基于小波处理飞行试验数据的在线鲁棒气动伺服弹性稳定裕度分析

Hong-chao Li, Zhong-ke Shi, Weixian Tang
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引用次数: 0

摘要

提出了一种基于鲁棒mu分析的多回路气动伺服弹性系统在线稳定裕度评估方法。对飞行数据进行时频域小波滤波预处理,去除噪声。介绍了系统的稳定性分析方法,并将经典的单输入单输出系统的稳定裕度推广到多回路系统。根据目前的不确定性定义,可以计算出给定mu值时增益和相位裕度的保证边界。采用非参数辨识方法从测试数据中确定开环传递函数。该方法使我们能够在没有理论模型的情况下实现在线稳定性评价。最后,将分析结果与返回差矩阵法进行了比较,说明了新方法的有效性
本文章由计算机程序翻译,如有差异,请以英文原文为准。
On-line robust aeroservoelastic stability margin analysis from wavelet-processed flight testing data
An on-line method based on robust mu analysis is presented to evaluate the stability margin of multi-loop aeroservoelastic system from flight testing data. The flight data is preprocessed to remove noise by wavelet filter in time-frequency domain. The method for stability analysis is described and the classical stability margin used for single-input-single-output (SISO) system has been extended to multi-loop system. With the present definition for uncertainty, the guaranteed bounds on gain and phase margin can been calculated for a specified mu value. A nonparametric identification is applied to determine the open-loop transfer function from testing data. This method enables us to implement on-line stability evaluation without theory model. Finally, the analysis results are compared with return difference matrix method to illustrate the efficiency of the new method
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