Pubblicazioni

Correction to: Lunar Descent and Landing via Two-Phase Explicit Guidance and Pulse-Modulated Reduced-Attitude Control

2022 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Pontani, M.; Celani, F.; Carletta, S.

An fpga-based risc-v computer architecture orbital laboratory on a pocketqube satellite

2020 - Advances in the Astronautical Sciences
Blasi, L.; Vigli, F.; Farissi, S. M.; Mastrandrea, A.; Menichelli, F.; Nascetti, A.; Olivieri, M.

New implicit neighboring optimal guidance and attitude control for three-dimensional lunar ascent

2017 - Proceedings of the 68th International Astronautical Congress
Pontani, Mauro; Celani, Fabio

Semi-analytical orbital parameters description for thermal fatigue analysis

2016 - AEROTECNICA MISSILI E SPAZIO
Gasbarri, Paolo; Monti, Riccardo

Artificial Equilibrium Orbital Configurations by Means of Continuous Thrust

2016 - AEROTECNICA MISSILI E SPAZIO
Sabatini, M.; Sgubini, S.; Palmerini, G. B.

Minimum-Fuel Finite-Thrust Relative Orbit Maneuvers via Indirect Heuristic Method

2015 - JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
Pontani, Mauro; B. A., Conway

A low cost thrust stand for testing of nano-satellite propulsion systems

2015 - Proceedings of the International astronautical congress, IAC
Bellini, Quirino; ARENA, LORENZO

Thermal and mechanical design and test campaign results of a single-piece structure for the URSA MAIOR nanosatellite

2015 - Proceedings of the International astronautical congress, IAC
Arena, Lorenzo; Angeletti, Federica; Curianò, Federico; De Zanet, Gianluca; Gradini, Raffaele; Pelligrino, Alice

Invariant manifold dynamics VIA polyhedral representation

2015 - Proceedings of the International astronautical congress, IAC
Pontani, Mauro; Teofilatto, Paolo

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