FERRARI, FABIO
 Distribuzione geografica
Continente #
EU - Europa 4.432
NA - Nord America 2.673
AS - Asia 862
SA - Sud America 88
AF - Africa 35
OC - Oceania 15
Continente sconosciuto - Info sul continente non disponibili 2
Totale 8.107
Nazione #
IT - Italia 2.860
US - Stati Uniti d'America 2.631
SG - Singapore 342
MC - Monaco 336
RU - Federazione Russa 179
AT - Austria 165
CN - Cina 164
IE - Irlanda 139
DE - Germania 128
VN - Vietnam 103
FI - Finlandia 98
GB - Regno Unito 98
NL - Olanda 97
SE - Svezia 93
BR - Brasile 74
FR - Francia 64
ES - Italia 57
PH - Filippine 55
ID - Indonesia 51
CA - Canada 37
BE - Belgio 26
HK - Hong Kong 19
CH - Svizzera 18
JP - Giappone 18
KR - Corea 16
AE - Emirati Arabi Uniti 14
LU - Lussemburgo 13
BJ - Benin 12
IN - India 12
JO - Giordania 11
AU - Australia 10
CI - Costa d'Avorio 10
UA - Ucraina 10
PT - Portogallo 9
TR - Turchia 9
RO - Romania 8
HU - Ungheria 6
TH - Thailandia 6
AR - Argentina 5
BD - Bangladesh 5
IR - Iran 5
NZ - Nuova Zelanda 5
PE - Perù 5
AZ - Azerbaigian 4
GR - Grecia 4
MX - Messico 4
PK - Pakistan 4
PL - Polonia 4
DK - Danimarca 3
EE - Estonia 3
IQ - Iraq 3
MY - Malesia 3
SK - Slovacchia (Repubblica Slovacca) 3
TW - Taiwan 3
BG - Bulgaria 2
CO - Colombia 2
CZ - Repubblica Ceca 2
DZ - Algeria 2
EU - Europa 2
KG - Kirghizistan 2
KH - Cambogia 2
LV - Lettonia 2
MA - Marocco 2
MO - Macao, regione amministrativa speciale della Cina 2
NO - Norvegia 2
SC - Seychelles 2
UZ - Uzbekistan 2
AL - Albania 1
BH - Bahrain 1
CL - Cile 1
CR - Costa Rica 1
CY - Cipro 1
EC - Ecuador 1
EG - Egitto 1
GA - Gabon 1
GE - Georgia 1
IL - Israele 1
KZ - Kazakistan 1
LB - Libano 1
LY - Libia 1
MD - Moldavia 1
MK - Macedonia 1
MU - Mauritius 1
NG - Nigeria 1
SA - Arabia Saudita 1
SN - Senegal 1
ZA - Sudafrica 1
Totale 8.107
Città #
Milan 1.449
Santa Clara 407
Monaco 336
Chandler 301
Woodbridge 152
Vienna 151
Singapore 141
Dublin 138
Fairfield 138
Ashburn 131
Wilmington 108
Rome 92
Council Bluffs 90
Boardman 87
Houston 86
Giussano 69
Amsterdam 66
Ann Arbor 65
Bovisio Masciago 63
Pedrengo 62
Seattle 62
Boltiere 58
Dong Ket 57
Beijing 50
Davao City 50
Jakarta 50
Cambridge 46
Helsinki 45
Lawrence 44
Medford 42
Dearborn 41
Redwood City 33
Robbiate 31
Pavia 30
Turin 26
Ottawa 25
Falkenstein 23
Málaga 23
Crema 22
Des Moines 21
Gessate 20
London 19
Redmond 19
Tucson 19
Bagnoli Di Sopra 18
Busto Garolfo 18
Besana in Brianza 17
Frankfurt am Main 17
Kraainem 17
Lappeenranta 16
Nuremberg 16
Busto Arsizio 15
Washington 15
Bologna 14
Boulder 14
Trecate 14
Santa Maria A Vico 13
Torino 13
Cotonou 12
Gavirate 12
Madrid 12
Amman 11
Glasgow 11
Abidjan 10
Hesperange 10
San Diego 10
Shanghai 9
Varese 9
Zibido San Giacomo 9
Barcelona 8
Bareggio 8
Fremont 8
Lissone 8
Los Angeles 8
Shenyang 8
Toulouse 8
Xian 8
Bergamo 7
Bresso 7
Ciampino 7
Dubai 7
Groningen 7
Hanover 7
Lecco 7
Mountain View 7
Munich 7
Paris 7
Pasadena 7
Rho 7
San Jose 7
Sydney 7
Charlotte 6
Harbin 6
Legnano 6
New York 6
Potsdam 6
Princeton 6
São Paulo 6
Tampa 6
West Lafayette 6
Totale 5.536
Nome #
Trajectory Options for Hera’s Milani CubeSat Around (65803) Didymos 513
Toward Self-Driving Interplanetary CubeSats: the ERC-Funded Project EXTREMA 305
The Hera Milani Cubesat Mission 256
N-body gravitational and contact dynamics for asteroid aggregation 255
Families of Bounded Orbits near Binary Asteroid 65803 Didymos 227
A parallel-GPU code for asteroid aggregation problems with angular particles 215
Preliminary mission profile of Hera’s Milani CubeSat 211
Suitable configurations for triangular formation flying about collinear libration points under the circular and elliptic restricted three-body problems 204
Ballistic landing design on binary asteroids: the AIM case study 202
