activity
20192026
most citedA Time-Dependent TSP Formulation for the Design of an Active Debris Removal Mission using Simulated Annealing

9 citations · 44 across the 11 of their papers we have counts for

collaborators

12 papers

eess.SY2026

Concept and Rationale for Stratospheric Balloon-Based Laser Debris Removal

F. Ruiz Vincueria, M. Divoky, E. Sanchez-Laulhe +9

Laser-based deorbiting has long been proposed as a promising technique for mitigating the growing population of orbital debris, particularly decimetre-scale objects -- large enough…

math.OC2022★ 2 cited

Autonomous Upper Stage Guidance with Robust Splash-Down Constraint

Boris Benedikter, Alessandro Zavoli, Guido Colasurdo +2

This paper presents a novel algorithm, based on model predictive control (MPC), for the optimal guidance of a launch vehicle upper stage. The proposed strategy not only maximizes t…

math.OC2022★ 2 cited

Stochastic Control of Launch Vehicle Upper Stage with Minimum-Variance Splash-Down

Boris Benedikter, Alessandro Zavoli, Guido Colasurdo +2

This paper presents a novel synthesis method for designing an optimal and robust guidance law for a non-throttleable upper stage of a launch vehicle, using a convex approach. In th…

astro-ph.EP2021★ 3 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.OC2020★ 2 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.LG2020★ 6 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.OC2019★ 5 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.OC2019★ 7 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…

math.OC2019

GTOC X: Solution Approach of Team Sapienza-PoliTo

Alessandro Zavoli, Lorenzo Federici, Boris Benedikter +2

This paper summarizes the solution approach and the numerical methods developed by the joint team Sapienza University of Rome and Politecnico di Torino (Team Sapienza-PoliTo) in th…

math.OC2019★ 9 cited

A Time-Dependent TSP Formulation for the Design of an Active Debris Removal Mission using Simulated Annealing

Lorenzo Federici, Alessandro Zavoli, Guido Colasurdo

This paper proposes a formulation of the Active Debris Removal (ADR) Mission Design problem as a modified Time-Dependent Traveling Salesman Problem (TDTSP). The TDTSP is a well-kno…

math.OC2019★ 8 cited

A Convex Optimization Approach for Finite-Thrust Time-Constrained Cooperative Rendezvous

Boris Benedikter, Alessandro Zavoli, Guido Colasurdo

This paper presents a convex approach to the optimization of a cooperative rendezvous, that is, the problem of two distant spacecraft that simultaneously operate to get closer. Con…