小波变换在飞机控制面故障检测中的应用

Xiao Chen, Xinmin Wang, Cheng Peng
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引用次数: 1

摘要

控制面故障会改变运动方程的结构,是故障检测中的一个难题。针对这种故障,提出了利用小波局部细化特性的小波分析方法来检测故障信号。小波基选择是小波分析方法中的关键问题之一。根据小波基的规则,给出了合适的选择。随后,提出了基于小波变换的故障检测算法。最后,针对F16战斗机升降舵卡滞问题进行了仿真。在仿真过程中,选取小波基db4,采用Mallat算法进行三层分解。结果表明,小波分析方法能有效地检测出故障发生的时间。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The Application of Wavelet Transform to Fault Detection of Aircraft Control Surface
Control surface failure which can change the structure of the motion equations is a difficult problem in fault detection. To this failure, the wavelet analysis method is presented to detect fault signal in accordance with wavelet local refinement properties. Wavelet basis selection is one of the key issues in the wavelet analysis method. According to the rules of the wavelet basis, a proper selection is given. Subsequently, fault detection algorithm based on wavelet transform is proposed. Finally, simulation is carried out based on the stuck of elevator of F16 fighter. In the process of simulation, wavelet basis db4 is selected and Mallat algorithm, 3-layer decomposition is adopted. The results show that wavelet analysis method can effectively detect the fault occurrence time.
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