Paolo Teofilatto | Ricerc@Sapienza

Pubblicazioni

Titolo	Pubblicato in	Anno
Large-Eddy Simulations of a Hypersonic Re-entry Capsule Coupled With the Supersonic Disk-Gap-Band Parachute	AEROSPACE	2024
Low-Thrust Nonlinear Orbit Control for Very Low Lunar Orbits	APPLIED SCIENCES	2024
Stereographic projection and static digraph for information routing in satellite constellations	IAC 2024 congress proceedings, 75th International Astronautical Congress (IAC), Milan, Italy	2024
Diversity Architecture for Robust GNSS/INS Navigation in Launcher Applications	Proceedings of the European Navigation Conference 2024	2024
A new indirect measurement method of the electron temperature for the Proto-sphera's pinch plasma	JOURNAL OF INSTRUMENTATION	2023
Near-Optimal Guidance and Pulse-Modulated Reduced-Attitude Control for Orbit Injection	Modeling and Optimization in Space Engineering	2023
Earth-Venus Mission Analysis via Weak Capture and Nonlinear Orbit Control	AEROSPACE	2023
Large constellations for fast acquisition and delivery of information. Design and analysis by stereographic projection onto the equatorial plane	INTERNATIONAL JOURNAL OF SATELLITE COMMUNICATIONS AND NETWORKING	2023
Lunar formation flying invariant under zonal harmonic perturbations	Proceedings of the International Astronautical Congress, IAC	2023
Characterization of Low-Energy Quasiperiodic Orbits in the Elliptic Restricted 4-Body Problem with Orbital Resonance	AEROSPACE	2022
Analytic Derivation of Ascent Trajectories and Performance of Launch Vehicles	APPLIED SCIENCES	2022
An Earth-Mars microsatellite mission leveraging low-energy capture and low-thrust propulsion	ACTA ASTRONAUTICA	2022
Stable configurations for bounded satellite formation flying in the presence of gravitational perturbations	Proceedings of the 11th International Workshop on Satellite Constellations & Formation Flying	2022
An optimal aerodynamic-driven rocket landing strategy	Proceedings of the 73rd International Astronautical Congress	2022
Design and experimental testing of a microlaunchers eject system operated from naval platform	Proceedings of the 73rd International Astronautical Congress	2022
Mars Constellation Design and Low-Thrust Deployment Using Nonlinear Orbit Control	THE JOURNAL OF THE ASTRONAUTICAL SCIENCES	2022
Deployment strategies of a satellite constellation for polar ice monitoring	ACTA ASTRONAUTICA	2022
Deployment of a Microsatellite Constellation around the Moon using Chaotic Multi body dynamics	Proceedings of the 72nd International Astronautical Congress	2021
Earth-Mars microsatellite mission using ballistic capture and low-thrust propulsion	Proceedings of the 72nd International Astronautical Congress	2021
A magnetometer-only attitude determination strategy for small satellites: design of the algorithm and hardware-in-the-loop testing	AEROSPACE	2020