| The Fully Networked Car, A Workshop on ICT in Vehicles |
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Jean-Tony MALATERRE
R&D Engineer
Technical Co-ordinator
Diagnostic Equipments
ACTIA
25 chemin de Pouvourville
BP 7421531432 TOULOUSE CEDEX 4 France
Tel. : +33 (5) 61 17 61 52
Fax : +33 (5) 61 55 42 31
Mail : tony.malaterre@actia.fr |
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| Session 5: |
Diagnostics |
| Title of Presentation: |
Diagnostic process and place of some standard |
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| Since 1997 for ACTIA: |
| 2003 - Present |
ISO expert for ACTIA Group. |
| 2000 – 2003 |
Senior Project Manager on software and hardware development ( for NXR, Renault Diagnostic tool, Multi-Di@g, ACTIA multi brand solution, and ORUS, diagnostic solution for PSA plant). |
| 1997 – 1999 |
Research and development on diagnostic methods. Use of CBR (Case-Based Reasoning) and PR (Pattern Recognition). In charge of the relation with Research Laboratory (CNRS). |
| 1996 |
Scientist for ONERA. Study of control and separation on turbulent boundary layer. |
| 1995 |
Engineer degree Ecole Nationale Supérieure de Mécanique et d’Aérotechnique.
Diplôme d’Etude Approfondie en Aérodynamique, Combustion et Thermique |
| Publications: |
- “About the use of CBR technology in automotive diagnosis” T.Malaterre – ACTIA – France, 14-15 June 2001, Stresa, Lago Maggiore, Italy
- “Diagnosis Application: the Peugeot Prototype”, T.Malaterre, DaimlerBenz Technology Workshop Case-Based Reasoning, ULM, 29 June 1998 - 1st July 1998
- “Control of 3D turbulent boundary layer separation caused by a wing-body junction”. Barberis D., Molton P. and Malaterre T., Experimental Thermal and Fluid Science 16 (1998)
- “Etude expérimentale du décollement tridimensionnel incompressible induit par un obstacle cylindrique”, Barberis, D., Molton, P. Malaterre, T. ONERA, RT 111/7078 AY, Décembre 1996
- “Caractérisation du champ aérodynamique d'un décollement tridimensionnel sur une plaque plane.” Molton P.;Barberis D.;Malaterre T.;Monnier J.C.;Stanislas M. 5ème congrès francophone de vélocimétrie laser, Rouen, 24-27 Septembre 1996.
- “Analysis and control of a 3D turbulent boundary layer separation caused by the wing/fuselage interface”;Barberis D., Molton P., Malaterre T., Flowcontrol Worshop, Cargese, France, July 1-5 1996
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