| Ion beam shepherd for contactless space debris removal C Bombardelli, J Peláez Journal of guidance, control, and dynamics 34 (3), 916-920, 2011 | 359 | 2011 |
| A New Kind of Dynamic Instability in Electrodynamic Tethers J Peláez, EC Lorenzini, O López- Rebollal, M Ruiz The Journal of the Astronautical Sciences 48 (4), 449-476, 2000 | 171 | 2000 |
| A special perturbation method in orbital dynamics J Peláez, JM Hedo, PR de Andrés Celestial Mechanics and Dynamical Astronomy 97, 131-150, 2007 | 130 | 2007 |
| Ion beam shepherd for asteroid deflection C Bombardelli, J Peláez Journal of Guidance, Control, and Dynamics 34 (4), 1270-1272, 2011 | 101 | 2011 |
| On the numerical continuation of periodic orbits-an intrinsic, 3-dimensional, differential, predictor-corrector algorithm M Lara, J Peláez Astronomy & Astrophysics 389 (2), 692-701, 2002 | 101 | 2002 |
| Bare tethers for electrodynamic spacecraft propulsion RD Estes, EC Lorenzini, J Sanmartin, J Pelaez, M Martinez-Sanchez, ... Journal of Spacecraft and Rockets 37 (2), 205-211, 2000 | 94 | 2000 |
| The ion beam shepherd: A new concept for asteroid deflection C Bombardelli, H Urrutxua, M Merino, J Pelaez, E Ahedo Acta Astronautica 90 (1), 98-102, 2013 | 85 | 2013 |
| 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 | 76 | 2011 |
| Dynamic stability of electrodynamic tethers in inclined elliptical orbits J Peláez, YN Andres Journal of Guidance, Control, and Dynamics 28 (4), 611-622, 2005 | 76 | 2005 |
| Libration control of electrodynamic tethers in inclined orbit J Pelaez, EC Lorenzini Journal of Guidance, Control, and Dynamics 28 (2), 269-279, 2005 | 72 | 2005 |
| Relative dynamics and control of an ion beam shepherd satellite C Bombardelli, H Urrutxua, M Merino Martínez, E Ahedo Galilea, ... Aeronauticos 143, 2145-2157, 2012 | 66 | 2012 |
| Periodic solutions in electrodynamic tethers on inclined orbits J Peláez, M Lara Journal of guidance, control, and dynamics 26 (3), 395-406, 2003 | 66 | 2003 |
| Two-bar model for the dynamics and stability of electrodynamic tethers J Peláez, M Ruiz, O López-Rebollal, EC Lorenzini, ML Cosmo Journal of guidance, control, and dynamics 25 (6), 1125-1135, 2002 | 56 | 2002 |
| 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 | 54 | 2015 |
| Ion beam shepherd satellite for space debris removal M Merino, E Ahedo, C Bombardelli, H Urrutxua, J Peláez Progress in Propulsion Physics 4, 789-802, 2013 | 51 | 2013 |
| Generator regime of self-balanced electrodynamic bare tethers J Peláez, M Sanjurjo Journal of Spacecraft and Rockets 43 (6), 1359-1369, 2006 | 47 | 2006 |
| On the stability of artificial equilibrium points in the circular restricted three-body problem C Bombardelli, J Peláez Celestial Mechanics and Dynamical Astronomy 109, 13-26, 2011 | 46 | 2011 |
| New analytic solution with continuous thrust: generalized logarithmic spirals J Roa, J Peláez, J Senent Journal of Guidance, Control, and Dynamics 39 (10), 2336-2351, 2016 | 44 | 2016 |
| Floating bare tether as upper atmosphere probe JR Sanmartin, M Charro, J Pelaez, I Tinao, S Elaskar, A Hilgers, ... Journal of Geophysical Research: Space Physics 111 (A11), 2006 | 43 | 2006 |
| DROMO propagator revisited H Urrutxua, M Sanjurjo-Rivo, J Peláez Celestial Mechanics and Dynamical Astronomy 124, 1-31, 2016 | 42 | 2016 |
Claudio BombardelliAssociate Professor, Space Dynamics Group, Technical University of MadridПодтвержден адрес электронной почты в домене upm.es
