RE.PUBLIC@POLIMI pubblicazioni di ricerca del Politecnico di Milano

ERCOLI, AMALIA
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 6.697
EU - Europa 4.510
AS - Asia 2.506
SA - Sud America 679
AF - Africa 115
OC - Oceania 14
Continente sconosciuto - Info sul continente non disponibili 6
Totale 14.527
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 6.573
RU - Federazione Russa 1.366
SG - Singapore 1.107
IT - Italia 1.003
CN - Cina 879
BR - Brasile 598
UA - Ucraina 491
SE - Svezia 327
DE - Germania 303
GB - Regno Unito 290
VN - Vietnam 209
FI - Finlandia 167
AT - Austria 157
IE - Irlanda 96
CA - Canada 90
FR - Francia 79
NL - Olanda 68
ES - Italia 58
MA - Marocco 49
IN - India 45
KR - Corea 42
AR - Argentina 33
BE - Belgio 30
JP - Giappone 27
TR - Turchia 27
HK - Hong Kong 25
MX - Messico 19
BD - Bangladesh 18
CI - Costa d'Avorio 18
IQ - Iraq 16
PL - Polonia 16
ZA - Sudafrica 16
ID - Indonesia 15
SA - Arabia Saudita 14
AU - Australia 12
JO - Giordania 12
VE - Venezuela 11
EC - Ecuador 10
PK - Pakistan 10
CH - Svizzera 9
IR - Iran 8
PY - Paraguay 8
UZ - Uzbekistan 8
CO - Colombia 7
RO - Romania 7
EG - Egitto 6
LT - Lituania 6
OM - Oman 6
AE - Emirati Arabi Uniti 5
EU - Europa 5
GR - Grecia 5
KE - Kenya 5
NO - Norvegia 5
PH - Filippine 5
PT - Portogallo 5
TN - Tunisia 5
AZ - Azerbaigian 4
LU - Lussemburgo 4
NP - Nepal 4
PE - Perù 4
UY - Uruguay 4
AL - Albania 3
BJ - Benin 3
CZ - Repubblica Ceca 3
DZ - Algeria 3
HN - Honduras 3
JM - Giamaica 3
MW - Malawi 3
MY - Malesia 3
TH - Thailandia 3
BA - Bosnia-Erzegovina 2
BG - Bulgaria 2
BH - Bahrain 2
CL - Cile 2
CR - Costa Rica 2
IL - Israele 2
KZ - Kazakistan 2
LK - Sri Lanka 2
MU - Mauritius 2
NG - Nigeria 2
NZ - Nuova Zelanda 2
TT - Trinidad e Tobago 2
BN - Brunei Darussalam 1
BO - Bolivia 1
BS - Bahamas 1
CY - Cipro 1
DK - Danimarca 1
DO - Repubblica Dominicana 1
ET - Etiopia 1
GH - Ghana 1
GI - Gibilterra 1
HU - Ungheria 1
IM - Isola di Man 1
KG - Kirghizistan 1
KW - Kuwait 1
LV - Lettonia 1
MG - Madagascar 1
NI - Nicaragua 1
PA - Panama 1
PS - Palestinian Territory 1
Totale 14.520
Salva come PNG Salva come JPEG
Città #
Woodbridge 633
Chandler 592
Singapore 551
Ashburn 536
Santa Clara 505
Houston 487
Fairfield 423
Ann Arbor 420
Milan 417
Wilmington 300
Jacksonville 264
Hefei 246
Dearborn 217
Moscow 186
Cambridge 162
Seattle 153
Vienna 153
Boardman 147
Council Bluffs 130
Beijing 121
Lawrence 115
Medford 115
San Jose 90
Dublin 84
Los Angeles 80
London 75
Ottawa 75
Dallas 63
Chongqing 57
Buffalo 51
Helsinki 48
São Paulo 48
Dong Ket 47
Málaga 47
Guangzhou 34
Ho Chi Minh City 34
Kenitra 34
Amsterdam 32
New York 32
Bovisio Masciago 31
The Dalles 31
Brussels 26
Des Moines 24
Zibido San Giacomo 23
San Diego 22
Seoul 22
Hanoi 20
Redwood City 20
Shanghai 19
Abidjan 18
Turin 18
Rome 17
Seongnam 17
Chengdu 16
Hong Kong 15
Berlin 14
Columbus 14
Atlanta 13
Istanbul 13
Norwalk 13
Orem 13
Amman 12
Brooklyn 12
Harbin 12
Kent 12
Ribeirão Preto 12
Rio de Janeiro 12
Belo Horizonte 11
Delft 11
Falkenstein 11
Verona 11
Warsaw 11
Casablanca 10
Tokyo 10
Zhengzhou 10
Boston 9
Brasília 9
Frankfurt am Main 9
Jeddah 9
Nanjing 9
Phoenix 9
Stockholm 9
Tianjin 9
Ankara 8
Auburn Hills 8
Oldham 8
Rho 8
Hangzhou 7
Jakarta 7
Johannesburg 7
Baghdad 6
Campinas 6
Caxias do Sul 6
Charlotte 6
Chicago 6
Cornate 6
Denver 6
Fortaleza 6
Guarulhos 6
Italy 6
Totale 8.565
Salva come PNG Salva come JPEG
Nome #
An Approach to the Design of Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 265
Amalia Mission Lunar Rover - the Conceptual Design of the Team Italia Rover, Candidate for the Google Lunar x Prize Challenge 265
