FERRARI, FABIO
 Distribuzione geografica
Continente #
EU - Europa 20.245
NA - Nord America 5.068
AS - Asia 3.764
SA - Sud America 528
AF - Africa 153
OC - Oceania 24
Continente sconosciuto - Info sul continente non disponibili 2
Totale 29.784
Nazione #
IT - Italia 15.320
US - Stati Uniti d'America 4.954
RU - Federazione Russa 2.820
SG - Singapore 1.266
CN - Cina 1.122
BR - Brasile 442
VN - Vietnam 407
MC - Monaco 336
GB - Regno Unito 262
KR - Corea 258
AT - Austria 210
DE - Germania 205
FR - Francia 205
IE - Irlanda 204
NL - Olanda 198
JP - Giappone 177
FI - Finlandia 118
HK - Hong Kong 108
SE - Svezia 105
ES - Italia 84
CA - Canada 65
PH - Filippine 62
ID - Indonesia 56
IN - India 54
MA - Marocco 50
BD - Bangladesh 45
BE - Belgio 35
MX - Messico 31
TW - Taiwan 26
TR - Turchia 25
AR - Argentina 24
CI - Costa d'Avorio 23
ZA - Sudafrica 23
CH - Svizzera 22
IQ - Iraq 21
PL - Polonia 21
AE - Emirati Arabi Uniti 19
UA - Ucraina 17
AU - Australia 16
EC - Ecuador 15
JO - Giordania 14
LU - Lussemburgo 14
PK - Pakistan 14
SA - Arabia Saudita 14
CL - Cile 13
BJ - Benin 12
PT - Portogallo 11
RO - Romania 11
CO - Colombia 10
PE - Perù 10
AZ - Azerbaigian 8
DZ - Algeria 8
KE - Kenya 8
MY - Malesia 8
TH - Thailandia 8
UZ - Uzbekistan 8
DK - Danimarca 7
GR - Grecia 7
NZ - Nuova Zelanda 7
EG - Egitto 6
HU - Ungheria 6
IR - Iran 6
IL - Israele 5
UY - Uruguay 5
VE - Venezuela 5
CR - Costa Rica 4
KH - Cambogia 4
NO - Norvegia 4
SK - Slovacchia (Repubblica Slovacca) 4
BG - Bulgaria 3
BS - Bahamas 3
CZ - Repubblica Ceca 3
EE - Estonia 3
ET - Etiopia 3
GE - Georgia 3
HN - Honduras 3
KG - Kirghizistan 3
KZ - Kazakistan 3
LV - Lettonia 3
NG - Nigeria 3
NP - Nepal 3
PY - Paraguay 3
TN - Tunisia 3
AL - Albania 2
AO - Angola 2
BH - Bahrain 2
EU - Europa 2
JM - Giamaica 2
LB - Libano 2
LY - Libia 2
MO - Macao, regione amministrativa speciale della Cina 2
MU - Mauritius 2
PR - Porto Rico 2
PS - Palestinian Territory 2
SC - Seychelles 2
SN - Senegal 2
SY - Repubblica araba siriana 2
AM - Armenia 1
BO - Bolivia 1
BY - Bielorussia 1
Totale 29.765
Città #
Milan 13.685
Ashburn 825
Singapore 737
San Jose 571
Santa Clara 434
Moscow 379
Monaco 336
Hefei 321
Chandler 301
Seoul 246
Dublin 203
Vienna 193
Tokyo 160
Dallas 153
Woodbridge 152
Council Bluffs 151
Beijing 138
Fairfield 138
Amsterdam 129
London 123
Rome 112
Wilmington 108
Los Angeles 106
The Dalles 102
Ho Chi Minh City 95
Houston 91
Boardman 88
Lauterbourg 85
Hong Kong 81
Hanoi 80
Giussano 69
North Charleston 66
Seattle 66
Ann Arbor 65
Bovisio Masciago 63
Pedrengo 62
Boltiere 58
Helsinki 58
Dong Ket 57
Buffalo 53
Jakarta 52
Davao City 51
Frankfurt am Main 47
Cambridge 46
Lawrence 44
New York 43
Medford 42
Dearborn 41
Turin 41
São Paulo 40
Las Vegas 38
Kent 37
Redwood City 33
Robbiate 31
Shanghai 31
Pavia 30
Casablanca 25
Falkenstein 25
Nuremberg 25
Ottawa 25
Des Moines 23
Málaga 23
Abidjan 22
Crema 22
Lappeenranta 22
Cercola 20
Chicago 20
Gessate 20
Naples 20
Busto Arsizio 19
Orem 19
Redmond 19
Tucson 19
Bagnoli Di Sopra 18
Basingstoke 18
Busto Garolfo 18
Kenitra 18
Taipei 18
Washington 18
Besana in Brianza 17
Bologna 17
Guangzhou 17
Kraainem 17
Salt Lake City 17
Boulder 15
Da Nang 15
Madrid 15
Redondo Beach 15
Warsaw 15
Amman 14
Belo Horizonte 14
Trecate 14
Brescia 13
Johannesburg 13
Santa Maria A Vico 13
Stockholm 13
Torino 13
Chengdu 12
Cotonou 12
Gavirate 12
Totale 22.366
Nome #
Trajectory Options for Hera’s Milani CubeSat Around (65803) Didymos 779
Toward Self-Driving Interplanetary CubeSats: the ERC-Funded Project EXTREMA 668
The EXTREMA Orbital Simulation Hub: a Facility for GNC Testing of Autonomous Interplanetary CubeSat 526
The Hera Milani Cubesat Mission 515
Zodiac Pioneer: an Interplanetary Small Satellite Platform for Asteroid Reconnaissance 499
Preliminary mission profile of Hera’s Milani CubeSat 463
LUMIO Cubesat: Current Status and Lessons Learnt (so Far) 437
N-body gravitational and contact dynamics for asteroid aggregation 433
Scientific and Technological Objectives for the NavCam Payload of Hera’s Milani CubeSat to Binary Asteroid Didymos 429
The ERC-Funded EXTREMA Project: Achieving Self-Driving Interplanetary CubeSats 417
A parallel-GPU code for asteroid aggregation problems with angular particles 411
Trajectory Design and Orbit Determination of Hera’s Milani CubeSat 402
Design of the Vision-Based GNC Subsystem of Hera’s Milani Mission 401
