Multivariate Data Analysis for Motor Failure Detection and Isolation in A Multicopter UAV Using Real-Flight Attitude Signals

A. Ashe, Srikanth Goli, Harikumar Kandath, Deepak Gangadharan
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Abstract

Reconfigurable aerial platforms such as multicopter unmanned aerial vehicles (UAVs) allow the design of fail-safe systems because of inherent redundancy in actuators and sensors to maintain stability with a reduction in flight performance. The methods based on univariate and multivariate time series analysis of just the attitude signals can pave the way for modelfree systems that can be generalized across a class of UAVs like multicopters. In this paper, we present a critical analysis of real-flight attitude time-series signals and investigate them for data-driven motor fault and failure detection and isolation (FDI), specifically for multicopters configurations like quadcopters and hexacopters. We analyze flight data for different scenarios of outdoor flights, healthy and faulty, hovering and cruising, loss of efficiency, and single-rotor failure of every motor. We tested it for small to medium-sized multi-copters. The failure detection and classification are performed without relying on analytical system modeling or the knowledge of the controller.Thus, we perform three major assessments: vector autoregression (VAR) using residual variance, time-frequency analysis, and dimensionality analysis of the recorded variables, to support the classification framework. To the author’s best knowledge, it is an early attempt at laying the foundation for engineering features from streaming attitude data, instead of simulations, that works on existing open-source autopilot hardware and is agnostic to the firmware as well. This foundation allows us to implement various FDI frameworks in real-time directly using the above variables on multicopters, which drastically increases the levels of safety and scalability of unmanned flights in drone applications.
基于真实飞行姿态信号的多旋翼无人机电机故障检测与隔离的多元数据分析
可重构的空中平台,如多旋翼无人机(uav),允许设计故障安全系统,因为执行器和传感器的固有冗余,可以在降低飞行性能的情况下保持稳定性。基于姿态信号的单变量和多变量时间序列分析方法为无模型系统的推广应用铺平了道路。在本文中,我们提出了对实时飞行姿态时间序列信号的关键分析,并研究了它们用于数据驱动的电机故障和故障检测和隔离(FDI),特别是针对多旋翼机配置,如四旋翼机和六旋翼机。我们分析了室外飞行、健康和故障、悬停和巡航、效率损失以及每个电机的单旋翼故障等不同场景的飞行数据。我们在小型到中型多架直升机上进行了测试。故障检测和分类执行不依赖于分析系统建模或控制器的知识。因此,我们进行了三种主要评估:使用残差方差的向量自回归(VAR)、时频分析和记录变量的维度分析,以支持分类框架。据作者所知,这是一个早期的尝试,为从流姿态数据而不是模拟的工程功能奠定基础,它适用于现有的开源自动驾驶硬件,并且对固件也不可知。该基础使我们能够直接在多旋翼机上使用上述变量实时实施各种FDI框架,从而大大提高了无人机应用中无人飞行的安全性和可扩展性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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