Scientific Use of the Sampler, Drill and Distribution Subsystem (SD2) 225
A Drill-Soil System Modelization for Future Mars Exploration 221
A Multi-Attribute Decision Making Approach Toward Space System Design Automation Through a Fuzzy Logic-Based Analytic Hierarchical Process 218
Aero-Gravity Assist Maneuvers: Controlled Dynamics Modeling and Optimization 217
Rosetta Philae SD2 Drill System and Its Operation on 67p/Churyumov-Gerasimenko 211
Preliminary Design Global Optimization for Space Vehicles During Atmospheric Maneuvers 195
A New Nuclear Powered Cycler to Mars 192
Combining Two and Three-Body Dynamics for Low Energy Transfer Trajectories of Practical Interest 189
Planning and implementation of the on-comet operations of the instrument SD2 onboard the lander Philae of Rosetta mission 188
SD2 - a Cometary Soil Drill and Sampler Device 181
A Distributed Approach for Space System Formation Operation Autonomous Planning and Scheduling 175
A Nuclear Powered Cycler Mission to Mars 175
Space System Formation Planning and Scheduling: a Distributed Approach 174
Lessons Learned from the SD2 Operations on the Comet 67/P 172
State Tracking and Control of a Lifted Autonomous Space Vehicle During the Atmospheric Re-Entry Phase: a Lyapunov Approach 171
SD2: Technological/Scientific Instrument to Understand a Comet 171
Equilibrium Analysis of a Large Multi-Hinged Space System 168
A Minimum Energy Robotic Arm for Mars Exploration 167
A Fuzzy Logic MADM Approach Towards the Spacecraft Design Automation 165
SD2 - How to Sample a Comet 162
In-Orbit Technology Validation for a University Microsatellite 159
En Route Toward a Comet 154
Aero-Gravity Assist Maneuvers for Interplanetary Missions: Controlled Dynamics Modelling and Optimization 154
Distributed Planning and Scheduling for Space System Flotillas 153
Atmospheric Re-Entry Trajectory Tracking and Control for an Unmanned Space Vehicle with a Lyapunov Approach 152
A MADM Approach Towards Space System Design Automation by a Fuzzy-Logic Based Analytic Hierarchical Process 151
Preliminary Design and Operations of Palamede Microsatellite 151
MonteCarlo Techniques for Thermal Analysis. Design Margin Determination Using Reduced Models and Experimental Data 150
Rosetta Philae Sampling Drilling and Distribution Subsystem: Operation and Results from the First On-Comet Phase 150
MonteCarlo Techniques in Space Thermal Analysis with Reduced Models: Design of Experiment and Statistic of Extremes Tools Applicability 149
Multiobjective Global Optimization of Space Mission Design Using Evolutionary Methods and Interval Analysis 149
Lessons Learned from the SD2 Operations on the Comet 67/P 148
A Vision System for Autonomous Landing Manoeuvres 148
Preliminary Spacecraft Design: Genetic Algorithms and AHP to Support the Concurrent Process Approach 146
Fuzzy Inductive Reasoning and Possibilistic Logic for Space Systems Failure Smart Detection and Identification 146
A Possible in Orbit Relativistic Experiment Mission with Very Accurate S/C Relative Control 145
Design of Robust Drag-Free Controllers with Given Structure 145
Long Term Space Program Scheduling and System Design Optimization 145
Interplanetary Mission Design with Aero-Assisted Manoeuvres Multi-Objective Evolutive Optimization 144
Montecarlo Techiniques for Thermal Analysis of Space Vehicles: Practical Examples of Robustness Determination in Preliminary Design 143
Project PALAMEDE at Politecnico di Milano: a Real Satellite to Teach Satellites Design Techniques 141
Space Probe Multidisciplinary Design During Atmospheric Phases 141
