ERCOLI, AMALIA
 Distribuzione geografica
Continente #
NA - Nord America 7.775
EU - Europa 5.383
AS - Asia 3.091
SA - Sud America 696
AF - Africa 128
OC - Oceania 14
Continente sconosciuto - Info sul continente non disponibili 6
Totale 17.093
Nazione #
US - Stati Uniti d'America 7.645
IT - Italia 1.665
RU - Federazione Russa 1.369
SG - Singapore 1.162
CN - Cina 992
BR - Brasile 607
UA - Ucraina 492
VN - Vietnam 383
SE - Svezia 328
DE - Germania 314
GB - Regno Unito 312
FI - Finlandia 203
FR - Francia 195
AT - Austria 159
KR - Corea 130
IE - Irlanda 98
CA - Canada 94
JP - Giappone 73
NL - Olanda 70
HK - Hong Kong 69
ES - Italia 64
IN - India 59
MA - Marocco 49
AR - Argentina 34
BE - Belgio 31
TR - Turchia 29
BD - Bangladesh 25
IQ - Iraq 22
MX - Messico 20
PL - Polonia 19
ZA - Sudafrica 19
CI - Costa d'Avorio 18
ID - Indonesia 16
SA - Arabia Saudita 15
JO - Giordania 14
VE - Venezuela 14
PK - Pakistan 13
AU - Australia 12
PH - Filippine 12
EC - Ecuador 10
TH - Thailandia 10
CH - Svizzera 9
UZ - Uzbekistan 9
EG - Egitto 8
IR - Iran 8
PY - Paraguay 8
TW - Taiwan 8
CO - Colombia 7
RO - Romania 7
TN - Tunisia 7
DZ - Algeria 6
KE - Kenya 6
LT - Lituania 6
OM - Oman 6
PT - Portogallo 6
AE - Emirati Arabi Uniti 5
AZ - Azerbaigian 5
EU - Europa 5
GR - Grecia 5
NO - Norvegia 5
PE - Perù 5
UY - Uruguay 5
CZ - Repubblica Ceca 4
LU - Lussemburgo 4
MY - Malesia 4
NP - Nepal 4
AL - Albania 3
BG - Bulgaria 3
BJ - Benin 3
BO - Bolivia 3
HN - Honduras 3
IL - Israele 3
JM - Giamaica 3
KG - Kirghizistan 3
MU - Mauritius 3
MW - Malawi 3
BA - Bosnia-Erzegovina 2
BH - Bahrain 2
CL - Cile 2
CR - Costa Rica 2
HU - Ungheria 2
KZ - Kazakistan 2
LK - Sri Lanka 2
NG - Nigeria 2
NZ - Nuova Zelanda 2
TT - Trinidad e Tobago 2
BN - Brunei Darussalam 1
BS - Bahamas 1
CY - Cipro 1
DK - Danimarca 1
DO - Repubblica Dominicana 1
ET - Etiopia 1
GH - Ghana 1
GI - Gibilterra 1
IM - Isola di Man 1
KW - Kuwait 1
LI - Liechtenstein 1
LV - Lettonia 1
MG - Madagascar 1
MN - Mongolia 1
Totale 17.081
Città #
Milan 1.068
Ashburn 665
Woodbridge 634
San Jose 601
Chandler 592
Singapore 586
Santa Clara 510
Houston 487
Fairfield 423
Ann Arbor 420
Wilmington 300
Jacksonville 264
Hefei 246
Dearborn 217
Moscow 186
Cambridge 162
Vienna 154
Seattle 153
The Dalles 150
Boardman 147
Council Bluffs 139
North Charleston 130
Beijing 124
Lawrence 115
Medford 115
Dallas 108
Seoul 105
Lauterbourg 100
Los Angeles 100
Dublin 86
Helsinki 84
London 78
Ottawa 75
Ho Chi Minh City 72
Hanoi 58
Chongqing 57
Buffalo 54
Tokyo 52
Hong Kong 50
São Paulo 49
Dong Ket 47
Málaga 47
Guangzhou 40
Kenitra 34
Amsterdam 33
New York 33
Bovisio Masciago 31
Brussels 27
Orem 27
Las Vegas 26
Des Moines 25
Zibido San Giacomo 23
San Diego 22
Shanghai 21
Turin 21
Redwood City 20
Abidjan 18
Da Nang 18
Rome 18
Chengdu 17
Seongnam 17
Frankfurt am Main 16
Atlanta 15
Berlin 14
Brooklyn 14
Columbus 14
Warsaw 14
Haiphong 13
Istanbul 13
Norwalk 13
Amman 12
Harbin 12
Kent 12
Ribeirão Preto 12
Rio de Janeiro 12
Tianjin 12
Belo Horizonte 11
Delft 11
Falkenstein 11
Phoenix 11
Verona 11
Casablanca 10
Stockholm 10
Zhengzhou 10
Boston 9
Brasília 9
Chennai 9
Hangzhou 9
Jeddah 9
Johannesburg 9
Nanjing 9
Ankara 8
Auburn Hills 8
Baghdad 8
Oldham 8
Rho 8
Can Tho 7
Glasgow 7
Jakarta 7
San Francisco 7
Totale 10.695
Nome #
An Approach to the Design of Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 389
Combining Two and Three-Body Dynamics for Low Energy Transfer Trajectories of Practical Interest 298
Amalia Mission Lunar Rover - the Conceptual Design of the Team Italia Rover, Candidate for the Google Lunar x Prize Challenge 293
A Drill-Soil System Modelization for Future Mars Exploration 246
A Multi-Attribute Decision Making Approach Toward Space System Design Automation Through a Fuzzy Logic-Based Analytic Hierarchical Process 245
Scientific Use of the Sampler, Drill and Distribution Subsystem (SD2) 240
Aero-Gravity Assist Maneuvers: Controlled Dynamics Modeling and Optimization 237
A New Nuclear Powered Cycler to Mars 227
Rosetta Philae SD2 Drill System and Its Operation on 67p/Churyumov-Gerasimenko 226
