
Marc Budinger
87
Documents
Présentation
Publications
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Publications
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Stress and energy release rate influence on ice shedding with resonant electro-mechanical de-icing systemsICAS 2022 - 33rd Congress of the International Council of the Aeronautical Sciences, Sep 2022, Stockholm, Sweden
Communication dans un congrès
hal-03823920
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A common framework for the design optimization of fixed-wing, multicopter and VTOL UAV configurations33rd Congress of the International Council of the Aeronautical Sciences, Sep 2022, Stockholm, Sweden
Communication dans un congrès
hal-03832115
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Incertitudes et conception de systèmes mécatroniques aéronautiquesPre-Forum des Rencontres Académie-Industrie AFIS, Association Française d'Ingénierie Système, Dec 2022, Toulouse, France
Communication dans un congrès
hal-04661454
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Proposition of a new qualification impact test for aerospace smart structuresICAS 2022 - 33rd Congress of the International Council of the Aeronautical Sciences, Sep 2022, Stockholm, Sweden
Communication dans un congrès
hal-03879795
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Design optimization of multirotor drones in forward flight32nd Congress of the International Council of the Aeronautical Sciences, Sep 2021, Shanghai, China
Communication dans un congrès
hal-03832135
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Trajectory and design optimization of multirotor drones with system simulationAIAA Scitech 2021 Forum, Jan 2021, Online, United States. ⟨10.2514/6.2021-0211⟩
Communication dans un congrès
hal-03121520
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Electro-mechanical Resonant Ice Protection Systems: Power requirements for fractures initiation and propagationAIAA Aviation 2021 Forum, Aug 2021, Online, United States. pp.AIAA 2021-2651, ⟨10.2514/6.2021-2651⟩
Communication dans un congrès
hal-03414409
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Extraction of compact transient thermal models for a global optimization of a power system based on SiC MOSFETs switches26th International Workshop on Thermal Investigations of ICs and Systems (THERMINIC 2020), Sep 2020, Berlin, Germany
Communication dans un congrès
hal-03655834
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SURROGATE MODELS OF PM BRUSHLESS MOTOR FOR THE PRELIMINARY DESIGN OF A MULTI-ROTOR DRONEAST 2019, Aircraft System Technologies, Feb 2019, Hamburg, Germany
Communication dans un congrès
hal-02065695
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A MORE INTEGRATED DESIGN APPROACH FOR EMBEDDED MECHATRONIC SYSTEMS: APPLICATION TO ELECTRICAL THRUST REVERSER ACTUATION SYSTEMSICAS 2018, Congres of the International Council of the Aeronautical Sciences, Sep 2018, Belo Horizonte, Brazil
Communication dans un congrès
hal-02065697
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Optimization of primary flight control actuation system using parametric sizing models of actuators, power electronics and structural analysis8th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2018, Toulouse, France. pp.132-138
Communication dans un congrès
hal-02020963
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Modelling and design approaches for the preliminary design of power electronic convertersELECTRIMACS, 2017, Toulouse, France
Communication dans un congrès
hal-02044400
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DIMENSIONAL ANALYSIS AND SURROGATE MODELS FOR THERMAL MODELLING OF POWER ELECTRONIC COMPONENTSElectrimacs, Jul 2017, Toulouse, France
Communication dans un congrès
hal-02044714
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A framework for the conceptual and preliminary design of aircraft equipmentsMore Electrical Aircraft, 2017, Bordeaux, France
Communication dans un congrès
hal-02042819
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A framework for the conceptual and preliminary design of embedded mechatronic systems6th International Workshop on Aircraft System Technologies (AST 2017), 2017, Hamburg, Germany
Communication dans un congrès
hal-02042821
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Dimensional analysis and surrogate models for the thermal modelling of power electronic componentsELECTRIMACS, 2017, Toulouse, France
Communication dans un congrès
hal-02045705
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Comparison of extensional and flexural modes for the design of piezoelectric ice protection systemsEUCASS 2017, Jul 2017, Milano, Italy
