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FFTG

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    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 : 115

    Articles dans des revues avec comité de lecture → 32 Voir

    2023


    Improving performance of adaptive feedforward noise attenuators using a dynamic adaptation gain
    Landau, Ioan Doré ; Vau, Bernard ; Airimitoaie, Tudor-Bogdan ; Buche, Gabriel
    Dans : Journal of Sound and Vibration
    https://hal.science/hal-04045279

    2022


    Robust Design of an Anticipative Feedforward-feedback Controller for MIMO Systems
    Achnib, Asma ; Airimitoaie, Tudor-Bogdan ; Lanusse, Patrick
    Dans : International Journal of Control, Automation and Systems
    https://hal.science/hal-03605660

    Nonlinear three-tank system fault detection and isolation using differential flatness
    Rammal, Rim ; Airimitoaie, Tudor-Bogdan ; Melchior, Pierre ; Cazaurang, Franck
    Dans : IFAC Journal of Systems and Control
    https://hal.science/hal-03708653

    Development of a high accuracy and stability test bench for ageing measurement of 16 nm FinFETs based FPGA
    Sobas, Justin ; Airimitoaie, Tudor-Bogdan ; Marc, Francois
    Dans : Microelectronics Reliability
    https://hal.science/hal-04017664

    2021


    Algorithms for Adaptive Feedforward Noise Attenuation--A Unified Approach and Experimental Evaluation
    Airimitoaie, Tudor-Bogdan ; Landau, Ioan Doré ; Melendez, Raul ; Dugard, Luc
    Dans : IEEE Transactions on Control Systems Technology
    https://hal.science/hal-02947816

    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.science/hal-01915210

    Beyond the delay barrier in adaptive feedforward active noise control using Youla -Kučera parametrization
    Landau, Ioan Doré ; Meléndez, Raúl ; Airimitoaie, Tudor-Bogdan ; Dugard, Luc
    Dans : Journal of Sound and Vibration
    https://hal.science/hal-02136074

    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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/hal-00875732

    2012


    A Youla–Kucera parametrized adaptive feedforward compensator for active vibration control with mechanical coupling
    Landau, Ioan Doré ; Airimitoaie, Tudor-Bogdan ; Alma, Marouane
    Dans : Automatica
    https://hal.science/hal-02156535

    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.science/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.science/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.science/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.science/hal-00392399

    2009


    Satellite path planning by flatness approach
    Cazaurang, Franck ; Lavigne, Loïc
    Dans : International Review of Aerospace Engineering
    https://hal.science/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.science/hal-00324646

    Flatness-based Hypersonic Reentry Guidance of a Lifting-body Vehicle
    Morio, Vincent ; Cazaurang, Franck ; Vernis, Philippe
    Dans : Control Engineering Practice
    https://hal.science/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.science/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.science/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.science/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.science/hal-00281804

    2006


    Adaptive nonlinear state-space modelling for the prediction of daily mean PM10 concentrations
    Zolghadri, Ali ; Cazaurang, Franck
    Dans : Environmental Modelling and Software
    https://hal.science/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.science/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.science/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.science/hal-00180812
    Communication dans un congrès → 67 Voir

    2023


    Artificial Intelligence for Defence in an EQF6 Training and Education Program, From the Design to the Execution
    Grivel, Eric ; Pesquet, Baptiste ; Airimitoaie, Tudor-Bogdan ; Zemmari, Akka
    Dans : Educon 2023, Kuweit city (Kuwait)
    https://hal.science/hal-04005245

    2022


    Does a general structure exist for adaptation/learning algorithms?
    Landau, Ioan Doré ; Airimitoaie, Tudor-Bogdan
    Dans : CDC 2022 - 61st IEEE Conference on Decision and Control, Cancun (Mexico)
    https://hal.science/hal-03738223

    2021


    Experimental evaluation of a new class of algorithms for active noise attenuation
    Landau, Ioan Doré ; Airimitoaie, Tudor-Bogdan ; Melendez, Raul ; Buche, Gabriel ; Dugard, Luc
    Dans : SIA- Automotive NVH Comfort 2020, Le Mans (France)
    https://hal.science/hal-02959422

    Model Predictive Control of engine intake manifold pressure with an uncertain model
    Shulga, Evgeny ; Lanusse, Patrick ; Airimitoaie, Tudor-Bogdan ; Maurel, Stéphane ; Trutet, Arnaud
    Dans : 7th IFAC Conference on Nonlinear Model Predictive Control, Bratislava (Slovakia)
    https://hal.science/hal-03580824

    2020


    Robust Anticipative Controller Design with Application to A High Dynamic Engine Testbed
    Airimitoaie, Tudor-Bogdan ; Lanusse, Patrick ; Achnib, Asma
    Dans : 21th World Congress of the International Federation of Automatic Control, Berlin (Germany)
    https://hal.science/hal-02885931

    Adaptive Youla-Kucera Parametrization for Active Noise and Vibration Attenuation
    Landau, Ioan Doré ; Airimitoaie, Tudor-Bogdan ; Melendez, Raul ; Buche, Gabriel ; Dugard, Luc
    Dans : ICSTCC 2020 - 24th International Conference on System Theory, Control and Computing, Sinaia (virtual conference) (Romania)
    https://hal.science/hal-03119913

