Research activity and Master Thesis in Space Flight Dynamics, Flexible Structures Attitude Control and Optimization Methods.
Applied attitude control on flexible structures, integrating attitude motion dynamics with low order finite element structural models. Developed a software simulator based on the derived equations and interfaced with a custom implementation of different Evolutionary Algorithms (GA, PSO) used to study optimal actuator placement.
Grade: 110/110 Cum Laude
Master thesis in Space Flight Dynamics: applied perturbative mathematical techniques on Gauss’ variational equations for both classical and equinoctial parameters. Obtained a semi analytical solution requiring only a few simple integrals that can be solved via numerical quadrature. Implemented the derived equations in a software simulator to be used for fast preliminary solution of multi-objective optimization in the context of complex, multi-phase, interplanetary orbital transfers.
Work later published in Acta Astronautica, Journal of Guidance, Control, and Dynamics, and Advances in the Astronautical Sciences journals (see publications).
Grade: 110/110 Cum Laude
Master thesis in Space Flight Dynamics: applied perturbative mathematical techniques on Gauss’ variational equations for both classical and equinoctial parameters. Obtained a semi analytical solution requiring only a few simple integrals that can be solved via numerical quadrature. Implemented the derived equations in a software simulator to be used for fast preliminary solution of multi-objective optimization in the context of complex, multi-phase, interplanetary orbital transfers.
Work later published in Acta Astronautica, Journal of Guidance, Control, and Dynamics, and Advances in the Astronautical Sciences journals (see publications).
Additional master degree received with the Alta Scuola Politecnica program.
Grade: 110/110 Cum Laude
Thesis in Space Flight Dynamics: developed a software simulator for orbital transfer maneuvers used to compute the Pareto front in Lambert’s Problem context, using a novel parametrization function of transfer orbit eccentricity.