PONTANI, MAURO

PONTANI, MAURO  

DIPARTIMENTO DI INGEGNERIA ASTRONAUTICA, ELETTRICA ED ENERGETICA  

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Titolo Data di pubblicazione Autore(i) File
A new guidance and control architecture for accurate orbit injection 2019 Pontani, M; Celani, F
A New Neighboring Optimal Guidance Algorithm for Space Trajectories 2014 Pontani, Mauro; G., Cecchetti; Teofilatto, Paolo
A new, general neighboring optimal guidance for aerospace vehicles 2016 Pontani, Mauro
A revisited and general Kane’s formulation applied to very flexible multibody spacecraft 2023 Madonna, D. P.; Gasbarri, P.; Pontani, M.; Gennari, F.; Scialanga, L.; Marchetti, A.
Accurate modeling and heuristic trajectory optimization of multistage launch vehicles 2017 Palaia, Guido; Pallone, Marco; Pontani, Mauro; Teofilatto, Paolo
Accurate modeling and near optimal ascent trajectory of microsatellite launch vehicles via firework algorithm 2016 Pallone, Marco; Pontani, Mauro; Teofilatto, Paolo
Advanced Spacecraft Dynamics 2023 Pontani, Mauro
An accurate modeling and performance of multistage launch vehicles for microsatellites via a firekwokk algorithm 2017 Pontani, M.; Pallone, M.; Teofilatto, P.
An Earth-Mars microsatellite mission leveraging low-energy capture and low-thrust propulsion 2022 Carletta, Stefano; Pontani, Mauro; Teofilatto, Paolo
An Iterative Guidance and Navigation Algorithm for Orbit Rendezvous of Cooperating CubeSats 2022 Battistini, S.; De Angelis, G.; Pontani, M.; Graziani, F.
Analisi delle traiettorie di fuga realizzabili mediante trasferimento WSB e gravity assist lunare 2005 Pontani, Mauro; Teofilatto, Paolo
Analytic Derivation of Ascent Trajectories and Performance of Launch Vehicles 2022 Teofilatto, Paolo; Carletta, Stefano; Pontani, Mauro
Analytic Derivation of Ascent Trajectories and Performance of Launch Vehicles 2022 Teofilatto, P; Carletta, S; Pontani, M
Ascent trajectories of multistage launch vehicles. Numerical optimization with second-order conditions verification 2014 Pontani, Mauro; G., Cecchetti
Ascent Trajectory Optimization and Neighboring Optimal Guidance of Multistage Launch Vehicles 2019 Palaia, G.; Pallone, M.; Pontani, M.; Teofilatto, P.
Attitude control and tra jectory planning of a space manipulator system using Kane's formulation 2023 Madonna, D. P.; Pontani, M.; Gasbarri, P.
ATTITUDE MANEUVERS OF A FLEXIBLE SPACECRAFT FOR SPACE DEBRIS DETECTION AND COLLISION AVOIDANCE 2022 Madonna, D. P.; Pontani, M.; Gasbarri, P.
Berthing proximity maneuvers and trajectory planning of a space manipulator via Kane’s formulation 2024 Madonna, David Paolo; Pontani, Mauro; Gasbarri, Paolo
Characterization of Low-Energy Quasiperiodic Orbits in the Elliptic Restricted 4-Body Problem with Orbital Resonance 2022 Carletta, Stefano; Pontani, Mauro; Teofilatto, Paolo
Complex orbit dynamics of decommissioned geostationary satellites 2020 Proietti, S.; Flores, R.; Pontani, M.; Fantino, E.