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FFTG

Présentation

 

FFTG crew members focus their research activities on fault tolerant guidance applied to  aerospace systems by flatness approach.
For a Flat system there is a set of outputs named flat outputs, such that all states variables and inputs can be expressed in terms of the flat outputs and a finite number of her derivatives. This property is very useful for both path planning and controller synthesis for nonlinear dynamical systems and members of FFTG team have used it, for previous research activities. Today, the team explore the possibility to use different sets of flat outputs for diagnosis which is required to realise a fault tolerant guidance controller. 
 FFTG research crew is composed of Franck CAZAURANG and Loïc LAVIGNE, both members of the Automatic Group of IMS Laboratory.
 Since 2010, FFTG crew worked on the following research projects:
Membres
     
Franck Cazaurang, PR Loic Lavigne, MCF Tudor Airimitoaie, MCF (since sept 2014)      

Compétences
  • Guidance and control by flatness approach
  • Diagnosis by flatness approach
  • Robust control for linear and nonlinear system
Team Details


Franck Cazaurang
 obtained the B.S and M.S degrees in Electrical Engineering from ENS Cachan in 1988 and 1990, respectively, the Ph. D. degree in Automatic control from University Bordeaux 1 in 1997 and the research degree for leading research and PhD students in 2009. From september 1992 to August 1998 he worked as lecturer (agrégé) at Bordeaux University. From september 1998 to August 2010 he worked as Associate Professor of Control engineering in Bordeaux University. Since 2010 he has been Professor of Control engineering in Bordeaux University.His main research interests include path planning, fault tolerant guidance dynamic inversion and robust control dedicated to aeronautics and space domains. Pr. Cazaurang is also the head of IMSAT, the aeronautical department of University Bordeaux.(Franck Cazaurang on ResearchGate)

 

Loïc Lavigne obtained his Ph.D. degree in Automatic Control from the University of Bordeaux in 2003. Since September 2005 he has been Associate Professor at Bordeaux University. His main research interests include fault detection and diagnosis, path planning, flat systems and robust control dedicated to aeronautics and space domains. Dr. Lavigne has been involved in two different European projects (GARTEUR, SIRASAS) which deals respectively on robust control and Fault Detection and Diagnosis in the Flight Control System. Dr. Lavigne is also responsible of IMA cursus in the Master GSAT of Bordeaux University.

Tudor Airimitoaie obtained his Ph.D degree in Automatic control jointly from the University of Grenoble anf University Politechnica of Bucarest, Romania in 2012. He spent 16 months as Post doctoral position in INRIA Rennes, and since september 2014 he has been Associate professor at Bordeaux University. His main reseach interests include robust and adaptative control dedicated to active control vibrations and fluid flow control. Currently he start a new joint research topic between Crone and FFTG teams. This topic is focused on the use of formal calculus to determine the sets of flat outputs in the case of non linear systems and noninteger systems.

FFTG for UAV project
parrot V2

The objective of this stuy is to provide a flatness based active fault tolerant control technique. The fault detection and isolation block has to provide a fast and accurate fault isolation. This action is carried out by exploiting the non-uniqueness property of the flat outputs. In fact, if a second set of flat outputs which are coupled by a differential equation of the first is calculated, the number of residues augments. Differentially coupled means that it exists an equation with time derivatives inside, that couple one element of the first set with one of the second. As a consequence of augmenting the number of residual signal more faults than in the one set case may be isolated. Regarding reconfiguration, if the flat system complies with the properties listed above, we will obtain versions of states and control inputs as much of flat output vectors, are found, because each control input and state is a function of the flat output. The proposed approach provides in this manner one measure related to a faulty flat output vector and one or more computed by using an unfaulty one. The redundant state signals could be used as reference of the controller in order to hide the fault effects. This will be helpful to provide an entirely flatness based fault-tolerant control strategy. The works presented are under the following hypothesis: The flat outputs are functions of the state of the system, however in this work the flat outputs are constrained to be states of the system or a linear combination of them. The control loop is closed with a state feedback controller. For purposes of this work flat outputs need to be measured. Faults affecting the actuators are considered rejected by the controller; by consequence reconfiguration is only carried out after a sensor fault occurs. Feasibility of the proposed approach is analyzed in two nonlinear plants, an unmanned quadrotor and a three tank system.

CesarThis work is the subject of PHD manuscript of César MARTINEZ TORRES. First, he earned his M.S degree in aerospace engineering from Bordeaux University, France in 2010 and also received the Engineer diploma with honours in electronics and telecommunications at FIME (Facultad de ingeniería Mecánica y Eléctrica), since september 2011 until march 2014, he is a PhD student in automatic control at IMS laboratory, University of Bordeaux working under a CONACYT (Consejo Nacional de Ciencia y Tecnología) grant and an international joint doctorate supervision signed by the university of Bordeaux and the UANL (Universidad Autónoma de Nuevo León). He is co-supervised by Efrain ALCORTA and David DIAZ from the department of electrical engineering at FIME. He is co-supervised by Loïc LAVIGNE and Franck CAZAURANG from IMS.

