ERCOLI, AMALIA
 Distribuzione geografica
Continente #
NA - Nord America 8.133
EU - Europa 6.543
AS - Asia 3.148
SA - Sud America 705
AF - Africa 128
Continente sconosciuto - Info sul continente non disponibili 81
OC - Oceania 14
Totale 18.752
Nazione #
US - Stati Uniti d'America 7.964
IT - Italia 2.814
RU - Federazione Russa 1.369
SG - Singapore 1.173
CN - Cina 1.001
BR - Brasile 615
UA - Ucraina 492
VN - Vietnam 415
SE - Svezia 328
GB - Regno Unito 319
DE - Germania 314
FI - Finlandia 203
FR - Francia 195
AT - Austria 159
KR - Corea 130
CA - Canada 116
IE - Irlanda 98
JP - Giappone 77
HK - Hong Kong 70
NL - Olanda 70
ES - Italia 66
IN - India 59
MA - Marocco 49
AR - Argentina 34
BE - Belgio 31
TR - Turchia 29
BD - Bangladesh 25
IQ - Iraq 22
MX - Messico 22
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 11
CH - Svizzera 10
TH - Thailandia 10
UZ - Uzbekistan 9
EG - Egitto 8
IR - Iran 8
PY - Paraguay 8
TW - Taiwan 8
CO - Colombia 7
RO - Romania 7
TN - Tunisia 7
CR - Costa Rica 6
DZ - Algeria 6
JM - Giamaica 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
HN - Honduras 4
LU - Lussemburgo 4
MY - Malesia 4
NP - Nepal 4
AL - Albania 3
BG - Bulgaria 3
BJ - Benin 3
BO - Bolivia 3
IL - Israele 3
KG - Kirghizistan 3
MU - Mauritius 3
MW - Malawi 3
NI - Nicaragua 3
BA - Bosnia-Erzegovina 2
BH - Bahrain 2
BS - Bahamas 2
CL - Cile 2
HU - Ungheria 2
KZ - Kazakistan 2
LK - Sri Lanka 2
NG - Nigeria 2
NZ - Nuova Zelanda 2
PR - Porto Rico 2
SK - Slovacchia (Repubblica Slovacca) 2
SV - El Salvador 2
TT - Trinidad e Tobago 2
BB - Barbados 1
BN - Brunei Darussalam 1
CY - Cipro 1
DK - Danimarca 1
DO - Repubblica Dominicana 1
ET - Etiopia 1
GH - Ghana 1
GI - Gibilterra 1
GT - Guatemala 1
Totale 18.663
Città #
Milan 1.979
Ashburn 689
Woodbridge 634
San Jose 631
Chandler 592
Singapore 592
Santa Clara 520
Houston 491
Fairfield 424
Ann Arbor 420
Wilmington 300
Jacksonville 264
Hefei 246
Dearborn 217
Moscow 186
Cambridge 162
Boardman 159
Council Bluffs 159
Vienna 154
Seattle 153
The Dalles 150
North Charleston 130
Beijing 129
Lawrence 115
Medford 115
Dallas 112
Seoul 105
Los Angeles 104
Lauterbourg 100
Dublin 86
Helsinki 84
London 78
Ottawa 78
Ho Chi Minh City 76
Hanoi 74
Rome 68
Chongqing 57
Buffalo 55
Tokyo 53
Hong Kong 50
São Paulo 50
Dong Ket 47
Málaga 47
Guangzhou 40
New York 36
Kenitra 34
Amsterdam 33
Bovisio Masciago 31
Orem 28
Brussels 27
Turin 27
Las Vegas 26
Des Moines 25
Zibido San Giacomo 23
San Diego 22
Shanghai 21
Da Nang 20
Redwood City 20
Abidjan 18
Brooklyn 17
Chengdu 17
Naples 17
Seongnam 17
Columbus 16
Frankfurt am Main 16
Atlanta 15
Haiphong 15
Berlin 14
Warsaw 14
Istanbul 13
Norwalk 13
Palermo 13
Phoenix 13
Amman 12
Belo Horizonte 12
Glasgow 12
Guarulhos 12
Harbin 12
Kent 12
Ribeirão Preto 12
Rio de Janeiro 12
Tianjin 12
Delft 11
Falkenstein 11
Verona 11
Casablanca 10
Florence 10
Stockholm 10
Zhengzhou 10
Boston 9
Brasília 9
Chennai 9
Chicago 9
Hangzhou 9
Jeddah 9
Johannesburg 9
Nanjing 9
Ankara 8
Auburn Hills 8
Baghdad 8
Totale 11.853
Nome #
An Approach to the Design of Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 529
Combining Two and Three-Body Dynamics for Low Energy Transfer Trajectories of Practical Interest 420
Optimal Bi-Impulsive Earth-Moon Transfers 304
Amalia Mission Lunar Rover - the Conceptual Design of the Team Italia Rover, Candidate for the Google Lunar x Prize Challenge 299
On-Comet Power Production: the Case of Rosetta Lander Philae 293
Power Production for Small Body Landers: Post-Launch Activities on Philae's Power Subsystem 291
LILT Measurements on Silicon Solar Cells of Rosetta Lander Philae 289
Solar Array Simulators for Low Power Space Missions 282
A Multi-Attribute Decision Making Approach Toward Space System Design Automation Through a Fuzzy Logic-Based Analytic Hierarchical Process 253
Scientific Use of the Sampler, Drill and Distribution Subsystem (SD2) 253
A Drill-Soil System Modelization for Future Mars Exploration 252
