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Numerical and Experimental UAV Structure Investigation by Pre-Flight Load Test

Numerical and Experimental UAV Structure Investigation by Pre-Flight Load Test

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_1931f93295fb4e9bb91d388022a71400

Numerical and Experimental UAV Structure Investigation by Pre-Flight Load Test

About this item

Full title

Numerical and Experimental UAV Structure Investigation by Pre-Flight Load Test

Publisher

Switzerland: MDPI

Journal title

Sensors (Basel, Switzerland), 2020-05, Vol.20 (11), p.3014

Language

English

Formats

Publication information

Publisher

Switzerland: MDPI

More information

Scope and Contents

Contents

This paper presents the preparation and execution of on-ground static and engine load tests for the composite unmanned aerial vehicle (UAV). The test was conducted for pre-flight structural strength verification of the remotely piloted aerial target named HORNET, after introducing some structural modifications. The ground tests were performed befor...

Alternative Titles

Full title

Numerical and Experimental UAV Structure Investigation by Pre-Flight Load Test

Identifiers

Primary Identifiers

Record Identifier

TN_cdi_doaj_primary_oai_doaj_org_article_1931f93295fb4e9bb91d388022a71400

Permalink

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_1931f93295fb4e9bb91d388022a71400

Other Identifiers

ISSN

1424-8220

E-ISSN

1424-8220

DOI

10.3390/s20113014

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