CubeSat Landing Simulations on Small Bodies using Blender 396
Families of Bounded Orbits near Binary Asteroid 65803 Didymos 390
LUMIO: Detecting Meteoroid Impacts on the Lunar Surface 385
Mission Analysis and Navigation Assessment for Hera’s Milani CubeSat 372
Achievement of the Planetary Defense Investigations of the Double Asteroid Redirection Test (DART) Mission 362
Zodiac Pioneer: an Interplanetary Small Satellite Platform for Asteroid Reconnaissance 358
Initial Trajectory Assessment of a low-thrust option for the RAMSES Mission to (99942) Apophis 355
Characterization of the Ejecta from the NASA/DART Impact on Dimorphos: Observations and Monte Carlo Models 352
Ballistic landing design on binary asteroids: the AIM case study 348
The Ramses Cubesat-1 Mission to (99942) Apophis 345
The Hera Milani Mission 343
Applied Trajectory Design for CubeSat Close-Proximity Operations around Asteroids: The Milani Case 343
Periodic motion around libration points in the Elliptic Restricted Three-Body Problem 338
Suitable configurations for triangular formation flying about collinear libration points under the circular and elliptic restricted three-body problems 338
Dynamical Evolution About Asteroids with High Fidelity Gravity Field and Perturbations Modeling 337
Asteroids Coupled Dynamics Analysis by Means of Accurate Mass Distribution and Perturbations Modeling 331
NASA’s Double Asteroid Redirection Test (DART): Mutual Orbital Period Change Due to Reshaping in the Near-Earth Binary Asteroid System (65803) Didymos 330
Momentum Transfer from the DART Mission Kinetic Impact on Asteroid Dimorphos 319
Nanosatellite Formation Flying to Enhance Science in Binary Asteroid Environment 314
The effect of a rocky terrain for CubeSat landing on asteroid surfaces 308
The COBRA IRIDES Experiment 308
Parameter Identification Using Microgravity Experiments on Asteroid-Related Scenarios 306
A new method for identifying dynamical transitions in rubble-pile asteroid scenarios 305
A New Environment to Simulate the Dynamics in the Close Proximity of Rubble-Pile Asteroids 299
Dynamical model of binary asteroid systems through patched three-body problems 294
Asteroid Impact Monitoring Mission: Mission Analysis and Innovative Strategies for Close Proximity Maneuvering 291
Successful Kinetic Impact into an Asteroid for Planetary Defense 286
After DART: Using the First Full-scale Test of a Kinetic Impactor to Inform a Future Planetary Defense Mission 285
Optimal Configurations for Nanosatellite Formation Flying in Binary Asteroid Environment 285
The Orbital Regime Index: a Comprehensive Parameter to Determine Orbital Regions Around Minor Bodies 284
The Dimorphos ejecta plume properties revealed by LICIACube 275
Close-Proximity Operations Concept of the Asteroid Impact Mission 275
A Code for the Study of Gravitational Aggregates with Non-Spherical Particles 275
Guidance and Control design for CubeSat small body landing using discrete firings of sliding mode control 272
Fast boulder fracturing by thermal fatigue detected on stony asteroids 271
Dynamical modelling of rubble pile asteroids using data-driven techniques 269
Physical properties of asteroid Dimorphos as derived from the DART impact 263
Asteroid Impact Mission: a Possible Approach to Design Effective Close Proximity Operations to Release Mascot-2 Lander 262
The Dynamical State of the Didymos System before and after the DART Impact 258
The role of fragment shapes in the simulations of asteroids as gravitational aggregates 258
Direct N-body Simulations of Satellite Formation around Small Asteroids: Insights from DART’s Encounter with the Didymos System 257
Ejecta from the DART-produced active asteroid Dimorphos 255
Modeling and Simulation of Milani CubeSat Contact Motion on the Surface of the Secondary Asteroid of Didymos Binary System 255
Contact dynamics investigation towards microgravity experiment for asteroid-related scenarios 253
Gas Plume Impingement Technique for Space Debris De-Tumbling 253
Double Asteroid Redirection Test (DART): Structural and Dynamic Interactions between Asteroidal Elements of Binary Asteroid (65803) Didymos 251
Consolidated Phase a Design of Asteroid Impact Mission: MASCOT-2 Landing on Binary Asteroid Didymos 251
Interior of top-shaped asteroids with cohesionless surface 250
