| Solar-sail trajectory design for a multiple near-earth-asteroid rendezvous mission A Peloni, M Ceriotti, B Dachwald Journal of Guidance, Control, and Dynamics 39 (12), 2712-2724, 2016 | 99 | 2016 |
| Low-thrust to solar-sail trajectories: a homotopic approach N Sullo, A Peloni, M Ceriotti Journal of Guidance, Control, and Dynamics 40 (11), 2796-2806, 2017 | 38 | 2017 |
| Multiple near-earth asteroid rendezvous mission: Solar-sailing options A Peloni, B Dachwald, M Ceriotti Advances in Space Research 62 (8), 2084-2098, 2018 | 35 | 2018 |
| Automated trajectory optimizer for solar sailing (atoss) A Peloni, AV Rao, M Ceriotti Aerospace Science and Technology 72, 465-475, 2018 | 29 | 2018 |
| Capabilities of Gossamer-1 derived small spacecraft solar sails carrying Mascot-derived nanolanders for in-situ surveying of NEAs JT Grundmann, W Bauer, J Biele, R Boden, M Ceriotti, F Cordero, ... Acta Astronautica 156, 330-362, 2019 | 23 | 2019 |
| Dynamic and structural performances of a new sailcraft concept for interplanetary missions A Peloni, D Barbera, S Laurenzi, C Circi The Scientific World Journal 2015 (1), 714371, 2015 | 16 | 2015 |
| Soil to sail-asteroid landers on near-term sailcraft as an evolution of the GOSSAMER small spacecraft solar sail concept for in-situ characterization JT Grundmann, R Boden, M Ceriotti, B Dachwald, E Dumont, CD Grimm, ... | 11 | 2017 |
| From low thrust to solar sailing: a homotopic approach N Sullo, A Peloni, M Ceriotti | 8 | 2016 |
| From Low Thrust to Solar Sailing: A Homotopic Approach, 26th AAS N Sullo, A Peloni, M Ceriotti AIAA Space Flight Mechanics Meeting, Paper, 16-426, 2016 | 7 | 2016 |
| Solar-sail mission design for multiple near-Earth asteroid rendezvous A Peloni University of Glasgow, 2018 | 6 | 2018 |
| ATOSS: Automated Trajectory Optimiser for Solar Sailing A Peloni, AV Rao, M Ceriotti Fourth European Optimisation in Space Engineering (OSE) Workshop, 27-30, 2017 | 6 | 2017 |
| Preliminary trajectory design of a multiple NEO rendezvous mission through solar sailing A Peloni, M Ceriotti, B Dachwald methods 10, 11, 2014 | 6 | 2014 |
| Responsive exploration and asteroid characterization through integrated solar sail and lander development using small spacecraft technologies JT Grundmann, W Bauer, R Boden, M Ceriotti, F Cordero, B Dachwald, ... | 5 | 2019 |
| Osculating keplerian elements for highly non-keplerian orbits A Peloni, CR McInnes, M Ceriotti Journal of Guidance, Control, and Dynamics 41 (11), 2489-2498, 2018 | 4 | 2018 |
| Multiple NEA rendezvous mission: Solar sailing options A Peloni, B Dachwald, M Ceriotti | 4 | 2017 |
| Sailing at the brink–The no-limits of near-/now-term-technology solar sails and SEP spacecraft in (multiple) NEO rendezvous M Ceriotti, G Viavattene, I Moore, A Peloni, CR McInnes, JT Grundmann Advances in Space Research 67 (9), 3012-3026, 2021 | 3 | 2021 |
| Responsive integrated small spacecraft solar sail and payload design concepts and missions JT Grundmann, W Bauer, R Boden, M Ceriotti, F Cordero, B Dachwald, ... | 2 | 2019 |
| Small spacecraft based multiple near-earth asteroid rendezvous and landing with near-term solar sails and ‘Now-Term ‘technologies JT Grundmann, W Bauer, J Biele, R Boden, M Ceriotti, F Cordero, ... | 2 | 2018 |
| Small Spacecraft Solar Sailing for Small Solar System Body Multiple Rendezvous and Landing JT Grundmann, W Bauer, J Biele, R Boden, K Borchers, M Ceriotti, ... | 2 | 2018 |
| Solar-Sailing Trajectory Design for Close-up NEA Observations Mission A Peloni, M Ceriotti, B Dachwald | 2 | 2015 |
