DocumentCode :
3054520
Title :
Discrete Flatness for Non Linear Systems FDI
Author :
Zhang, Nan ; Doncescu, Andrei ; Mora-Camino, Felix
Author_Institution :
LAAS, LARA-ENAC, Toulouse, France
fYear :
2010
fDate :
4-6 Nov. 2010
Firstpage :
488
Lastpage :
494
Abstract :
This Fault detection is essential for the survivability of many systems. Since many systems present highly nonlinear dynamics, the applicability of general fault detection techniques designed mainly for linear systems is very questionable. The purpose of this communication is to investigate the usefulness of the differential flatness theory of a non linear system such as a four rotor aircraft to design an efficient fault detection scheme. In this communication, after introducing the concept of difference flat nonlinear systems, a fault detection scheme based on difference flatness.
Keywords :
aircraft; discrete systems; fault diagnosis; linear systems; nonlinear control systems; nonlinear dynamical systems; rotors; differential flatness theory; discrete flatness; fault detection and identification; nonlinear dynamics; nonlinear system; rotor aircraft; system survivability; Current measurement; Fault detection; Fault diagnosis; Linear systems; Measurement errors; Nonlinear dynamical systems; Rotors; Differential flatness; Discrete system; Fault detection; Rotorcraft flight mechanics; component;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Broadband, Wireless Computing, Communication and Applications (BWCCA), 2010 International Conference on
Conference_Location :
Fukuoka
Print_ISBN :
978-1-4244-8448-5
Electronic_ISBN :
978-0-7695-4236-2
Type :
conf
DOI :
10.1109/BWCCA.2010.119
Filename :
5633907
Link To Document :
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