ROMANO, MARCELLO
 Distribuzione geografica
Continente #
NA - Nord America 3.478
AS - Asia 3.448
EU - Europa 2.996
SA - Sud America 312
AF - Africa 69
OC - Oceania 24
Totale 10.327
Nazione #
US - Stati Uniti d'America 3.383
IT - Italia 1.448
SG - Singapore 1.076
VN - Vietnam 916
CN - Cina 428
DE - Germania 365
HK - Hong Kong 272
RU - Federazione Russa 266
BR - Brasile 230
GB - Regno Unito 213
KR - Corea 206
FR - Francia 166
IE - Irlanda 155
IN - India 116
BD - Bangladesh 103
TR - Turchia 75
BG - Bulgaria 61
CA - Canada 56
JP - Giappone 56
BE - Belgio 54
NL - Olanda 54
AR - Argentina 33
FI - Finlandia 31
TH - Thailandia 31
SE - Svezia 28
UA - Ucraina 28
AT - Austria 26
PH - Filippine 26
IQ - Iraq 23
MX - Messico 21
CI - Costa d'Avorio 20
AU - Australia 19
ES - Italia 19
CO - Colombia 18
ID - Indonesia 18
ZA - Sudafrica 18
TW - Taiwan 17
EC - Ecuador 13
DK - Danimarca 12
PT - Portogallo 12
CH - Svizzera 11
UZ - Uzbekistan 11
AE - Emirati Arabi Uniti 10
PK - Pakistan 9
PL - Polonia 9
IR - Iran 8
RO - Romania 8
MA - Marocco 7
MY - Malesia 7
AZ - Azerbaigian 6
DZ - Algeria 6
JO - Giordania 6
NZ - Nuova Zelanda 5
PE - Perù 5
CL - Cile 4
JM - Giamaica 4
KE - Kenya 4
MD - Moldavia 4
SA - Arabia Saudita 4
AM - Armenia 3
BO - Bolivia 3
CR - Costa Rica 3
EG - Egitto 3
GR - Grecia 3
IL - Israele 3
KG - Kirghizistan 3
KZ - Kazakistan 3
LT - Lituania 3
NO - Norvegia 3
NP - Nepal 3
TN - Tunisia 3
AL - Albania 2
BY - Bielorussia 2
CZ - Repubblica Ceca 2
DO - Repubblica Dominicana 2
ET - Etiopia 2
HN - Honduras 2
HU - Ungheria 2
KH - Cambogia 2
LU - Lussemburgo 2
PY - Paraguay 2
SN - Senegal 2
SY - Repubblica araba siriana 2
UY - Uruguay 2
VE - Venezuela 2
BA - Bosnia-Erzegovina 1
BB - Barbados 1
BH - Bahrain 1
BW - Botswana 1
DM - Dominica 1
EE - Estonia 1
GT - Guatemala 1
HR - Croazia 1
LA - Repubblica Popolare Democratica del Laos 1
LB - Libano 1
LK - Sri Lanka 1
LY - Libia 1
MT - Malta 1
MU - Mauritius 1
NI - Nicaragua 1
Totale 10.319
Città #
Singapore 628
Turin 476
Council Bluffs 451
San Jose 350
Chandler 247
Ho Chi Minh City 238
Hanoi 234
Ashburn 222
Santa Clara 217
Hong Kong 211
Ann Arbor 195
Princeton 189
Dublin 154
Los Angeles 135
Berlin 117
Seoul 112
Rome 102
Southend 100
Beijing 97
Milan 95
Dallas 92
Munich 84
Boardman 78
Torino 74
Houston 64
Lauterbourg 60
New York 59
Genoa 52
Istanbul 50
Da Nang 42
Haiphong 39
Buffalo 35
Savigliano 33
Nottingham 32
Orem 31
Tokyo 31
Chicago 28
Hefei 27
Seattle 26
Frankfurt am Main 25
Naples 25
Atlanta 23
Toronto 23
São Paulo 22
Bologna 21
Brussels 21
Abidjan 20
Amsterdam 19
Melle 17
Moscow 17
Cambridge 16
Vienna 16
Toulouse 15
Fairfield 14
Sydney 14
Can Tho 13
Columbus 13
Helsinki 13
Manchester 13
Nuremberg 13
Redondo Beach 13
The Dalles 13
Bangkok 12
Jakarta 12
Santa Cruz 12
Chennai 11
Guangzhou 11
Hải Dương 11
Izmir 11
San Francisco 11
Yubileyny 11
Braunschweig 10
Jacksonville 10
Mumbai 10
Baghdad 9
Biên Hòa 9
Des Moines 9
Johannesburg 9
Long Xuyen 9
Mexico City 9
Palermo 9
Tashkent 9
Trani 9
Xi'an 9
Ames 8
Bến Tre 8
Catania 8
Changsha 8
Copenhagen 8
Delft 8
Denver 8
Frisco 8
Glasgow 8
Lappeenranta 8
San Ramon 8
Stockholm 8
Verona 8
Andover 7
Ankara 7
Florence 7
Totale 6.253
Nome #
Tube-based robust model predictive control for spacecraft proximity operations in the presence of persistent disturbance 317
Dynamics and Aerodynamic Control of a Cross-Track Tether Satellite System 307
An Offline-Sampling SMPC Framework with Application to Autonomous Space Maneuvers 307
Space Robotics 295
Modeling and Experimental Parameter Identification of a Multicopter via a Compound Pendulum Test Rig 277
A Roadmap Toward a Planetary Sunshade for Space-Based Solar Geoengineering 226
Artificial Potential Field and Sliding Mode Strategies for Proximity Operations with Obstacle Avoidance 225
Spacecraft Proximity Operations Via Tube-Based Robust Model Predictive Control with Additive Disturbances 221
Lunar Wireless power transmission: key subsystems for a constellation of laser energy-transmitting satellites 220
Attitude Control of a Small Spacecraft for Earth Observation via Tube-based Robust Model Predictive Control 204
Extended Reality for Space and Astronautical Engineering Applications 202
