Diogene Alessandro Dei Tos
Diogene Alessandro Dei Tos
Verified email at ac.jaxa.jp
Title
Cited by
Cited by
Year
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
282017
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
222018
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
152019
On the advantages of exploiting the hierarchical structure of astrodynamical models
DA Dei Tos, F Topputo
Acta Astronautica 136, 236-247, 2017
142017
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
102018
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
82018
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
82018
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
52019
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
52019
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
52018
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
52015
Trajectory optimization of limited control authority spacecraft in high-fidelity models
DA DEI TOS
Italy, 2018
42018
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
42018
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
42018
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
42018
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
32018
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
32017
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
22020
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
22020
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
22015
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Articles 1–20