UNIVERSITY PROJECTS
Spacecraft orbital transfers characterization
This project aims to: characterize a given initial orbit, characterize a given final orbit, described by classical Keplerian parameters, identify the best orbital transfer.
Design of a model-rocket with TVC system
This project aims to: characterize and optimize the model rocket components, solve a make or by problem, design the TVC system and study the internal combustion of the engine.
Interplanetary and Planetary Mision Analisys
This project aims to characterize the interplanetary trajectory for an explorer mission and to characterize the orbit for a Earth observation mission.
Attitude Dynamics and Control for a 6U CubeSat
This report aims to model the attitude and control system of a 6U CubeSat; the simulations have been carried out inside the Matlab&Simulink environment.
POLISPACE PROJECTS
Experimental Payload V0
The experimental payload EPv0 is a project of the italian company Sidereus Space Dynamics developed, designed and built with the contribution of PoliSpace. EPv0 aims to characterize through measurements the payload bay of Sidereus’ launcher EOS.
My role inside the team is to help in the design process and in the 3D printing of the components.
SKILLS
Matlab / Simulink
2+ Years
Spice Matlab
1 Year
GMAT
2+ Years
LaTeX
1 Year
Autodesk Inventor
3+ Years
Autodesk Fusion
2+ Years
SolidWorks
3+ Years
SolidEdge
3+ Years
C Language
3+ Years
Arduino
1+ Year
WordPress - Elementor
2+ Years
Cura - 3D Printing
1+ Year