Periodic motion around libration points in the Elliptic Restricted Three-Body Problem 186
The EXTREMA Orbital Simulation Hub: a Facility for GNC Testing of Autonomous Interplanetary CubeSat 179
The COBRA IRIDES Experiment 172
Dynamical Evolution About Asteroids with High Fidelity Gravity Field and Perturbations Modeling 165
Dynamical model of binary asteroid systems through patched three-body problems 157
CubeSat Landing Simulations on Small Bodies using Blender 156
Trajectory Design and Orbit Determination of Hera’s Milani CubeSat 155
Asteroids Coupled Dynamics Analysis by Means of Accurate Mass Distribution and Perturbations Modeling 139
Mission Analysis and Navigation Assessment for Hera’s Milani CubeSat 117
Design of the Vision-Based GNC Subsystem of Hera’s Milani Mission 109
Close-Proximity Operations Concept of the Asteroid Impact Mission 109
Nanosatellite Formation Flying to Enhance Science in Binary Asteroid Environment 109
Asteroid Impact Monitoring Mission: Mission Analysis and Innovative Strategies for Close Proximity Maneuvering 108
The role of fragment shapes in the simulations of asteroids as gravitational aggregates 108
Asteroid Impact Mission: a Possible Approach to Design Effective Close Proximity Operations to Release Mascot-2 Lander 103
Optimal Configurations for Nanosatellite Formation Flying in Binary Asteroid Environment 101
The European Asteroid Impact Mission: Phase a Design and Mission Analysis 98
A New Environment to Simulate the Dynamics in the Close Proximity of Rubble-Pile Asteroids 96
Gas Plume Impingement Technique for Space Debris De-Tumbling 95
Momentum Transfer from the DART Mission Kinetic Impact on Asteroid Dimorphos 94
Numerical Simulation of N-Body Asteroid Aggregation with GPU-Parallel Hierarchical Treecode Algorithm 93
A Code for the Study of Gravitational Aggregates with Non-Spherical Particles 89
Formation Flying and Relative Dynamics Under the Circular Restricted Three-Body Problem Formulation 89
Assessment of GNC Impacts of Chemical Plume Impingement in the Case of Prisma Irides Experiment 87
Consolidated Phase a Design of Asteroid Impact Mission: MASCOT-2 Landing on Binary Asteroid Didymos 85
Trajectory Design About Binary Asteroids Through Coupled Three Body Problems 82
Coupling High Fidelity Body Modeling with Non-Keplerian Dynamics to Design Aim-Mascot-2 Landing Trajectories on Didymos Binary Asteroid 79
The effect of a rocky terrain for CubeSat landing on asteroid surfaces 77
Characterization of the Ejecta from the NASA/DART Impact on Dimorphos: Observations and Monte Carlo Models 77
Successful Kinetic Impact into an Asteroid for Planetary Defense 77
NASA’s Double Asteroid Redirection Test (DART): Mutual Orbital Period Change Due to Reshaping in the Near-Earth Binary Asteroid System (65803) Didymos 75
Initial Trajectory Assessment of a low-thrust option for the RAMSES Mission to (99942) Apophis 71
Applied Trajectory Design for CubeSat Close-Proximity Operations around Asteroids: The Milani Case 71
Zodiac Pioneer: an Interplanetary Small Satellite Platform for Asteroid Reconnaissance 70
Libration-induced Orbit Period Variations Following the DART Impact 69
The ERC-Funded EXTREMA Project: Achieving Self-Driving Interplanetary CubeSats 69
The Asteroid Impact Mission: Consolidated Mission Analysis and Scientific Payload Operations at Binary Asteroid Didymos 68
Coupled Dynamics Analysis Around Asteroids by Means of Accurate Shape and Perturbations Modeling 66
A new method for identifying dynamical transitions in rubble-pile asteroid scenarios 65
Guidance and Control design for CubeSat small body landing using discrete firings of sliding mode control 65
Formation Flying Dynamics in Circular Restricted Three-Body Problem and Applications to Binary Asteroid Systems 64
