Mauro Pontani

Pubblicazioni

Titolo Pubblicato in Anno
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
Mars Constellation Design and Low-Thrust Deployment Using Nonlinear Orbit Control THE JOURNAL OF THE ASTRONAUTICAL SCIENCES 2022
New guidance and control techniques for lunar ascent and orbit injection AIP Conference Proceedings 2022
Optimal low-thrust lunar orbit transfers with shadowing effect using a multiple-arc formulation ACTA ASTRONAUTICA 2022
An Iterative Guidance and Navigation Algorithm for Orbit Rendezvous of Cooperating CubeSats APPLIED SCIENCES 2022
Deployment strategies of a satellite constellation for polar ice monitoring ACTA ASTRONAUTICA 2022
Lunar ascent and orbit injection via locally-flat near-optimal guidance and nonlinear reduced-attitude control ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE 2022
Low-Thrust Lunar Capture Leveraging Nonlinear Orbit Control AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 2022
ATTITUDE MANEUVERS OF A FLEXIBLE SPACECRAFT FOR SPACE DEBRIS DETECTION AND COLLISION AVOIDANCE Proceedings of the International Astronautical Congress, IAC Volume 2022 -September 2022 2022
Nonlinear Earth orbit control using low-thrust propulsion ACTA ASTRONAUTICA 2021
Optimal space trajectories with multiple coast arcs using modified equinoctial elements JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS 2021
Long-term orbit dynamics of decommissioned geostationary satellites ACTA ASTRONAUTICA 2021
Earth-Mars microsatellite mission using ballistic capture and low-thrust propulsion Proceedings of the 72nd International Astronautical Congress 2021
Explicit near-optimal guidance and pulse-modulated control for lunar descent and touchdown Proceedings of the XXVI AIDAA International Congress 2021
Discrete-variable-thrust guidance for orbital rendezvous based on feedback linearization Proceedings of the XXVI AIDAA International Congress 2021
Low-thrust orbit dynamics and periodic trajectories in the Earth-Moon system Proceedings of the XXVI AIDAA International Congress 2021
Neighboring optimal guidance and constrained attitude control for accurate orbit injection AEROTECNICA MISSILI E SPAZIO 2021

Progetti di Ricerca

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