Preliminary Design Global Optimization for Space Vehicles During Atmospheric Maneuvers 214
Planning and implementation of the on-comet operations of the instrument SD2 onboard the lander Philae of Rosetta mission 209
A Fuzzy Logic MADM Approach Towards the Spacecraft Design Automation 197
SD2 - a Cometary Soil Drill and Sampler Device 196
A Distributed Approach for Space System Formation Operation Autonomous Planning and Scheduling 193
A Nuclear Powered Cycler Mission to Mars 193
Space System Formation Planning and Scheduling: a Distributed Approach 191
Lessons Learned from the SD2 Operations on the Comet 67/P 191
State Tracking and Control of a Lifted Autonomous Space Vehicle During the Atmospheric Re-Entry Phase: a Lyapunov Approach 189
SD2 - How to Sample a Comet 187
SD2: Technological/Scientific Instrument to Understand a Comet 187
Optimal Bi-Impulsive Earth-Moon Transfers 185
A Minimum Energy Robotic Arm for Mars Exploration 182
En Route Toward a Comet 182
Equilibrium Analysis of a Large Multi-Hinged Space System 181
Atmospheric Re-Entry Trajectory Tracking and Control for an Unmanned Space Vehicle with a Lyapunov Approach 173
In-Orbit Technology Validation for a University Microsatellite 173
On-Comet Power Production: the Case of Rosetta Lander Philae 173
A Vision System for Autonomous Landing Manoeuvres 172
Rosetta Philae Sampling Drilling and Distribution Subsystem: Operation and Results from the First On-Comet Phase 171
A MADM Approach Towards Space System Design Automation by a Fuzzy-Logic Based Analytic Hierarchical Process 170
Power Production for Small Body Landers: Post-Launch Activities on Philae's Power Subsystem 169
Distributed Planning and Scheduling for Space System Flotillas 168
Multiobjective Global Optimization of Space Mission Design Using Evolutionary Methods and Interval Analysis 168
LILT Measurements on Silicon Solar Cells of Rosetta Lander Philae 168
Preliminary Design and Operations of Palamede Microsatellite 167
Aero-Gravity Assist Maneuvers for Interplanetary Missions: Controlled Dynamics Modelling and Optimization 167
MonteCarlo Techniques for Thermal Analysis. Design Margin Determination Using Reduced Models and Experimental Data 165
MonteCarlo Techniques in Space Thermal Analysis with Reduced Models: Design of Experiment and Statistic of Extremes Tools Applicability 165
Application of the Multibody Approach to the Control of Robotic Manipulators 164
Lessons Learned from the SD2 Operations on the Comet 67/P 164
A Possible in Orbit Relativistic Experiment Mission with Very Accurate S/C Relative Control 162
Long Term Space Program Scheduling and System Design Optimization 161
Solar Array Simulators for Low Power Space Missions 161
Aero-Gravity Assist Manoeuvres Within Preliminary Interplanetary Mission Design: a Multi-Objective Evolutive Algorithm Approach 161
Optimal Formation Flying Reconfiguration and Station Keeping Maneuvers Using Low Thrust Propulsion 160
Preliminary Spacecraft Design: Genetic Algorithms and AHP to Support the Concurrent Process Approach 160
Design of Robust Drag-Free Controllers with Given Structure 160
A Space Engineering Summer School for European Students: Training on a Real Space Project 160
A Tool for Preliminary Design of Low Thrust Gravity-Assist Trajectories 160
Project PALAMEDE at Politecnico di Milano: a Real Satellite to Teach Satellites Design Techniques 159
Interplanetary Mission Design with Aero-Assisted Manoeuvres Multi-Objective Evolutive Optimization 159
Spacecraft Design as a Multi-Criteria Decision-Making 158
Fuzzy Inductive Reasoning and Possibilistic Logic for Space Systems Failure Smart Detection and Identification 158
Montecarlo Techiniques for Thermal Analysis of Space Vehicles: Practical Examples of Robustness Determination in Preliminary Design 157
Large Multi-Hinged Space Systems: a Parametric Stability Analysis 155
SD2-Sampler, Drill and Distribution System 155
Space Probe Multidisciplinary Design During Atmospheric Phases 153
