DEI TOS, DIOGENE ALESSANDRO

DEI TOS, DIOGENE ALESSANDRO  

DIPARTIMENTO DI SCIENZE E TECNOLOGIE AEROSPAZIALI  

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Risultati 1 - 20 di 23 (tempo di esecuzione: 0.03 secondi).
Titolo Data di pubblicazione Autori File
Automated Trajectory Refinement of Three-Body Orbits in the Real Solar System Model 1-gen-2015 DEI TOS, DIOGENE ALESSANDROTOPPUTO, FRANCESCO
Design and Feasibility Assessment of Ultra Low Thrust Trajectories to the Sun-Earth Saddle Point 1-gen-2018 Topputo, FrancescoDei Tos, Diogene A. +
Design and Validation of Ultra Low Thrust Transfers to the Sun-Earth Saddle Point with Application to LISA PathFinder Mission Extension 1-gen-2017 TOPPUTO, FRANCESCODEI TOS, DIOGENE ALESSANDRO +
Feasibility analysis of fractioned cubesats formation for Moon observations 1-gen-2017 D. A. Dei TosD. FilippettoA. RivoltaK. V. Mani
GTOC8: Results and Methods of POLIMI-UPM 1-gen-2016 Topputo, F.Dei Tos, D. A.Filippetto, D.Massari, M.Di Lizia, P.Gonzalo Gomez, J. L.Pesce, V.Colagrossi, A. +
High-Fidelity Trajectory Optimization with Application to Saddle-Point Transfers 1-gen-2019 Dei Tos, Diogene A.Topputo, Francesco
LISA Pathfinder mission extension: A feasibility analysis 1-gen-2019 Dei Tos, Diogene A.Topputo, Francesco +
LUMIO: a Cubesat at Earth-Moon L2 1-gen-2018 Topputo, F.Massari, M.Biggs, J.Di Lizia, P.Dei Tos, D.Mani, K.Ceccherini, S.Franzese, V. +
LUMIO: achieving autonomous operations for Lunar exploration with a CubeSat 1-gen-2018 Topputo, FrancescoBiggs, JamesDi Lizia, PierluigiMassari, MauroMani, KarthikDei Tos, DiogeneCeccherini, SimoneFranzese, Vittorio +
LUMIO: an Autonomous CubeSat for Lunar Exploration 1-gen-2019 Topputo, F.Biggs, J.Di Lizia, P.Massari, M.Mani, K.Dei Tos, D.Ceccherini, S.Franzese, V. +
LUMIO: Charazterizing Lunar Meteoroid Impacts with a CubeSat 1-gen-2018 Topputo, F.Massari, M.Biggs, J.Di Lizia, P.Dei Tos, D.Mani, K.Ceccherini, S.Franzese, V. +
A Note on a Geometrical Method to Solve Spacecraft Formation Flying Control 1-gen-2016 RIVOLTA, AURELIANODEI TOS, DIOGENE ALESSANDROFILIPPETTO, DANIELE
On the advantages of exploiting the hierarchical structure of astrodynamical models 1-gen-2017 DEI TOS, DIOGENE ALESSANDROTOPPUTO, FRANCESCO
On the Advantages of Using a Strict Hierarchy to Model Astrodynamical Problems 1-gen-2015 DEI TOS, DIOGENE ALESSANDROTOPPUTO, FRANCESCO
On the Sophisticated Orbit Design of the Lunar Meteoroid Impacts Observer CubeSat 1-gen-2018 Dei Tos, D.Topputo, F.Massari, M.Biggs, J. +
Orbit Design for LUMIO: The Lunar Meteoroid Impacts Observer 1-gen-2018 Dei Tos, Diogene A.Topputo, Francesco +
The Sun–Earth saddle point: characterization and opportunities to test general relativity 1-gen-2018 Topputo, FrancescoDei Tos, Diogene A. +
Survey of Mars Ballistic Capture Trajectories using Periodic Orbits 1-gen-2017 DEI TOS, DIOGENE ALESSANDROTOPPUTO, FRANCESCO +
Survey of Mars Ballistic Capture Trajectories Using Periodic Orbits as Generating Mechanisms 1-gen-2018 Dei Tos, Diogene A.Topputo, Francesco +
System Design of LUMIO: a CubeSat at Earth-Moon l2 for Observing Lunar Meteoroid Impacts 1-gen-2018 Topputo, F.Massari, M.Biggs, J.Di Lizia, P.Dei Tos, D.Mani, K.Ceccherini, S.Franzese, V. +