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Giulio Baù
Giulio Baù
Associate Professor, Department of Mathematics, University of Pisa
unipi.it의 이메일 확인됨 - 홈페이지
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Asymptotic solution for the two-body problem with constant tangential thrust acceleration
C Bombardelli, G Baù, J Peláez
Celestial Mechanics and Dynamical Astronomy 110, 239-256, 2011
722011
Non-singular orbital elements for special perturbations in the two-body problem
G Baù, C Bombardelli, J Peláez, E Lorenzini
Monthly Notices of the Royal Astronomical Society 454 (3), 2890-2908, 2015
452015
A new set of integrals of motion to propagate the perturbed two-body problem
G Baù, C Bombardelli, J Peláez
Celestial Mechanics and Dynamical Astronomy 116 (1), 53-78, 2013
412013
Time Elements for Enhanced Performance of the Dromo Orbit Propagator
G Baù, C Bombardelli
The Astronomical Journal 148 (3), 43, 2014
312014
Non-averaged regularized formulations as an alternative to semi-analytical orbit propagation methods
D Amato, C Bombardelli, G Baù, V Morand, AJ Rosengren
Celestial Mechanics and Dynamical Astronomy 131 (5), 21, 2019
302019
Orbit determination with the two-body integrals: III
GF Gronchi, G Baù, S Marò
Celestial Mechanics and Dynamical Astronomy 123 (2), 105-122, 2015
282015
Accurate orbit propagation in the presence of planetary close encounters
D Amato, G Baù, C Bombardelli
Monthly Notices of the Royal Astronomical Society, 2017
262017
A generalization of the equinoctial orbital elements
G Baù, J Hernando-Ayuso, C Bombardelli
Celestial Mechanics and Dynamical Astronomy 133, 1-29, 2021
182021
Accurate analytical approximation of asteroid deflection with constant tangential thrust
C Bombardelli, G Baù
Celestial Mechanics and Dynamical Astronomy 114 (3), 279-295, 2012
162012
EDROMO: an accurate propagator for elliptical orbits in the perturbed two-body problem
G Baù, H Urrutxua, J Peláez
Adv. Astronaut. Sci 152, 379-399, 2014
152014
DROMO: a new regularized orbital propagator
G Bau, A Hunh, H Urrutxua, C Bombardelli, J Peláez
Proceedings of International Symposium on Orbit Propagation and …, 2011
142011
Keplerian integrals, elimination theory and identification of very short arcs in a large database of optical observations
GF Gronchi, G Bau, A Milani
Celestial Mechanics and Dynamical Astronomy 127 (2), 211-232, 2017
122017
Uniform formulation for orbit computation: the intermediate elements
G Baù, J Roa
Celestial Mechanics and Dynamical Astronomy 132 (2), 10, 2020
102020
Preliminary orbits with line-of-sight correction for LEO satellites observed with radar
H Ma, G Baù, D Bracali Cioci, GF Gronchi
Celestial Mechanics and Dynamical Astronomy 130 (10), 70, 2018
102018
Efficient numerical propagation of planetary close encounters with regularized element methods
D Amato, C Bombardelli, G Baù
6th International Conference on Astrodynamics Tools and Techniques (ICATT), 2016
52016
Near-Linear Orbit Uncertainty Propagation Using the Generalized Equinoctial Orbital Elements
J Hernando-Ayuso, C Bombardelli, G Baù, A Martínez-Cacho
Journal of Guidance, Control, and Dynamics 46 (4), 654-665, 2023
42023
Generalization of a method by Mossotti for initial orbit determination
GF Gronchi, G Baù, Ó Rodríguez, R Jedicke, J Moeyens
Celestial Mechanics and Dynamical Astronomy 133 (9), 41, 2021
42021
Satellite Dynamics and Space Missions
G Baù, A Celletti, CB Galeș, GF Gronchi
Springer, 2019
42019
Numerical behaviour of the Keplerian Integrals methods for initial orbit determination
Ó Rodríguez, GF Gronchi, G Baù, R Jedicke
Icarus 384, 115080, 2022
32022
Near-Linear Orbit Uncertainty Propagation in Low-Earth Orbit
J HERNANDO-AYUSO, C BOMBARDELLI, G BAU, A MARTINEZ CACHO
[第 31 回アストロダイナミクスシンポジウム講演後刷り集]= The 31th Workshop on JAXA …, 2021
32021
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학술자료 1–20