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
51 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
32 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
12 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 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 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
8 2015 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