From November 2013 |
EDL/GNC Engineer for Thales Alenia Space Italy |
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Thales Alenia Space, Torino(TO) , Italy |
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▪ Responsible of Guidance Navigation and Control design and analysis for the Entry Descent and Landing Mission phase of the Descent Module for the Exomars 2018 project:
▫ Design of the GNC global architecture in collaboration with Russian Team: ▫ Validation of the GNC algorithms through the End to End Simulator ▫ Implementation and validation of the RCS performance model for the Descent Module ▫ Develop of the GNC On Board Software for what concern main requirement and technical aspect of the system ▪ Support to the reviews of the project (System Requirement Review and System Preliminary Design Review) through the development of GNC technical documentation: ▫ Error Budget ▫ Design Report ▫ Budget Report ▫ Requirement Specification ▫ Software Technical Specification ▪ Support to the Procurement of the GNC Sensor and Actuators of the Descent Module: ▫ Inertial Measurement Unit ▫ Radar Doppler Altimeter ▫ Reaction Control System Participation at the 9th International ESA Conference on Guidance Navigation and Control Systems with the publication of the paper: “Travelling to and Landing on Mars Carrying the ExoMars2018 Rover”
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April 2013-November 2013 |
Internship at Thales Alenia Space Italy |
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Thales Alenia Space, Torino(TO) , Italy |
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▪ Development of control algorithms, in C or Matlab/Simulink environment, for the End-to-End Simulator for the EXOMARS 2018 mission analysis: ▫ Support to System Requirement Review on control algorithms design: ▫ Assessment of parachute deployment algorithms ▫ Definition of powered descent algorithms requirements ▪ Analysis of Entry, Descent and Landing phase of EXOMARS 2018 mission: ▫End-to-End EXOMARS 2016 simulator adaptation to EXOMARS 2018 scenario |
June 2012-December 2012
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Trainee at Italian Aerospace Research Center (CIRA) |
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Italian Aerospace Research Center, Capua(CE) , Italy |
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▪ Development and implementation in Matlab/Simulink environment a simulation model of the Reaction Control System (RCS) installed on-board an Unmanned Space Vehicle (USV) which should perform an atmosphere re-entry mission. ▪ Analysis of the behaviour of RCS characteristics through the simulation model of the control system |
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September 2009-February 2010 |
Trainee at Department of Aerospace Engineering (DIAS) |
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Università degli Studi di Napoli Federico II, Napoli, Italy |
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▪ Design and production of some special components for the laboratory test on amorphous carbon samples ▪ Evaluation of the behaviour of the amorphous carbon in inductors oven at high temperature |
EDUCATION AND TRAINING |
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2010-2012
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Master’s degree in Aerospace and Astronautic Engineer (vote 107/110) |
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Università degli studi di Napoli “Federico II” |
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Thesis: “ Control-Oriented Simulation Model for an Unmanned Space Vehicle: The FTB-X Reaction Control System” |
2006-2010 |
Bachelor’s degree in Aerospace Engineer (vote 103/110) |
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Università degli studi di Napoli Federico II Thesis: “ Caratterizzazione di emissività del carbonio amorfo ad alte Temperature” |
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2001-2006 |
Scientific High school degree (vote 97/100) Liceo Scientifico Statale “F. Silvestri
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PERSONAL SKILLS |
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Mother tongue(s) |
Italian |
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Other language(s) |
English |
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Communication skills |
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Organisational / managerial skills |
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Job-related skills |
▪ ▪ Good command of issues concerning control system for spatial vehicle that should perform an atmospheric re-entry mission and a Martian Entry Descent and Landing mission. ▪ Well Understanding of ESA Normative (ECSS) ▪ Good Knowledge in: § Attitude and control dynamic of spatial vehicle § Simulation Model of RCS and of USV control system § Behaviour of Hydrazine thrusters § Aerodynamic Analysis of a rotor’s performance § Hypersonic regime characterization and application § Aerodynamics of an airfoil, Aerodynamics of a light aircraft, numerical Analysis § Guidance, Navigation and Control for Space Vehicle § Accelerometers and Gyroscope § Radar Doppler Altimeter § Kalman Filter |
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Computer skills |
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Other skills |
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Driving licence |
Automotive cat.B |
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