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Denis Efimov
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Documents
Présentation
I received my Ph.D. degree in Automatic Control from the Saint-Petersburg State Electrical Engineering University (Russia) in 2001, and Dr.Sc. degree in Automatic control in 2006 from the Institute for Problems of Mechanical Engineering RAS (Saint-Petersburg, Russia).
From 2000 to 2009 I was a research fellow at the Institute for Problems of Mechanical Engineering RAS, Control of Complex Systems Laboratory. From 2006 to 2011 I was working in the LSS (Supelec, France), the Montefiore Institute (University of Liege, Belgium) and the Automatic control group at the IMS laboratory (University of Bordeaux I, France).
In 2011, I joined Inria (Lille - Nord Europe center). Starting from 2018 I am the head of [Valse team](https://team.inria.fr/valse/).
I am a member of several IFAC TCs and a Senior Member of IEEE. I am also serving as an Associate Editor for IEEE Transactions on Automatic Control, IFAC Journal on Nonlinear Analysis: Hybrid Systems and Asian Journal of Control.
Publications
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Blood Glucose Regulation in Patients with Type 1 Diabetes Mellitus: A Robust MRAC Approach60th IEEE Conference on Decision and Control, Dec 2021, Austin, United States
Communication dans un congrès
hal-03328014v1
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Regulación de Glucosa en la Sangre en Pacientes con Diabetes Mellitus Tipo 1: Un enfoque MRAC RobustoCongreso Nacional De Control Automatico (CNCA), Oct 2021, Ciudad de Guanajuato, México
Communication dans un congrès
hal-03328022v1
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Signal and model-based fault detection for aircraft systemsPreprints, 9th IFAC Symposium on Fault Detection, Supervision and, Sep 2015, Paris, France. ⟨10.1016/j.ifacol.2015.09.673⟩
Communication dans un congrès
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A Method for Actuator Lock-in-place Failure Detection in Aircraft Control Surface Servo-loopsIFAC World Congress'14, Aug 2014, Cape Town, South Africa
Communication dans un congrès
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Enhanced distinguishability in Supervisory Fault Tolerant ControlIFAC World Congress'14, Aug 2014, Cape Town, South Africa
Communication dans un congrès
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Oscillatory Failure Case Detection for Aircraft using Non‐Homogeneous Differentiator in Noisy Environment2nd CEAS Specialist Conference on Guidance, Navigation & Control, Apr 2013, Delft, Netherlands
Communication dans un congrès
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A LPV approach for early fault detection in aircraft control surfaces servo-loopsSAFEPROCESS'2012, Aug 2012, Mexico. To appear
Communication dans un congrès
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INPUT ESTIMATION VIA SLIDING-MODE DIFFERENTIATION FOR EARLY OFC DETECTIONIFAC SAFEPROCESS 2012, Aug 2012, Mexico
Communication dans un congrès
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Supervisory Fault Tolerant Control Scheme based on Bumpless scheme and Dwell-time ConditionsSAFEPROCESS'2012, Aug 2012, Mexico. To appear
Communication dans un congrès
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A Hinf/H- approach for Fault Diagnosis in Electrical Aircraft Flight Control Systems9th European Workshop on Advanced Control and Diagnosis, Nov 2011, Budapest, Hungary
Communication dans un congrès
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Supervisory fault tolerant control based on dwell-time conditionsProc. IFAC WC 2011, Aug 2011, Milan, Italy. pp.1-6
Communication dans un congrès
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Fault Detection and Diagnosis in Electrical Aircraft Flight Control SystemAIAA conference GNC, Aug 2011, United States. pp.NC
Communication dans un congrès
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Supervisory Fault Tolerant Control Via Common Lyapunov Function ApproachConference on Control and Fault Tolerant Systems Nice, France, October 6-8,, 2010, Nice, France. pp.582-587
Communication dans un congrès
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Observer-based structures to Active Fault Tolerant Control ProblemsControl and Fault Tolerant Systems (SysTol'2010), 2010, France. pp.NC
Communication dans un congrès
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Fault Diagnosis and Fault-Tolerant Control and Guidance for Aerospace Vehicles: From theory to applicationSpringer London Ltd, pp.216, 2013, Advances in Industrial Control, 978-1-4471-5312-2. ⟨10.1007/978-1-4471-5313-9⟩
Ouvrages
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Method and device for detecting a failure on an aircraftUnited States, Patent n° : US010209162B2. 2019
Brevet
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Procédé et dispositif de détection d'une anomalie sur un aéronefFrance, N° de brevet: FR3007162 (B1). 2016
Brevet
hal-02342088v1
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Method and device for detecting a failure on an aircraftUnited States, Patent n° : US 06510051. 2014
Brevet
hal-01016216v1
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Procédé et dispositif de détection d'une anomalie sur un aéronefFrance, N° de brevet: FR20130055665. 2013
Brevet
hal-00869250v1
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