Xuefeng Chen
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引用次数: 0

Abstract

Helicopter vibration primarily originates from high-order harmonic vibrations induced by rotor loads. Complex external operating conditions and rotor variable-speed technologies necessitate active vibration control systems capable of adapting to frequency-varying vibrations. Conventional Filtered-x Least Mean Square (FxLMS) algorithms employ constant single convergence factors, making it difficult to adapt to variable working conditions. This paper proposes a new parallel multi-harmonic neural network adaptive filtering hybrid control algorithm to suppress multi-harmonic vibrations under variable working conditions. Bandpass filters are adopted to separate multiple harmonics for parallel control. Leveraging neural networks' strong approximation and memory capabilities, the proposed algorithm conducts reinforcement learning-guided supervised training across multiple environments, significantly enhancing training efficiency and the network's adaptability to frequency changes. In addition, state normalization and denormalization methods are adopted to eliminate the influence of vibration amplitude variation on the network control performance. Concurrently, adaptive filtering ensures the steady-state performance of the algorithm. An active vibration control system for helicopters equipped with electromagnetic inertial actuators has been established. The simulation and experimental results show that compared with the conventional FxLMS algorithm, the proposed control algorithm has a better convergence speed and similar multi-harmonic control effect. Meanwhile, the results of various variable working condition experiments also verify that the proposed algorithm has better adaptability and robustness, thereby effectively adapting to the active vibration control of helicopters with variable rotor speeds.
针对直升机变工况下的主动振动控制,提出了一种新的并行多谐神经网络自适应滤波混合控制算法
直升机振动主要来源于旋翼载荷引起的高次谐波振动。复杂的外部运行条件和转子变速技术需要能够适应变频振动的主动振动控制系统。传统的滤波-x最小均方(filter -x Least Mean Square, FxLMS)算法采用恒定的单收敛因子,难以适应可变的工作条件。提出了一种新的并行多谐神经网络自适应滤波混合控制算法,用于抑制变工况下的多谐振动。采用带通滤波器分离多重谐波,实现并联控制。该算法利用神经网络强大的逼近和记忆能力,在多环境下进行强化学习引导的监督训练,显著提高了训练效率和网络对频率变化的适应能力。此外,采用状态归一化和反归一化方法,消除了振动幅值变化对网络控制性能的影响。同时,自适应滤波保证了算法的稳态性能。建立了一种采用电磁惯性作动器的直升机振动主动控制系统。仿真和实验结果表明,与传统的FxLMS算法相比,所提出的控制算法具有更好的收敛速度和相似的多谐波控制效果。同时,各种变工况实验结果也验证了所提算法具有较好的自适应性和鲁棒性,能够有效适应直升机变旋翼速度的主动振动控制。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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