DocumentCode
1781651
Title
A negative selection algorithm applied to helicopter actuator fault detection
Author
Rakotomamonjy, Thomas ; Le Boulanger, Morgane
Author_Institution
ONERA ? The French Aerosp. Lab., Salon-de-Provence, France
fYear
2014
fDate
3-5 Nov. 2014
Firstpage
309
Lastpage
314
Abstract
In order to detect the failure of an actuator of a helicopter swashplate, a simple detection method based on a negative selection algorithm (NSA) is developed. This technique, inspired by existing rules found in the biological immunity, rely on a set of elemental detectors which have been trained in order to recognize only the non-self (i.e. faulty) behaviors of the system, without needing an explicit model of the system dynamics. A simple model for the actuator failure is developed and coupled with a helicopter flight dynamics model, and some trajectories for the algorithm training and validation are simulated. A procedure for improving the efficiency of the algorithm by introducing weighting coefficients to the detection function is proposed and successfully tested. Moreover, the performance of the algorithm is slightly improved by observing the covariance of the flight dynamics states, instead of the variables themselves.
Keywords
actuators; aircraft control; failure (mechanical); fault diagnosis; helicopters; NSA; algorithm efficiency improvement; algorithm training; algorithm validation; biological immunity; detection function; elemental detectors; flight dynamics states; helicopter actuator fault detection; helicopter flight dynamics model; helicopter swashplate actuator failure detection; negative selection algorithm; nonself faulty system behavior recognition; weighting coefficients; Actuators; Blades; Detectors; Fault detection; Helicopters; Rotors; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Control, Decision and Information Technologies (CoDIT), 2014 International Conference on
Conference_Location
Metz
Type
conf
DOI
10.1109/CoDIT.2014.6996912
Filename
6996912
Link To Document