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Marco Ciarcià
Marco Ciarcià
Colorado State University, Mechanical Engineering Department
Verified email at colostate.edu - Homepage
Title
Cited by
Cited by
Year
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
822017
Optimal trajectories for spacecraft rendezvous
A Miele, MW Weeks, M Ciarcia
Journal of optimization theory and applications 132, 353-376, 2007
662007
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
452016
A near-optimal guidance for cooperative docking maneuvers
M Ciarcia, A Grompone, M Romano
Acta Astronautica 102, 367-377, 2014
382014
Guidance trajectories for spacecraft rendezvous
A Miele, M Ciarcià, MW Weeks
Journal of optimization theory and applications 132, 377-400, 2007
282007
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
262016
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
222017
Reflections on the Hohmann transfer
A Miele, M Ciarcià, J Mathwig
Journal of Optimization Theory and Applications 123, 233-253, 2004
192004
Suboptimal guidance for orbital proximity maneuver with path constraints capability
M Ciarcià, M Romano
AIAA Guidance, Navigation, and Control Conference, 4920, 2012
172012
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
112010
Nonlinear programming solvers for unconstrained and constrained optimization problems: a benchmark analysis
G Lavezzi, K Guye, M Ciarcià
arXiv preprint arXiv:2204.05297, 2022
92022
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
92013
Attitude Control Strategies for an Imaging CubeSat
G Lavezzi, ME Grøtte, M Ciarcià
2019 IEEE International Conference on Electro Information Technology (EIT …, 2019
82019
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
82017
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
82008
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
62021
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
62009
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
62008
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
52012
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
32022
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