Matteo Ceriotti
Matteo Ceriotti
Senior Lecturer in Space Systems Engineering, University of Glasgow
Verified email at - Homepage
Cited by
Cited by
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
Generation of optimal trajectories for Earth hybrid pole sitters
M Ceriotti, CR McInnes
Journal of Guidance, Control, and Dynamics 34 (3), 847-859, 2011
Displaced geostationary orbit design using hybrid sail propulsion
J Heiligers, M Ceriotti, CR McInnes, JD Biggs
Journal of Guidance, Control, and Dynamics 34 (6), 1852-1866, 2011
MGA trajectory planning with an ACO-inspired algorithm
M Ceriotti, M Vasile
Acta Astronautica 67 (9-10), 1202-1217, 2010
Systems design of a hybrid sail pole-sitter
M Ceriotti, CR McInnes
Advances in Space Research 48 (11), 1754-1762, 2011
Close proximity formation flying via linear quadratic tracking controller and artificial potential function
L Palacios, M Ceriotti, G Radice
Advances in Space Research 56 (10), 2167-2176, 2015
Trajectory and spacecraft design for a pole-sitter mission
M Ceriotti, J Heiligers, CR McInnes
Journal of Spacecraft and Rockets 51 (1), 311-326, 2014
Automated multigravity assist trajectory planning with a modified ant colony algorithm
M Ceriotti, M Vasile
Journal of Aerospace Computing, Information, and Communication 7 (9), 261-293, 2010
Displaced geostationary orbits using hybrid low-thrust propulsion
J Heiligers, CR McInnes, JD Biggs, M Ceriotti
Acta Astronautica 71, 51-67, 2012
Global optimisation of multiple gravity assist trajectories
M Ceriotti
University of Glasgow, 2010
Variable-geometry solar sailing: the possibilities of the quasi-rhombic pyramid
M Ceriotti, P Harkness, M McRobb
Advances in solar sailing, 899-919, 2014
Natural and sail-displaced doubly-symmetric Lagrange point orbits for polar coverage
M Ceriotti, CR McInnes
Celestial Mechanics and Dynamical Astronomy 114, 151-180, 2012
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
Multiple near-earth asteroid rendezvous mission: Solar-sailing options
A Peloni, B Dachwald, M Ceriotti
Advances in Space Research 62 (8), 2084-2098, 2018
Automated trajectory optimizer for solar sailing (atoss)
A Peloni, AV Rao, M Ceriotti
Aerospace Science and Technology 72, 465-475, 2018
Hybrid solar sail and solar electric propulsion for novel Earth observation missions
M Ceriotti, CR McInnes
Acta Astronautica 69 (9-10), 809-821, 2011
Attitude stability and altitude control of a variable-geometry earth-orbiting solar sail
L Felicetti, M Ceriotti, P Harkness
Journal of Guidance, Control, and Dynamics 39 (9), 2112-2126, 2016
Control of asteroid retrieval trajectories to libration point orbits
M Ceriotti, JP Sanchez
Acta Astronautica 126, 342-353, 2016
Design of optimal Earth pole-sitter transfers using low-thrust propulsion
J Heiligers, M Ceriotti, CR McInnes, JD Biggs
Acta Astronautica 79, 253-268, 2012
Optimal law for inclination change in an atmosphere through solar sailing
V Stolbunov, M Ceriotti, C Colombo, CR McInnes
Journal of Guidance, Control, and Dynamics 36 (5), 1310-1323, 2013
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