SYRENA project

The SYRENA project inclued two main work packages. The first one is focused on diagnosis methods for fuel system on a Turbo machinery. The second one is focused on critical system command and diagnosis applied to actuators for airborne system.

Diagnosis for Fuel System workpackage
TurboSchemArriel

The fist workpackage is based on the alliance of automatic control skills of the IMS laboratory LAPS department and the expertise of David REUNGOAT from TREFLE laboratory in hydraulic systems modeling. Indeed this project requires on one hand the realization of models in the field of mechanics fluids (TREFLE) and on the other hand the development of model-based diagnosis algorithm which constitutes one of the automatic group thematic fields. 

This study focuses on the development and evaluation of a diagnostic algorithm for the fuel system of a gas turbine based on nonlinear multi-physics models. This algorithm allows detection of internal leakage faults of the gear pump in the fuel metering system from pressure measurements. The 1D multi physics approach combines hydraulic, kinematic and dynamic equations of all components of the fuel metering system. The parameters of the simulation bench test meet the technical specifications of each component while the associated tolerance intervals are used for setting the detection threshold of the algorithm in order to ensure a certain degree of robustness to the risk of false alarm. This approach is compared with the results obtained by conventional linear methods and contributions are specified. This diagnostic tool allows maintenance costs reduction of the gas engine fuel system by proposing a new architecture consisting of modular units and line replaceable units. This new architecture is defined from failure characteristics of the components and provides a level of security comparable to the previous architecture.

Sifi
This study is presented in the PhD manuscript of Mohcine SIFI. He earned the B.S. and M.S. degrees with honors in aerospace engineering from Bordeaux University, France, in 2008 and 2010, respectively. Since October 2010 until January 2015, he is a PhD student in automatic control at IMS laboratory, University of Bordeaux. He is co-supervised by David Reungoat from TREFLE Laboratory. His current research interests include modeling of fuel flow control and nonlinear dynamic inversion applied to the diagnosis of a turbomachine. The work falls within the scope of the SYRENA project piloted by Turbomeca. This work is granted by "la région d'Aquitaine".

 

 
 
 
 
Critical System Command and Diagnosis workpackage
Circuit critique

The second workpackage is focused on Flight-Critical Systems (FCS) such as Electromechanical Actuators (EMA) controlled by Engine Control Units (ECU) or Flight Control Units (FCU) which are designed and developed regarding drastic safety requirements. In this study, a flight critical redundant architecture is proposed regarding designed to be airborne must be compliant with ARP4754 and ARP4761 standard. In case of fault occurrences, material redundancies in avionic equipment allow the critical system to reconfigure or to switching into a safe mode. However, duplex or triplex rows of sensors and actuators used for material redundancies increase equipment volume, weight and then cost in aircrafts. Analytical redundancies, based on dynamical models is an interesting way to further enhance safety and availability without increasing the number of redundant items . Model-based fault detection and isolation (FDI) methods such as observers, parity space and parameter estimation are often used for robust fault analysis but mostly using linear models. Indeed, a FDI method based on a complex nonlinear model needs usually more output sensors to be able to process estimated outputs than in a linear case.

AlexandreThis study is presented in the PhD manuscript of Alexandre Bobrinskoy. He obtained the MSc. in digital Signal and Image Processing at Cranfield University (UK) in 2011 and also received the Engineer Diploma in automatic processes at ESTIA (Ecole Supérieure des Technologies Industrielles Avancées) in Bidart in 2010. From June 2011 to January 2015 he is a PhD. Student at the IMS Laboratory, University of Bordeaux working under a CIFRE Grant in partnership with Thales Airborne system, Pessac. He is co-supervised by Bruno BLITEAU from ESTIA Recherche Laboratory.  His current research interests include critical system command and diagnosis applied to actuators for airborne system. The work falls within the scope of the SYRENA project driven by Turbomeca.He start in January 2015 a new career as an design engineer in an high-tech company, holds world or European leadership positions in optronics, avionics, electronics and critical software for both civil and military market.

Path planning by Flatness Approach for Satellite
 
Parasol
 In this cooperative research work with CNES Toulouse center, we have proposed an innovative attitude estimation filter based on differential flatness of the satellite dynamics with Rodriguez Modified Parameters for star tracker only Attitude and Orbit Control System (AOCS) architectures. The main characteristic of this estimator is to be able to maintain the satellite Absolute Pointing Error (APE) within safe limits, avoiding safe hold mode recovery in case of long duration loss of measurements (attitude control with no measurements for 1000s). This filter has been selected for in flight testing on PARASOL CNES microsatellite, and was experimented in May 2013.  The experimentation proved the efficiency of the proposed approach.
Publications

Total : 94

Articles dans des revues avec comité de lecture → 25 Voir

2019


Discrete-time robust control with an anticipative action for preview systems
Achnib, Asma ; Airimitoaie, Tudor-Bogdan ; Lanusse, Patrick ; Abrashov, Sergey ; Aoun, Mohamed ; Chetoui, Manel
Dans : Journal of Dynamic Systems, Measurement, and Control
https://hal.archives-ouvertes.fr/hal-01915210