New Results on the Mass/Cost-Optimization Analysis of a Planetary Sunshade System 191
Modeling and Analysis of Tethered System Dynamics for Venus Aerobots and Towed Probes 183
Development and Experimentation of a CubeSat Magnetic Attitude Control System Testbed 168
Development of a tip-tilt air-bearing testbed for physically emulating proximity-flight orbital mechanics 166
Planetary Sunshade for Solar Geoengineering: Preliminary Design of a Precursor System and Mission 165
Angularly Unbounded Three-Axis Spacecraft Simulator 162
Attitude stabilization of spacecraft in very low earth orbit by center-of-mass shifting 161
Low-Thrust Propulsion and Drift Orbit Optimization for Multi-Client Servicing Missions in Low Earth Orbit 158
A convex-programming-based guidance algorithm to capture a tumbling object on orbit using a spacecraft equipped with a robotic manipulator 157
A distributed space radar sounder using a cross-track flying tethered satellite system 155
Equilibrium-Based Force and Torque Control for an Aerial Manipulator to Interact with a Vertical Surface 142
Rendezvous maneuvers of multiple spacecraft using differential drag under J2 perturbation 142
Planetary sunshade for solar geoengineering: Preliminary design of a precursor system and mission 141
Orbital hopping maneuvers with Astrobee on-board the International Space Station 139
Hardware-in-the-Loop Testing of Spacecraft Relative Dynamics and Tethered Satellite System on a Tip-Tilt Flat-Table Facility 136
Gravity-gradient effects on the rotational mechanics of a satellite in near-rectilinear halo orbits 130
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 121
Development and experimental validation of a multi-algorithmic hybrid attitude determination and control system for a small satellite 121
Exact analytic solution for the rotation of a rigid body having spherical ellipsoid of inertia and subjected to a constant torque 118
Survey And Comparison Of In-Space And In-Atmosphere Geoengineering Concepts For Climate Change Mitigation 117
Characterization of a shape memory alloy interference coupling 117
Orbital hopping maneuvers with two Astrobee free-flyers: Ground and flight experiments 115
Space Sustainability in LEO: a multidisciplinary approach to identify and mitigate economic, operational and technological risks of active debris removal solutions. 115
Optimal Multi-Client Trajectory Planning for A Low-Thrust Servicing Satellite in the Presence of Perturbations 113
Equations of Motion of Free-Floating Spacecraft-Manipulator Systems: An Engineer's Tutorial 112
On-orbit Demonstration of Spacecraft Hopping Maneuvers using the NASA Astrobee Free-Flyers 111
Development and experimentation of LQR/APF guidance and control for autonomous proximity maneuvers of multiple spacecraft 111
A ballistic-pendulum test stand to characterize small cold-gas thruster nozzles 111
Real-Time Autonomous Spacecraft Proximity Maneuvers and Docking Using an Adaptive Artificial Potential Field Approach 110
Laboratory Experimentation of Autonomous Spacecraft Approach and Docking to a Collaborative Target 108
Optimal low-thrust orbital transfer for servicing multiple satellites in elliptical orbits 107
Orbital Capacity and Maximum Potential Energy Output for a Space-Based Solar Power Constellation. 106
Dynamic Air-Bearing Hardware-in-the-Loop Testbed to Experimentally Evaluate Autonomous Spacecraft Proximity Maneuvers 104
Attitude Dynamics/Control of a Dual-Body Spacecraft with Variable-Speed Control Moment Gyros 103
Automatic Mass Balancing of a Spacecraft Three-Axis Simulator: Analysis and Experimentation 102
Decoupled-natural-dynamics model for the relative motion of two spacecraft without and with J2 perturbation 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 99
Optimal Rendezvous Trajectories of a Controlled Spacecraft and a Tumbling Object 95
Ad Hoc Wireless Networking and Shared Computation for Autonomous Multirobot Systems 95
Time-optimal control of linear time invariant systems between two arbitrary states 94
Reachability Analysis of Planar Spacecraft Docking with Rotating Body in Close Proximity 94
Simultaneous capture and detumble of a resident space object by a free-flying spacecraft-manipulator system 93
