ROMANO, MARCELLO
ROMANO, MARCELLO
DIPARTIMENTO DI INGEGNERIA AEROSPAZIALE (attivo dal 01/01/1900 al 31/12/2012)
Automatic Mass Balancing for Small Three-Axis Spacecraft Simulator Using Sliding Masses
2012-01-01 S., Chesi; V., Pellegrini; Q., Gong; R., Cristi; Romano, Marcello
Concise Form of the Dynamic and Kinematic Solutions of the Euler-Poinsot Problem
2012-01-01 Romano, Marcello
Control of Satellites with Minimum Number of Control Actuators
2008-01-01 J. S., Hall; Romano, Marcello
Failure-Robust Thruster Commanding for Space Vehicles Control
2010-01-01 F., Curti; R., Bevilacqua; Romano, Marcello
Laboratory Experimentation of Guidance and Control of Spacecraft During On-Orbit Proximity Maneuvers, Mechatronic Systems Simulation Modeling and Control
2010-01-01 Hall, J.; Romano, Marcello
Novel Three-Axis Attitude Control System for CubeSats with High Agility and Pointing Accuracy Requirements, Advances in the Astronautical Sciences
2009-01-01 P. M., Oppenheimer; Romano, Marcello; A., Blocker; J., Hall
Optimization of a Spacecraft Maneuver to Dock with a Tumbling Object
2010-01-01 G. A., Boyarko; O. A., Yakimenko; Romano, Marcello
Spacecraft Proximity Maneuver Guidance Based on Inverse Dynamic and Sequential Gradient-Restoration Algorithm
2012-01-01 M., Ciarcia; Romano, Marcello
Three Axis Attitude Control Simulators for Bifocal Relay Mirror Spacecraft
2003-01-01 B. N., Agrawal; Romano, Marcello; T. Y., Martinez
Use of Variable Speed Control Moment Gyros for a Fine Pointing Dual-Line-of-Sight-Spacecraft
2003-01-01 Romano, Marcello; B. N., Agrawal