Mauro Pontani

Pubblicazioni

Titolo Pubblicato in Anno
Variable-time-domain neighboring optimal guidance and attitude control for low-thrust orbit transfers Space Flight Mechanics Meeting, 2018 2018
Lunar Ascent and Orbit Injection via Neighboring Optimal Guidance and Constrained Attitude Control JOURNAL OF AEROSPACE ENGINEERING 2018
Long-term capture orbits for low-energy space missions CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY 2018
Dynamics of capture orbits from libration region analysis 69th International Astronautical Congress (IAC), Bremen, Germany, 1-5 October 2018 2018
Performance evaluation methodology for multistage launch vehicles with high-fidelity modeling ACTA ASTRONAUTICA 2018
LUNISAT ORBIT MAINTENANCE AND LOW-THRUST MANEUVERS Advances in the Astronautical Sciences Volume 163, 2018, Pages 729-746 2018
Lunar orbit dynamics and maneuvers for Lunisat missions ACTA ASTRONAUTICA 2018
LUNISAT ORBIT MAINTENANCE AND LOW-THRUST MANEUVERS Advances in the Astronautical Sciences 4th IAA Dynamics and Control of Space Systems Conference, Volume 163 2018
Invariant manifold connections via polyhedral representation ACTA ASTRONAUTICA 2017
Particle swarm optimization of cooperative and competitive relative orbit maneuvers Particle Swarm Optimization (PSO): Advances in Research and Applications 2017
Long-term capture orbits for low-energy space missions Abstracts CELMEC VII 2017
Neighboring optimal guidance and attitude control for lunar ascent and orbit injection Third IAA Conference on Dynamics and Control of Space Systems 2017, DyCoSS'2017 M 2017
New implicit neighboring optimal guidance and attitude control for three-dimensional lunar ascent Proceedings of the 68th International Astronautical Congress 2017
Accurate modeling and heuristic trajectory optimization of multistage launch vehicles Advances in the Astronautical Sciences 2017
An accurate modeling and performance of multistage launch vehicles for microsatellites via a firekwokk algorithm Advances in Mathematics Research 2017
LUNISAT: A microsatellite mission to the moon Advances in the Astronautical Sciences 2017
Optimal low-thrust hyperbolic rendezvous for interplanetary missions Proceedings of the International Astronautical Congress, IAC 2017
Earth-Moon transfer trajectory for the Lunisat microsat Proceedings of the International Astronautical Congress, IAC 2017
Lunar orbit dynamics for Lunisat missions Proceedings of the International Astronautical Congress, IAC 2017
Reconfigurable S-band patch antenna system for cubesat satellites IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE 2016

© Università degli Studi di Roma "La Sapienza" - Piazzale Aldo Moro 5, 00185 Roma