    Unimodular Completion for Computation of Fractionally Flat Outputs for Linear Fractionally Flat Systems
    Rammal, Rim ; Airimitoaie, Tudor-Bogdan ; Melchior, Pierre ; Cazaurang, Franck
    Dans : 21th World Congress of the International Federation of Automatic Control, Berlin (Germany)
    https://hal.science/hal-02885984

    On the Choice of Multiple Flat Outputs for Fault Detection and Isolation of a Flat System
    Rammal, Rim ; Airimitoaie, Tudor-Bogdan ; Cazaurang, Franck ; Lévine, Jean ; Melchior, Pierre
    Dans : 21th World Congress of the International Federation of Automatic Control, Berlin (Germany)
    https://hal.science/hal-02885978

    Preview control of engine intake manifold pressure
    Shulga, Evgeny ; Lanusse, Patrick ; Airimitoaie, Tudor-Bogdan ; Maurel, Stéphane ; Trutet, Arnaud
    Dans : 28th Mediterranean Conference on Control and Automation, Saint-Raphaël (France)
    https://hal.science/hal-02891103

    2019


    Convertible delta-wing aircraft for teaching and research
    Airimitoaie, Tudor-Bogdan ; Farges, Christophe ; Lavigne, Loïc ; Cazaurang, Franck
    Dans : 21st IFAC Symposium on Automatic Control in Aerospace ACA 2019, Cranfield (United Kingdom)
    https://hal.science/hal-02378547

    Why one should use Youla-Kucera parametrization in adaptive feedforward noise attenuation?
    Landau, Ioan Doré ; Airimitoaie, Tudor-Bogdan ; Meléndez, Raúl ; Dugard, Luc
    Dans : CDC 2019 - 58th IEEE Conference on Decision and Control, Nice (France)
    https://hal.science/hal-02190768

    2018


    Anticipative Robust Design Applied to a Water Level Control System
    Achnib, Asma ; Airimitoaie, Tudor-Bogdan ; Lanusse, Patrick ; Guefrachi, Ayadi ; Aoun, Mohamed ; Chetoui, Manel
    Dans : 2018 17th European Control Conference (ECC), Limassol (Cyprus)
    https://hal.science/hal-02056814

    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.science/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.science/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.science/hal-01701080

    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.science/hal-01719041

    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.science/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.science/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.science/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.science/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.science/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.science/hal-01394202

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

    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.science/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.science/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.science/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.science/hal-01719066

    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.science/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.science/hal-00987487

    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.science/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.science/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.science/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.science/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.science/hal-00841176

    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.science/hal-00987495

    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.science/hal-00736269

    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.science/hal-00750310

    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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/hal-00274306

    Fault recovery by nominal trajectory tracking
    Staroswiecki, Marcel ; Cazaurang, Franck
    Dans : American Control Conference 2008, Seattle, WA, (United States)
    https://hal.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/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.science/hal-00180623

    Modeling a disturbed simplified aircraft model with flatness property
    Lavigne, Loïc ; Cazaurang, Franck ; Bergeon, Benoit
    Dans : Journées doctorales JDA'2001, Toulouse (France)
    https://hal.science/hal-00193830

    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.science/hal-00186316

    1996


    Anti Windup Position control of synchronous machine with current limitation
    Cazaurang, Franck ; Ygorra, Stephane ; Bergeon, Benoît ; Fadel, Maurice ; Faucher, Jean
    Dans : ElectrIMACS'96, International Association for Mathematics and Computer in Simulation, Saint-Nazaire (France)
    https://ut3-toulouseinp.hal.science/hal-03553925
    Chapitres d'ouvrages scientifiques → 2 Voir

    2019


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

    2002


    LFT Generation by Flatness Approach, for Mu-Analysis of HIRMplus Fighter Aircraft
    Cazaurang, Franck ; Lavigne, Loïc ; Bergeon, Benoit
    https://hal.science/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.science/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.science/hal-00975013
    Ouvrages scientifiques → 2 Voir

    2020


    Multi-rotor Platform Based UAV Systems
    Cazaurang, Franck ; Cohen, Kelly ; Kumar, Manish
    https://hal.science/hal-02426536

    2017


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

    2015


    Système critique et procédé de surveillance
    Bobrinskoy, Alexandre ; Gatti, Marc ; Guerineau, Olivier ; Cazaurang, Franck ; Bluteau, Bruno
    https://hal.science/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.science/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.science/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.science/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.science/hal-01522311
    Theses → 5 Voir

    2015


    Algorithms and architectures for control and diagnosis of flight critical systems
    Bobrinskoy, Alexandre
    https://theses.hal.science/tel-01249590

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

    Nonlinear model based diagnosis : Application to the fuel system of a gas turbine
    Sifi, Mohcine
    https://theses.hal.science/tel-01249601

    2003


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

    1997


    ROBUST CONTROL OF FLAT SYSTEMS <br />APPLICATION ON CONTROL OF SYNCHRONOUS MOTOR
    Cazaurang, Franck
    https://theses.hal.science/tel-00012110