activity
20192021
most citedA Time-Dependent TSP Formulation for the Design of an Active Debris Removal Mission using Simulated Annealing

9 citations · 32 across the 8 of their papers we have counts for

collaborators

9 papers

astro-ph.EP20213 cited

Analysis of 3GM Callisto Gravity Experiment of the JUICE Mission

Mauro Di Benedetto, Paolo Cappuccio, Serena Molli +2

The ESA's JUICE mission will provide a thorough investigation of the Jupiter system and the Galilean moons during its nominal tour, comprising flybys of Europa and Callisto, and an…

math.OC20202 cited

Convex Optimization of Launch Vehicle Ascent Trajectory with Heat-Flux and Splash-Down Constraints

Boris Benedikter, Alessandro Zavoli, Guido Colasurdo +2

This paper presents a convex programming approach to the optimization of a multistage launch vehicle ascent trajectory, from the liftoff to the payload injection into the target or…

cs.LG20206 cited

Reinforcement Learning for Low-Thrust Trajectory Design of Interplanetary Missions

Alessandro Zavoli, Lorenzo Federici

This paper investigates the use of Reinforcement Learning for the robust design of low-thrust interplanetary trajectories in presence of severe disturbances, modeled alternatively…

cs.NE2020

EOS: a Parallel, Self-Adaptive, Multi-Population Evolutionary Algorithm for Constrained Global Optimization

Lorenzo Federici, Boris Benedikter, Alessandro Zavoli

This paper presents the main characteristics of the evolutionary optimization code named EOS, Evolutionary Optimization at Sapienza, and its successful application to challenging,…

math.OC20195 cited

Convex Optimization of Linear Impulsive Rendezvous

Boris Benedikter, Alessandro Zavoli

This note aims at providing a concise and self-contained document that describes a clear and easy-to-understand method, that could be useful for a reader that is approaching the li…

math.OC20197 cited

Integrated Optimization of Ascent Trajectory and SRM Design of Multistage Launch Vehicles

Lorenzo Federici, Alessandro Zavoli, Guido Colasurdo +2

This paper presents a methodology for the concurrent first-stage preliminary design and ascent trajectory optimization, with application to a Vega-derived Light Launch Vehicle. The…