Communication dans un congrès
hal-02065709
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A framework for sizing embedded mechatronic systems during preliminary designInternational Federation of Automatic Control World Congress, 2017, Toulouse, France
Communication dans un congrès
hal-02044401
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Hybrid Regional Aircraft: A Comparative Review of New Potentials Enabled by Electric Power52nd AIAA/SAE/ASEE Joint Propulsion Conference, Jul 2016, Salt Lake City, United States. pp. 1-15
Communication dans un congrès
hal-01392448
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Dimensional analysis and surrogate modelling technique for the sizing of actuation systemsRecent Advances in Aerospace Actuation Systems and Components, 2016, Toulouse, France. pp.158-165
Communication dans un congrès
hal-02048651
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Hybrid Propulsion for Regional Aircraft: a Comparative Analysis based on Energy EfficiencyESARS-ITEC 2016, Nov 2016, Toulouse, France. pp.0
Communication dans un congrès
hal-01413276
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L'analyse dimensionnelle et les méta-modèles au service de la thermique des systèmes multi- physiquesCongrès Français de Themique SFT 2016, May 2016, Toulouse, France
Communication dans un congrès
hal-01396627
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Methodologies for the optimal design of the Integrated Modular Power Electronics Cabinet (IMPEC)MEA 2015 More Electric Aircraft, Feb 2015, Toulouse, France
Communication dans un congrès
hal-02514790
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Scaling-law-based metamodels for the sizing of actuation systems6th International Conference on Recent Advances in Aerospace Actuation Systems and Components, 2014, Toulouse, France. pp.129-135
Communication dans un congrès
hal-02054266
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Mission profiles analysis: guidelines to aircraft actuators new technology specificationProceedings of 29th congress of the International Council of the Aeronautical Sciences, St Petersbourg, 7-12 september 2014., 2014, St Petersbourg, Russia
Communication dans un congrès
hal-02054339
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Modelica Preliminary Design Library for Electromechanical ActuatorsAST 2013, 4th International Workshop on Aircraft System Technologies, TUHH, Hamburg, Germany, April 23-24, 2013, 2013, Hamburg, Germany
Communication dans un congrès
hal-02183708
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ACTUATION 2015, Model based design of electromechanical actuatorsDesign of complex dynamic systems, Modelica and FMI standards, 17 septembre 2013, Toulouse, 2013, Toulouse, France
Communication dans un congrès
hal-02181630
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From Airframer Requirements to Detailed Technical Specification of Electromechanical Actuators Aided by Knowledge-Based MethodsSAE 2013 AeroTech Congress & Exhibition, Montréal, Quebec, Canada September 24-26, 2013, 2013, Montréal, Quebec, Canada. ⟨10.4271/2013-01-2163⟩
Communication dans un congrès
hal-02182184
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Modelling approachs for the simulation-based preliminary design and optimization of electromecanical and hydraulic actuation systems8th AIAA Multidisciplinary Design Optimization Specialist Conference, 23-26 April 2012, Honolulu, Hawaii, USA., 2012, Honolulu, Hawaï, United States
Communication dans un congrès
hal-02187110
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Knowledge-based system for aircraft electrical power system reconfiguration2nd International Conference on Electrical Systems for Aircraft Railway And Ship Propulsion 2012 (ESARS 2012) - Bologne, 2012, Bologne, Italy. ⟨10.1109/ESARS.2012.6387377⟩
Communication dans un congrès
hal-02186306
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Comparative study of stochastic optimization methods to solve load allocation problem for aircraft electrical power system designXII-th International Workshop on Optimization and Inverse Problems in Electromagnetism (OIPE 2012) - Ghent, 2012, Ghent, Belgium
Communication dans un congrès
hal-02186315
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Optimal preliminary design of electromechanical actuation systems« More electrical » aircraft technologies, Symposium SPEC, November 8 & 9, 2011, Lyon., 2012, Lyon, France
Communication dans un congrès
hal-02187146
