| Asymptotic solution for the two-body problem with constant tangential thrust acceleration C Bombardelli, G Bał, J Pelįez Celestial Mechanics and Dynamical Astronomy 110, 239-256, 2011 | 60 | 2011 |
| Non-singular orbital elements for special perturbations in the two-body problem G Bał, C Bombardelli, J Pelįez, E Lorenzini Monthly Notices of the Royal Astronomical Society 454 (3), 2890-2908, 2015 | 38 | 2015 |
| A new set of integrals of motion to propagate the perturbed two-body problem G Bał, C Bombardelli, J Pelįez Celestial Mechanics and Dynamical Astronomy 116 (1), 53-78, 2013 | 36 | 2013 |
| Time Elements for Enhanced Performance of the Dromo Orbit Propagator G Bał, C Bombardelli The Astronomical Journal 148 (3), 43, 2014 | 29 | 2014 |
| Accurate orbit propagation in the presence of planetary close encounters D Amato, G Bał, C Bombardelli Monthly Notices of the Royal Astronomical Society, 2017 | 24 | 2017 |
| Orbit determination with the two-body integrals: III GF Gronchi, G Bał, S Marņ Celestial Mechanics and Dynamical Astronomy 123 (2), 105-122, 2015 | 24 | 2015 |
| Non-averaged regularized formulations as an alternative to semi-analytical orbit propagation methods D Amato, C Bombardelli, G Bał, V Morand, AJ Rosengren Celestial Mechanics and Dynamical Astronomy 131 (5), 21, 2019 | 19 | 2019 |
| Accurate analytical approximation of asteroid deflection with constant tangential thrust C Bombardelli, G Bał 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 Bał, H Urrutxua, J Pelįez Adv. Astronaut. Sci 152, 379-399, 2014 | 14 | 2014 |
| DROMO: a new regularized orbital propagator G Bau, A Hunh, H Urrutxua, C Bombardelli, J Pelįez Proceedings of International Symposium on Orbit Propagation and …, 2011 | 12 | 2011 |
| A generalization of the equinoctial orbital elements G Bał, J Hernando-Ayuso, C Bombardelli Celestial Mechanics and Dynamical Astronomy 133, 1-29, 2021 | 11 | 2021 |
| Preliminary orbits with line-of-sight correction for LEO satellites observed with radar H Ma, G Bał, D Bracali Cioci, GF Gronchi Celestial Mechanics and Dynamical Astronomy 130 (10), 70, 2018 | 10 | 2018 |
| 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 | 9 | 2017 |
| Uniform formulation for orbit computation: the intermediate elements G Bał, J Roa Celestial Mechanics and Dynamical Astronomy 132 (2), 10, 2020 | 7 | 2020 |
| Efficient numerical propagation of planetary close encounters with regularized element methods D Amato, C Bombardelli, G Bał 6th International Conference on Astrodynamics Tools and Techniques (ICATT), 2016 | 4 | 2016 |
| Near-Linear Orbit Uncertainty Propagation in Low-Earth Orbit J HERNANDO-AYUSO, C BOMBARDELLI, G BAU, CA MARTINEZ [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 |
| Mitigation of Trajectory Propagation Error in Spacecraft Fly-Bys D Amato, C Bombardelli, G Bał International workshop on “Key Topics in Orbit Propagation Applied to Space …, 2014 | 3 | 2014 |
| Generalization of a method by Mossotti for initial orbit determination GF Gronchi, G Bał, Ó Rodrķguez, R Jedicke, J Moeyens Celestial Mechanics and Dynamical Astronomy 133 (9), 41, 2021 | 2 | 2021 |
| Uncertainty propagation in the N-body problem using Dromo elements J Hernando-Ayuso, C Bombardelli, G Bał Acta Astronautica 156, 252-261, 2019 | 2 | 2019 |
| Accurate and Fast Orbit Propagation With a New Complete Set of Elements G Bał, C Bombardelli, J Pelįez Spaceflight Mechanics 2013. Proceedings of the 23rd AAS/AIAA Space Flight …, 2013 | 2 | 2013 |
