Using principal component based aerodynamic model

Conference proceedings article

Authors/Editors

ANNOP RUANGWISET

Strategic Research Themes

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Publication Details

Author list: Ruangwiset A., Suwantragul B.

Publisher: Hindawi

Publication year: 2008

Start page: 150

End page: 154

Number of pages: 5

ISBN: 9781424426324

ISSN: 0146-9428

eISSN: 1745-4557

URL: https://www.scopus.com/inward/record.uri?eid=2-s2.0-64949163226&doi=10.1109%2fICMA.2008.4798742&partnerID=40&md5=9f6e9064929d8e5fa5260b46ed23a2e8

Languages: English-Great Britain (EN-GB)

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Abstract

In our previous work the fault detection using aerodynamic model was proposed as more directly method to detect the fault such as configuration damage of the UAV. In this paper the wind tunnel test is performed with the object of verifying the capability of this method to detect the damage during flight. The result shows that by observing the residual of the aerodynamic force coefficient the damage can be detected instantaneously when it occurs. ฉ 2008 IEEE.

Keywords

Aerodynamic model, Configuration damage, Fault detection, Principal component