2018


Combined adaptive feedback and feedforward compensation for active vibration control using Youla–Kučera parametrization
Airimitoaie, Tudor-Bogdan ; Landau, Ioan Doré
Dans : Journal of Sound and Vibration
https://hal.archives-ouvertes.fr/hal-01870542

2016


Robust and Adaptive Active Vibration Control Using an Inertial Actuator
Airimitoaie, Tudor-Bogdan ; Landau, Ioan Doré
Dans : IEEE Transactions on Industrial Electronics
https://hal.archives-ouvertes.fr/hal-01394199

Lithium-ion Open Circuit Voltage (OCV) curve modelling and its ageing adjustment
Lavigne, Loïc ; Sabatier, J. ; Francisco, J. Mbala ; Guillemard, F. ; Noury, A.
Dans : Journal of Power Sources
https://hal.archives-ouvertes.fr/hal-01719062

2015


Adaptive attenuation of unknown and time-varying narrow band and broadband disturbances
Landau, Ioan Doré ; Airimitoaie, Tudor-Bogdan ; Castellanos Silva, Abraham
Dans : International Journal of Adaptive Control and Signal Processing
https://hal.archives-ouvertes.fr/hal-01168620

Lithium-ion batteries modeling: A simple fractional differentiation based model and its associated parameters estimation method
Sabatier, Jocelyn ; Francisco, Junior Mbala ; Guillemard, Franck ; Lavigne, Loïc ; Moze, Mathieu ; Merveillaut, Mathieu
Dans : Signal Processing
https://hal.archives-ouvertes.fr/hal-01719065

2014


On the computation of $\pi$-flat outputs for differential-delay systems
Cazaurang, Franck ; Middeke, Johannes ; Antritter, Felix ; Lévine, Jean
Dans : Systems and Control Letters
https://hal-mines-paristech.archives-ouvertes.fr/hal-01070189

Flatness-based fault tolerant control
Martinez Torres, Cesar ; Lavigne, Loïc ; Cazaurang, Franck ; Alcorta Garcia, Efrain ; Diaz, David
Dans : DYNA
https://hal.archives-ouvertes.fr/hal-01098605

2013


Benchmark on Adaptive Regulation - Rejection ofunknown/time-varying multiple narrow band disturbances
Landau, Ioan Doré ; Castellanos Silva, Abraham ; Airimitoaie, Tudor-Bogdan ; Buche, Gabriel ; Noe, Mathieu
Dans : European Journal of Control
https://hal.archives-ouvertes.fr/hal-01394189

New sequential probability ratio test: Validation on A380 flight data
Lavigne, Loïc ; Cazaurang, Franck ; Fadiga, Lamine ; Goupil, Philippe
Dans : Control Engineering Practice
https://hal.archives-ouvertes.fr/hal-00875732

2011


A model-based technique for early and robust detection of oscillatory failure case in A380 actuators.
Lavigne, Loïc ; Zolghadri, Ali ; Goupil, Philippe ; SIMON, Pascal
Dans : International Journal of Control, Automation and Systems
https://hal.archives-ouvertes.fr/hal-00525092

2010


Motion planning for flat systems using positive B-splines: An LMI approach
Louembet, Christophe ; Cazaurang, Franck ; Zolghadri, Ali
Dans : Automatica
https://hal.archives-ouvertes.fr/hal-00636595

Génération de trajectoires d'attitude sur orbites: Approche par platitude et collocation
Louembet, Christophe ; Cazaurang, Franck ; Zolghadri, Ali ; Charbonnel, Catherine ; Pittet-Mechin, Christelle
Dans : Journal Européen des Systèmes Automatisés (JESA)
https://hal.archives-ouvertes.fr/hal-00417817

Robust Terminal Area Energy Management Guidance using Flatness Approach
Morio, Vincent ; Cazaurang, Franck ; Falcoz, Alexandre ; Vernis, Philippe
Dans : IET Control Theory and Applications
https://hal.archives-ouvertes.fr/hal-00392399

2009


Satellite path planning by flatness approach
Cazaurang, Franck ; Lavigne, Loïc
Dans : International Review of Aerospace Engineering
https://hal.archives-ouvertes.fr/hal-00401281

Path planning for satellite slew maneuvers: A combined Flatness and Collocation based Approach
Louembet, Christophe ; Cazaurang, Franck ; Zolghadri, Ali
Dans : IET Control Theory and Applications
https://hal.archives-ouvertes.fr/hal-00324646

Flatness-based Hypersonic Reentry Guidance of a Lifting-body Vehicle
Morio, Vincent ; Cazaurang, Franck ; Vernis, Philippe
Dans : Control Engineering Practice
https://hal.archives-ouvertes.fr/hal-00332394

Coupled LPV and Flatness-based Approach for Space Reentry Vehicles Guidance
Zerar, Madjid ; Cazaurang, Franck ; Zolghadri, Ali
Dans : IEE Proceedings. Control Theory and Applications
https://hal.archives-ouvertes.fr/hal-00367295

