Diego Di Leo

Diego Di Leo

Research Assistant - Control Systems Engineer

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location of Diego Di LeoBari, Apulia, Italy

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  • Timeline

  • About me

    Staff Engineer - Controls IPT Leader | Avio Aero - a GE Aerospace Company

  • Education

    • Politecnico di Bari

      2013 - 2015
      Master’s Degree Control Systems Engineering 110/110 (full marks with honors)

      Thesis: "Robust Control of Bistable Dielectric ElectroActive Polymer Actuators via Linear Matrix Inequalities Methods"Main courses:Advanced Control of Dynamics Systems, System Identification and Intelligent Control, Robot Mechanics and Control, Electric Drives for Automation, Programmable Systems, Internet of Things.

    • Politecnico di Bari

      2009 - 2013
      Bachelor’s Degree Control Systems Engineering

      Thesis: "Simulation and Control of the Automotive ABS System"Main courses:Automation and Digital Control, Informatics for Automation, Electrical Machines and Control, Modeling of Dynamic Systems.

  • Experience

    • Saarland University - ZeMA GmbH

      Jun 2014 - Dec 2014
      Research Assistant - Control Systems Engineer

      Control of Dielectric ElectroActive Polymers (DEAP) actuators for micro-positioning;nonlinear and robust control; control system development through MATLAB/Simulink;experimental validation through LabView/FPGA.

    • Avio Aero

      Jul 2015 - Apr 2016
      Control Systems Engineer

      - Advanced TurboProp Project (ATP):propeller control system design and development; propeller pitch actuation system control and test; propeller sensor fault detection.- More Electric Aircraft Project (MEA):modeling and control of hybrid-electric powertrain for UAVs (Unmanned Aerial Vehicles);power management optimization for fuel consumption reduction.

    • Distretto Aerospaziale Pugliese

      Apr 2016 - Sept 2018
      Control Systems Engineer (Consultant)

      Consulting Control Systems Engineer at Avio Aero on ATP project:- Turbine and Propeller control system development in MATLAB/Simulink environment;- Propeller pitch actuation system high-fidelity modeling in Simscape/SimHydraulics environment, requirements definition and dynamics analysis;- Test Rig requirements definition, modeling and control system design for electric motors and hydraulic systems (turbine driving and propeller load actuation system);- Algorithm design.

    • Avio Aero

      Sept 2018 - now

      AMBER technical leader, covering technical and program management across controls, electrical and SW sub-sections. Responsible for controls integration with system and modules, team activities planning, leadership and execution.Main work scope includes, but not limited to:- Serve as Controls primary point of contact with Engine System department- Drive Control System requirements, architecture and interfaces definition- Drive Control System design and hybrid powerplant modeling in simulation environment- Develop, own and ensure execution of the integrated Controls and Accessories design review process- Align Controls activities and deliverables with Program priorities- Manage risks and potential deviations to meet program schedules, developing action plans to anticipate and respond to issues Show less AMBER technical leader, covering technical and program management across controls, electrical and SW sub-sections. Responsible for controls integration with system and modules, team activities planning, leadership and execution.Main work scope includes, but not limited to:- Serve as Controls primary point of contact with Engine System department- Drive Control System requirements, architecture and interfaces definition- Drive Control System design and hybrid powerplant modeling in simulation environment- Develop, own and ensure execution of the integrated Controls and Accessories design review process- Align Controls activities and deliverables with Program priorities- Manage risks and potential deviations to meet program schedules, developing action plans to anticipate and respond to issues Show less EuroDrone Program:- Propeller integration studies- Control System design CFM RISE Program:- FPAS (Fan Pitch Actuation System) design support- PCU (Propeller Control Unit) design and preliminary sizing- PCU & FPAS high-fidelity modeling- Control System design support GE Catalyst Program:- SW test for system requirements validation (SPOCT)- engine flight test support- flight data analysis- tools development (MATLAB & Python)- SW design- team coordination- certification reports writing (CFR Part 33) Show less

      • Staff Engineer - Controls IPT Leader

        Jun 2024 - now
      • Advanced Lead Engineer - Controls Technical Leader

        Sept 2023 - Jun 2024
      • Technical Leader - Controls & Accessories

        Feb 2023 - Sept 2023
      • Control Systems Lead Engineer

        Jul 2021 - Feb 2023
      • Turbomachinery Actuation Systems Designer

        Sept 2018 - Jun 2021
  • Licenses & Certifications

    • Professional Qualification

      Feb 2016