| Trajectory refinement of three-body orbits in the real solar system model DA Dei Tos, F Topputo Advances in Space Research 59 (8), 2117-2132, 2017 | 28 | 2017 |
| Orbit design for LUMIO: The lunar meteoroid impacts observer AM Cipriano, DA Dei Tos, F Topputo Frontiers in Astronomy and Space Sciences 5, 29, 2018 | 22 | 2018 |
| LUMIO: an autonomous CubeSat for lunar exploration S Speretta, A Cervone, P Sundaramoorthy, R Noomen, S Mestry, ... Space operations: inspiring Humankind's future, 103-134, 2019 | 15 | 2019 |
| On the advantages of exploiting the hierarchical structure of astrodynamical models DA Dei Tos, F Topputo Acta Astronautica 136, 236-247, 2017 | 14 | 2017 |
| Survey of Mars ballistic capture trajectories using periodic orbits as generating mechanisms DA Dei Tos, RP Russell, F Topputo Journal of Guidance, Control, and Dynamics 41 (6), 1227-1242, 2018 | 10 | 2018 |
| LUMIO: a cubesat at Earth-Moon L2 F Topputo, M Massari, J Biggs, P Di Lizia, D Dei Tos, K Mani, ... 4S Symposium, 1-15, 2018 | 8 | 2018 |
| LUMIO: achieving autonomous operations for Lunar exploration with a CubeSat S Speretta, F Topputo, J Biggs, P Di Lizia, M Massari, K Mani, D Dei Tos, ... 2018 SpaceOps Conference, 2599, 2018 | 8 | 2018 |
| LISA Pathfinder mission extension: A feasibility analysis DA Dei Tos, M Rasotto, F Renk, F Topputo Advances in Space Research 63 (12), 3863-3883, 2019 | 5 | 2019 |
| High-fidelity trajectory optimization with application to saddle-point transfers DA Dei Tos, F Topputo Journal of Guidance, Control, and Dynamics 42 (6), 1343-1352, 2019 | 5 | 2019 |
| Design and feasibility assessment of ultra low thrust trajectories to the Sun-Earth saddle point F Topputo, DA Dei Tos, M Rasotto, F Renk 2018 Space Flight Mechanics Meeting, 1691, 2018 | 5 | 2018 |
| Automated trajectory refinement of three-body orbits in the real solar system model DA Dei Tos, F Topputo 25th AAS/AIAA Space Flight Mechanics Meeting, 263-282, 2015 | 5 | 2015 |
| Trajectory optimization of limited control authority spacecraft in high-fidelity models DA DEI TOS Italy, 2018 | 4 | 2018 |
| Trajectory design in high-fidelity models F Topputo, DA Dei Tos, KV Mani, S Ceccherini, C Giordano, V Franzese, ... 7th International Conference on Astrodynamics Tools and Techniques (ICATT), 1-9, 2018 | 4 | 2018 |
| Lumio: Charazterizing lunar meteoroid impacts with a cubesat F Topputo, M Massari, J Biggs, P Di Lizia, D Dei Tos, K Mani, ... 69th International Astronautical Congress (IAC 2018), 1-11, 2018 | 4 | 2018 |
| System design of LUMIO: A CubeSat at Earth-Moon L2 for observing lunar meteoroid impacts P Sundaramoorthy, F Topputo, M Massari, J Biggs, P Di Lizia, D Dei Tos, ... 69th International Astronautical Congress (IAC 2018), 1-8, 2018 | 4 | 2018 |
| The Sun–Earth saddle point: characterization and opportunities to test general relativity F Topputo, DA Dei Tos, M Rasotto, M Nakamiya Celestial Mechanics and Dynamical Astronomy 130 (4), 1-20, 2018 | 3 | 2018 |
| Design and Validation of Ultra Low Thrust Transfers to the Sun-Earth Saddle Point with Application to LISA PathFinder Mission Extension F Topputo, D Dei Tos, M Rasotto, F Renk 26th International Symposium on Space Flight Dynamics, 3-9, 2017 | 3 | 2017 |
| Operations-driven low-thrust trajectory optimization with applications to DESTINY+ DA Dei Tos, T Yamamoto, N Ozaki, Y Tanaka, F Gonzalez-Franquesa, ... AIAA Scitech 2020 Forum, 2182, 2020 | 2 | 2020 |
| Genetic optimization for the orbit maintenance of libration point orbits with applications to EQUULEUS and LUMIO DA Dei Tos, N Baresi AIAA Scitech 2020 Forum, 0466, 2020 | 2 | 2020 |
| On the advantages of using a strict hierarchy to model astrodynamical problems DA Dei Tos, F Topputo 66th International Astronautical Congress (IAC 2015), 5479-5490, 2015 | 2 | 2015 |
Francesco TopputoAssociate Professor, Politecnico di MilanoVerified email at polimi.it
