ROMANO, MARCELLO
ROMANO, MARCELLO
DIPARTIMENTO DI INGEGNERIA AEROSPAZIALE (attivo dal 01/01/1900 al 31/12/2012)
A 4-PI steradians dynamic three-axis simulator for satellite hardware-in-the-loop experiments
2013-01-01 Romano, Marcello; Chesi, S.
A ballistic-pendulum test stand to characterize small cold-gas thruster nozzles
2009-01-01 C., Lugini; Romano, Marcello
Acquisition, tracking and pointing control of the Bifocal Relay Mirror Spacecraft
2003-01-01 Romano, Marcello; B. N., Agrawal
Active Attitude Control System for Small Spacecraft
2010-01-01 Romano, Marcello; Oppenheimer, P.
Ad hoc wireless networking and shared computation for autonomous multirobot systems
2009-01-01 R., Bevilacqua; J. S., Hall; J., Horning; Romano, Marcello
Advanced Methods for Astronaut Training: Computer Based Training and Virtual Reality Technology
2000-01-01 M., Bergamasco; L., Bessone; R. A., Henderson; Romano, Marcello; F., Rossito
Attitude Dynamics and Control of a Dual-Body Spacecraft Using Variable-Speed Control Moment Gyros
2004-01-01 Romano, Marcello; B. N., Agrawal
Attitude dynamics/control of dual-body spacecraft with variable-speed control moment gyros
2004-01-01 Romano, Marcello; B. N., Agrawal
Automatic Mass Balancing for Small Three-Axis Spacecraft Simulator using Sliding Masses Only
In corso di stampa Chesi, S.; Pellegrini, V.; Cristi, R.; Gong, Q.; Romano, Marcello
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
Autonomous distributed control algorithm for multiple spacecraft in close proximity operations
2007-01-01 S. B., Mccamish; Romano, Marcello; X., Yun
Autonomous Distributed Control of Simultaneous Multiple Spacecraft Proximity Maneuvers
2010-01-01 S. B., Mccamish; Romano, Marcello; X., Yun
Concise Form of the Dynamic and Kinematic Solutions of the Euler-Poinsot Problem
2012-01-01 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
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
Detumbling and nutation canceling maneuvers with complete analytic reduction for axially symmetric spacecraft
2010-01-01 Romano, Marcello
Development and experimentation of LQR/APF guidance and control for autonomous proximity maneuvers of multiple spacecraft
2011-01-01 R., Bevilacqua; T., Lehmann; 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
Exact analytic solutions for the rotation of an axially symmetric rigid body subjected to a constant torque
2008-01-01 Romano, Marcello