DocumentCode
622322
Title
Robust Fault Estimation on a real quadrotor UAV using optimized Adaptive Thau Observer
Author
Zhaohui Cen ; Noura, H. ; Al Younes, Younes
Author_Institution
Dept. of Electr. Eng., UAE Univ., Al Ain, United Arab Emirates
fYear
2013
fDate
28-31 May 2013
Firstpage
550
Lastpage
556
Abstract
As a result of modeling uncertainties, data decade unbalanceand noise, Fault Estimation (FE) for real quadrotor is rough with low accuracy when model observer based FE scheme-Adaptive Thau Observer(ATO) is applied. Based on these issues, this paper proposes a comprehensive optimization approach on FE accuracy for quadrotor using ATO. First, the ATO observer is improved by adding unmolded terms with parameters derived from identification. Secondly, a data adjustment based on amplifying and reducing is introduced to overcome the data decade unbalance. Thirdly, the Infinite Impulse Response (IIR) filter is utilized to decrease the noise in measurement signals. Finally, experiments for injecting the rotor fault have been carried out to show the effectiveness of the proposed optimization method and the results are discussed.
Keywords
IIR filters; adaptive control; autonomous aerial vehicles; fault diagnosis; noise; observers; optimal control; optimisation; robust control; rotors; ATO observer; IIR filter; data adjustment; data decade unbalance; identification; infinite impulse response filter; measurement signal; model observer based FE scheme; noise; optimization; optimized adaptive Thau observer; real quadrotor UAV; robust fault estimation; rotor fault; uncertainties modeling; IIR filters; Iron; Noise; Observers; Optimization; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Unmanned Aircraft Systems (ICUAS), 2013 International Conference on
Conference_Location
Atlanta, GA
Print_ISBN
978-1-4799-0815-8
Type
conf
DOI
10.1109/ICUAS.2013.6564732
Filename
6564732
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