Foil control Systems:- Project management (Jira)- Functionnal specification- System architecture definition- Actuators selection and integration- Supplier follow-up- Performance calculation, Test analysis (Python)Boat control systems:- Thermal management software (Simulink, Stateflow, Ecocoder)- Thermal models (simulink) - Git implementation

Interface between technical department / production / customer service / sales:- Calls for bids technical analysis- Flight demonstrations- In service product management - customer support- Failure analysis - Corrective action planOptimize UAV use for various applications (Topography, industrial inspections, security), and support operations: - RTK georeferencing - UAV photogrammetry optimization - Aerial thermography - Video broadcast (RTMP, RTSP)

Fixedwing and rotorcraft autopilot design:- Inertial sensors fusion (AHRS, INS)- Attitude, horizontal and vertical navigation control loops- Flight plans procedures: check-list, take-off, survey, landing and associated emmergency procedures- Flight dynamics simulation- Flight tests analysis- Definition of ground and flight tests procedures- User manual redaction- Delta-Y and Delta-H UAV pilot for devellopment, commercial flights and demonstrations.

Mitsubishi Regional Jet Program :Since January 2009:MRJ elevator servocontrol design, focused on performance and cost optimization. Follow-up with suppliers and customer.Writing technical proposalStatic and dynamic performances sizingWriting specifications of the servovalve and the LVDT (position sensor)EMA A30X/MODENE Program:Since September 2008:Electromechanical actuator « EMA » studies for the future Airbus single aisle aircraft, Control systems design and simulation. Position and load control loops Load and power limitationAirbus A380 Program:A380 flight control actuators design of static and dynamic performance. Control loops tuning, stability study, non-linear simulations considering worst cases, test analysis and model correlation, performance justification.; Acceptance test results verification for the first 100 actuators delivered «Entry into service» qualification and product integration on the A380.Performance justification calculation, specification compliance of the products demonstration, DDP writing (Performance Declaration)September 2003 to March 2005 :Development tests, control loop validation«First Flight» Qualification temperature testsTest results batch processing programmingValidation of non-linear models, correlation with qualification test less than 5%September 2001 to September 2003 :A380 Flight control actuators hydraulic and mechanical design, modeling and simulation of the static and dynamic behavior, control loop design. Matlab graphical user interface development for simulation launch and results processing and visualization. Specification, test and validation of test bench (software and hardware)Airbus A400M and Eurocopter EC120 programsTechnical proposals: sizing of servocontrols, static and dynamic performance analysis In service managementTechnical support to « In service » product teams: Airbus A320, A330/340, AgustaWestland Lynx servococontrols.

Renault: MATLAB/Simulink programs for controllers development and calibration, user training.E.D.F. : Modeling of hydroelectric and thermal plants. DGA, Laboratoire de Recherche en Balistique et Aérodynamique: Programming of a trajectory simulator software.