| Issue |
Volume 6, 2013
Progress in Flight Dynamics, Guidance, Navigation, Control, Fault Detection, and Avionics
|
|
|---|---|---|
| Page(s) | 375 - 392 | |
| Section | Fault detection and control | |
| DOI | https://doi.org/10.1051/eucass/201306375 | |
| Published online | 02 December 2013 | |
Nonlinear observer techniques for oscillatory failure case detection
1
INRIA − LNE Parc Scientifique de la Haute Borne 40 Avenue Halley, Bât. A Park Plaza, Villeneuve d'Ascq 59650, France
2
University of Bordeaux, IMS-lab, Automatic Control Group 351 Cours de la Libération, Talence 33405, France
The problem of observer design for fault detection in a class of nonlinear systems subject to parametric and signal uncertainties is studied. The design procedure includes formalized optimization of observer free parameters in terms of trade-offs for fault detection performance and robustness to external disturbances or model uncertainties. The technique makes use of some monotonicity conditions imposed on the estimation error dynamics. Efficiency of the proposed approach is demonstrated through the Oscillatory Failure Case (OFC) in aircraft control surface servoloops.
© Owned by the authors, published by EDP Sciences, 2013
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