Jean-Philippe CONDOMINES
Présentation
Publications
Publications
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An Equivariant von Mises-Gaussian distribution on SE(n) for Unscented Kalman Filtering2025 IEEE 64th Conference on Decision and Control (CDC), Dec 2025, Rio de Janeiro, France. pp.462-469, ⟨10.1109/CDC57313.2025.11312481⟩ |
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Evaluation of drag coefficient for a quadrotor model13th International Micro Air Vehicle Conference, Sep 2022, Delft, Netherlands. pp.39--46 |
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Estimating wind using a quadrotorinternational micro air vehicle conference (IMAV2021), Nov 2021, Puebla, Mexico. pp.124-130 |
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Towards a unified model-free control architecture for tailsitter micro air vehicles: Flight simulation analysis and experimental flightsAIAA Scitech 2020 Forum, Jan 2020, Orlando, United States. ⟨10.2514/6.2020-2075⟩ |
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Economic Model-Predictive Control Strategies for Aircraft Deep-stall Recovery with Stability GuaranteesCDC 2019, 58th Conference on Decision and Control, Dec 2019, Nice, France. pp.ISBN: 978-1-7281-1397-5, ⟨10.1109/CDC40024.2019.9030207⟩ |
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Full model-free control architecture for hybrid UAVsAmerican Control Conference, ACC 2019, Jul 2019, Philadelphia, PA, United States. ⟨10.23919/ACC.2019.8814993⟩ |
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Invariant Unscented Kalman Filter with application to attitude estimationCDC 2017, 56th IEEE conference on decision and control, Dec 2017, Melbourne, Australia. pp.ISBN: 978-1-5090-2874-0, ⟨10.1109/CDC.2017.8264063⟩ |
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Tightly coupled navigation and wind estimation for mini UAVsAIAA GNC 2018, AIAA Guidance, Navigation, and Control Conference, Jan 2018, Kissimee, United States. ⟨10.2514/6.2018-1843⟩ |
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Fixed-wind UAV with transitioning flight capabilities: Model-Based or Model-Free Control approach? A preliminary studyInternational Conference on Unmanned Aircraft Systems, ICUAS'18, Jun 2018, Dallas, TX, United States. pp.1157-1164 |
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Model-free control approach for fixed-wing UAVs with uncertain parameters analysis23rd International Conference on Methods & Models in Automation & Robotics, MMAR 2018, Aug 2018, Miedzyzdroje, Poland. ⟨10.1109/MMAR.2018.8486083⟩ |
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Design of a novel network intrusion detection system for drone communicationsDASC 2018, 37th AIAA/IEEE Digital Avionics Systems Conference, Sep 2018, Londres, United Kingdom. ⟨10.1109/DASC.2018.8569300⟩ |
Piece-wise Identification and Analysis of the Aerodynamic Coefficients, Trim Conditions, and Safe Sets of the Generic Transport ModelGNC 2018 AIAA Guidance, Navigation, and Control Conference, Jan 2018, Kissimmee, United States. pp.ISBN : 978-1-62410-526-5, ⟨10.2514/6.2018-1114⟩ |
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The Invariant Unscented Kalman FilterCDC 2017, 56th IEEE Conference on Decision and Control, Dec 2017, Melbourne, Australia |
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Unscented Kalman Filtering on Lie GroupsIROS 2017, EEE/RSJ International Conference on Intelligent Robots and Systems, IEEE/RSJ, Sep 2017, Vancouver, Canada |
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Non-linear Analysis and Control Proposal for In-flight Loss-of-control20th World Congress of the International Federation of Automatic Control, Jul 2017, Toulouse, France. pp.ISSN: 2405-8963 |
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Design of a robust Controller/Observer for TCP/AQM network: First application to intrusion detection systems for drone fleetIROS 2017, EEE/RSJ International Conference on Intelligent Robots and Systems, Sep 2017, Vancouver, Canada. pp. 1707-1712, ISBN: 978-1-5386-2681-8 |
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Team MAVion entry in the IMAV'17 outdoor challenge – A tail-sitting trajectory-tracking µUAVIMAV 2017, 9th International Micro Air Vehicle Conference and Competition, Sep 2017, Toulouse, France |
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Full-envelope Equations of Motion of the Generic Transport Model based on Piece-wise Polynomial Aerodynamic Coefficients4th International Workshop on Research, Education and Development on Unmanned Aerial Systems, Oct 2017, Linköping, Sweden. ⟨10.1109/RED-UAS.2017.8101652⟩ |
Fleets of enduring drones to probe atmospheric phenomena with cloudsISARRA 2016 4th Conference of the International Society for Atmospheric Research using Remotely-piloted Aircraft, May 2016, Toulouse, France |
