ROMANO, MARCELLO
 Distribuzione geografica
Continente #
NA - Nord America 3.794
AS - Asia 3.560
EU - Europa 3.150
Continente sconosciuto - Info sul continente non disponibili 407
SA - Sud America 329
AF - Africa 69
OC - Oceania 24
Totale 11.333
Nazione #
US - Stati Uniti d'America 3.668
IT - Italia 1.554
SG - Singapore 1.116
VN - Vietnam 917
CN - Cina 436
DE - Germania 372
HK - Hong Kong 277
RU - Federazione Russa 266
BR - Brasile 244
GB - Regno Unito 214
KR - Corea 206
FR - Francia 176
BD - Bangladesh 155
IE - Irlanda 155
IN - India 116
TR - Turchia 75
CA - Canada 69
BE - Belgio 62
BG - Bulgaria 62
NL - Olanda 62
JP - Giappone 56
AR - Argentina 33
SE - Svezia 33
FI - Finlandia 31
TH - Thailandia 31
UA - Ucraina 29
PH - Filippine 27
AT - Austria 26
IQ - Iraq 23
ES - Italia 21
MX - Messico 21
CI - Costa d'Avorio 20
CO - Colombia 20
AU - Australia 19
ID - Indonesia 19
ZA - Sudafrica 18
TW - Taiwan 17
EC - Ecuador 14
DK - Danimarca 13
PT - Portogallo 12
CH - Svizzera 11
IR - Iran 11
UZ - Uzbekistan 11
AE - Emirati Arabi Uniti 10
JM - Giamaica 9
PK - Pakistan 9
PL - Polonia 9
MY - Malesia 8
RO - Romania 8
MA - Marocco 7
AZ - Azerbaigian 6
DZ - Algeria 6
JO - Giordania 6
CR - Costa Rica 5
NZ - Nuova Zelanda 5
PE - Perù 5
CL - Cile 4
GT - Guatemala 4
KE - Kenya 4
MD - Moldavia 4
SA - Arabia Saudita 4
AM - Armenia 3
BO - Bolivia 3
EE - Estonia 3
EG - Egitto 3
GR - Grecia 3
HN - Honduras 3
IL - Israele 3
KG - Kirghizistan 3
KZ - Kazakistan 3
LT - Lituania 3
NO - Norvegia 3
NP - Nepal 3
TN - Tunisia 3
TT - Trinidad e Tobago 3
AL - Albania 2
BY - Bielorussia 2
CZ - Repubblica Ceca 2
DO - Repubblica Dominicana 2
ET - Etiopia 2
HU - Ungheria 2
KH - Cambogia 2
LU - Lussemburgo 2
LV - Lettonia 2
NI - Nicaragua 2
PY - Paraguay 2
SN - Senegal 2
SY - Repubblica araba siriana 2
UY - Uruguay 2
VE - Venezuela 2
VI - Stati Uniti Isole Vergini 2
BA - Bosnia-Erzegovina 1
BB - Barbados 1
BH - Bahrain 1
BW - Botswana 1
DM - Dominica 1
GP - Guadalupe 1
HR - Croazia 1
LA - Repubblica Popolare Democratica del Laos 1
LB - Libano 1
Totale 10.914
Città #
Singapore 630
Turin 490
Council Bluffs 452
San Jose 365
Ashburn 281
Chandler 247
Ho Chi Minh City 239
Hanoi 234
Santa Clara 227
Hong Kong 213
Ann Arbor 195
Princeton 189
Dublin 154
Los Angeles 140
Milan 136
Berlin 117
Rome 117
Seoul 112
Southend 100
Beijing 98
Dallas 98
Munich 85
Boardman 78
Torino 74
New York 70
Houston 64
Lauterbourg 60
Genoa 52
Istanbul 50
Da Nang 42
Haiphong 39
Buffalo 36
Savigliano 33
Nottingham 32
Orem 31
Tokyo 31
Chicago 30
Frankfurt am Main 30
Toronto 29
Atlanta 28
Seattle 28
Hefei 27
Naples 27
Toulouse 23
Brussels 22
São Paulo 22
Bologna 21
Abidjan 20
Amsterdam 19
Melle 19
Cambridge 18
Campinas 17
Moscow 17
Vienna 16
Columbus 14
Fairfield 14
Sydney 14
Can Tho 13
Helsinki 13
Jakarta 13
Manchester 13
Nuremberg 13
Redondo Beach 13
San Francisco 13
The Dalles 13
Bangkok 12
Delft 12
Santa Cruz 12
Chennai 11
Denver 11
Guangzhou 11
Hải Dương 11
Izmir 11
Palermo 11
Yubileyny 11
Braunschweig 10
Frisco 10
Jacksonville 10
Mumbai 10
Washington 10
Baghdad 9
Biên Hòa 9
Des Moines 9
Johannesburg 9
Long Xuyen 9
Mexico City 9
Stockholm 9
Tashkent 9
Trani 9
Xi'an 9
Ames 8
Bến Tre 8
Catania 8
Changsha 8
Charlotte 8
Copenhagen 8
Glasgow 8
Lappeenranta 8
San Ramon 8
Verona 8
Totale 6.503
Nome #
