Type de projet
Résultats 1-4 de 4
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A non-conservative $H_{-} / H_{\infty}$ solution for early and robust fault diagnosis in aircraft control surface servo-loops
Control Engineering Practice, Elsevier, 01-10-2014, 31, 183–199Compte-rendu et recension critique d'ouvrage -
Actuator fault detection in aircraft systems: Oscillatory Failure Case study
Annual Reviews in Control, Elsevier, 2013, 37; 1, 180 - 190Compte-rendu et recension critique d'ouvragetexte intégral -
Design of a non-homogeneous differentiator for actuator oscillatory failure case reconstruction in noisy environment
Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, SAGE Publications, 01-03-2015, 229; 3, 266-275Compte-rendu et recension critique d'ouvrage -
Oscillatory Failure Case Detection for Aircraft using Non‐Homogeneous Differentiator in Noisy Environment
2nd CEAS Specialist Conference on Guidance, Navigation & Control, Delft, 04-2013, co-sponsored by IEEE and AIAA, 04-2013Communication dans un congrès avec actes