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Model Based Methodologies for the Assessment of More Electric Flight Control ActuatorsProceedings of the 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference, American Institute of Aeronautics and Astronautics, Fortworth, USA, 13-15 September, 2010, Fortworth, United States
Communication dans un congrès
hal-02193659
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Optimal geometrical integration of electromechanical actuators ,OPTIMUS User Meeting 2010, Antwerp, 22 and 23 November 2010., 2010, Antwerp, France
Communication dans un congrès
hal-02193755
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Optimal geometrical integration of electromechanical actuatorsProceedings of the 4th internation conference on Recent Advances in Aerospace Actuation Systems and Components, June 24-26, 2010, Toulouse, France
Communication dans un congrès
hal-02193657
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Coupling CAD and system simulation framework for the preliminary design of electromechanical actuatorsProceedings of IDMME - Virtual Concept 2010, Bordeaux, France, October 20 – 22, 2010, Bordeaux, France
Communication dans un congrès
hal-02193658
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Design for reliability of electromechanical actuatorsProceedings of the 4th international conference on Recent Advances in Aerospace Actuation Systems and Components, June 24-26, 2010, Toulouse, France
Communication dans un congrès
hal-02193660
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Comparative analysis of energy losses in servo-hydraulic, electro-hydrostatic and electro-mechanical actuatorsThe 11th Scandinavian International Conference on Fluid Power, SICFP’09, Linköping, Sweden, June 2-4, 2009, Linköping, Sweden
Communication dans un congrès
hal-02194565
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Preliminary Design of Electromechanical Actuators with ModelicaModelica 2009, 7th Modelica Conference, Como, Italy, Sep. 20-22, 2009, Sep 2009, Como, Italy. ⟨10.3384/ecp09430099⟩
Communication dans un congrès
hal-02194563
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Model based Design of Electromechanical Actuators with ModelicaIDETC 09, San Diego, 30 aout, 2 septembre 2009., 2009, San Diego, United States
Communication dans un congrès
hal-02194564
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New screen-printed thermal microactuator2nd IEEE International Conference on Nano/Micro Engineered and Molecular Systems, Jan 2007, Bangkok, Thailand. pp.851-855
Communication dans un congrès
hal-00164487
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New screen-printed MEMS : study of a thermal microactuatorSmart System Integration, Mar 2007, Paris, France
Communication dans un congrès
hal-00164491
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Modeling of water vapor permeation inside BCB-sealed packages for microsystemsProc. of DTIP Conference on Design, Test, Integration and Packaging of MEMS and MOEMS, 2005, Switzerland. pp.1
Communication dans un congrès
hal-00183073
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Modélisation analytique de micro actionneurs thermiques2èmes Journées du RTP Fiabilité, 2004, France. pp.1
Communication dans un congrès
hal-00183080
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Claquage électrostatique et protection en surtension des MEMS2èmes Journées du RTP Fiabilité, 2004, France. pp.1
Communication dans un congrès
hal-00183076
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Transformateur piézoélectrique et intégration hybride, évaluation du potentiel par une modélisation analytique7èmes journées du pole Microrobotique, 2004, Suisse. pp.1
Communication dans un congrès
hal-00183082
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Chaînes de transmission de puissance mécatroniques - Mise en place des modèles d'estimation pour la conception préliminaireTechniques de l’Ingénieur, Référence BM8025, 2011
Ouvrages
hal-02191712
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Chaînes de transmission de puissance mécatroniques - Modèles d'estimationTechniques de l'ingénieur, 2013
Chapitre d'ouvrage
hal-01756784
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Contribution à la conception et à la modélisation d'actionneurs piézoélectriques cylindriques à deux degrés de liberté de type rotation et translationVibrations [physics.class-ph]. Institut National Polytechnique de Toulouse - INPT, 2003. Français. ⟨NNT : ⟩
Thèse
tel-00864606
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Preliminary design and sizing of actuation systemsMechanical engineering [physics.class-ph]. UPS Toulouse, 2014
HDR
tel-01112448
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