Tube-based robust model predictive control for spacecraft proximity operations in the presence of persistent disturbance 331
A Roadmap Toward a Planetary Sunshade for Space-Based Solar Geoengineering 319
Dynamics and Aerodynamic Control of a Cross-Track Tether Satellite System 316
An Offline-Sampling SMPC Framework with Application to Autonomous Space Maneuvers 315
Space Robotics 296
Modeling and Experimental Parameter Identification of a Multicopter via a Compound Pendulum Test Rig 278
Lunar Wireless power transmission: key subsystems for a constellation of laser energy-transmitting satellites 246
Artificial Potential Field and Sliding Mode Strategies for Proximity Operations with Obstacle Avoidance 226
Spacecraft Proximity Operations Via Tube-Based Robust Model Predictive Control with Additive Disturbances 222
Extended Reality for Space and Astronautical Engineering Applications 220
Attitude Control of a Small Spacecraft for Earth Observation via Tube-based Robust Model Predictive Control 205
New Results on the Mass/Cost-Optimization Analysis of a Planetary Sunshade System 202
Modeling and Analysis of Tethered System Dynamics for Venus Aerobots and Towed Probes 189
Planetary Sunshade for Solar Geoengineering: Preliminary Design of a Precursor System and Mission 177
Planetary sunshade for solar geoengineering: Preliminary design of a precursor system and mission 172
Development and Experimentation of a CubeSat Magnetic Attitude Control System Testbed 169
Low-Thrust Propulsion and Drift Orbit Optimization for Multi-Client Servicing Missions in Low Earth Orbit 168
Development of a tip-tilt air-bearing testbed for physically emulating proximity-flight orbital mechanics 168
Angularly Unbounded Three-Axis Spacecraft Simulator 166
Attitude stabilization of spacecraft in very low earth orbit by center-of-mass shifting 163
A convex-programming-based guidance algorithm to capture a tumbling object on orbit using a spacecraft equipped with a robotic manipulator 158
A distributed space radar sounder using a cross-track flying tethered satellite system 157
Rendezvous maneuvers of multiple spacecraft using differential drag under J2 perturbation 153
Hardware-in-the-Loop Testing of Spacecraft Relative Dynamics and Tethered Satellite System on a Tip-Tilt Flat-Table Facility 149
Equilibrium-Based Force and Torque Control for an Aerial Manipulator to Interact with a Vertical Surface 145
Orbital hopping maneuvers with Astrobee on-board the International Space Station 144
Gravity-gradient effects on the rotational mechanics of a satellite in near-rectilinear halo orbits 143
New Families of Halo Orbits about the Photo-Gravitational Equilibrium in the Sun-Earth-Moon System’s Center of Mass Elliptic Restricted Three-Body Problem for Planetary Sunshade Missions 141
Space Sustainability in LEO: a multidisciplinary approach to identify and mitigate economic, operational and technological risks of active debris removal solutions. 124
Development and experimental validation of a multi-algorithmic hybrid attitude determination and control system for a small satellite 123
Survey And Comparison Of In-Space And In-Atmosphere Geoengineering Concepts For Climate Change Mitigation 122
Exact analytic solution for the rotation of a rigid body having spherical ellipsoid of inertia and subjected to a constant torque 122
Equations of Motion of Free-Floating Spacecraft-Manipulator Systems: An Engineer's Tutorial 120
