FERRARI, FABIO
 Distribuzione geografica
Continente #
EU - Europa 30.213
NA - Nord America 5.695
AS - Asia 3.877
SA - Sud America 532
AF - Africa 153
OC - Oceania 24
Continente sconosciuto - Info sul continente non disponibili 2
Totale 40.496
Nazione #
IT - Italia 25.253
US - Stati Uniti d'America 5.539
RU - Federazione Russa 2.820
SG - Singapore 1.268
CN - Cina 1.129
BR - Brasile 445
VN - Vietnam 428
MC - Monaco 336
GB - Regno Unito 264
KR - Corea 260
AT - Austria 210
DE - Germania 210
FR - Francia 206
IE - Irlanda 204
NL - Olanda 204
JP - Giappone 185
FI - Finlandia 120
HK - Hong Kong 113
SE - Svezia 105
ES - Italia 90
CA - Canada 85
MY - Malesia 68
PH - Filippine 62
ID - Indonesia 56
IN - India 54
BD - Bangladesh 51
MA - Marocco 50
BE - Belgio 38
MX - Messico 32
TW - Taiwan 26
AR - Argentina 25
CH - Svizzera 25
TR - Turchia 25
CI - Costa d'Avorio 23
PL - Polonia 23
ZA - Sudafrica 23
IQ - Iraq 21
AE - Emirati Arabi Uniti 20
UA - Ucraina 17
AU - Australia 16
EC - Ecuador 15
SA - Arabia Saudita 15
JO - Giordania 14
LU - Lussemburgo 14
PK - Pakistan 14
CL - Cile 13
BJ - Benin 12
PT - Portogallo 12
JM - Giamaica 11
RO - Romania 11
CO - Colombia 10
PE - Perù 10
AZ - Azerbaigian 8
CR - Costa Rica 8
DK - Danimarca 8
DZ - Algeria 8
KE - Kenya 8
TH - Thailandia 8
UZ - Uzbekistan 8
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
CZ - Repubblica Ceca 4
KH - Cambogia 4
NO - Norvegia 4
SK - Slovacchia (Repubblica Slovacca) 4
BG - Bulgaria 3
BS - Bahamas 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
PR - Porto Rico 3
PY - Paraguay 3
TN - Tunisia 3
TT - Trinidad e Tobago 3
AL - Albania 2
AO - Angola 2
BH - Bahrain 2
BY - Bielorussia 2
EU - Europa 2
GT - Guatemala 2
LB - Libano 2
LT - Lituania 2
LY - Libia 2
MO - Macao, regione amministrativa speciale della Cina 2
MU - Mauritius 2
NI - Nicaragua 2
PS - Palestinian Territory 2
SC - Seychelles 2
Totale 40.472
Città #
Milan 23.339
Ashburn 891
Singapore 739
San Jose 615
Santa Clara 455
Moscow 379
Monaco 336
Hefei 321
Chandler 302
Seoul 248
Dublin 203
Vienna 193
Council Bluffs 183
Rome 165
Tokyo 163
Dallas 157
Woodbridge 152
Beijing 141
Fairfield 138
Boardman 135
Amsterdam 129
London 123
Los Angeles 112
Wilmington 108
The Dalles 102
Ho Chi Minh City 101
Houston 95
Hanoi 89
Hong Kong 86
Lauterbourg 85
Giussano 69
Seattle 67
Kuala Lumpur 66
North Charleston 66
Ann Arbor 65
Bovisio Masciago 63
Pedrengo 62
Helsinki 60
Boltiere 58
Dong Ket 57
Buffalo 56
Turin 53
Jakarta 52
Davao City 51
New York 51
Frankfurt am Main 47
Memphis 47
Cambridge 46
Lawrence 44
Medford 42
Dearborn 41
Naples 41
São Paulo 41
Las Vegas 40
Kent 37
Redwood City 33
Robbiate 31
Shanghai 31
Pavia 30
Frisco 27
Casablanca 25
Des Moines 25
Falkenstein 25
Nuremberg 25
Ottawa 25
Bologna 24
Málaga 23
Orem 23
Abidjan 22
Chicago 22
Crema 22
Lappeenranta 22
Cercola 20
Gessate 20
Busto Arsizio 19
Redmond 19
Tucson 19
Washington 19
Bagnoli Di Sopra 18
Basingstoke 18
Busto Garolfo 18
Kenitra 18
Taipei 18
Atlanta 17
Besana in Brianza 17
Brescia 17
Da Nang 17
Guangzhou 17
Kraainem 17
Salt Lake City 17
Boulder 16
Figino 16
Montreal 16
Madrid 15
Redondo Beach 15
Warsaw 15
Amman 14
Belo Horizonte 14
Trecate 14
Charlotte 13
Totale 32.515
Nome #
Trajectory Options for Hera’s Milani CubeSat Around (65803) Didymos 877
Toward Self-Driving Interplanetary CubeSats: the ERC-Funded Project EXTREMA 778
The EXTREMA Orbital Simulation Hub: a Facility for GNC Testing of Autonomous Interplanetary CubeSat 627
The Hera Milani Cubesat Mission 621
Zodiac Pioneer: an Interplanetary Small Satellite Platform for Asteroid Reconnaissance 598
Preliminary mission profile of Hera’s Milani CubeSat 561
LUMIO Cubesat: Current Status and Lessons Learnt (so Far) 535
N-body gravitational and contact dynamics for asteroid aggregation 526
Scientific and Technological Objectives for the NavCam Payload of Hera’s Milani CubeSat to Binary Asteroid Didymos 523
A parallel-GPU code for asteroid aggregation problems with angular particles 520
The ERC-Funded EXTREMA Project: Achieving Self-Driving Interplanetary CubeSats 517
Design of the Vision-Based GNC Subsystem of Hera’s Milani Mission 500
CubeSat Landing Simulations on Small Bodies using Blender 496
Trajectory Design and Orbit Determination of Hera’s Milani CubeSat 496