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Experimental Wind-Field EstimationISARRA 4th Conference of the International Society for Atmospheric Research using Remotely-piloted Aircraft, May 2016, Toulouse, France |
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Experimental Wind Field Estimation and Aircraft IdentificationIMAV 2015: International Micro Air Vehicles Conference and Flight Competition, Sep 2015, Aachen, Germany |
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Pi-Invariant Unscented Kalman Filter for Sensor FusionCDC 2014, 53rd IEEE Conference on Decision and Control, Dec 2014, Los Angeles, United States. pp.1035-1040, ⟨10.1109/CDC.2014.7039518⟩ |
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Nonlinear state estimation using an invariant unscented Kalman filterAIAA GNC 2013, AIAA Guidance, Navigation and Control Conference, Aug 2013, Boston, United States. pp 1-15 ; ISBN : 978-1-62410-224-0, ⟨10.2514/6.2013-4869⟩ |
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Development of an 18cm Micro Air Vehicle : QUARKIMAV 2013, International Micro Air Vehicle Conference and Flight Competition, Sep 2013, Toulouse, France. pp xxxx |
Introduction au contrôle des mini-drones : de la conception à la mise en œuvreEllipses, 2020, Formations & Techniques, 9782340040397 |
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Filtrage de Kalman non linéaire pour la navigation multicapteurs d'un mini drone : Application au pilotage-guidage robuste en milieu complexeISTE Press, 2018, 9781784055172 |
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Nonlinear Kalman Filter for Multi-Sensor Navigation of Unmanned Aerial Vehicles: Application to Guidance and Navigation of Unmanned Aerial Vehicles Flying in a Complex EnvironmentISTE Press, 2018, 978-1785482854 |
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Optimal Invariant Observers Theory for Nonlinear State EstimationEdited by Fourati Hassen Belkhiat Djamel Eddine Chouaib Iniewski Krzysztof. Multisensor Attitude Estimation Fundamental Concepts and Applications Edited by Fourati Hassen Belkhiat Djamel Eddine Chouaib Iniewski Krzysztof , Taylor & Francis, pp 391-408, 2016, 978-1-4987-4571-0, eBook ISBN: 978-1-4987-4580-2 |
PROCEDE DE SURVEILLANCE D'UN SYSTEME, DISPOSITIFS, SYSTEME ET PROGRAMME CORRESPONDANTFrance, Patent n° : WO 2021/165511. 2022 |
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Flight control system and method for a convertible fixed-wing drone providing a stabilized continuous transition between a vertical stationary flight and a horizontal cruise flightSuisse, N° de brevet: WO2019238375A1. 2019 |
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Système et procédé de contrôle de vol d'un drone convertible à voilure fixe permettant une transition continue stabilisée entre un vol stationnaire vertical et un vol de croisière à l'horizontalSuisse, N° de brevet: WO2019238375A1. 2019 |
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Reducing Computational Cost in the Invariant Unscented Kalman Filtering For Attitude Estimation2019 |
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Invariant Unscented Kalman filtering : A Parametric formulation study for Attitude Estimation2019 |
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Analysis of the Aerodynamic Coefficients for the Evolvable Demonstrator for Upset Recovery Approaches with Evaluation in the Wind-tunnel2018 |
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Network intrusion detection system for drone fleet using both spectral analysis and robust controller / observer[Research Report] RR-ENAC-2018-01, ENAC. 2018 |
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Piecewise Polynomial Model of the Aerodynamic Coefficients of the Generic Transport Model and its Equations of Motion[Technical Report] Third corrected version, ONERA -- The French Aerospace Lab; École Nationale de l'Aviation Civile. 2018 |
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Estimation non linéaire basée sur la théorie des observateurs invariants[Rapport de recherche] RR-ENAC-2017-001, ENAC. 2017 |
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Développement d’un estimateur d’état non linéaire embarqué pour le pilotage-guidage robuste d’un micro-drone en milieu complexePhysique de l'espace [physics.space-ph]. INSTITUT SUPERIEUR DE L'AERONAUTIQUE ET DE L'ESPACE (ISAE), 2015. Français. ⟨NNT : ⟩ |
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De l’estimation et du contrôle non linéaire à l’avionique de systèmes de drones plus sûrs et robustesSciences de l'ingénieur [physics]. Université Toulouse 3 - Paul Sabatier, 2022 |