ROMANO, MARCELLO
 Distribuzione geografica
Continente #
AS - Asia 3.335
NA - Nord America 3.203
EU - Europa 2.891
SA - Sud America 310
AF - Africa 69
OC - Oceania 23
Totale 9.831
Nazione #
US - Stati Uniti d'America 3.124
IT - Italia 1.381
SG - Singapore 1.068
VN - Vietnam 916
CN - Cina 416
DE - Germania 357
HK - Hong Kong 271
RU - Federazione Russa 266
BR - Brasile 229
KR - Corea 206
GB - Regno Unito 195
FR - Francia 166
IE - Irlanda 155
IN - India 114
TR - Turchia 75
BG - Bulgaria 61
JP - Giappone 54
BE - Belgio 53
NL - Olanda 46
CA - Canada 44
AR - Argentina 33
FI - Finlandia 31
TH - Thailandia 31
UA - Ucraina 28
AT - Austria 26
PH - Filippine 26
SE - Svezia 26
IQ - Iraq 23
CI - Costa d'Avorio 20
MX - Messico 20
AU - Australia 18
CO - Colombia 18
ES - Italia 18
ID - Indonesia 18
ZA - Sudafrica 18
TW - Taiwan 17
BD - Bangladesh 16
DK - Danimarca 12
EC - Ecuador 12
PT - Portogallo 12
CH - Svizzera 11
AE - Emirati Arabi Uniti 10
UZ - Uzbekistan 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
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
JM - Giamaica 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
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
HN - Honduras 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
PA - Panama 1
Totale 9.824
Città #
Singapore 627
Turin 462
Council Bluffs 413
San Jose 295
Chandler 247
Ho Chi Minh City 238
Hanoi 234
Santa Clara 213
Hong Kong 210
Ashburn 199
Ann Arbor 195
Princeton 189
Dublin 154
Los Angeles 122
Berlin 117
Seoul 112
Southend 100
Beijing 95
Milan 94
Rome 94
Dallas 86
Munich 80
Torino 74
Boardman 66
Houston 61
Lauterbourg 60
Genoa 51
Istanbul 50
New York 49
Da Nang 42
Haiphong 39
Savigliano 32
Tokyo 31
Buffalo 30
Orem 30
Hefei 27
Seattle 26
Chicago 23
Nottingham 23
São Paulo 22
Brussels 21
Frankfurt am Main 21
Abidjan 20
Atlanta 20
Naples 19
Toronto 19
Bologna 18
Amsterdam 17
Melle 17
Moscow 17
Vienna 16
Cambridge 15
Toulouse 15
Fairfield 14
Sydney 14
Can Tho 13
Helsinki 13
Nuremberg 13
Redondo Beach 13
Bangkok 12
Columbus 12
Jakarta 12
Santa Cruz 12
The Dalles 12
Chennai 11
Guangzhou 11
Hải Dương 11
Izmir 11
Manchester 11
Yubileyny 11
Braunschweig 10
Mumbai 10
Baghdad 9
Biên Hòa 9
Des Moines 9
Jacksonville 9
Johannesburg 9
Long Xuyen 9
Trani 9
Xi'an 9
Ames 8
Bến Tre 8
Copenhagen 8
Denver 8
Lappeenranta 8
Mexico City 8
Palermo 8
San Francisco 8
San Ramon 8
Stockholm 8
Tashkent 8
Andover 7
Ankara 7
Catania 7
Fremont 7
Gainesville 7
Harbin 7
Hartford 7
Lisbon 7
Menlo Park 7
Totale 5.996
Nome #
Tube-based robust model predictive control for spacecraft proximity operations in the presence of persistent disturbance 313
Dynamics and Aerodynamic Control of a Cross-Track Tether Satellite System 304
An Offline-Sampling SMPC Framework with Application to Autonomous Space Maneuvers 302
Space Robotics 293
Modeling and Experimental Parameter Identification of a Multicopter via a Compound Pendulum Test Rig 277
Artificial Potential Field and Sliding Mode Strategies for Proximity Operations with Obstacle Avoidance 224
Spacecraft Proximity Operations Via Tube-Based Robust Model Predictive Control with Additive Disturbances 221
Attitude Control of a Small Spacecraft for Earth Observation via Tube-based Robust Model Predictive Control 204
Modeling and Analysis of Tethered System Dynamics for Venus Aerobots and Towed Probes 175
New Results on the Mass/Cost-Optimization Analysis of a Planetary Sunshade System 173
Extended Reality for Space and Astronautical Engineering Applications 171
Development and Experimentation of a CubeSat Magnetic Attitude Control System Testbed 166
Development of a tip-tilt air-bearing testbed for physically emulating proximity-flight orbital mechanics 164
