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| HAL : hal-00692404, version 1 |
| Fiche détaillée |  Récupérer au format |
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| International Conference on Recent Advances in Aerospace Actuation Systems and Components, Toulouse : France (2012) |
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| AIRBUS EFFORTS TOWARDS ADVANCED FAULT DIAGNOSIS FOR FLIGHT CONTROL SYSTEM ACTUATORS |
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| Philippe Goupil 1Ali Zolghadri 2 |
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| (13/06/2012) |
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| Many innovative solutions have been developed recently by the aeronautical sector towards achieving the future "sustainable" aircraft. In this context, the Electrical Flight Control System (EFCS) design objectives, originating for example from structural loads design constraints, are becoming more and more stringent. In termss of fault or failure detection, this means that the minimum detectable amplitude and the detection time must be decreased. Several EFCS-failure cases may have an influence on structural loads. This paper will present the Airbus efforts towards advanced Fault Detection and Diagnosis (FDD) of three of them for achieving the aforementioned rigorous detection objectives. Robust model-based FDD scheme will be presented for early detection of EFCS-failure cases, as well as their application in a real-time environment and the results obtained during industrial validation campaigns. |
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| 1 : | Airbus France EYC - CC - Flight Control System |
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Airbus France |
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| 2 : | Laboratoire de l'intégration, du matériau au système (IMS) |
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CNRS : UMR5218 – Université Sciences et Technologies - Bordeaux I – Institut Polytechnique de Bordeaux |
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| 3 : | Airbus Operations SAS |
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Airbus |
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| Domaine | : | Sciences de l'ingénieur/Automatique / Robotique |
| hal-00692404, version 1 | |
| http://hal.archives-ouvertes.fr/hal-00692404 | |
| oai:hal.archives-ouvertes.fr:hal-00692404 | |
| Contributeur : Ali Zolghadri | |
| Soumis le : Lundi 30 Avril 2012, 11:50:18 | |
| Dernière modification le : Lundi 30 Avril 2012, 11:50:18 | |
