使用变步长过滤-x 最小均方算法的叶片主动振动控制研究

Jinhua Jiang, Zhiyuan Gao, Hesheng Zhang, Xiaojin Zhu
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引用次数: 0

摘要

发动机叶片是航空发动机的重要部件之一,振动会导致发动机叶片脱落或断裂。主动振动控制(AVC)具有更高的灵活性,越来越多地被用于抑制叶片的振动。过滤-x 最小均方(FxLMS)算法是主动振动控制中常用的自适应算法,但其固定步长在收敛速度和稳态误差之间存在矛盾。本文提出了一种基于双曲正割函数的新型可变步长 FxLMS(VSSFxLMS)算法,其正割函数可确保控制信号有界。在早期阶段,较大的步长可使误差迅速减小。随着误差的减小,步长也随之减小,较小的步长可确保较小的稳态误差。本文首先总结了三种 VSSFxLMS 算法,并提出了一种改进算法;其次,对上述算法进行了对比分析;然后,利用 ADAMS 和 Simulink 搭建了联合仿真平台,验证了所提算法的有效性;最后,搭建了实验平台,利用几种 VSSFxLMS 算法完成了叶片振动主动控制实验,实验结果验证了所提算法具有更好的振动抑制效果。
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Research on active vibration control of blade using variable-step-size filtered-x least mean square algorithm
The engine blade is one of the important parts of the aero engine, vibration can lead to engine blade off or fracture. Active Vibration Control (AVC) has a higher flexibility is increasingly used to suppress the vibration of the blade. The filtered-x least mean square (FxLMS) algorithm is an adaptive algorithm commonly used in active vibration control, but its fixed step size has a contradiction between convergence speed and steady-state error. A new variable-step-size FxLMS (VSSFxLMS) algorithm based on hyperbolic secant function was proposed, and the sech function ensures the control signal is bounded. In the early stage, a larger step size enables the error to decrease rapidly. The step size decreases as the error decreases, and a smaller step size ensures a smaller steady-state error. Firstly, this paper summarizes three VSSFxLMS algorithms and proposes an improved algorithm; Secondly, it compares and analyses the mentioned algorithms; Then, a joint simulation platform using ADAMS and Simulink is built to verify the effectiveness of the proposed algorithms; Finally, an experimental platform was built to complete the blade vibration active control experiments using several VSSFxLMS algorithms, and the results of the experiment verify the better vibration suppression effect of the proposed algorithm.
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