A Roadmap Toward a Planetary Sunshade for Space-Based Solar Geoengineering 163
Planetary Sunshade for Solar Geoengineering: Preliminary Design of a Precursor System and Mission 162
Attitude stabilization of spacecraft in very low earth orbit by center-of-mass shifting 161
Angularly Unbounded Three-Axis Spacecraft Simulator 160
A convex-programming-based guidance algorithm to capture a tumbling object on orbit using a spacecraft equipped with a robotic manipulator 156
A distributed space radar sounder using a cross-track flying tethered satellite system 152
Low-Thrust Propulsion and Drift Orbit Optimization for Multi-Client Servicing Missions in Low Earth Orbit 147
Lunar Wireless power transmission: key subsystems for a constellation of laser energy-transmitting satellites 147
Equilibrium-Based Force and Torque Control for an Aerial Manipulator to Interact with a Vertical Surface 141
Orbital hopping maneuvers with Astrobee on-board the International Space Station 135
Planetary sunshade for solar geoengineering: Preliminary design of a precursor system and mission 132
Rendezvous maneuvers of multiple spacecraft using differential drag under J2 perturbation 132
Hardware-in-the-Loop Testing of Spacecraft Relative Dynamics and Tethered Satellite System on a Tip-Tilt Flat-Table Facility 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 117
Characterization of a shape memory alloy interference coupling 117
Gravity-gradient effects on the rotational mechanics of a satellite in near-rectilinear halo orbits 115
Orbital hopping maneuvers with two Astrobee free-flyers: Ground and flight experiments 114
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
Survey And Comparison Of In-Space And In-Atmosphere Geoengineering Concepts For Climate Change Mitigation 110
A ballistic-pendulum test stand to characterize small cold-gas thruster nozzles 110
Optimal Multi-Client Trajectory Planning for A Low-Thrust Servicing Satellite in the Presence of Perturbations 109
Space Sustainability in LEO: a multidisciplinary approach to identify and mitigate economic, operational and technological risks of active debris removal solutions. 109
Development and experimentation of LQR/APF guidance and control for autonomous proximity maneuvers of multiple spacecraft 109
Real-Time Autonomous Spacecraft Proximity Maneuvers and Docking Using an Adaptive Artificial Potential Field Approach 109
Laboratory Experimentation of Autonomous Spacecraft Approach and Docking to a Collaborative Target 106
Optimal low-thrust orbital transfer for servicing multiple satellites in elliptical orbits 105
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 102
Orbital Capacity and Maximum Potential Energy Output for a Space-Based Solar Power Constellation. 100
Automatic Mass Balancing of a Spacecraft Three-Axis Simulator: Analysis and Experimentation 100
Decoupled-natural-dynamics model for the relative motion of two spacecraft without and with J2 perturbation 99
Historical survey of kinematic and dynamic spacecraft simulators for laboratory experimentation of on-orbit proximity maneuvers 99
Experiments on Command Shaping Control of a Manipulator with Flexible Links 97
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 95
Optimal Rendezvous Trajectories of a Controlled Spacecraft and a Tumbling Object 95
Ad Hoc Wireless Networking and Shared Computation for Autonomous Multirobot Systems 95
Reachability Analysis of Planar Spacecraft Docking with Rotating Body in Close Proximity 94
Time-optimal control of linear time invariant systems between two arbitrary states 93
Simultaneous capture and detumble of a resident space object by a free-flying spacecraft-manipulator system 92
