Segui
Francesco Topputo
Titolo
Citata da
Citata da
Anno
Survey of Direct Transcription for Low‐Thrust Space Trajectory Optimization with Applications
F Topputo, C Zhang
Abstract and Applied Analysis 2014 (1), 851720, 2014
2072014
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
2042015
On optimal two-impulse Earth–Moon transfers in a four-body model
F Topputo
Celestial Mechanics and Dynamical Astronomy 117, 279-313, 2013
1702013
Low-energy, low-thrust transfers to the Moon
G Mingotti, F Topputo, F Bernelli-Zazzera
Celestial Mechanics and Dynamical Astronomy 105, 61-74, 2009
1502009
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
1142005
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
972018
Weak stability boundary and invariant manifolds
E Belbruno, M Gidea, F Topputo
SIAM Journal on Applied Dynamical Systems 9 (3), 1061-1089, 2010
942010
Earth–Mars transfers with ballistic capture
F Topputo, E Belbruno
Celestial Mechanics and Dynamical Astronomy 121 (4), 329-346, 2015
882015
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
862021
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
832012
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
802010
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
782007
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
772021
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
762005
Computation of weak stability boundaries: Sun–Jupiter system
F Topputo, E Belbruno
Celestial Mechanics and Dynamical Astronomy 105, 3-17, 2009
752009
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
752008
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
742011
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
702011
Rapid low-thrust trajectory optimization in deep space based on convex programming
C Hofmann, F Topputo
Journal of Guidance, Control, and Dynamics 44 (7), 1379-1388, 2021
632021
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
622019
Il sistema al momento non può eseguire l'operazione. Riprova più tardi.
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