Stochastic Analysis in Space Engineering: a Survay of Existing Tools and Methodologies for Thermal Analysis 151
High-Order Robust Guidance of Interplanetary Trajectories Based on Differential Algebra 150
"Spazio per tutti" : A Hands-On Experience toward Space Engineering 148
Fuzzy Logic and Decisional Processes Towards a Space System Activity Autonomous Scheduler 145
SD2: How to Drill a Comet 140
Sampler, Drill and Distribution System for in Situ Analysis of a Cometary Nucleus 138
Rosetta Mission: On-Comet Operation Planning for the Sampler, Drill and Distribution Subsystem 136
Extremely Accurate Line of Sight Control Between a Pointing and a Target Spacecraft 131
Fuzzy Logic in Spacecraft Design 131
Composites and Smart Materials for Structural Space Applications: a Review 130
Sampler, Drill and Distribution System for Cometary Soil Analysis 130
Industria aerospaziale italiana: le attività in ambito spazio di Galileo Avionica s.p.a. 129
Spacecraft Attitude Control for Extremely Accurate Line of Sight Pointing 128
Rosetta Mission : the Solar Array Photovoltaic Assembly 128
Feedback Dynamic Compensation via Multibody Models and Applications to Robot Control 124
Optimal Trajectory Generation and Control for Reconfiguration Maneuvers of Formation Flying Using Low-Thrust Propulsion 122
An Educational Hands-On Experience Toward Space Engineering: "Spazio per Tutti" 120
Space System Activity Scheduling Automation: a Decisional Theory Approach 119
Concurrent Processes Within Preliminary Spacecraft Design: an Autonomous Decisional Support Based on a Genetic Algorithms and Analytic Hierarchical Process 119
Fuzzy Logic and Predicate Calculus to Automate the Spacecraft Activity Scheduling 117
Atmospheric Re-Entry Vehicles: a Lyapunov Approach to Track and Control the System States 117
Attitude Maneuvers of a Flexible Space Station by Means of Deployable Tethers 115
The Sample Drill and Distribution Subsystem of the Rosetta Lander 114
Mars Dust Devil Test Facility 114
Globalisation of Aerospace Engineering Education 113
Modified Discrete-Time Velocity Feedback for Vibration Suppression of a LSS Laboratory Model 113
Spacecraft Design Automation with Fuzzy Multiple Criteria Decision Making 111
Particular Aspects of the Forced Response of Finite-Dimensional Modular Structures 111
Experiment Proposal for the Detection of Possible Photons Trajectory Perturbation Caused by Maxwellian Fields 110
Decisional Methods in Supporting Space System Design Processes 109
Italian Partecipation in the Mars Exploration Program 109
Equilibrium of a Large Multi-Hinged Space Sistems 108
Robust Aero-Gravity Assisted Maneuvers for a Multi-Objective Interplanetary Trajectory Design Optimization 108
Multi-Criteria Optimization for Space Mission Design: a New Approach 107
Multi-Criteria Design Optimization of a Space System with a Fuzzy Logic Approach 107
Economical Earth-Moon Transfers: a Quality Study 105
Interplanetary Mission Design with Aero-Assisted Manoeuvers Multi-Objective Evolutive Optimization 105
Shape and Vibration Control of a Multibody Flexible Structure Using Recurrent Neural Networks 105
Interplanetary Mission Design with Aero-Assisted Manoeuvers Multi-Objective Evolutive Optimization 105
Space System Design Automation Through a Fuzzy Multi-Criteria Decision Making Approach 103
Dynamics and Control of 1g Rotating Space Station 103
Lunar Orbital Dynamics by Finite Element in Time Method 103
Scientific Use of the Sampler, Drill and Distribution Subsystem (SD2) 102
Totale 15.807
Categoria #
all - tutte 42.504
article - articoli 10.009
book - libri 0
conference - conferenze 30.821
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.674
Totale 85.008


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021303 0 0 0 0 0 0 0 0 0 124 63 116
2021/20221.052 42 129 13 79 173 42 43 99 66 87 92 187
2022/20231.152 185 124 62 129 97 161 13 85 134 74 67 21
2023/2024598 46 111 26 51 31 39 36 27 127 46 9 49
2024/20252.305 22 63 65 59 445 293 107 253 272 175 265 286
2025/20266.575 1.077 1.057 431 565 304 334 930 353 715 809 0 0
Totale 17.168