Aerodynamic Three-Axis Attitude Stabilization of a Spacecraft by Center-of-Mass Shifting 93
Simulations of Multiple Spacecraft Maneuvering with MATLAB/Simulink and Satellite Tool Kit 91
Autonomous distributed control of simultaneous multiple spacecraft proximity maneuvers 91
Emulating Scaled Clohessy–Wiltshire Dynamics on an Air-Bearing Spacecraft Simulation Testbed 91
Model Predictive Control of Spacecraft Relative Motion with Convexified Keep-Out-Zone Constraints 90
A new form of osculating Keplerian approximation of N-Body non-Keplerian motion for the design of GNC algorithms. 89
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
Trajectory Optimization for Low-Thrust Multi-Platform Servicing Missions in Elliptical Orbits: A Fourier-Based Approach 87
New Families of Halo Orbits about the Photo-Gravitational Equilibrium between Sun and the Earth-Moon System for Planetary Sunshade Missions 87
A Conceptual Framework for Climate Change Mitigation Actions Employing In-Space Geoengineering 87
Exact analytic solution for the spin-up maneuver of an axially symmetric spacecraft 83
An updated re-entry analysis of the Hubble Space Telescope 82
Laboratory experiments of resident space object capture by a spacecraft–manipulator system 79
Orbital Logistics: Optimal Planning to Service Multiple Satellites in LEO through Mixed Integer Linear Programming and Q-law 77
Online generation of quasi-optimal spacecraft rendezvous trajectories 77
Rendezvous Maneuvers of Multiple Spacecraft Using Differential Drag Under J2 Perturbation 76
Exact analytic solutions for the rotation of an axially symmetric rigid body subjected to a constant torque 75
Fast and Near-Optimal Guidance for Docking to Uncontrolled Spacecraft 71
Experimental Characterization of Inverse Dynamics Guidance in Docking with a Rotating Target 70
Request-Centric Modeling and Architecture Optimization for Earth–Moon Space Logistics 69
Survey, Statistical Analysis and Classification of Launched CubeSat Missions with Emphasis on the Attitude Control Method 69
Experimental evaluation of model predictive control and inverse dynamics control for spacecraft proximity and docking maneuvers 69
Spacecraft Thruster Control via Sigma–Delta Modulation 68
Multiple spacecraft rendezvous maneuvers by differential drag and low thrust engines 68
A near-optimal guidance for cooperative docking maneuvers 68
Lyapunov-Based Thrusters' Selection for Spacecraft Control: Analysis and Experimentation 67
Performance evaluation of the inverse dynamics method for optimal spacecraft reorientation 66
Flight Testing of Multiple-Spacecraft Control on SPHERES During Close-Proximity Operations 63
Time-Optimal Reorientation of a Spacecraft Using an Inverse Dynamics Optimization Method 63
Low-Thrust Propulsion and Drift Orbit Optimization for Multi-Client Servicing Missions in Low Earth Orbit 29
A Cost-Benefit Analysis of a Tethered Satellite System for Climate Change Monitoring in Very Low Earth Orbit 29
Lyapunov-Based Low-Thrust Control and Stabilization of a Tethered Satellite System in Arbitrary Attitude Configurations 28
Tethered Satellite System for Cross-Track Formation Flying: Architecture and Performance Analysis 26
Satellite Cross-track Tethered Satellite System in LEO/VLEO: Mission Characterization and Design Analysis 20
An Aerodynamically Controlled Cross-track Tethered CubeSat System for Remote Sensing Applications 14
Dynamics of Gyroscopic Stabilized Tether Satellite System in LEO 13
A Novel Radar Remote Sensing Orbiting System Using Tethered Satellites 11
Satellite Shape Optimization for Maximum Lift over Drag Ratio in LEO and VLEO 11
null 10
Modeling and Real-Time Simulation of Spacecraft Berthing: Orbital Dynamics and Lumped Parameter Systems in Proximity Operations 9
Totale 10.734
Categoria #
all - tutte 34.550
article - articoli 23.860
book - libri 0
conference - conferenze 9.572
curatela - curatele 0
other - altro 0
patent - brevetti 484
selected - selezionate 0
volume - volumi 634
Totale 69.100


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20217 0 0 0 0 0 0 0 0 0 0 0 7
2021/2022795 7 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
2025/20265.433 211 248 289 518 376 249 758 405 1.131 686 296 266
Totale 10.734