Aero-Gravity Assist Maneuvers: Controlled Dynamics Modeling and Optimization 241
Rosetta Philae SD2 Drill System and Its Operation on 67p/Churyumov-Gerasimenko 232
A New Nuclear Powered Cycler to Mars 230
Preliminary Design Global Optimization for Space Vehicles During Atmospheric Maneuvers 226
Planning and implementation of the on-comet operations of the instrument SD2 onboard the lander Philae of Rosetta mission 223
A Fuzzy Logic MADM Approach Towards the Spacecraft Design Automation 206
SD2 - a Cometary Soil Drill and Sampler Device 204
Space System Formation Planning and Scheduling: a Distributed Approach 203
State Tracking and Control of a Lifted Autonomous Space Vehicle During the Atmospheric Re-Entry Phase: a Lyapunov Approach 201
Lessons Learned from the SD2 Operations on the Comet 67/P 199
A Distributed Approach for Space System Formation Operation Autonomous Planning and Scheduling 198
A Nuclear Powered Cycler Mission to Mars 198
SD2 - How to Sample a Comet 195
SD2: Technological/Scientific Instrument to Understand a Comet 195
A Minimum Energy Robotic Arm for Mars Exploration 192
Lessons Learned from the SD2 Operations on the Comet 67/P 188
Equilibrium Analysis of a Large Multi-Hinged Space System 186
En Route Toward a Comet 184
In-Orbit Technology Validation for a University Microsatellite 183
Multiobjective Global Optimization of Space Mission Design Using Evolutionary Methods and Interval Analysis 179
A MADM Approach Towards Space System Design Automation by a Fuzzy-Logic Based Analytic Hierarchical Process 178
Atmospheric Re-Entry Trajectory Tracking and Control for an Unmanned Space Vehicle with a Lyapunov Approach 178
MonteCarlo Techniques for Thermal Analysis. Design Margin Determination Using Reduced Models and Experimental Data 177
Rosetta Philae Sampling Drilling and Distribution Subsystem: Operation and Results from the First On-Comet Phase 177
A Vision System for Autonomous Landing Manoeuvres 177
Application of the Multibody Approach to the Control of Robotic Manipulators 174
Distributed Planning and Scheduling for Space System Flotillas 174
Design of Robust Drag-Free Controllers with Given Structure 174
Aero-Gravity Assist Maneuvers for Interplanetary Missions: Controlled Dynamics Modelling and Optimization 172
Preliminary Spacecraft Design: Genetic Algorithms and AHP to Support the Concurrent Process Approach 171
A Possible in Orbit Relativistic Experiment Mission with Very Accurate S/C Relative Control 170
Preliminary Design and Operations of Palamede Microsatellite 170
MonteCarlo Techniques in Space Thermal Analysis with Reduced Models: Design of Experiment and Statistic of Extremes Tools Applicability 168
Large Multi-Hinged Space Systems: a Parametric Stability Analysis 168
Long Term Space Program Scheduling and System Design Optimization 168
A Space Engineering Summer School for European Students: Training on a Real Space Project 167
Interplanetary Mission Design with Aero-Assisted Manoeuvres Multi-Objective Evolutive Optimization 166
Montecarlo Techiniques for Thermal Analysis of Space Vehicles: Practical Examples of Robustness Determination in Preliminary Design 166
Aero-Gravity Assist Manoeuvres Within Preliminary Interplanetary Mission Design: a Multi-Objective Evolutive Algorithm Approach 165
Project PALAMEDE at Politecnico di Milano: a Real Satellite to Teach Satellites Design Techniques 164
A Tool for Preliminary Design of Low Thrust Gravity-Assist Trajectories 164
Optimal Formation Flying Reconfiguration and Station Keeping Maneuvers Using Low Thrust Propulsion 163
Space Probe Multidisciplinary Design During Atmospheric Phases 160
Spacecraft Design as a Multi-Criteria Decision-Making 160
Fuzzy Inductive Reasoning and Possibilistic Logic for Space Systems Failure Smart Detection and Identification 158
Fuzzy Logic and Decisional Processes Towards a Space System Activity Autonomous Scheduler 158
