Activities:• Flight Control System (ATA 27) and Automatic Flight Control System (ATA 22) verification according to the ARP4754A.• Creation and execution of test procedures based on requirements for FCS/AFCS development and certification.• Execution of ground test certification campaigns, including FCS/AFCS MOC4, FAR 25.671d (Dual Engine Flameout), and Failure Propagation.• Support for pilot-in-the-loop tests at the Iron Bird for customer demonstrations, investigation of issues found in the fleet, and system evaluation with certification authorities.• Specification, validation, and verification (V&V) of test bench requirements.• Integration and troubleshooting of different test benches at the Iron Bird, such as primary/secondary flight control systems, avionics, and powerplant rigs.• Execution of test campaigns at suppliers' facilities in the USA.• Development of tools to speed up ground testing, such as an application to automate test execution, a data recorder, and a program to automatically identify unexpected system behaviors.• Awarded six times Embraer's "Top Ideas Prize", resulting in over 2.3 million USD in cost savings.• Engagement in three generations of Embraer's full fly-by-wire programs: Legacy 450/500 (Business Jet), KC-390 (Military Transport Aircraft), and E-Jets E2 (Regional Airliner).Knowledge in:• Automated test development• Integration of test benches from different suppliers• Fly-by-Wire Flight Control Systems• Avionics (Honeywell and Collins)• Flight Management Systems, flight plan, and performance• Autopilot, Autoland (CAT III), Steep Approach, and Autothrottle• Aerodynamics• IBM Rational DOORS• JIRA for issues management• A429, TTP, CAN, AFDX (Collins), ASCB-D (Honeywell) communication protocols• National Instruments data acquisition• Data recording and application of compression methods• GE Fanuc Reflective Memory for test bench integration• Python, C, FORTRAN, MATLAB, Bash, Qt, Tk

• Wind tunnel testing for the "Silent Aircraft", a project of aerodynamics and aeroacoustics led by Embraer to reduce the aircraft external noise. • Detection of noise sources on wings and landing gears using microphone arrays (beamforming).• Wind tunnel model instrumentation, data acquisition, and post-processing.

• Application of the linear stability theory for boundary layer transition prediction in wind tunnel and flight test results.• Engagement in a wind tunnel test at DLR to study the boundary layer transition due to steps on the wing surface.• Evaluation of hybrid laminar flow control systems and comparison of different design tools for the A320 hybrid laminar fin.• Optimization of boundary layer suction systems using genetic algorithms.

• Scholarship from the State of São Paulo Research Foundation (FAPESP) to develop Computational Fluid Dynamic models of rocket nozzles.