Characterization of a shape memory alloy interference coupling 119
Orbital hopping maneuvers with two Astrobee free-flyers: Ground and flight experiments 117
Optimal Multi-Client Trajectory Planning for A Low-Thrust Servicing Satellite in the Presence of Perturbations 117
Real-Time Autonomous Spacecraft Proximity Maneuvers and Docking Using an Adaptive Artificial Potential Field Approach 116
Development and experimentation of LQR/APF guidance and control for autonomous proximity maneuvers of multiple spacecraft 115
Orbital Capacity and Maximum Potential Energy Output for a Space-Based Solar Power Constellation. 114
A ballistic-pendulum test stand to characterize small cold-gas thruster nozzles 114
On-orbit Demonstration of Spacecraft Hopping Maneuvers using the NASA Astrobee Free-Flyers 112
Laboratory Experimentation of Autonomous Spacecraft Approach and Docking to a Collaborative Target 111
Optimal low-thrust orbital transfer for servicing multiple satellites in elliptical orbits 110
Dynamic Air-Bearing Hardware-in-the-Loop Testbed to Experimentally Evaluate Autonomous Spacecraft Proximity Maneuvers 109
Decoupled-natural-dynamics model for the relative motion of two spacecraft without and with J2 perturbation 105
Automatic Mass Balancing of a Spacecraft Three-Axis Simulator: Analysis and Experimentation 104
Attitude Dynamics/Control of a Dual-Body Spacecraft with Variable-Speed Control Moment Gyros 104
A new form of osculating Keplerian approximation of N-Body non-Keplerian motion for the design of GNC algorithms. 101
Historical survey of kinematic and dynamic spacecraft simulators for laboratory experimentation of on-orbit proximity maneuvers 101
Experiments on Command Shaping Control of a Manipulator with Flexible Links 100
Reachability Analysis of Planar Spacecraft Docking with Rotating Body in Close Proximity 98
Optimal Rendezvous Trajectories of a Controlled Spacecraft and a Tumbling Object 97
New Families of Halo Orbits about the Photo-Gravitational Equilibrium between Sun and the Earth-Moon System for Planetary Sunshade Missions 96
Time-optimal control of linear time invariant systems between two arbitrary states 96
Aerodynamic Three-Axis Attitude Stabilization of a Spacecraft by Center-of-Mass Shifting 96
Ad Hoc Wireless Networking and Shared Computation for Autonomous Multirobot Systems 96
Simulations of Multiple Spacecraft Maneuvering with MATLAB/Simulink and Satellite Tool Kit 93
Simultaneous capture and detumble of a resident space object by a free-flying spacecraft-manipulator system 93
Autonomous distributed control of simultaneous multiple spacecraft proximity maneuvers 93
Emulating Scaled Clohessy–Wiltshire Dynamics on an Air-Bearing Spacecraft Simulation Testbed 93
Trajectory Optimization for Low-Thrust Multi-Platform Servicing Missions in Elliptical Orbits: A Fourier-Based Approach 92
Model Predictive Control of Spacecraft Relative Motion with Convexified Keep-Out-Zone Constraints 91
An updated re-entry analysis of the Hubble Space Telescope 91
A Conceptual Framework for Climate Change Mitigation Actions Employing In-Space Geoengineering 90
Detumbling and nutation canceling maneuvers with complete analytic reduction for axially symmetric spacecraft 89
Fuel-Optimal Spacecraft Rendezvous with Hybrid On-Off Continuous and Impulsive Thrust 88