Families of Bounded Orbits near Binary Asteroid 65803 Didymos 486
LUMIO: Detecting Meteoroid Impacts on the Lunar Surface 480
Mission Analysis and Navigation Assessment for Hera’s Milani CubeSat 477
Initial Trajectory Assessment of a low-thrust option for the RAMSES Mission to (99942) Apophis 459
Zodiac Pioneer: an Interplanetary Small Satellite Platform for Asteroid Reconnaissance 457
Achievement of the Planetary Defense Investigations of the Double Asteroid Redirection Test (DART) Mission 456
Characterization of the Ejecta from the NASA/DART Impact on Dimorphos: Observations and Monte Carlo Models 449
Applied Trajectory Design for CubeSat Close-Proximity Operations around Asteroids: The Milani Case 449
The Hera Milani Mission 445
The Ramses Cubesat-1 Mission to (99942) Apophis 444
Ballistic landing design on binary asteroids: the AIM case study 440
NASA’s Double Asteroid Redirection Test (DART): Mutual Orbital Period Change Due to Reshaping in the Near-Earth Binary Asteroid System (65803) Didymos 433
Suitable configurations for triangular formation flying about collinear libration points under the circular and elliptic restricted three-body problems 432
Dynamical Evolution About Asteroids with High Fidelity Gravity Field and Perturbations Modeling 430
A new method for identifying dynamical transitions in rubble-pile asteroid scenarios 425
Asteroids Coupled Dynamics Analysis by Means of Accurate Mass Distribution and Perturbations Modeling 425
Periodic motion around libration points in the Elliptic Restricted Three-Body Problem 424
Momentum Transfer from the DART Mission Kinetic Impact on Asteroid Dimorphos 420
A New Environment to Simulate the Dynamics in the Close Proximity of Rubble-Pile Asteroids 412
Nanosatellite Formation Flying to Enhance Science in Binary Asteroid Environment 404
The effect of a rocky terrain for CubeSat landing on asteroid surfaces 402
The COBRA IRIDES Experiment 398
Parameter Identification Using Microgravity Experiments on Asteroid-Related Scenarios 395
Dynamical model of binary asteroid systems through patched three-body problems 387
Successful Kinetic Impact into an Asteroid for Planetary Defense 386
The Orbital Regime Index: a Comprehensive Parameter to Determine Orbital Regions Around Minor Bodies 382
A Code for the Study of Gravitational Aggregates with Non-Spherical Particles 380
After DART: Using the First Full-scale Test of a Kinetic Impactor to Inform a Future Planetary Defense Mission 378
Asteroid Impact Monitoring Mission: Mission Analysis and Innovative Strategies for Close Proximity Maneuvering 378
Optimal Configurations for Nanosatellite Formation Flying in Binary Asteroid Environment 376
Dynamical modelling of rubble pile asteroids using data-driven techniques 374
The Dimorphos ejecta plume properties revealed by LICIACube 372
Guidance and Control design for CubeSat small body landing using discrete firings of sliding mode control 368
Fast boulder fracturing by thermal fatigue detected on stony asteroids 368
Close-Proximity Operations Concept of the Asteroid Impact Mission 367
Physical properties of asteroid Dimorphos as derived from the DART impact 365
Gas Plume Impingement Technique for Space Debris De-Tumbling 363
The Dynamical State of the Didymos System before and after the DART Impact 357
Contact dynamics investigation towards microgravity experiment for asteroid-related scenarios 355
Direct N-body Simulations of Satellite Formation around Small Asteroids: Insights from DART’s Encounter with the Didymos System 351
Ejecta from the DART-produced active asteroid Dimorphos 350
Interior of top-shaped asteroids with cohesionless surface 350
Asteroid Impact Mission: a Possible Approach to Design Effective Close Proximity Operations to Release Mascot-2 Lander 349
Coupling High Fidelity Body Modeling with Non-Keplerian Dynamics to Design Aim-Mascot-2 Landing Trajectories on Didymos Binary Asteroid 347
Modeling and Simulation of Milani CubeSat Contact Motion on the Surface of the Secondary Asteroid of Didymos Binary System 347
Morphology of ejecta features from the impact on asteroid Dimorphos 346
Assessment of GNC Impacts of Chemical Plume Impingement in the Case of Prisma Irides Experiment 345
