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Alessandro Zavoli
Alessandro Zavoli
Research Assistant, Sapienza Università di Roma
在 uniroma1.it 的电子邮件经过验证 - 首页
标题
引用次数
引用次数
年份
Reinforcement learning for robust trajectory design of interplanetary missions
A Zavoli, L Federici
Journal of Guidance, Control, and Dynamics 44 (8), 1440-1453, 2021
782021
Deep learning techniques for autonomous spacecraft guidance during proximity operations
L Federici, B Benedikter, A Zavoli
Journal of Spacecraft and Rockets 58 (6), 1774-1785, 2021
772021
Convex approach to three-dimensional launch vehicle ascent trajectory optimization
B Benedikter, A Zavoli, G Colasurdo, S Pizzurro, E Cavallini
Journal of Guidance, Control, and Dynamics 44 (6), 1116-1131, 2021
502021
Tour of Jupiter Galilean moons: Winning solution of GTOC6
G Colasurdo, A Zavoli, A Longo, L Casalino, F Simeoni
Acta Astronautica 102, 190-199, 2014
502014
EOS: a parallel, self-adaptive, multi-population evolutionary algorithm for constrained global optimization
L Federici, B Benedikter, A Zavoli
2020 IEEE Congress on Evolutionary Computation (CEC), 1-10, 2020
322020
Convex optimization of launch vehicle ascent trajectory with heat-flux and splash-down constraints
B Benedikter, A Zavoli, G Colasurdo, S Pizzurro, E Cavallini
Journal of Spacecraft and Rockets 59 (3), 900-915, 2022
282022
A convex approach to rocket ascent trajectory optimization
B Benedikter, A Zavoli, G Colasurdo
8th European Conference for Aeronautics and Space Sciences (EUCASS), 1-15, 2019
262019
Spacecraft dynamics under the action of Y-dot magnetic control law
A Zavoli, F Giulietti, G Avanzini, G De Matteis
Acta Astronautica 122, 146-158, 2016
262016
Convex approach to covariance control with application to stochastic low-thrust trajectory optimization
B Benedikter, A Zavoli, Z Wang, S Pizzurro, E Cavallini
Journal of Guidance, Control, and Dynamics 45 (11), 2061-2075, 2022
242022
A time-dependent TSP formulation for the design of an active debris removal mission using simulated annealing
L Federici, A Zavoli, G Colasurdo
arXiv preprint arXiv:1909.10427, 2019
242019
Evolutionary optimization of multirendezvous impulsive trajectories
L Federici, A Zavoli, G Colasurdo
International Journal of Aerospace Engineering 2021 (1), 9921555, 2021
232021
Autonomous upper stage guidance using convex optimization and model predictive control
B Benedikter, A Zavoli, G Colasurdo, S Pizzurro, E Cavallini
ASCEND 2020, 4268, 2020
222020
Autonomous guidance for cislunar orbit transfers via reinforcement learning
L Federici, A Scorsoglio, A Zavoli, R Furfaro
AAS/AIAA Astrodynamics Specialist Conference, 2021
212021
A convex optimization approach for finite-thrust time-constrained cooperative rendezvous
B Benedikter, A Zavoli, G Colasurdo
arXiv preprint arXiv:1909.09443, 2019
212019
Single-axis pointing of an underactuated spacecraft equipped with two reaction wheels
A Zavoli, G De Matteis, F Giulietti, G Avanzini
Journal of Guidance, Control, and Dynamics 40 (6), 1465-1471, 2017
202017
Indirect optimization of satellite deployment into a highly elliptic orbit
F Simeoni, L Casalino, A Zavoli, G Colasurdo
International Journal of Aerospace Engineering 2012 (1), 152683, 2012
202012
Meta-reinforcement learning for adaptive spacecraft guidance during finite-thrust rendezvous missions
L Federici, A Scorsoglio, A Zavoli, R Furfaro
Acta Astronautica 201, 129-141, 2022
182022
Preliminary capture trajectory design for europa tomography probe
L Federici, A Zavoli, G Colasurdo
International Journal of Aerospace Engineering 2018 (1), 6890173, 2018
182018
Image-based meta-reinforcement learning for autonomous guidance of an asteroid impactor
L Federici, A Scorsoglio, L Ghilardi, A D’Ambrosio, B Benedikter, A Zavoli, ...
Journal of Guidance, Control, and Dynamics 45 (11), 2013-2028, 2022
172022
Covariance control for stochastic low-thrust trajectory optimization
B Benedikter, A Zavoli, Z Wang, S Pizzurro, E Cavallini
AIAA SCITECH 2022 Forum, 2474, 2022
162022
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