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Francesco Topputo
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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
1812015
Survey of direct transcription for low-thrust space trajectory optimization with applications
F Topputo, C Zhang
Abstract and Applied Analysis 2014, 2014
1772014
On optimal two-impulse Earth–Moon transfers in a four-body model
F Topputo
Celestial Mechanics and Dynamical Astronomy 117, 279-313, 2013
1452013
Low-energy, low-thrust transfers to the Moon
G Mingotti, F Topputo, F Bernelli-Zazzera
Celestial Mechanics and Dynamical Astronomy 105, 61-74, 2009
1442009
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
982005
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
892018
Weak stability boundary and invariant manifolds
E Belbruno, M Gidea, F Topputo
SIAM Journal on Applied Dynamical Systems 9 (3), 1061-1089, 2010
882010
Earth–Mars transfers with ballistic capture
F Topputo, E Belbruno
Celestial Mechanics and Dynamical Astronomy 121 (4), 329-346, 2015
842015
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
782012
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
742007
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
722011
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
722008
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
722005
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
712010
Computation of weak stability boundaries: Sun–Jupiter system
F Topputo, E Belbruno
Celestial Mechanics and Dynamical Astronomy 105, 3-17, 2009
712009
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
682021
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
682011
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
622021
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
512017
Resonant motion, ballistic escape, and their applications in astrodynamics
F Topputo, E Belbruno, M Gidea
Advances in Space Research 42 (8), 1318-1329, 2008
502008
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Articles 1–20