Fast and near-optimal guidance for docking to uncontrolled spacecraft J Ventura, M Ciarcià, M Romano, U Walter Journal of Guidance, Control, and Dynamics 40 (12), 3138-3154, 2017 | 85 | 2017 |
Optimal trajectories for spacecraft rendezvous A Miele, MW Weeks, M Ciarcia Journal of optimization theory and applications 132, 353-376, 2007 | 67 | 2007 |
Experimental characterization of inverse dynamics guidance in docking with a rotating target M Wilde, M Ciarcià, A Grompone, M Romano Journal of Guidance, Control, and Dynamics 39 (6), 1173-1187, 2016 | 44 | 2016 |
A near-optimal guidance for cooperative docking maneuvers M Ciarcia, A Grompone, M Romano Acta Astronautica 102, 367-377, 2014 | 39 | 2014 |
Guidance trajectories for spacecraft rendezvous A Miele, M Ciarcià, MW Weeks Journal of optimization theory and applications 132, 377-400, 2007 | 28 | 2007 |
An inverse dynamics-based trajectory planner for autonomous docking to a tumbling target J Ventura, M Ciarcia, M Romano, U Walter AIAA guidance, navigation, and control conference, 0876, 2016 | 25 | 2016 |
Emulating scaled clohessy–wiltshire dynamics on an air-bearing spacecraft simulation testbed M Ciarcià, R Cristi, MM Romano Journal of Guidance, Control, and Dynamics 40 (10), 2496-2510, 2017 | 22 | 2017 |
Reflections on the Hohmann transfer A Miele, M Ciarcià, J Mathwig Journal of Optimization Theory and Applications 123, 233-253, 2004 | 20 | 2004 |
Suboptimal guidance for orbital proximity maneuver with path constraints capability M Ciarcià, M Romano AIAA Guidance, Navigation, and Control Conference, 4920, 2012 | 17 | 2012 |
Nonlinear programming solvers for unconstrained and constrained optimization problems: a benchmark analysis G Lavezzi, K Guye, M Ciarcià arXiv preprint arXiv:2204.05297, 2022 | 12 | 2022 |
Collision avoidance for an aircraft in abort landing: Trajectory optimization and guidance A Miele, T Wang, JA Mathwig, M Ciarcia Journal of optimization theory and applications 146, 233-254, 2010 | 11 | 2010 |
Simulations of multiple spacecraft maneuvering with matlab/simulink and satellite tool kit SB McCamish, M Ciarcià, M Romano Journal of Aerospace Information Systems 10 (7), 348-358, 2013 | 10 | 2013 |
Attitude Control Strategies for an Imaging CubeSat G Lavezzi, ME Grøtte, M Ciarcià 2019 IEEE International Conference on Electro Information Technology (EIT …, 2019 | 9 | 2019 |
Experimental emulation of the scaled clohessy-wiltshire dynamics on a flat air-bearing testbed M Ciarcia, R Cristi, M Romano AIAA Guidance, Navigation, and Control Conference, 1047, 2017 | 8 | 2017 |
Optimal starting conditions for the rendezvous maneuver, part 1: Optimal control approach A Miele, M Ciarcia Journal of optimization theory and applications 137, 593-624, 2008 | 8 | 2008 |
Mars drone configurations and approaches to rotor design: a review A Saez, M Manzo, M Ciarcià ASME International Mechanical Engineering Congress and Exposition 85611 …, 2021 | 6 | 2021 |
Rendezvous guidance trajectories via multiple-subarc sequential gradient-restoration algorithm A Miele, M Ciarcià, MW Weeks Journal of Aerospace Engineering 22 (2), 160-172, 2009 | 6 | 2009 |
Optimal starting conditions for the rendezvous maneuver, part 2: Mathematical programming approach A Miele, M Ciarcià Journal of optimization theory and applications 137, 625-639, 2008 | 6 | 2008 |
Spacecraft proximity maneuver guidance based on inverse dynamic and sequential gradient-restoration algorithm M Ciarcia, M Romano Advances in the Astronautical Sciences, 142, 3679-3698, 2012 | 5 | 2012 |
A direct method-based suboptimal attitude guidance for accurate ground-target tracking maneuvers G Lavezzi, M Ciarcià Advances in Space Research 69 (11), 3983-4000, 2022 | 4 | 2022 |