| A magnetometer-only attitude determination strategy for small satellites: Design of the algorithm and hardware-in-the-loop testing S Carletta, P Teofilatto, MS Farissi Aerospace 7 (1), 3, 2020 | 30 | 2020 |
| Implementation and hardware-in-the-loop simulation of a magnetic detumbling and pointing control based on three-axis magnetometer data MS Farissi, S Carletta, A Nascetti, P Teofilatto Aerospace 6 (12), 133, 2019 | 24 | 2019 |
| Design and Numerical Validation of an Algorithm for the Detumbling and Angular Rate Determination of a CubeSat Using Only Three‐Axis Magnetometer Data S Carletta, P Teofilatto International Journal of Aerospace Engineering 2018 (1), 9768475, 2018 | 23 | 2018 |
| Long-term capture orbits for low-energy space missions S Carletta, M Pontani, P Teofilatto Celestial Mechanics and Dynamical Astronomy 130 (7), 46, 2018 | 12 | 2018 |
| Dynamics of three-dimensional capture orbits from libration region analysis S Carletta, M Pontani, P Teofilatto Acta Astronautica 165, 331-343, 2019 | 11 | 2019 |
| Design of low-energy capture trajectories in the elliptic restricted four-body problem S Carletta, M Pontani, P Teofilatto International Astronautical Congress, IAC, 2019, 0 | 10* | |
| A low-cost earth-moon-mars mission using a microsatellite platform F Graziani, N Sparvieri, C Stefano International Astronautical Congress, IAC, 2020, 0 | 10* | |
| Characterization of Low-Energy Quasiperiodic Orbits in the Elliptic Restricted 4-Body Problem with Orbital Resonance S Carletta, M Pontani, P Teofilatto Aerospace 9 (4), 175, 2022 | 8 | 2022 |
| Design of fuel-saving lunar captures using finite thrust and gravity-braking S Carletta Acta Astronautica 181, 190-200, 2021 | 8 | 2021 |
| Station-keeping about sun-mars three-dimensional quasi-periodic collinear libration point trajectories S Carletta, M Pontani, P Teofilatto Advances in the Astronautical Sciences 173 (227), 299-311, 0 | 8* | |
| Analytic derivation of ascent trajectories and performance of launch vehicles P Teofilatto, S Carletta, M Pontani Applied Sciences 12 (11), 5685, 2022 | 6 | 2022 |
| Deployment of a microsatellite constellation around the Moon using chaotic multi body dynamics KF Hussain, KF Hussain, S Carletta, P Teofilatto Proceedings of the 72nd International Astronautical Congress, 1-8, 2021 | 6 | 2021 |
| Astrobio cubesat: Enabling technologies for astrobiology research in space L Iannascoli, A Nascetti, S Carletta, L Schirone, A Meneghin, JR Brucato, ... Proceedings of the 71st International Astronautical Congress 2020, 1-5, 2020 | 5 | 2020 |
| An Earth-Mars microsatellite mission leveraging low-energy capture and low-thrust propulsion S Carletta, M Pontani, P Teofilatto Acta Astronautica 200, 635-646, 2022 | 4 | 2022 |
| Dynamics of capture orbits from libration region analysis S Carletta, M Pontani, P Teofilatto 69th International Astronautical Congress (IAC), Bremen, Germany, 1-5 …, 2018 | 4 | 2018 |
| Lunar descent and landing via two-phase explicit guidance and pulse-modulated reduced-attitude control M Pontani, F Celani, S Carletta Acta Astronautica 212, 672-685, 2023 | 3 | 2023 |
| A single-launch deployment strategy for lunar constellations S Carletta Applied Sciences 13 (8), 5104, 2023 | 3 | 2023 |
| Characterization and Testing of the Passive Magnetic Attitude Control System for the 3U AstroBio CubeSat S Carletta, A Nascetti, SS Gosikere Matadha, L Iannascoli, ... Aerospace 9 (11), 723, 2022 | 3 | 2022 |
| Design and hardware-in-the-loop test of an active magnetic detumbling and pointing control based only on three-axis magnetometer data MS Farissi, S Carletta, A Nascetti Proceedings of the 70th International astronautical confress, 1-10, 2019 | 3 | 2019 |
| Explicit near-optimal guidance and pulse-modulated control for lunar descent and touchdown M Pontani, F Celani, S Carletta Aerotecnica Missili & Spazio 101 (4), 361-370, 2022 | 2 | 2022 |
