| 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 | 72 | 2011 |
| 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 | 45 | 2015 |
| 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 | 41 | 2013 |
| Time Elements for Enhanced Performance of the Dromo Orbit Propagator G Baù, C Bombardelli The Astronomical Journal 148 (3), 43, 2014 | 31 | 2014 |
| 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 | 30 | 2019 |
| Orbit determination with the two-body integrals: III GF Gronchi, G Baù, S Marò Celestial Mechanics and Dynamical Astronomy 123 (2), 105-122, 2015 | 28 | 2015 |
| Accurate orbit propagation in the presence of planetary close encounters D Amato, G Baù, C Bombardelli Monthly Notices of the Royal Astronomical Society, 2017 | 26 | 2017 |
| A generalization of the equinoctial orbital elements G Baù, J Hernando-Ayuso, C Bombardelli Celestial Mechanics and Dynamical Astronomy 133, 1-29, 2021 | 18 | 2021 |
| Accurate analytical approximation of asteroid deflection with constant tangential thrust C Bombardelli, G Baù Celestial Mechanics and Dynamical Astronomy 114 (3), 279-295, 2012 | 16 | 2012 |
| 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 | 15 | 2014 |
| 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 | 14 | 2011 |
| 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 | 12 | 2017 |
| Uniform formulation for orbit computation: the intermediate elements G Baù, J Roa Celestial Mechanics and Dynamical Astronomy 132 (2), 10, 2020 | 10 | 2020 |
| 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 | 10 | 2018 |
| 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 | 5 | 2016 |
| 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 | 4 | 2023 |
| 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 | 4 | 2021 |
| Satellite Dynamics and Space Missions G Baù, A Celletti, CB Galeș, GF Gronchi Springer, 2019 | 4 | 2019 |
| Numerical behaviour of the Keplerian Integrals methods for initial orbit determination Ó Rodríguez, GF Gronchi, G Baù, R Jedicke Icarus 384, 115080, 2022 | 3 | 2022 |
| 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 | 3 | 2021 |
