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

被引:1
作者
Ashe, Avijit Kumar [1 ]
Goli, Srikanth [1 ]
Kandath, Harikumar [1 ]
Gangadharan, Deepak [2 ]
机构
[1] IIIT Hyderabad, RRC, Hyderabad, Telangana, India
[2] IIIT Hyderabad, CSG, Hyderabad, Telangana, India
来源
2023 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS, ICUAS | 2023年
关键词
reconfigurable aerial platforms; time series analysis; fail-safe systems; rotor failure; fault isolation; multicopter; quadcopter; hexacopter;
D O I
10.1109/ICUAS57906.2023.10155856
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
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 model-free 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.
引用
收藏
页码:9 / 16
页数:8
相关论文
共 12 条
  • [1] Active Fault-Tolerant Control of UAV Dynamics against Sensor-Actuator Failures
    Caliskan, Fikret
    Hajiyev, Chingiz
    [J]. JOURNAL OF AEROSPACE ENGINEERING, 2016, 29 (04)
  • [2] Statistical residual-based time series methods for multicopter fault detection and identification
    Dutta, Airin
    McKay, Michael
    Kopsaftopoulos, Fotis
    Gandhi, Farhan
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 112
  • [3] ON CERTAIN INTEGRALS OF LIPSCHITZ-HANKEL TYPE INVOLVING PRODUCTS OF BESSEL FUNCTIONS
    EASON, G
    NOBLE, B
    SNEDDON, IN
    [J]. PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1955, 247 (935) : 529 - 551
  • [4] Actuator and sensor fault estimation based on a proportional multiple-integral sliding mode observer for linear parameter varying systems with inexact scheduling parameters
    Gomez-Penate, Samuel
    Lopez-Estrada, Francisco-Ronay
    Valencia-Palomo, Guillermo
    Rotondo, Damiano
    Guerrero-Sanchez, Maria-Eusebia
    [J]. INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2021, 31 (17) : 8420 - 8441
  • [5] Fault detection and isolation for Unmanned Aerial Vehicle sensors by using extended PMI filter
    Guo, Dingfei
    Wang, Yulin
    Zhong, Maiying
    Zhao, Yan
    [J]. IFAC PAPERSONLINE, 2018, 51 (24): : 818 - 823
  • [6] Hamadi Hussein, 2020, DISS
  • [7] Krishnamoorthy Kiruthika, 2015, FAULT TOLERANCE ANAL
  • [8] Narasimhan A, 2020, Arxiv, DOI arXiv:2011.00481
  • [9] Nguyen Tien, 2020, IEEEASME T MECHATRON
  • [10] Active versus passive fault-tolerant control of a redundant multirotor UAV
    Saied, M.
    Lussier, B.
    Fantoni, I
    Shraim, H.
    Clovis, F.
    [J]. AERONAUTICAL JOURNAL, 2020, 124 (1273) : 385 - 408