Assessment of GNC Impacts of Chemical Plume Impingement in the Case of Prisma Irides Experiment 250
Morphology of ejecta features from the impact on asteroid Dimorphos 249
Predictions for the Dynamical States of the Didymos System before and after the Planned DART Impact 249
Coupled Dynamics Analysis Around Asteroids by Means of Accurate Shape and Perturbations Modeling 248
Coupling High Fidelity Body Modeling with Non-Keplerian Dynamics to Design Aim-Mascot-2 Landing Trajectories on Didymos Binary Asteroid 247
Numerical Simulation of N-Body Asteroid Aggregation with GPU-Parallel Hierarchical Treecode Algorithm 246
Libration-induced Orbit Period Variations Following the DART Impact 245
Ejecta Evolution Following a Planned Impact into an Asteroid: The First Five Weeks 236
Effects of Impact and Target Parameters on the Results of a Kinetic Impactor: Predictions for the Double Asteroid Redirection Test (DART) Mission 236
Pre-encounter Predictions of DART Impact Ejecta Behavior and Observability 235
Formation Flying and Relative Dynamics Under the Circular Restricted Three-Body Problem Formulation 235
Ejecta Formation, Early Collisional Processes, and Dynamical Evolution after the DART Impact on Dimorphos 234
Dynamical Evolution of the Didymos−Dimorphos Binary Asteroid as Rubble Piles following the DART Impact 232
The European Asteroid Impact Mission: Phase a Design and Mission Analysis 231
Trajectory Design About Binary Asteroids Through Coupled Three Body Problems 224
Design Drivers for Formation Flying Near Collinear Libration Points in the Circular and Elliptic Restricted Three-Body Problems 222
VISTA: Dust and Volatile Sensor for the ESA Hera Mission 220
GRAINS: a New Numerical Method for the Study of Gravitational Aggregates 212
N-body simulations of rubble-pile aggregates with angular particles 210
Dynamical Models for Spacecraft Landings in Low-Gravity Environments Using Polynomial Chaos 207
Free Tumbling Objects Attitude Control via Contactless Chaser Authority Exploiting a Formation Flying Architecture 206
Formation Flying Dynamics in Circular Restricted Three-Body Problem and Applications to Binary Asteroid Systems 203
Numerical Simulation of N-Body Asteroid Aggregation 201
The Asteroid Impact Mission: Consolidated Mission Analysis and Scientific Payload Operations at Binary Asteroid Didymos 198
Triangular Formation Flying Under the Elliptic Restricted Three-Body Problem Formulation 197
Small Celestial Bodies Model Refinement by Means of N-Body Gravitational Dynamics 195
ESA’s Asteroid Impact Mission: Mission Analysis and Payload Operations State of the Art 193
Investigating (65803) Didymos Properties and Dynamical Evolution as an N-Body System 192
Orbital Capture of the DART Impact Ejecta Around the Didymos Binary Asteroid System 191
Optimization of Triangular Formation Flying Configurations Under the Circular and Elliptic Three-Body Problem Dynamics Modelling 188
Global Optimization of Relative Configurations Between Spacecraft Near Lagrangian Point Orbits 185
Evidence for multi-fragmentation and mass shedding of boulders on rubble-pile binary asteroid system (65803) Didymos 180
Characterizing the Influence of Stochastic Forces on the Dynamics around Non-Spherical Bodies 180
On The Resonant Dynamics of Particles in Non-Symmetric Potentials 170
Microgravity Experiments for Contact Dynamics Characterization in the Asteroid Environment 169
MASCOT-2 Landing Opportunities Using Three-Body Solutions for Asteroid Impact Mission 163
Elliptical ejecta of asteroid Dimorphos is due to its surface curvature 143
Multiple moonlet mergers as the origin of the Dinkinesh-Selam system 121
Dimorphos’s Orbit Period Change and Attitude Perturbation due to Its Reshaping after the DART Impact 115
Totale 29.048
Categoria #
all - tutte 190.692
article - articoli 106.494
book - libri 0
conference - conferenze 83.391
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 807
Totale 381.384


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021189 0 0 0 0 0 0 0 0 0 21 43 125
2021/2022815 14 48 36 140 157 32 47 73 55 28 72 113
2022/20231.482 93 100 409 119 155 108 38 95 146 72 95 52
2023/2024773 37 93 28 66 56 58 99 31 75 84 48 98
2024/20254.297 343 65 197 251 777 310 180 192 459 160 278 1.085
2025/202619.998 1.683 1.078 487 677 511 429 1.254 928 9.564 3.387 0 0
Totale 29.915