Lorenzo Federici

Lorenzo Federici

orcid

Research Focus & Metrics

Academic Career Length

9Years (2018-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

View All Publications
1 August 2021 in Journal of Guidance, Control, and Dynamics
Verified
Journal Article
Closed access
Alessandro ZavoliAlessandro Zavoli
Alessandro Zavoli
LFLorenzo Federici
Lorenzo Federici
This paper investigates the use of reinforcement learning for the robust design of low-thrust interplanetary trajectories in presence of severe uncertainties and disturbances, alternately modeled a...

1 November 2021 in Journal of Spacecraft and Rockets
Verified
Journal Article
Closed access
LFLorenzo Federici
Lorenzo Federici
BBBoris Benedikter
Boris Benedikter
Alessandro ZavoliAlessandro Zavoli
Alessandro Zavoli
This paper investigates the use of deep learning techniques for real-time optimal spacecraft guidance during terminal rendezvous maneuvers, in presence of both operational constraints and stochasti...

2 September 2022 in Acta Astronautica
Verified
Journal Article
Closed access
LFLorenzo Federici
Lorenzo Federici
ASAndrea Scorsoglio
Andrea Scorsoglio
Alessandro ZavoliAlessandro Zavoli
Alessandro Zavoli
RFRoberto Furfaro
Roberto Furfaro

1 November 2022 in Journal of Guidance, Control, and Dynamics
Verified
Journal Article
Closed access
LFLorenzo Federici
Lorenzo Federici
ASAndrea Scorsoglio
Andrea Scorsoglio
LGLuca Ghilardi
Luca Ghilardi
ADAndrea D'Ambrosio
Andrea D'Ambrosio
BBBoris Benedikter
Boris Benedikter
RFRoberto Furfaro
Roberto Furfaro
This paper focuses on the use of meta-reinforcement learning for the autonomous guidance of a spacecraft during the terminal phase of an impact mission toward a binary asteroid system. The control ...

1 May 2021 in Journal of Spacecraft and Rockets
Verified
Journal Article
Closed access
LFLorenzo Federici
Lorenzo Federici
Alessandro ZavoliAlessandro Zavoli
Alessandro Zavoli
GCGuido Colasurdo
Guido Colasurdo
LMLucandrea Mancini
Lucandrea Mancini
ANAgostino Neri
Agostino Neri
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 reuse as first s...