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 | 52 | 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 | 49 | 2018 |
Mission design of DESTINY+: Toward active asteroid (3200) Phaethon and multiple small bodies N Ozaki, T Yamamoto, F Gonzalez-Franquesa, R Gutierrez-Ramon, ... Acta Astronautica 196, 42-56, 2022 | 33 | 2022 |
Trajectory design and maintenance of the Martian moons eXploration mission around Phobos N Baresi, DA Dei Tos, H Ikeda, Y Kawakatsu Journal of Guidance, Control, and Dynamics 44 (5), 996-1007, 2021 | 31 | 2021 |
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 | 27 | 2019 |
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 | 26 | 2018 |
On the advantages of exploiting the hierarchical structure of astrodynamical models DA Dei Tos, F Topputo Acta Astronautica 136, 236-247, 2017 | 26 | 2017 |
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 | 24 | 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 | 22 | 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 | 22 | 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 | 19 | 2019 |
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 | 15 | 2020 |
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 | 13 | 2019 |
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, ... INTERNATIONAL ASTRONAUTICAL CONGRESS: IAC PROCEEDINGS, 1-8, 2018 | 11 | 2018 |
Trajectory optimization of limited control authority spacecraft in high-fidelity models DA DEI TOS Politecnico di Milano, 2018 | 9 | 2018 |
Automated trajectory refinement of three-body orbits in the real solar system model DA DEI TOS, F Topputo Advances in the Astronautical Sciences, 263-282, 2015 | 9 | 2015 |
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 | 8 | 2020 |
The New Trajectory Design of EQUULEUS N Baresi, T Chikazawa, DA Dei Tos, S Campagnola, Y Kawabata, ... International Symposium on Space Technology and Science (ISTS), Fukui, Japan …, 2019 | 6 | 2019 |
LUMIO: Characterizing lunar meteoroid impacts with a CubeSat F Topputo, A Cervone, P Sundaramoorthy, S Speretta, S Mestry, ... 69th International Astronautical Congress, IAC-18, A3, 2A, 7, x47249, 2018 | 6 | 2018 |
Multiple-Target Low-Thrust Interplanetary Trajectory of O Çelik, DA Dei Tos, T Yamamoto, N Ozaki, Y Kawakatsu, CH Yam Journal of Spacecraft and Rockets 58 (3), 830-847, 2021 | 5 | 2021 |