Sfoglia per Autore
Exact analytic solutions for the rotation of an axially symmetric rigid body subjected to a constant torque
2008-01-01 Romano, Marcello
Control of Satellites with Minimum Number of Control Actuators
2008-01-01 J. S., Hall; Romano, Marcello
Exact analytic solution for the rotation of a rigid body having spherical ellipsoid of inertia and subjected to a constant torque
2008-01-01 Romano, Marcello
Rendezvous Maneuvers of multiple spacecraft using differential drag under J2 perturbation
2008-01-01 R., Bevilacqua; 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
Flight testing of multiple-spacecraft control on SPHERES during close-proximity operations
2009-01-01 S. B., Mccamish; Romano, Marcello; S., Nolet; C. M., Edwards; D. W., Miller
Ad hoc wireless networking and shared computation for autonomous multirobot systems
2009-01-01 R., Bevilacqua; J. S., Hall; J., Horning; Romano, Marcello
Online generation of quasi-optimal spacecraft rendezvous trajectories
2009-01-01 R., Bevilacqua; Romano, Marcello; O., Yakimenko
A ballistic-pendulum test stand to characterize small cold-gas thruster nozzles
2009-01-01 C., Lugini; 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
Spacecraft Docking Interface Mechanism
2010-01-01 Romano, Marcello; Oppenheimer, P.
Active Attitude Control System for Small Spacecraft
2010-01-01 Romano, Marcello; Oppenheimer, P.
Spacecraft proximity navigation and autonomous assembly based on augmented state estimation: analysis and experiments
2010-01-01 V., Pellegrini; R., Bevilacqua; Romano, Marcello; F., Curti
Lyapunov-based thrusters' selection for spacecraft control: analysis and experimentation
2010-01-01 F., Curti; Romano, Marcello; R., Bevilacqua
Decoupled-natural-dynamics Model for the Relative Motion of two Spacecraft without and with J2 Perturbation
2010-01-01 R., Bevilacqua; Romano, Marcello; F., Curti
Time-optimal reorientation of a spacecraft using a direct optimization method based on inverse dynamics
2010-01-01 G. A., Boyarko; Romano, Marcello; O. A., Yakimenko
Optimization of a Spacecraft Maneuver to Dock with a Tumbling Object
2010-01-01 G. A., Boyarko; O. A., Yakimenko; Romano, Marcello
Failure-Robust Thruster Commanding for Space Vehicles Control
2010-01-01 F., Curti; R., Bevilacqua; Romano, Marcello
Quaternion feedback regulator for large angle maneuvers of underactuated spacecraft
2010-01-01 J. S., Hall; Romano, Marcello; R., Cristi
Multiple spacecraft rendezvous maneuvers by differential drag and low thrust engines
2010-01-01 R., Bevilacqua; J. S., Hall; Romano, Marcello
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