Simulations of Multiple Spacecraft Maneuvering with MATLAB/Simulink and Satellite Tool Kit 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
Autonomous distributed control of simultaneous multiple spacecraft proximity maneuvers 90
Aerodynamic Three-Axis Attitude Stabilization of a Spacecraft by Center-of-Mass Shifting 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 87
A new form of osculating Keplerian approximation of N-Body non-Keplerian motion for the design of GNC algorithms. 83
A Conceptual Framework for Climate Change Mitigation Actions Employing In-Space Geoengineering 82
Exact analytic solution for the spin-up maneuver of an axially symmetric spacecraft 82
An updated re-entry analysis of the Hubble Space Telescope 80
Laboratory experiments of resident space object capture by a spacecraft–manipulator system 79
Rendezvous Maneuvers of Multiple Spacecraft Using Differential Drag Under J2 Perturbation 76
Online generation of quasi-optimal spacecraft rendezvous trajectories 76
Exact analytic solutions for the rotation of an axially symmetric rigid body subjected to a constant torque 75
New Families of Halo Orbits about the Photo-Gravitational Equilibrium between Sun and the Earth-Moon System for Planetary Sunshade Missions 73
Fast and Near-Optimal Guidance for Docking to Uncontrolled Spacecraft 71
Experimental Characterization of Inverse Dynamics Guidance in Docking with a Rotating Target 70
Experimental evaluation of model predictive control and inverse dynamics control for spacecraft proximity and docking maneuvers 69
Orbital Logistics: Optimal Planning to Service Multiple Satellites in LEO through Mixed Integer Linear Programming and Q-law 68
Request-Centric Modeling and Architecture Optimization for Earth–Moon Space Logistics 68
Spacecraft Thruster Control via Sigma–Delta Modulation 68
A near-optimal guidance for cooperative docking maneuvers 68
Survey, Statistical Analysis and Classification of Launched CubeSat Missions with Emphasis on the Attitude Control Method 68
Trajectory Optimization for Low-Thrust Multi-Platform Servicing Missions in Elliptical Orbits: A Fourier-Based Approach 67
Multiple spacecraft rendezvous maneuvers by differential drag and low thrust engines 67
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
A Cost-Benefit Analysis of a Tethered Satellite System for Climate Change Monitoring in Very Low Earth Orbit 19
Tethered Satellite System for Cross-Track Formation Flying: Architecture and Performance Analysis 18
Low-Thrust Propulsion and Drift Orbit Optimization for Multi-Client Servicing Missions in Low Earth Orbit 16
Lyapunov-Based Low-Thrust Control and Stabilization of a Tethered Satellite System in Arbitrary Attitude Configurations 14
Satellite Cross-track Tethered Satellite System in LEO/VLEO: Mission Characterization and Design Analysis 12
An Aerodynamically Controlled Cross-track Tethered CubeSat System for Remote Sensing Applications 11
null 10
A Novel Radar Remote Sensing Orbiting System Using Tethered Satellites 9
Satellite Shape Optimization for Maximum Lift over Drag Ratio in LEO and VLEO 8
Dynamics of Gyroscopic Stabilized Tether Satellite System in LEO 6
Totale 10.235
Categoria #
all - tutte 32.053
article - articoli 22.841
book - libri 0
conference - conferenze 8.124
curatela - curatele 0
other - altro 0
patent - brevetti 471
selected - selezionate 0
volume - volumi 617
Totale 64.106


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/202120 0 0 0 0 0 0 0 0 0 0 13 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
2025/20264.934 211 248 289 518 376 249 758 405 1.131 686 63 0
Totale 10.235