Fault detection and isolation in a greenhouse using parity relations

Kabbaj, Mohammed Nabil; Ramzi, Mustapha; Dahhou, B.; Youlal, H.; Enea, Gilles

doi:10.1109/etfa.2003.1248773

Cited by 1 publication

(1 citation statement)

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“…This approach served in [14] to detect failures in a nonlinear model of generic servoactuator used for manipulating robots; this work showed how the use of nonlinear parity equations avoids modeling errors and the need for linearization of nonlinear models. Kabbaj et al presented in [15] an application of this technique to detect failures in greenhouse processes for both sensors and actuators failures and described the used of fixed threshold as an issue of their implementation. This method, however, as was presented in presented by Mercadal in [16] can suffer of high sensitivity to modeling error and noise.…”

Section: Literature Reviewmentioning

confidence: 99%

Development and evaluation of a fault detection and identification scheme for the WVU YF-22 UAV using the artificial immune system approach

Sanchez¹

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A failure detection and identification (FDI) scheme is developed for a small remotely controlled jet aircraft based on the Artificial Immune System (AIS) paradigm. Pilot-in-the-loop flight data are used to develop and test a scheme capable of identifying known and unknown aircraft actuator and sensor failures. Negative selection is used as the main mechanism for self/non-self definition; however, an alternative approach using positive selection to enhance performance is also presented. Tested failures include aileron and stabilator locked at trim and angular rate sensor bias. Hyper-spheres are chosen to represent detectors. Different definitions of distance for the matching rules are applied and their effect on the behavior of hyper-bodies is discussed. All the steps involved in the creation of the scheme are presented including design selections embedded in the different algorithms applied to generate the detectors set. The evaluation of the scheme is performed in terms of detection rate, false alarms, and detection time for normal conditions and upset conditions. The proposed detection scheme achieves good detection performance for all flight conditions considered. This approach proves promising potential to cope with the multidimensional characteristics of integrated/comprehensive detection for aircraft subsystem failures. A preliminary performance comparison between an AIS based FDI scheme and a Neural Network and Floating Threshold based one is presented including groundwork on assessing possible improvements on pilot situational awareness aided by FDI schemes. Initial results favor the AIS approach to FDI due to its rather undemanding adaptation capabilities to new environments. The presence of the FDI scheme suggests benefits for the interaction between the pilot and the upset conditions by improving the accuracy of the identification of each particular failure and decreasing the detection delays. DEDICATION To my family for being always supportive in every decision I made and for helping me become who I am today. iii ACKNOWLEDGEMENTS First and foremost, I would like to thank Prof. Perhinschi and Prof. Napolitano for giving me the opportunity to further extend my college education. Specials thanks go to Prof. Perhinschi for letting me take part of this groundbreaking research giving me the best guidance one can expect from an Advisor. I would also like to thank Dr. Bojan Cukic for eagerly agreeing to form part of my committee and for providing positive feedback towards the successful completion of this work. My parents, Olga and Vicente, deserve a special thank for always letting me choose my own path and giving me an education one cannot learn from books; their generosity is out of imaginable limits. I would also like to express my sincere appreciation to my siblings Javier and Mariana for always believing in me even more than myself. I would also like to extend my gratitude to my friends, now spread throughout the world, for being the siblings one gets to choose to walk side by side through life, I am su...

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Section: Literature Reviewmentioning

confidence: 99%

Development and evaluation of a fault detection and identification scheme for the WVU YF-22 UAV using the artificial immune system approach

Sanchez¹

View full text Add to dashboard Cite

show abstract

Fault detection and isolation in a greenhouse using parity relations

Cited by 1 publication

References 4 publications

Development and evaluation of a fault detection and identification scheme for the WVU YF-22 UAV using the artificial immune system approach

Development and evaluation of a fault detection and identification scheme for the WVU YF-22 UAV using the artificial immune system approach

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