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Online Actuator Failure Detection using Direct Approach

机译:使用直接方法在线执行器故障检测

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摘要

A novel actuator failure detection algorithm is developed in this paper. An actuator failure is considered to occur when it produces an input to the structure that is different from the commanded input. In this paper, an error function, one for each actuator, is developed to monitor the working status of the examined actuator in real-time, regardless the status of other actuators. Non-zero signal profile in the error function indicates the time instant of failure of the examined actuator (for measurement noise free case). The coefficients of the error function are calculated directly from the healthy input data (from the examined actuator) and all outputs without having to identify the state-space model of the system. Thus the need to know the state-space model of the plant is bypassed in the presented direct approach. Experimental results from a NASA eight bay truss show that the direct method can successfully isolate and identify the failure of the examined actuator in real-time.
机译:本文提出了一种新颖的执行器故障检测算法。当执行器向结构产生的输入与命令输入不同时,就认为发生了执行器故障。在本文中,开发了一种误差函数(每个致动器一个),以实时监视所检查致动器的工作状态,而与其他致动器的状态无关。误差函数中的非零信号曲线表示所检查的执行器故障的瞬间(对于无测量噪声的情况)。误差函数的系数直接从健康的输入数据(来自检查的执行器)和所有输出中计算出来,而无需识别系统的状态空间模型。因此,在提出的直接方法中,无需了解工厂的状态空间模型。来自NASA八托架的实验结果表明,直接方法可以成功地实时隔离和识别被检查执行器的故障。

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