2008


New model-based strategies for guidance and health monitoring of experimental reentry vehicles
Cazaurang, Franck ; Morio, Vincent ; Falcoz, Alexandre ; Henry, David ; Zolghadri, Ali
Dans : International Review of Aerospace Engineering.
https://hal.archives-ouvertes.fr/hal-00338024

Onboard Path Planning for Reusable Launch Vehicles Application to the Shuttle Orbiter Reentry Mission
Morio, Vincent ; Cazaurang, Franck ; Zolghadri, Ali
Dans : International Review of Aerospace Engineering
https://hal.archives-ouvertes.fr/hal-00338021

Caractérisation LPV des systèmes non linéaires plats. Application à un Démonstrateur de Rentrée Atmosphérique.
Zerar, Madjid ; Cazaurang, Franck ; Zolghadri, Ali
Dans : Journal Européen des Systèmes Automatisés (JESA)
https://hal.archives-ouvertes.fr/hal-00281804

2006


Adaptive nonlinear state-space modelling for the prediction of daily mean PM10 concentrations
Zolghadri, Ali ; Cazaurang, Franck
Dans : Environmental modelling & software
https://hal.archives-ouvertes.fr/hal-00180794

2004


H-infinity design and multivariable delay margin - application to the dynamical control of a four-wheeled vehicle
Bergeon, Benoit ; Cazaurang, Franck
Dans : Journal Européen des Systèmes Automatisés (JESA)
https://hal.archives-ouvertes.fr/hal-00180810

2002


Fault diagnosis in induction machines using the generalized structured singular value
Henry, David ; Zolghadri, Ali ; Monsion, M. ; Cazaurang, Franck
Dans : Control Engineering Practice
https://hal.archives-ouvertes.fr/hal-00164899

2001


Méthodologie de commande robuste linéaire.Extensions aux systèmes plats et saturés
Bergeon, Benoit ; Cazaurang, Franck ; Ygorra, Stephane
Dans : Journal Européen des Systèmes Automatisés (JESA)
https://hal.archives-ouvertes.fr/hal-00180812
Communications avec actes (nationales) → 5 Voir

2016


Atténuation active robuste et adaptative desinterférences vibrationnelles
Landau, Ioan Doré ; Airimitoaie, Tudor-Bogdan
Dans : 13e Congrès Français d'Acoustique et le 20e colloque VIbrations, SHocks and NOise (CFA 2016 - VISHNO), Le Mans (France)
https://hal.archives-ouvertes.fr/hal-01394183

2014


Adaptive active vibration isolation – A control perspective
Landau, Ioan Doré ; Airimitoaie, Tudor-Bogdan ; Castellanos Silva, Abraham ; Alma, Marouane
Dans : 4ième Colloque Francophone Analyse Vibratoire Expérimentale, Blois (France)
https://hal.archives-ouvertes.fr/hal-01237933

2013


Modélisation unidimensionnelle multi-physique du comportement d'un joint à faces radiales pour la maintenance d'un circuit carburant
Ben Abdelwahed, Mohamed Amine ; Reungoat, D. ; Sommier, Alain ; Cazaurang, Franck ; Le Borgne, Eric
Dans : Congrès Français de Mécanique, Bordeaux (France)
https://hal.archives-ouvertes.fr/hal-00987487

Modélisation multi physiques d'un circuit carburant d'une turbomachine
Sifi, Mohcine ; Reungoat, D. ; Cazaurang, Franck ; Le Borgne, Eric ; De Barbeyrac, Philippe
Dans : 21ème Congrès Français de Mécanique, Bordeaux (France)
https://hal.archives-ouvertes.fr/hal-00987495

2001


Modeling a disturbed simplified aircraft model with flatness property
Lavigne, Loïc ; Cazaurang, Franck ; Bergeon, Benoit
Dans : Journées doctorales JDA'2001, Toulouse (France)
https://hal.archives-ouvertes.fr/hal-00193830
Communications avec actes (internationales) → 47 Voir

2018


Convertible Aircraft Dynamic Modelling and Flatness Analysis
Airimitoaie, Tudor-Bogdan ; Prieto Aguilar, Gemma ; Lavigne, Loïc ; Farges, Christophe ; Cazaurang, Franck
Dans : 9th Vienna International Conference on Mathematical Modelling, Vienna (Austria)
https://hal.archives-ouvertes.fr/hal-01719054

2017


Model Predictive Control Tuning: Methods and Issues. Application to steering wheel position control
Abrashov, Sergey ; Airimitoaie, Tudor-Bogdan ; Lanusse, Patrick ; Aioun, François ; Malti, Rachid ; Moreau, Xavier ; Guillemard, Franck
Dans : 20th IFAC World Congress, Toulouse (France)
https://hal.archives-ouvertes.fr/hal-01707608

Generalized predictive controller performances in an anticipative context
Achnib, Asma ; Airimitoaie, Tudor-Bogdan ; Abrashov, Sergey ; Lanusse, Patrick
Dans : 2017 14th International Multi-Conference on Systems, Signals & Devices (SSD), Marrakech (France)
https://hal.archives-ouvertes.fr/hal-01701080