Consolidated Phase a Design of Asteroid Impact Mission: MASCOT-2 Landing on Binary Asteroid Didymos 345
The role of fragment shapes in the simulations of asteroids as gravitational aggregates 345
Coupled Dynamics Analysis Around Asteroids by Means of Accurate Shape and Perturbations Modeling 342
Predictions for the Dynamical States of the Didymos System before and after the Planned DART Impact 341
Double Asteroid Redirection Test (DART): Structural and Dynamic Interactions between Asteroidal Elements of Binary Asteroid (65803) Didymos 341
Libration-induced Orbit Period Variations Following the DART Impact 336
Numerical Simulation of N-Body Asteroid Aggregation with GPU-Parallel Hierarchical Treecode Algorithm 335
Effects of Impact and Target Parameters on the Results of a Kinetic Impactor: Predictions for the Double Asteroid Redirection Test (DART) Mission 334
Ejecta Evolution Following a Planned Impact into an Asteroid: The First Five Weeks 331
Dynamical Evolution of the Didymos−Dimorphos Binary Asteroid as Rubble Piles following the DART Impact 330
Ejecta Formation, Early Collisional Processes, and Dynamical Evolution after the DART Impact on Dimorphos 328
Pre-encounter Predictions of DART Impact Ejecta Behavior and Observability 326
VISTA: Dust and Volatile Sensor for the ESA Hera Mission 325
Formation Flying and Relative Dynamics Under the Circular Restricted Three-Body Problem Formulation 324
The European Asteroid Impact Mission: Phase a Design and Mission Analysis 320
Trajectory Design About Binary Asteroids Through Coupled Three Body Problems 315
Design Drivers for Formation Flying Near Collinear Libration Points in the Circular and Elliptic Restricted Three-Body Problems 315
Dynamical Models for Spacecraft Landings in Low-Gravity Environments Using Polynomial Chaos 309
GRAINS: a New Numerical Method for the Study of Gravitational Aggregates 305
N-body simulations of rubble-pile aggregates with angular particles 305
Free Tumbling Objects Attitude Control via Contactless Chaser Authority Exploiting a Formation Flying Architecture 296
Formation Flying Dynamics in Circular Restricted Three-Body Problem and Applications to Binary Asteroid Systems 294
Orbital Capture of the DART Impact Ejecta Around the Didymos Binary Asteroid System 290
Numerical Simulation of N-Body Asteroid Aggregation 288
Investigating (65803) Didymos Properties and Dynamical Evolution as an N-Body System 286
Small Celestial Bodies Model Refinement by Means of N-Body Gravitational Dynamics 286
ESA’s Asteroid Impact Mission: Mission Analysis and Payload Operations State of the Art 285
Characterizing the Influence of Stochastic Forces on the Dynamics around Non-Spherical Bodies 285
Evidence for multi-fragmentation and mass shedding of boulders on rubble-pile binary asteroid system (65803) Didymos 283
The Asteroid Impact Mission: Consolidated Mission Analysis and Scientific Payload Operations at Binary Asteroid Didymos 283
Triangular Formation Flying Under the Elliptic Restricted Three-Body Problem Formulation 281
Optimization of Triangular Formation Flying Configurations Under the Circular and Elliptic Three-Body Problem Dynamics Modelling 280
Microgravity Experiments for Contact Dynamics Characterization in the Asteroid Environment 278
Global Optimization of Relative Configurations Between Spacecraft Near Lagrangian Point Orbits 272
On The Resonant Dynamics of Particles in Non-Symmetric Potentials 268
MASCOT-2 Landing Opportunities Using Three-Body Solutions for Asteroid Impact Mission 253
Elliptical ejecta of asteroid Dimorphos is due to its surface curvature 241
The Hera Space Mission in the Context of Small Near-Earth Asteroid Missions in the Past, Present and Future 226
Orbital Capture of Ejecta into Periodic Orbits around Binary Asteroid (65803) Didymos 215
Totale 38.700
Categoria #
all - tutte 203.755
article - articoli 112.961
book - libri 0
conference - conferenze 89.853
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 941
Totale 407.510


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
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
2025/202629.187 1.683 1.078 487 677 511 429 1.254 928 9.564 3.752 5.152 3.672
2026/20271.528 1.528 0 0 0 0 0 0 0 0 0 0 0
Totale 40.632