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Fault Detection and Identification Method for Quadcopter Based on Airframe Vibration Signals

Fault Detection and Identification Method for Quadcopter Based on Airframe Vibration Signals

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_975b1f29250e472bbb1d8cdf1bc1c7d4

Fault Detection and Identification Method for Quadcopter Based on Airframe Vibration Signals

About this item

Full title

Fault Detection and Identification Method for Quadcopter Based on Airframe Vibration Signals

Publisher

Switzerland: MDPI AG

Journal title

Sensors (Basel, Switzerland), 2021-01, Vol.21 (2), p.581

Language

English

Formats

Publication information

Publisher

Switzerland: MDPI AG

More information

Scope and Contents

Contents

Quadcopters are widely used in a variety of military and civilian mission scenarios. Real-time online detection of the abnormal state of the quadcopter is vital to the safety of aircraft. Existing data-driven fault detection methods generally usually require numerous sensors to collect data. However, quadcopter airframe space is limited. A large nu...

Alternative Titles

Full title

Fault Detection and Identification Method for Quadcopter Based on Airframe Vibration Signals

Authors, Artists and Contributors

Identifiers

Primary Identifiers

Record Identifier

TN_cdi_doaj_primary_oai_doaj_org_article_975b1f29250e472bbb1d8cdf1bc1c7d4

Permalink

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_975b1f29250e472bbb1d8cdf1bc1c7d4

Other Identifiers

ISSN

1424-8220

E-ISSN

1424-8220

DOI

10.3390/s21020581

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