Mauro Pontani | Ricerc@Sapienza

Pubblicazioni

Titolo	Pubblicato in	Anno
Low-thrust transfer to quasi-synchronous Martian elliptic orbit via nonlinear feedback control	AEROSPACE	2023
Low-thrust lunar capture leveraging nonlinear orbit control	THE JOURNAL OF THE ASTRONAUTICAL SCIENCES	2023
Earth-Venus Mission Analysis via Weak Capture and Nonlinear Orbit Control	AEROSPACE	2023
A revisited and general Kane’s formulation applied to very flexible multibody spacecraft	Aeronautics and Astronautics - AIDAA XXVII International Congress	2023
Intersatellite and downlink agile attitude maneuvers	APPLIED SCIENCES	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
Trajectory optimization and multiple-sliding-surface terminal guidance in the lifting atmospheric reentry	Aeronautics and Astronautics – AIDAA XXVII International Congress	2023
Advanced Spacecraft Dynamics		2023
Near-optimal feedback guidance for low-thrust earth orbit transfers	Materials Research Proceedings	2023
Low-energy earth-moon mission analysis using low-thrust optimal and feedback control	Materials Research Proceedings	2023
ATTITUDE CONTROL AND TRA JECTORY PLANNING OF A SPACE MANIPULATOR SYSTEM USING KANE'S FORMULATION	Proceedings of the International Astronautical Congress, IAC	2023
NON-INERTIAL STRUCTURAL EFFECTS IN FLEXIBLE SPACECRAFT WITH SPINNING APPENDAGE	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
Nonlinear slewing control of a large flexible spacecraft using reaction wheels	AEROSPACE	2022
Explicit Near-Optimal Guidance and Pulse-Modulated Control for Lunar Descent and Touchdown	AEROTECNICA MISSILI E SPAZIO	2022
Correction to: Lunar Descent and Landing via Two-Phase Explicit Guidance and Pulse-Modulated Reduced-Attitude Control	AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022	2022
Lunar descent and landing via two-phase explicit guidance and pulse-modulated reduced-attitude control	AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022	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

Progetti di Ricerca

A New Optimization, Guidance, and Control Methodology for Aerospace Vehicles
Nonlinear Control Techniques for Aerospace Vehicles in Challenging Mission Scenarios