Free Tumbling Objects Attitude Control via Contactless Chaser Authority Exploiting a Formation Flying Architecture 63
GRAINS: a New Numerical Method for the Study of Gravitational Aggregates 63
Effects of Impact and Target Parameters on the Results of a Kinetic Impactor: Predictions for the Double Asteroid Redirection Test (DART) Mission 63
Achievement of the Planetary Defense Investigations of the Double Asteroid Redirection Test (DART) Mission 62
Design Drivers for Formation Flying Near Collinear Libration Points in the Circular and Elliptic Restricted Three-Body Problems 62
ESA’s Asteroid Impact Mission: Mission Analysis and Payload Operations State of the Art 61
Small Celestial Bodies Model Refinement by Means of N-Body Gravitational Dynamics 60
Double Asteroid Redirection Test (DART): Structural and Dynamic Interactions between Asteroidal Elements of Binary Asteroid (65803) Didymos 59
Numerical Simulation of N-Body Asteroid Aggregation 59
After DART: Using the First Full-scale Test of a Kinetic Impactor to Inform a Future Planetary Defense Mission 57
Ejecta Evolution Following a Planned Impact into an Asteroid: The First Five Weeks 55
Ejecta from the DART-produced active asteroid Dimorphos 54
Interior of top-shaped asteroids with cohesionless surface 54
Triangular Formation Flying Under the Elliptic Restricted Three-Body Problem Formulation 54
Direct N-body Simulations of Satellite Formation around Small Asteroids: Insights from DART’s Encounter with the Didymos System 53
Global Optimization of Relative Configurations Between Spacecraft Near Lagrangian Point Orbits 51
Optimization of Triangular Formation Flying Configurations Under the Circular and Elliptic Three-Body Problem Dynamics Modelling 51
Predictions for the Dynamical States of the Didymos System before and after the Planned DART Impact 50
N-body simulations of rubble-pile aggregates with angular particles 50
LUMIO Cubesat: Current Status and Lessons Learnt (so Far) 48
Physical properties of asteroid Dimorphos as derived from the DART impact 47
Dynamical Evolution of the Didymos−Dimorphos Binary Asteroid as Rubble Piles following the DART Impact 47
Scientific and Technological Objectives for the NavCam Payload of Hera’s Milani CubeSat to Binary Asteroid Didymos 46
The Dimorphos ejecta plume properties revealed by LICIACube 46
Pre-encounter Predictions of DART Impact Ejecta Behavior and Observability 46
Ejecta Formation, Early Collisional Processes, and Dynamical Evolution after the DART Impact on Dimorphos 45
Parameter Identification Using Microgravity Experiments on Asteroid-Related Scenarios 39
Modeling and Simulation of Milani CubeSat Contact Motion on the Surface of the Secondary Asteroid of Didymos Binary System 37
MASCOT-2 Landing Opportunities Using Three-Body Solutions for Asteroid Impact Mission 35
The Hera Milani Mission 34
Fast boulder fracturing by thermal fatigue detected on stony asteroids 34
The Dynamical State of the Didymos System before and after the DART Impact 29
LUMIO: Detecting Meteoroid Impacts on the Lunar Surface 27
The Orbital Regime Index: a Comprehensive Parameter to Determine Orbital Regions Around Minor Bodies 26
Zodiac Pioneer: an Interplanetary Small Satellite Platform for Asteroid Reconnaissance 17
Totale 8.216
Categoria #
all - tutte 161.100
article - articoli 92.606
book - libri 0
conference - conferenze 68.151
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 343
Totale 322.200


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020153 0 0 0 0 0 0 0 0 45 45 42 21
2020/2021402 22 34 33 19 12 24 13 34 22 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
2024/20252.596 343 65 197 251 777 310 180 192 281 0 0 0
Totale 8.216