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    In-Flight Detection of Vibration Anomalies in Unmanned Aerial Vehicles

    Source: Journal of Nondestructive Evaluation, Diagnostics and Prognostics of Engineering Systems:;2020:;volume( 003 ):;issue: 004::page 041105-1
    Author:
    Banerjee, Portia
    ,
    Okolo, Wendy A.
    ,
    Moore, Andrew J.
    DOI: 10.1115/1.4047468
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Owing to the frequency of occurrence and high risk associated with bearings, identification, and characterization of bearing faults in motors via nondestructive evaluation (NDE) methods have been studied extensively, among which vibration analysis has been found to be a promising technique for early diagnosis of anomalies. However, a majority of the existing techniques rely on vibration sensors attached onto or in close proximity to the motor in order to collect signals with a relatively high SNR. Due to weight and space restrictions, these techniques cannot be used in unmanned aerial vehicles (UAVs), especially during flight operations since accelerometers cannot be attached onto motors in small UAVs. Small UAVs are often subjected to vibrational disturbances caused by multiple factors such as weather turbulence, propeller imbalance, or bearing faults. Such anomalies may not only pose risks to UAV’s internal circuitry, components, or payload, they may also generate undesirable noise level particularly for UAVs expected to fly in low-altitudes or urban canyon. This paper presents a detailed discussion of challenges in in-flight detection of bearing failure in UAVs using existing approaches and offers potential solutions to detect overall vibration anomalies in small UAV operations based on IMU data.
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      In-Flight Detection of Vibration Anomalies in Unmanned Aerial Vehicles

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    contributor authorBanerjee, Portia
    contributor authorOkolo, Wendy A.
    contributor authorMoore, Andrew J.
    date accessioned2022-02-04T22:15:31Z
    date available2022-02-04T22:15:31Z
    date copyright6/26/2020 12:00:00 AM
    date issued2020
    identifier issn2572-3901
    identifier othernde_3_3_030301.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4275204
    description abstractOwing to the frequency of occurrence and high risk associated with bearings, identification, and characterization of bearing faults in motors via nondestructive evaluation (NDE) methods have been studied extensively, among which vibration analysis has been found to be a promising technique for early diagnosis of anomalies. However, a majority of the existing techniques rely on vibration sensors attached onto or in close proximity to the motor in order to collect signals with a relatively high SNR. Due to weight and space restrictions, these techniques cannot be used in unmanned aerial vehicles (UAVs), especially during flight operations since accelerometers cannot be attached onto motors in small UAVs. Small UAVs are often subjected to vibrational disturbances caused by multiple factors such as weather turbulence, propeller imbalance, or bearing faults. Such anomalies may not only pose risks to UAV’s internal circuitry, components, or payload, they may also generate undesirable noise level particularly for UAVs expected to fly in low-altitudes or urban canyon. This paper presents a detailed discussion of challenges in in-flight detection of bearing failure in UAVs using existing approaches and offers potential solutions to detect overall vibration anomalies in small UAV operations based on IMU data.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleIn-Flight Detection of Vibration Anomalies in Unmanned Aerial Vehicles
    typeJournal Paper
    journal volume3
    journal issue4
    journal titleJournal of Nondestructive Evaluation, Diagnostics and Prognostics of Engineering Systems
    identifier doi10.1115/1.4047468
    journal fristpage041105-1
    journal lastpage041105-1
    page1
    treeJournal of Nondestructive Evaluation, Diagnostics and Prognostics of Engineering Systems:;2020:;volume( 003 ):;issue: 004
    contenttypeFulltext
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