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Alessandro Peloni
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Year
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
852016
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
312017
Multiple near-earth asteroid rendezvous mission: Solar-sailing options
A Peloni, B Dachwald, M Ceriotti
Advances in Space Research 62 (8), 2084-2098, 2018
292018
Automated trajectory optimizer for solar sailing (atoss)
A Peloni, AV Rao, M Ceriotti
Aerospace Science and Technology 72, 465-475, 2018
242018
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
192019
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, 2015
142015
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, ...
102017
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
72016
From Low Thrust to Solar Sailing: A Homotopic Approach
N Sullo, A Peloni, M Ceriotti
72016
Solar-sail mission design for multiple near-Earth asteroid rendezvous
A Peloni
University of Glasgow, 2018
62018
ATOSS: Automated Trajectory Optimiser for Solar Sailing
A Peloni, AV Rao, M Ceriotti
Fourth European Optimisation in Space Engineering (OSE) Workshop, 27-30, 2017
62017
Preliminary trajectory design of a multiple NEO rendezvous mission through solar sailing
A Peloni, M Ceriotti, B Dachwald
methods 10, 11, 2014
62014
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, ...
52019
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
42018
Multiple NEA rendezvous mission: Solar sailing options
A Peloni, B Dachwald, M Ceriotti
42017
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
32021
Responsive integrated small spacecraft solar sail and payload design concepts and missions
JT Grundmann, W Bauer, R Boden, M Ceriotti, F Cordero, B Dachwald, ...
22019
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, ...
22018
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, ...
22018
Solar-Sailing Trajectory Design for Close-up NEA Observations Mission
A Peloni, M Ceriotti, B Dachwald
22015
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