Position, Attitude and Fault Tolerant Control of Tilt Rotor Quadcopter,
Kumar, Rumit ; Kumar, Manish ; Cohen, Kelly ; Cazaurang, Franck
Dans : 42nd Dayton-Cincinnati Aerospace Sciences Symposium, Dayton (United States)
https://hal.archives-ouvertes.fr/hal-01719048

Position and Attitude Control by Rotor Tilt and Rotor Speed Synchronization for Single Axis Tilting-Rotor Quadcopter
Kumar, Rumit ; Nemati, Alireza ; Kumar, Manish ; Cohen, Kelly ; Cazaurang, Franck
Dans : ASME 2017 Dynamic Systems and Control Conference, Tysons (United States)
https://hal.archives-ouvertes.fr/hal-01719037

Tilting-Rotor Quadcopter for Aggressive Flight Maneuvers Using Differential Flatness Based Flight Controller
Kumar, Rumit ; Nemati, Alireza ; Kumar, Manish ; Sharma, Rajnikant ; Cohen, Kelly ; Cazaurang, Franck
Dans : ASME 2017 Dynamic Systems and Control Conference, Tysons (United States)
https://hal.archives-ouvertes.fr/hal-01719035

Iterative Genetic Fuzzy Logic System for Solving the Aircraft Conflict Resolution Problem
Sathyan,, Anoop ; Ernest,, Nicholas ; Lavigne, Loïc ; Cazaurang, Franck ; Kumar, Manish ; Cohen, Kelly
Dans : 42nd Dayton-Cincinnati Aerospace Sciences Symposium , Dayton (United States)
https://hal.archives-ouvertes.fr/hal-01586007

A Genetic Fuzzy Logic Based Approach to Solving the Aircraft Conflict Resolution Problem
Sathyan,, Anoop ; Ernest,, Nicholas ; Lavigne, Loïc ; Cazaurang, Franck ; Kumar, Manish ; Cohen, Kelly
Dans : AIAA Information Systems-AIAA Infotech @ Aerospace, Grapevine (United States)
https://hal.archives-ouvertes.fr/hal-01585983

2016


Atténuation active des interférences vibrationnelles – Méthodologie et Evaluation expérimentale
Airimitoaie, Tudor-Bogdan ; Landau, Ioan Doré
Dans : 5ème Colloque Analyse Vibrationelle Expérimentale, Blois (France)
https://hal.archives-ouvertes.fr/hal-01394202

Lithium-ion Batteries Aging Motinoring Througth Open Circuit Voltage (OCV) Curve Modelling and Adjustment
Lavigne, Loïc ; Sabatier, Jocelyn ; Francisco, Junior Mbala ; Guillemard, Franck ; Noury, Agnieszka
Dans : 13th International Conference on Informatics in Control, Automation and Robotics, Lisbon (France)
https://hal.archives-ouvertes.fr/hal-01719072

2014


Model-based fault diagnosis for an electromechanical actuator of a helicopter turboshaft engine
Bobrinskoy, Alexandre ; Cazaurang, Franck ; Bluteau, Bruno ; Guerineau, Olivier ; Gatti, Marc
Dans : SAE 2014 Aerospace Systems and Technology Conference (ASTC), Cincinnati, Ohio (United States)
https://hal.archives-ouvertes.fr/hal-00987838

Model-based Fault Diagnosis of a Flight-Critical Actuator
Bobrinskoy, Alexandre ; Cazaurang, Franck ; Gatti, Marc ; Guerineau, Olivier ; Bluteau, Bruno
Dans : Recent Advances in Aerospace Actuation Systems and Components, Toulouse (France)
https://hal.archives-ouvertes.fr/hal-00974985

Lithium-ion battery state of charge estimation using a fractional battery model
Francisco, M. ; Sabatier, Jocelyn ; Lavigne, Loïc ; Guillemard, F. ; Moze, M. ; Tari, M. ; Merveillaut, M. ; Noury, A.
Dans : 2014 International Conference on Fractional Differentiation and its Applications (ICFDA), Catania (France)
https://hal.archives-ouvertes.fr/hal-01719066

2013


Dynamic inversion of flight critical actuator for fault diagnosis
Bobrinskoy, Alexandre ; Cazaurang, Franck ; Gatti, Marc ; Guerineau, Olivier ; Bluteau, Bruno
Dans : 32nd Digital Avionics Systems Conference, SYRACUSE (United States)
https://hal.archives-ouvertes.fr/hal-00838317

Control reconfiguration for differentially flat systems.
Martinez Torres, Cesar ; Lavigne, Loïc ; Cazaurang, Franck ; Alcorta Garcia, Efrain ; Diaz, David
Dans : Congreso Nacional de Control Automático AMCA 2013, México (Mexico)
https://hal.archives-ouvertes.fr/hal-00854361

Fault tolerant control of a three tank system: a flatness based approach
Martinez Torres, Cesar ; Lavigne, Loïc ; Cazaurang, Franck ; Alcorta Garcia, Efrain ; Diaz, David
Dans : 2nd International Conference on Control and Fault-Tolerant Systems, SysTol'13, Nice (France)
https://hal.archives-ouvertes.fr/hal-00854360