SD2-Sampler, Drill and Distribution System 158
"Spazio per tutti" : A Hands-On Experience toward Space Engineering 154
Stochastic Analysis in Space Engineering: a Survay of Existing Tools and Methodologies for Thermal Analysis 154
High-Order Robust Guidance of Interplanetary Trajectories Based on Differential Algebra 153
SD2: How to Drill a Comet 150
Rosetta Mission: On-Comet Operation Planning for the Sampler, Drill and Distribution Subsystem 142
Sampler, Drill and Distribution System for in Situ Analysis of a Cometary Nucleus 141
Fuzzy Logic in Spacecraft Design 141
Extremely Accurate Line of Sight Control Between a Pointing and a Target Spacecraft 137
Feedback Dynamic Compensation via Multibody Models and Applications to Robot Control 137
Rosetta Mission : the Solar Array Photovoltaic Assembly 137
Sampler, Drill and Distribution System for Cometary Soil Analysis 136
Industria aerospaziale italiana: le attività in ambito spazio di Galileo Avionica s.p.a. 134
Composites and Smart Materials for Structural Space Applications: a Review 133
Spacecraft Attitude Control for Extremely Accurate Line of Sight Pointing 132
An Educational Hands-On Experience Toward Space Engineering: "Spazio per Tutti" 131
Optimal Trajectory Generation and Control for Reconfiguration Maneuvers of Formation Flying Using Low-Thrust Propulsion 126
Fuzzy Logic and Predicate Calculus to Automate the Spacecraft Activity Scheduling 125
Space System Activity Scheduling Automation: a Decisional Theory Approach 124
Atmospheric Re-Entry Vehicles: a Lyapunov Approach to Track and Control the System States 121
Concurrent Processes Within Preliminary Spacecraft Design: an Autonomous Decisional Support Based on a Genetic Algorithms and Analytic Hierarchical Process 121
The Sample Drill and Distribution Subsystem of the Rosetta Lander 120
Globalisation of Aerospace Engineering Education 119
Decisional Methods in Supporting Space System Design Processes 119
Modified Discrete-Time Velocity Feedback for Vibration Suppression of a LSS Laboratory Model 118
Attitude Maneuvers of a Flexible Space Station by Means of Deployable Tethers 118
Mars Dust Devil Test Facility 118
Robust Aero-Gravity Assisted Maneuvers for a Multi-Objective Interplanetary Trajectory Design Optimization 116
Spacecraft Design Automation with Fuzzy Multiple Criteria Decision Making 115
Particular Aspects of the Forced Response of Finite-Dimensional Modular Structures 115
Italian Partecipation in the Mars Exploration Program 114
Multi-Criteria Design Optimization of a Space System with a Fuzzy Logic Approach 112
Interplanetary Mission Design with Aero-Assisted Manoeuvers Multi-Objective Evolutive Optimization 112
Equilibrium of a Large Multi-Hinged Space Sistems 111
Experiment Proposal for the Detection of Possible Photons Trajectory Perturbation Caused by Maxwellian Fields 111
Economical Earth-Moon Transfers: a Quality Study 110
Space System Design Automation Through a Fuzzy Multi-Criteria Decision Making Approach 110
Shape and Vibration Control of a Multibody Flexible Structure Using Recurrent Neural Networks 110
Multi-Criteria Optimization for Space Mission Design: a New Approach 109
Scientific Use of the Sampler, Drill and Distribution Subsystem (SD2) 109
Dynamics and Control of 1g Rotating Space Station 109
Lunar Orbital Dynamics by Finite Element in Time Method 109
Interplanetary Mission Design with Aero-Assisted Manoeuvers Multi-Objective Evolutive Optimization 108
Totale 17.294
Categoria #
all - tutte 47.301
article - articoli 10.820
book - libri 0
conference - conferenze 34.654
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.827
Totale 94.602


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.010 0 129 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
2025/20267.685 1.077 1.057 431 565 304 334 930 353 715 859 421 639
2026/2027474 355 119 0 0 0 0 0 0 0 0 0 0
Totale 18.752