| Rendezvous in cis-lunar space near rectilinear halo orbit: Dynamics and control issues G Bucchioni, M Innocenti Aerospace 8 (3), 68, 2021 | 21 | 2021 |
| Phasing maneuver analysis from a low lunar orbit to a near rectilinear halo orbit G Bucchioni, M Innocenti Aerospace 8 (3), 70, 2021 | 16 | 2021 |
| Closed loop guidance during close range rendezvous in a three body problem M Galullo, G Bucchioni, G Franzini, M Innocenti The Journal of the Astronautical Sciences 69 (1), 28-50, 2022 | 11 | 2022 |
| Two and three impulses phasing strategy with a spacecraft orbiting on an Earth–Moon NRHO A Fossà, G Bucchioni, E Blazquez, E Canalias, S Lizy-Destrez, R Bertrand, ... Acta Astronautica 198, 669-679, 2022 | 10 | 2022 |
| Phasing with near rectilinear Halo orbits: Design and comparison G Bucchioni, S Lizy-Destrez, T Vaujour, V Thoraval, L Rouverand, C Silva Advances in Space Research 71 (5), 2449-2466, 2023 | 7 | 2023 |
| Open loop safe trajectory design for cislunar NRHO rendezvous G Bucchioni, M Innocenti 2020 American Control Conference (ACC), 4337-4342, 2020 | 7 | 2020 |
| Dynamical issues in rendezvous operations with third body perturbation G Bucchioni, M Innocenti Advances in the Astronautical Sciences 1, 549-564, 2020 | 5 | 2020 |
| Guidance and Control for Phasing, Rendezvous and Docking in the Three Body Lunar Space G BUCCHIONI | 4 | 2021 |
| Rossonero: a tool for preliminary rendezvous mission design in the restricted three-body problem G Franzini, G Bucchioni, M Innocenti, M Casasco 7th International Conference on Astrodynamics Tools and Techniques 1, 1-7, 2018 | 4 | 2018 |
| Optimal time-fixed impulsive non-Keplerian orbit to orbit transfer algorithm based on primer vector theory G Bucchioni, G Gemignani, F Lombardi, A Bellome, JPF Leitão, ... Communications in Nonlinear Science and Numerical Simulation 124, 107307, 2023 | 3 | 2023 |
| Bearings-only guidance in cis-lunar rendezvous F D’Onofrio, G Bucchioni, M Innocenti Journal of Guidance, Control, and Dynamics 44 (10), 1862-1874, 2021 | 3 | 2021 |
| Ephemeris validation of Rendezvous Guidance in Lunar NRHO G Bucchioni, M Innocenti AIAA Scitech 2021 Forum, 0975, 2021 | 3 | 2021 |
| A Minimum-propellant Pontryagin-based Nonlinear MPC for Spacecraft Rendezvous in Lunar Orbit: the Extended Version M Pagone, G Bucchioni, F Alfino, C Novara arXiv preprint arXiv:2309.05453, 2023 | 2 | 2023 |
| Failure Mitigation during Rendezvous in Cislunar Orbit M Innocenti, F D'Onofrio, G Bucchioni AIAA SCITECH 2022 Forum, 0861, 2022 | 2 | 2022 |
| Design of Phasing Trajectories From a Low Lunar Orbit To a Near Rectilinear Halo Orbit G Bucchioni, M Innocenti Ptoceedings of the 2020 AAS/AIAA Astrodynamics Specialist Conference 1 (1), 1-20, 2020 | 2 | 2020 |
| Realistic Guidance Performances during Lunar Rendezvous with the Third Body Perturbation G Bucchioni, M Casasco, M Innocenti AIAA Scitech 2020 Forum, 1601, 2020 | 2 | 2020 |
| Primer Vector Based Optimal Guidance for Orbital transfers in Cislunar Environment G Gemignani | 1 | 2023 |
| Dynamics and control analysis during rendezvous in non-Keplerian Earth—Moon orbits M Innocenti, G Bucchioni, G Franzini, M Galullo, FD Onofrio, A Cropp, ... Frontiers in Space Technologies 3, 929179, 2022 | 1 | 2022 |
| Fully Safe Rendezvous Strategy in Cis-Lunar Space: Passive and Active Collision Avoidance G Bucchioni, M De Benedetti, F D’Onofrio, M Innocenti The Journal of the Astronautical Sciences 69 (5), 1319-1346, 2022 | 1 | 2022 |
| Closed-loop neural control for the final phase of a cislunar rendezvous G Tofanelli, G Bucchioni, M Innocenti Proceedings of the 2021 AAS/AIAA Astrodynamics Specialist Conference 1 (AAS …, 2021 | 1 | 2021 |
Mario InnocentiProfessor of Automatic Control, Department of Information Engineering, University of Pisa, ItalyAdresse e-mail validée de unipi.it