Fault detection and isolation on a three tank system using differential flatness.
Martinez Torres, Cesar ; Lavigne, Loïc ; Cazaurang, Franck ; Alcorta Garcia, Efrain ; Diaz, David
Dans : European Control Conference (ECC 13), Zurich (Switzerland)
https://hal.archives-ouvertes.fr/hal-00838271

Flat Stellar Dynamic Filter For Gyroless Attitude Estimation
Pittet-Mechin, Christelle ; Cazaurang, Franck ; Lavigne, Loïc
Dans : 19th IFAC Conference on. Automatic Control in. Aerospace. ACA 2013., Würzburg (Germany)
https://hal.archives-ouvertes.fr/hal-00841176

2012


MODEL-BASED FAULT DETECTION AND ISOLATION DESIGN FOR FLIGHT-CRITICAL ACTUATORS IN A HARSH ENVIRONMENT
Bobrinskoy, Alexandre ; Cazaurang, Franck ; Gatti, Marc ; Guérineau, Olivier ; Bluteau, Bruno
Dans : 31st Digital Avionics Systems Conference, Williamsburg (United States)
https://hal.archives-ouvertes.fr/hal-00736269

Oscillatory failure detection in Flight Control System of civil aircraft: EHA actuator servo loop case study.
Sifi, Mohcine ; Lavigne, Loïc ; Cazaurang, Franck ; Goupil, Philippe
Dans : R3ASC'12 (Recent Advances in Aerospace Actuation Systems and Components), Toulouse (France)
https://hal.archives-ouvertes.fr/hal-00703836

2011


Sequential Probability Ratio Test Using First Laplace Distribution for Oscillatory Fault Detection of an Hydraulic Actuator.
Fadiga, Lamine ; Cazaurang, Franck ; Lavigne, Loïc ; Goupil, Philippe
Dans : 18th IFAC World Congress, (Italy)
https://hal.archives-ouvertes.fr/hal-00610527

Commande Linéaire Quadratique d'une maquette pédagogique d'hélicoptère.
Lavigne, Loïc ; Farges, Christophe ; Cazaurang, Franck
Dans : CETSIS 2011 9e Colloque sur l'Enseignement des Technologies et des Sciences de l'Information et des Systèmes, (Canada)
https://hal.archives-ouvertes.fr/hal-00610532

Conception d'une maquette avionique pour l'étude du codage Gillham de l'altitude
Michaud, Denis ; Devos, Olivier ; Cazaurang, Franck ; Duchamp, Geneviève
Dans : CETSIS 2011, (Canada)
https://hal.archives-ouvertes.fr/hal-00671612

2009


Nonlinear Observer-Based OFC Detection for A380 Aircraft.
Alcorta Garcia, Efrain ; Zolghadri, Ali ; Goupil, Philippe ; Lavigne, Loïc ; SIMON, Pascal
Dans : 7th IFAC Symposium on Fault Detection, Supervision and Safety of Technical Processes. SAFEPROCESS 2009, Barcelone (Spain)
https://hal.archives-ouvertes.fr/hal-00365002

A new Path Planner based on Flatness Approach. Application to an Atmospheric Reentry Mission
Morio, Vincent ; Cazaurang, Franck ; Zolghadri, Ali ; Vernis, Philippe
Dans : European Control Conference, Budapest (Hungary)
https://hal.archives-ouvertes.fr/hal-00392572

2008


Oscillatory Failure Case detection for new generation Airbus aircraft: a model-based challenge
Lavigne, Loïc ; Zolghadri, Ali ; Goupil, Philippe ; SIMON, Pascal
Dans : 47th IEEE Conference on Decision and Control, Cancun (Mexico)
https://hal.archives-ouvertes.fr/hal-00299206

Robust and Early Detection of Oscillatory Failure Case for New Generation Airbus
Lavigne, Loïc ; Zolghadri, Ali ; Goupil, Philippe ; SIMON, Pascal
Dans : AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu (United States)
https://hal.archives-ouvertes.fr/hal-00263820

Sur la Caractérisation Formelle de Sorties Plates d'Ordre Réduit sur un Algèbre de Weyl
Morio, Vincent ; Cazaurang, Franck ; Zolghadri, Ali
Dans : Conférence Internationale Francophone d'Automatique, Bucarest (Romania)
https://hal.archives-ouvertes.fr/hal-00287404

Onboard Terminal Area Path Planning using Flatness Approach- Application to Shuttle Orbiter STS-1 Vehicle
Morio, Vincent ; Cazaurang, Franck ; Zolghadri, Ali ; Vernis, Philippe
Dans : 2nd international ARA Days, Arcachon (France)
https://hal.archives-ouvertes.fr/hal-00287402

SICVER Project: Innovative FDIR Strategies for Experimental Reentry Vehicles
Morio, Vincent ; Falcoz, Alexandre ; Cazaurang, Franck ; Henry, David ; Zolghadri, Ali ; Ganet, Martine ; Vernis, Philippe ; Bornschlegl, Eric
Dans : 2nd International ARA Days, Arcachon (France)
https://hal.archives-ouvertes.fr/hal-00287400

