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Work experience: 
01/2011
Navigation System Engineer
Location: 
Defense & Space
Airbus Defence and Space
- Project EGNOS V3 phases A and B (European Space Agency, 20M€) System performance architect Coordination of project partners contributions to system performance : Astrium GmbH (Germany), Astrium France, Astrium UK, DEIMOS (Spain) Delivery manager for Astrium France contributions on RAMS & performance studies Technical synthesis and cost reporting for Astrium France contributions Team activities planning - Galileo Service Centre Project Manager (EC project) - Business Development, R&D: answer to ESA and CNES Invitations To Tender, coordination of technical studies.
01/2008 to 01/2011
R&D Navigation System Engineer
Location: 
Defense & Space
Astrium
- CNES R&D and Missile Defense: Technical Manager for navigation algorithms design, performance evaluation and navigation chain sizing - Technical coordinator on the european FP7 study AEROFAST aiming at developing the technologies needed to archieve an aerocapture on Mars. - Technical proposals to ESA Invitations To Tenders on interplanetary navigation studies.
01/2004 to 01/2008
Navigation Sensors Engineer
Location: 
Defense & Space
EADS Astrium
·Technical product manager for the Inertial Measurement Unit (I.M.U.) on M51 programme (French deterrence missile): SAGEM design and development follow-up, system performance evaluations on simulated and real data, definition of integration and qualification tests. ·ARIANE 5 : Technical Responsible for IMU performance assessment and models for GNC studies. ·ATV Rendez-Vous sensors integration tests : technical coordination of the tests, processing of the optical sensors telemetries, performance evaluation, solving of the sensors anomalies in partnership with the suppliers and ESA. ·Definition of a hybridised GNSS/I.M.U. architecture for GEO and MEO missions for the Ariane 5 launcher evolution.
01/2003 to 01/2004
Radionavigation system engineer
Location: 
Airlines/Aviation
Teuchos SAFRAN Group
Development for Airbus France of the Thales equipement « Multi Mode Receiver » which includes the MLS (Microwave Landing System) function: integration tests monitoring and elaboration of the certification file to be presented to the aeronautical authorities

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