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alessandro.zavoli@uniroma1.it
Alessandro Zavoli
Ricercatore
Struttura:
DIPARTIMENTO DI INGEGNERIA MECCANICA E AEROSPAZIALE
E-mail:
alessandro.zavoli@uniroma1.it
Pagina istituzionale corsi di laurea
Curriculum Sapienza
Pubblicazioni
Titolo
Pubblicato in
Anno
Single axis pointing for underactuated spacecraft with a residual angular momentum
AEROSPACE SCIENCE AND TECHNOLOGY
2022
Chance-constraint optimization of interplanetary trajectories with a hybrid multiple-shooting approach
AAS/AIAA Astrodynamics Conference
2022
Surrogate neural network for rapid flight performance evaluation of hybrid rocket engines
JOURNAL OF SPACECRAFT AND ROCKETS
2022
Estimation of aerodynamic angles and wind components for a launch vehicle
AAS/AIAA Astrodynamics Conference
2022
Convex Approach to Covariance Control with Application to Stochastic Low-Thrust Trajectory Optimization
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
2022
Meta-reinforcement learning for adaptive spacecraft guidance during finite-thrust rendezvous missions
ACTA ASTRONAUTICA
2022
Image-Based Meta-Reinforcement Learning for Autonomous Guidance of an Asteroid Impactor
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
2022
Robust Design of Interplanetary Trajectories under Severe Uncertainty via Meta-Reinforcement Learning
Proceedings of the International Astronautical Congress, IAC
2022
Optimization of chaser trajectory for active debris removal missions
Proceedings of the International Astronautical Congress, IAC
2022
Optimal tuning for robust control of a small fixed-wing UAV
AIAA Scitech 2021 Forum
2021
Machine learning techniques for autonomous spacecraft guidance during proximity operation
AIAA Scitech 2021 Forum
2021
Advanced Hinf Synthesis for Launch Vehicle Attitude Control in Atmospheric Flight
AIAA Scitech 2021 Forum
2021
Reinforcement learning for robust trajectory design of interplanetary missions
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
2021
On the use of A* search for active debris removal mission planning
JOURNAL OF SPACE SAFETY ENGINEERING
2021
Genetic algorithm based parameter tuning for robust control of launch vehicle in atmospheric flight
IEEE ACCESS
2021
Evolutionary optimization of multirendezvous impulsive trajectories
INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING
2021
Convex Approach to Three-Dimensional Launch Vehicle Ascent Trajectory Optimization
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
2021
Integrated optimization of first-stage SRM and ascent trajectory of multistage launch vehicles
JOURNAL OF SPACECRAFT AND ROCKETS
2021
Autonomous Upper Stage Guidance with Robust Splash-Down Constraint
72nd International Astronautical Congress
2021
Tracking filter integration in the adaptive augmenting controller of a launch vehicle
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
2021
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