A Comparative Study of Three Differentiation Schemes for the Detection of Runaway Faults in Aircraft Control Surfaces

Abstract : In this paper, three different differentiation schemes are studied for the development of a generic fault detection scheme. The case of runawayfault is investigated. A runaway is an uncontrolled deflection of a control surface which can go until its physical limitation if it remains undetected. The proposed technique is a signal-based one that relaxes the need of an accurate actuator modelling. The core element of the proposed fault detection scheme is a differentiation scheme. In this context, a comparative study is made by using noisy signals. Note that the assessment of differentiation is done by using the Absolute Mean Error (AME) ratio, the percentage Variance Accounted For (VAF) and the Index of Agreement (IoA).
Type de document :
Communication dans un congrès
Elseveir. Proceedings of the 20th IFAC Symposium on Automatic Control in Aerospace, , Aug 2016, Sherbrooke, Canada. 2016, 〈10.1016/j.ifacol.2016.09.013〉
Liste complète des métadonnées

https://hal.archives-ouvertes.fr/hal-01385563
Contributeur : Jérome Cieslak <>
Soumis le : vendredi 21 octobre 2016 - 15:49:21
Dernière modification le : mardi 5 février 2019 - 15:04:08

Identifiants

Citation

Jérome Cieslak, Ali Zolghadri, Goupil Philippe, Rémy Dayre. A Comparative Study of Three Differentiation Schemes for the Detection of Runaway Faults in Aircraft Control Surfaces . Elseveir. Proceedings of the 20th IFAC Symposium on Automatic Control in Aerospace, , Aug 2016, Sherbrooke, Canada. 2016, 〈10.1016/j.ifacol.2016.09.013〉. 〈hal-01385563〉

Partager

Métriques

Consultations de la notice

40