Wind tunnel test of UAV fault detection using principal component based aerodynamic model

Author

Ruangwiset, Annop ; Suwantragul, Banterng

Author_Institution

Dept. of Mech. Eng., King Mongkut´´s Univ. of Technol. Thonburi, Bangkok

fYear

2008

fDate

5-8 Aug. 2008

Firstpage

150

Lastpage

154

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.

Keywords

aerodynamics; aerospace control; aerospace testing; fault diagnosis; mobile robots; principal component analysis; remotely operated vehicles; wind tunnels; UAV fault detection; aerodynamic model; configuration damage; principal component; unmanned aerial vehicle; wind tunnel test; Aerodynamics; Aircraft manufacture; Electronic mail; Fault detection; Force measurement; Mechanical engineering; Observers; Testing; Unmanned aerial vehicles; Wind; aerodynamic model; configuration damage; fault detection; principal component;

fLanguage

English

Publisher

ieee

Conference_Titel

Mechatronics and Automation, 2008. ICMA 2008. IEEE International Conference on

Conference_Location

Takamatsu

Print_ISBN

978-1-4244-2631-7

Electronic_ISBN

978-1-4244-2632-4

Type

conf

DOI

10.1109/ICMA.2008.4798742

Filename

4798742