On the Formal Characterization of Reduced-Order Flat Outputs over an Ore Algebra
Morio, Vincent ; Cazaurang, Franck ; Zolghadri, Ali
Dans : 2nd IEEE Multi-conference on Systems and Control (MSC) / 9th IEEE International Symposium on Computer-aided Control System Design (CACSD), San Antonio, Texas (United States)
https://hal.archives-ouvertes.fr/hal-00287399

An Effective Algorithm for Analytical Computation of Flat Outputs over the Weyl Algebra
Morio, Vincent ; Cazaurang, Franck ; Zolghadri, Ali
Dans : IFAC WORD CONGRESS, SEOUL (North Korea)
https://hal.archives-ouvertes.fr/hal-00287385

Détection de pannes oscillatoires dans une chaîne d'asservissement en position d'une gouverne de l'A380
SIMON, Pascal ; Lavigne, Loïc ; Zolghadri, Ali ; Goupil, Philippe
Dans : CIFA 2008, Bucarest (Romania)
https://hal.archives-ouvertes.fr/hal-00274306

Fault recovery by nominal trajectory tracking
Staroswiecki, Marcel ; Cazaurang, Franck
Dans : American Control Conference 2008, Seattle, WA, (United States)
https://hal.archives-ouvertes.fr/hal-00349870

2007


Design of Algorithms for Satellite Slew Manoeuver by Flatness and Collocation
Louembet, Christophe ; Cazaurang, Franck ; Zolghadri, Ali
Dans : American Control Conference, New York (United States)
https://hal.archives-ouvertes.fr/hal-00180798

On the Design of a Flatness-based Guidance Algorithm for the Terminal Area Energy Management of a Winged-body Vehicle
Morio, Vincent ; Falcoz, Alexandre ; Vernis, Philippe ; Cazaurang, Franck
Dans : 17th IFAC Symposium on Automatic Control in Aerospace, TOULOUSE (France)
https://hal.archives-ouvertes.fr/hal-00180803

Coupled LPV and flatness based approach for ARD guidance
Zerar, Madjid ; Cazaurang, Franck ; Zolghadri, Ali
Dans : 17th IFAC Symposium on Automatic Control in Aerospace, TOULOUSE (France)
https://hal.archives-ouvertes.fr/hal-00180805

2006


Génération de trajectoire pour satellite AGILE par platitude et collocation
Cazaurang, Franck ; Louembet, Christophe ; Zolghadri, Ali
Dans : Conférence Internationale Francophone d'Automatique CIFA 2006, Bordeaux (France)
https://hal.archives-ouvertes.fr/hal-00180809

Flatness and collocation based methodology for satellite trajectory planning
Louembet, Christophe ; Cazaurang, Franck ; Zolghadri, Ali
Dans : IEEE International Symposium on Control, Communications, and Signal Processing, Marrakech (Morocco)
https://hal.archives-ouvertes.fr/hal-00243129

Hypersonic Reentry and Flatness Theory - Application to medium L/D Entry Vehicle
Morio, Vincent ; Vernis, Philippe ; Cazaurang, Franck
Dans : 1st international ARA Days, ARCACHON (France)
https://hal.archives-ouvertes.fr/hal-00180808

2005


LPV Modeling of Atmospheric re-entry demonstrator for guidance re-entry problem
Zerar, Madjid ; Cazaurang, Franck ; Zolghadri, Ali
Dans : Decision and Control, 2005 and 2005 European Control Conference. CDC-ECC '05., (Spain)
https://hal.archives-ouvertes.fr/hal-00243128

2004


Satellite path planning by flatness approach
Lavigne, Loïc ; Cazaurang, Franck ; Maini, Massimiliano ; Zerar, Madjid
Dans : Proceedings of SMC'2004, The Hague (Netherlands)
https://hal.archives-ouvertes.fr/hal-00186333

Robust tracking of nonlinear MIMO uncertain flat systems
Zerar, Madjid ; Cazaurang, Franck ; Zolghadri, Ali
Dans : Systems, Man and Cybernetics, 2004 IEEE International Conference, (France)
https://hal.archives-ouvertes.fr/hal-00243127

2003


Modelling of a longitudinal disturbed aircraft model by flatness approach.
Cazaurang, Franck ; Bergeon, Benoît ; Lavigne, Loïc
Dans : AIAA Conference, Guidance, Navigation and Contol, Austin (United States)
https://hal.archives-ouvertes.fr/hal-00186340

2002


LFT representation of a longitudinal perturbed aircraft model by flatness approach.
Cazaurang, Franck ; Lavigne, Loïc ; Bergeon, Benoît
Dans : Proceedings of IEEE CACSD 230, Glasgow (United Kingdom)
https://hal.archives-ouvertes.fr/hal-00186318

2001


Integrity monitoring of induction machines : A frequency domain model-based approach
Henry, David ; Zolghadri, Ali ; Monsion, M. ; Cazaurang, Franck
Dans : ECC'2001, Porto (Portugal)
https://hal.archives-ouvertes.fr/hal-00180623

