Zobrazeno 1 - 10
of 245
pro vyhledávání: '"Amato, Davide"'
This work presents a deep-learning approach to estimate atmospheric density profiles for use in planetary entry guidance problems. A long short-term memory (LSTM) neural network is trained to learn the mapping between measurements available onboard a
Externí odkaz:
http://arxiv.org/abs/2310.19684
This study presents incremental correction methods for refining neural network parameters or control functions entering into a continuous-time dynamic system to achieve improved solution accuracy in satisfying the interim point constraints placed on
Externí odkaz:
http://arxiv.org/abs/2209.03698
With the upcoming launch of large constellations of satellites in the low-Earth orbit (LEO) region it will become important to organize the physical space occupied by the different operating satellites in order to minimize critical conjunctions and a
Externí odkaz:
http://arxiv.org/abs/2012.09240
Publikováno v:
Cel. Mech. Dyn. Astr. 135 (2020), 35
Luna 3 (or Lunik 3 in Russian sources) was the first spacecraft to perform a flyby of the Moon. Launched in October 1959 on a translunar trajectory with large semi-major axis and eccentricity, it collided with the Earth in late March 1960. The short,
Externí odkaz:
http://arxiv.org/abs/2006.08827
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Non-averaged regularized formulations as an alternative to semi-analytical orbit propagation methods
Publikováno v:
Celestial Mechanics and Dynamical Astronomy, Vol. 131, Issue 5, May 2019
This paper is concerned with the comparison of semi-analytical and non-averaged propagation methods for Earth satellite orbits. We analyse the total integration error for semi-analytical methods and propose a novel decomposition into dynamical, model
Externí odkaz:
http://arxiv.org/abs/1810.11418
Autor:
Bartoli, Mattia, Troiano, Maurizio, Giudicianni, Paola, Amato, Davide, Giorcelli, Mauro, Solimene, Roberto, Tagliaferro, Alberto
Publikováno v:
In Applications in Energy and Combustion Science December 2022 12
A realistic mission scenario for the deflection of fictitious asteroid 2015PDC is investigated that makes use of the ion beam shepherd concept as primary deflection technique. The article deals with the design of a low thrust rendezvous trajectory to
Externí odkaz:
http://arxiv.org/abs/1504.02854
Autor:
D'Amato, Davide1 (AUTHOR) davide.damato@poliba.it, Lorito, Marco2 (AUTHOR), Monopoli, Vito Giuseppe1 (AUTHOR) davide.damato@poliba.it, Consoletti, Rinaldo1 (AUTHOR), Maiellaro, Giuseppe2 (AUTHOR), Cupertino, Francesco1 (AUTHOR)
Publikováno v:
Energies (19961073). Feb2023, Vol. 16 Issue 3, p1205. 22p.
Akademický článek
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