Exact analytic solution for the spin-up maneuver of an axially symmetric spacecraft 87
Orbital Logistics: Optimal Planning to Service Multiple Satellites in LEO through Mixed Integer Linear Programming and Q-law 86
Laboratory experiments of resident space object capture by a spacecraft–manipulator system 83
Online generation of quasi-optimal spacecraft rendezvous trajectories 79
Exact analytic solutions for the rotation of an axially symmetric rigid body subjected to a constant torque 78
Request-Centric Modeling and Architecture Optimization for Earth–Moon Space Logistics 77
Rendezvous Maneuvers of Multiple Spacecraft Using Differential Drag Under J2 Perturbation 77
Fast and Near-Optimal Guidance for Docking to Uncontrolled Spacecraft 73
Multiple spacecraft rendezvous maneuvers by differential drag and low thrust engines 71
Experimental Characterization of Inverse Dynamics Guidance in Docking with a Rotating Target 71
A near-optimal guidance for cooperative docking maneuvers 70
Survey, Statistical Analysis and Classification of Launched CubeSat Missions with Emphasis on the Attitude Control Method 70
Experimental evaluation of model predictive control and inverse dynamics control for spacecraft proximity and docking maneuvers 70
Performance evaluation of the inverse dynamics method for optimal spacecraft reorientation 69
Spacecraft Thruster Control via Sigma–Delta Modulation 69
Lyapunov-Based Thrusters' Selection for Spacecraft Control: Analysis and Experimentation 69
Flight Testing of Multiple-Spacecraft Control on SPHERES During Close-Proximity Operations 64
Time-Optimal Reorientation of a Spacecraft Using an Inverse Dynamics Optimization Method 64
A Cost-Benefit Analysis of a Tethered Satellite System for Climate Change Monitoring in Very Low Earth Orbit 61
Low-Thrust Propulsion and Drift Orbit Optimization for Multi-Client Servicing Missions in Low Earth Orbit 42
Tethered Satellite System for Cross-Track Formation Flying: Architecture and Performance Analysis 39
Lyapunov-Based Low-Thrust Control and Stabilization of a Tethered Satellite System in Arbitrary Attitude Configurations 32
Satellite Cross-track Tethered Satellite System in LEO/VLEO: Mission Characterization and Design Analysis 28
Modeling and Real-Time Simulation of Spacecraft Berthing: Orbital Dynamics and Lumped Parameter Systems in Proximity Operations 25
A Novel Radar Remote Sensing Orbiting System Using Tethered Satellites 17
An Aerodynamically Controlled Cross-track Tethered CubeSat System for Remote Sensing Applications 16
Dynamics of Gyroscopic Stabilized Tether Satellite System in LEO 14
Satellite Shape Optimization for Maximum Lift over Drag Ratio in LEO and VLEO 12
null 10
Totale 11.333
Categoria #
all - tutte 37.490
article - articoli 25.067
book - libri 0
conference - conferenze 11.279
curatela - curatele 0
other - altro 0
patent - brevetti 497
selected - selezionate 0
volume - volumi 647
Totale 74.980


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022788 0 2 8 5 6 15 5 7 11 14 475 240
2022/20231.158 161 169 36 135 116 137 73 85 143 18 59 26
2023/2024949 41 318 109 71 45 52 18 24 88 51 64 68
2024/20251.832 93 242 115 198 133 140 132 143 233 102 110 191
2025/20265.608 211 248 289 518 376 249 758 405 1.131 686 296 441
2026/2027424 347 77 0 0 0 0 0 0 0 0 0 0
Totale 11.333