Modelization of disturbed flat system for robust control design.
Lavigne, Loïc ; Cazaurang, Franck ; Bergeon, Benoît
Dans : 5th IFAC Symposium "Nonlinear Control System" (NOLCOS'01), Saint Pétersbourg (Russia)
https://hal.archives-ouvertes.fr/hal-00186316
Communications sans actes → 2 Voir

2017


Model Identification and control of a Convertible Aircraft (MICA)
Airimitoaie, Tudor-Bogdan ; Lavigne, Loïc ; Cohen, Kelly ; Farges, Christophe ; Cazaurang, Franck
Dans : 42nd Dayton-Cincinnati Aerospace Sciences Symposium, Dayton (United States)
https://hal.archives-ouvertes.fr/hal-01719041

2012


Fault tolerant guidance based on flatness approach: Application in a UAV.
Martinez Torres, Cesar ; Lavigne, Loïc ; Cazaurang, Franck ; Alcorta Garcia, Efrain ; Diaz, David
Dans : 1st AETOS conference "Research challenges for future UAV systems", Merignac (France)
https://hal.archives-ouvertes.fr/hal-00750310
Chapitres d'ouvrages scientifiques → 2 Voir

2017


Performances and robustness of GPC controller in an anticipative context
Achnib, Asma ; Airimitoaie, Tudor-Bogdan ; Abrashov, Sergey ; Lanusse, Patrick ; Aoun, Mohamed
https://hal.archives-ouvertes.fr/hal-01707571

2002


LFT Generation by Flatness Approach, for Mu-Analysis of HIRMplus Fighter Aircraft
Cazaurang, Franck ; Lavigne, Loïc ; Bergeon, Benoit
https://hal.archives-ouvertes.fr/hal-00180795
Habilitation à diriger des recherches → 1 Voir

2009


Du concept de platitude appliquéà la commande et au guidage autonomede systèmes aérospatiaux
Cazaurang, Franck
https://hal.archives-ouvertes.fr/tel-01097609
Preprint, Working Paper, Document sans référence, etc. → 1 Voir

2013


Système critique et procédé de surveillance
Bobrinskoy, Alexandre ; Gatti, Marc ; Guerineau, Olivier ; Cazaurang, Franck ; Bluteau, Bruno
https://hal.archives-ouvertes.fr/hal-00975013
Ouvrages scientifiques → 1 Voir

2017


Adaptive and robust active vibration control
Landau, Ioan Doré ; Airimitoaie, Tudor-Bogdan ; Castellanos Silva, Abraham ; Constantinescu, Aurelian
https://hal.archives-ouvertes.fr/hal-01237936
Brevets → 4 Voir

2015


Système critique et procédé de surveillance
Bobrinskoy, Alexandre ; Gatti, Marc ; Guerineau, Olivier ; Cazaurang, Franck ; Bluteau, Bruno
https://hal.archives-ouvertes.fr/hal-01303084

2012


Procédé et dispositif de détection de pannes oscillatoires dans une chaîne d'asservissement en position d'une gouverne d'aéronef.
Lavigne, Loïc ; Cazaurang, Franck ; Sifi, Mohcine ; Goupil, Philippe ; Babando, Olivier
https://hal.archives-ouvertes.fr/hal-00703847

2010


Etats Unis: Method and device for detecting oscillatory failures in a position servocontrol subsystem of an aircraft control surface.
Goupil, Philippe ; Zolghadri, Ali ; Lavigne, Loïc
https://hal.archives-ouvertes.fr/hal-00621314

2007


France: Procédé et dispositif de détection de pannes oscillatoires dans une chaîne d'asservissement en position d'une gouverne d'aéronef.
Philippe, Goupil ; Zolghadri, Ali ; Lavigne, Loïc
https://hal.archives-ouvertes.fr/hal-00618215
Rapport de recherche → 1 Voir

2017


Critique Constructive des Techniques Utilisées pour l'Estimation et la Validation des Modèles de Prédiction en Data Mining
Landau, Ioan Doré ; Landau, Vlad ; Airimitoaie, Tudor-Bogdan ; Robu, Bogdan
https://hal.archives-ouvertes.fr/hal-01522311
Theses → 5 Voir

2015


Algorithms and architectures for control and diagnosis of flight critical systems
Bobrinskoy, Alexandre
https://tel.archives-ouvertes.fr/tel-01249590

Design of an architecture for measurement and diagnosis of physical parameters in critical airborne systems
Martin, Romain
https://tel.archives-ouvertes.fr/tel-01249592

Nonlinear model based diagnosis : Application to the fuel system of a gas turbine
Sifi, Mohcine
https://tel.archives-ouvertes.fr/tel-01249601

2003


Outils d'analyse et de synthèse des lois de commande robuste des systèmes dynamiques plats.
Lavigne, Loïc
https://tel.archives-ouvertes.fr/tel-00186323

1997


ROBUST CONTROL OF FLAT SYSTEMS <br />APPLICATION ON CONTROL OF SYNCHRONOUS MOTOR
Cazaurang, Franck
https://tel.archives-ouvertes.fr/tel-00012110