FADEC integration and FAR 33 turbine engine control system certification experience on Eclipse 500, Cessna Citation Mustang, Embraer Phenom 100, Cessna Citation Encore+, Cessna Citation XLS+, Embraer Phenom 300, Changhe Z-8F, Eurocopter EC175, Sikorsky S-76D, Agusta Westland AW169.Post-certification improvements and obsolescence management on engine control systems for Agusta Westland AW139, Bombardier Q400, T-6A Texan II, Pilatus PC-21, Embraer EMB-314 Super Tucano, Dassault F7X, Eurocopter EC135, Kazan Ansat, Bell M427 & M429, Airbus A380 APU.System Safety Assessment, Fault Tree Analysis and Functional Hazard Assessment of turbine engine control systems and powerplant integration for Sikorsky S-76D, Eurocopter EC175, Eurocopter X4. Advanced engineering activities defining next generation engine control architecture and characteristics for fixed wing and rotorcraft applications.Development of turbine engine control closed-loop test benches including installation conformity assurance, HIRF and lightning transient hardening for DO-160 certification testing.SAE AE-2 committee work including RTCA/DO-160 revision G section 22 user guide.Lightning transient protection design to 15kA cable and B4 pin, HIRF to Environment III (tested to RTCA/DO-160), RF emissions reduction to 20 dBuV/m.Mixed signal, analog and power electronics design for turbine engine control, data acquisition, supervisory and safety systems for mobile power generation, embedded instrumentation applications, intrinsic safety and electromagnetic compatibility.Linear system and adaptive control design in continuous, discrete and mixed systems.Fully bilingual including technical writing in both French and English.