DocumentCode :
164246
Title :
Robust sensor fault diagnosis and tracking controller for a UAV modelled as LPV system
Author :
Lopez-Estrada, F.R. ; Ponsart, J.-C. ; Theilliol, Didier ; Astorga-Zaragoza, C.M. ; Zhang, Y.M.
Author_Institution :
CRAN, Univ. of Lorraine, Vandoeuvre-les-Nancy, France
fYear :
2014
fDate :
27-30 May 2014
Firstpage :
1311
Lastpage :
1316
Abstract :
This work is dedicated to the robust fault detection and tracking problem for a UAV system with external disturbances. A quadrotor modelled as a Linear Parameter Varying system (LPV) is considered as a target to design and to illustrate recent advanced control methods. Firstly, the fault detection problem is addressed by considering the design of a robust fault detection observer with H performance. The challenge is to attenuate external disturbances and a to generate useful residual signals to detect and isolate faults in sensors. Second, a feedback controller is designed by considering a comparator integrator control scheme to stabilize the system and to reach the tracking signal. In both cases the Lyapunov theory and ℒ2-gain technique are used to obtain sufficient stability conditions in LMIs (linear matrix inequalities) formulation. Finally, some simulations in fault-free and faulty cases are done on the quadrotor system.
Keywords :
H control; Lyapunov methods; aircraft control; autonomous aerial vehicles; control system synthesis; fault diagnosis; feedback; helicopters; linear matrix inequalities; mobile robots; observers; robust control; tracking; ℒ2-gain technique; H performance; LMI; LPV system; Lyapunov theory; UAV system; comparator integrator control scheme; control design; external disturbance attenuation; fault tracking controller; fault-free cases; faulty cases; feedback controller design; linear matrix inequalities; linear parameter varying system; quadrotor system; residual signal generation; robust fault detection observer design; robust fault detection problem; robust sensor fault diagnosis; sensor fault isolation; sufficient stability conditions; system stabilization; tracking signal; Fault detection; Fault diagnosis; Mathematical model; Observers; Robustness; Rotors; Vectors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Unmanned Aircraft Systems (ICUAS), 2014 International Conference on
Conference_Location :
Orlando, FL
Type :
conf
DOI :
10.1109/ICUAS.2014.6842389
Filename :
6842389
Link To Document :
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