Francesco Topputo

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Vittorio FranzeseResearch Associate ad University of LuxembourgVerified email at uni.lu
Carmine GiordanoPostDoc Fellow, Politecnico di MilanoVerified email at polimi.it
Mattia PugliattiPostDoc at University of Colorado BoulderVerified email at colorado.edu
Pierluigi Di LiziaPolitecnico di MilanoVerified email at polimi.it
Paolo PanicucciAssistant Professor of Space Systems, Politecnico di MilanoVerified email at polimi.it
Diogene Alessandro Dei TosJAXAVerified email at ac.jaxa.jp
Angelo CervoneDelft University of TechnologyVerified email at tudelft.nl
Mauro MassariPolitecnico di MilanoVerified email at polimi.it
Fabio FerrariNASA Jet Propulsion LaboratoryVerified email at jpl.nasa.gov
Roberto FurfaroProfessor of systems and industrial engineering, aerospace and mechanical engineeringVerified email at email.arizona.edu
Stefano SperettaDelft University of TechnologyVerified email at tudelft.nl
Eleonora AndreisPolitecnico di MilanoVerified email at polimi.it
Massimiliano VasileProfessor of Space Systems Engineering, Aerospace Centre of Excellence, University of StrathclydeVerified email at strath.ac.uk
Demetrio LabateProgram Manager Earth Observation and Deep Space Payloads, Leonardo (former Finmeccanica / Selex ES)Verified email at leonardocompany.com
Yang WangPolitecnico di MilanoVerified email at polimi.it
Simone ceccheriniResearch Assistant, Politecnico di MilanoVerified email at polimi.it
Alessandra MenicucciTechnical University DelftVerified email at tudelft.nl
Richard LinaresAssociate Professor, Dept. of Aeronautics & Astronautics, MITVerified email at mit.edu
Roberto ArmellinThe University of AucklandVerified email at auckland.ac.nz
Alessandro MorselliPolitecnico di MilanoVerified email at polimi.it

Francesco Topputo

Full Professor, Politecnico di Milano

Verified email at polimi.it - Homepage

low-energy low-thrust space trajectories ballistic capture Lagrange points nonlinear optimal control modeling and simulation


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Survey of Direct Transcription for Low‐Thrust Space Trajectory Optimization with Applications F Topputo, C Zhang Abstract and Applied Analysis 2014 (1), 851720, 2014	206	2014
Low-thrust minimum-fuel optimization in the circular restricted three-body problem C Zhang, F Topputo, F Bernelli-Zazzera, YS Zhao Journal of Guidance, Control, and Dynamics 38 (8), 1501-1510, 2015	203	2015
On optimal two-impulse Earth–Moon transfers in a four-body model F Topputo Celestial Mechanics and Dynamical Astronomy 117, 279-313, 2013	166	2013
Low-energy, low-thrust transfers to the Moon G Mingotti, F Topputo, F Bernelli-Zazzera Celestial Mechanics and Dynamical Astronomy 105, 61-74, 2009	149	2009
Low energy interplanetary transfers exploiting invariant manifolds of the restricted three-body problem F Topputo, M Vasile, F Bernelli-Zazzera The Journal of the Astronautical Sciences 53, 353-372, 2005	113	2005
Deep learning for autonomous lunar landing R Furfaro, I Bloise, M Orlandelli, P Di Lizia, F Topputo, R Linares Advances in the Astronautical Sciences 167, 3285-3306, 2018	96	2018
Weak stability boundary and invariant manifolds E Belbruno, M Gidea, F Topputo SIAM Journal on Applied Dynamical Systems 9 (3), 1061-1089, 2010	93	2010
Earth–Mars transfers with ballistic capture F Topputo, E Belbruno Celestial Mechanics and Dynamical Astronomy 121 (4), 329-346, 2015	88	2015
Preliminary mission profile of Hera’s Milani CubeSat F Ferrari, V Franzese, M Pugliatti, C Giordano, F Topputo Advances in Space Research 67 (6), 2010-2029, 2021	83	2021
Efficient invariant-manifold, low-thrust planar trajectories to the Moon G Mingotti, F Topputo, F Bernelli-Zazzera Communications in Nonlinear Science and Numerical Simulation 17 (2), 817-831, 2012	83	2012
Method to design ballistic capture in the elliptic restricted three-body problem N Hyeraci, F Topputo Journal of guidance, control, and dynamics 33 (6), 1814-1823, 2010	80	2010
Combined optimal low-thrust and stable-manifold trajectories to the Earth-Moon halo orbits G Mingotti, F Topputo, F Bernelli-Zazzera New Trends in Astrodynamics and Applications III(AIP Conference Proceedings …, 2007	78	2007
Envelop of reachable asteroids by M-ARGO CubeSat F Topputo, Y Wang, C Giordano, V Franzese, H Goldberg, F Perez-Lissi, ... Advances in Space Research 67 (12), 4193-4221, 2021	76	2021
Computation of weak stability boundaries: Sun–Jupiter system F Topputo, E Belbruno Celestial Mechanics and Dynamical Astronomy 105, 3-17, 2009	75	2009
Optimal low-thrust invariant manifold trajectories via attainable sets G Mingotti, F Topputo, F Bernelli-Zazzera Journal of guidance, control, and dynamics 34 (6), 1644-1656, 2011	74	2011
Resonance transitions associated to weak capture in the restricted three-body problem E Belbruno, F Topputo, M Gidea Advances in Space Research 42 (8), 1330-1351, 2008	74	2008
Earth‐to‐Moon Low Energy Transfers Targeting L₁ Hyperbolic Transit Orbits F Topputo, M Vasile, F BERNELLI‐ZAZZERA Annals of the New York Academy of Sciences 1065 (1), 55-76, 2005	74	2005
Earth–Mars transfers with ballistic escape and low-thrust capture G Mingotti, F Topputo, F Bernelli-Zazzera Celestial Mechanics and Dynamical Astronomy 110, 169-188, 2011	70	2011
Autonomous optical navigation for the lunar meteoroid impacts observer V Franzese, P Di Lizia, F Topputo Journal of Guidance, Control, and Dynamics 42 (7), 1579-1586, 2019	61	2019
Trajectory options for hera’s milani cubesat around (65803) didymos F Ferrari, V Franzese, M Pugliatti, C Giordano, F Topputo The Journal of the Astronautical Sciences 68 (4), 973-994, 2021	60	2021

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