Optimal Formation Flying Reconfiguration and Station Keeping Maneuvers Using Low Thrust Propulsion 140
Spacecraft Design as a Multi-Criteria Decision-Making 138
A Tool for Preliminary Design of Low Thrust Gravity-Assist Trajectories 138
High-Order Robust Guidance of Interplanetary Trajectories Based on Differential Algebra 137
Aero-Gravity Assist Manoeuvres Within Preliminary Interplanetary Mission Design: a Multi-Objective Evolutive Algorithm Approach 137
Large Multi-Hinged Space Systems: a Parametric Stability Analysis 136
SD2-Sampler, Drill and Distribution System 135
Stochastic Analysis in Space Engineering: a Survay of Existing Tools and Methodologies for Thermal Analysis 135
Application of the Multibody Approach to the Control of Robotic Manipulators 134
Fuzzy Logic and Decisional Processes Towards a Space System Activity Autonomous Scheduler 130
A Space Engineering Summer School for European Students: Training on a Real Space Project 128
SD2: How to Drill a Comet 125
"Spazio per tutti" : A Hands-On Experience toward Space Engineering 124
Sampler, Drill and Distribution System for in Situ Analysis of a Cometary Nucleus 124
Composites and Smart Materials for Structural Space Applications: a Review 120
Industria aerospaziale italiana: le attività in ambito spazio di Galileo Avionica s.p.a. 118
Rosetta Mission: On-Comet Operation Planning for the Sampler, Drill and Distribution Subsystem 117
Extremely Accurate Line of Sight Control Between a Pointing and a Target Spacecraft 115
Fuzzy Logic in Spacecraft Design 115
Spacecraft Attitude Control for Extremely Accurate Line of Sight Pointing 114
Rosetta Mission : the Solar Array Photovoltaic Assembly 114
Feedback Dynamic Compensation via Multibody Models and Applications to Robot Control 112
Sampler, Drill and Distribution System for Cometary Soil Analysis 110
An Educational Hands-On Experience Toward Space Engineering: "Spazio per Tutti" 107
Fuzzy Logic and Predicate Calculus to Automate the Spacecraft Activity Scheduling 106
Space System Activity Scheduling Automation: a Decisional Theory Approach 104
Globalisation of Aerospace Engineering Education 104
Concurrent Processes Within Preliminary Spacecraft Design: an Autonomous Decisional Support Based on a Genetic Algorithms and Analytic Hierarchical Process 103
Modified Discrete-Time Velocity Feedback for Vibration Suppression of a LSS Laboratory Model 103
Optimal Trajectory Generation and Control for Reconfiguration Maneuvers of Formation Flying Using Low-Thrust Propulsion 103
Spacecraft Design Automation with Fuzzy Multiple Criteria Decision Making 100
Attitude Maneuvers of a Flexible Space Station by Means of Deployable Tethers 100
Mars Dust Devil Test Facility 99
Atmospheric Re-Entry Vehicles: a Lyapunov Approach to Track and Control the System States 98
The Sample Drill and Distribution Subsystem of the Rosetta Lander 98
Economical Earth-Moon Transfers: a Quality Study 96
Equilibrium of a Large Multi-Hinged Space Sistems 96
Multi-Criteria Design Optimization of a Space System with a Fuzzy Logic Approach 96
Robust Aero-Gravity Assisted Maneuvers for a Multi-Objective Interplanetary Trajectory Design Optimization 96
Decisional Methods in Supporting Space System Design Processes 95
Italian Partecipation in the Mars Exploration Program 93
Particular Aspects of the Forced Response of Finite-Dimensional Modular Structures 93
Multi-Criteria Optimization for Space Mission Design: a New Approach 92
Experiment Proposal for the Detection of Possible Photons Trajectory Perturbation Caused by Maxwellian Fields 90
Dynamics and Control of 1g Rotating Space Station 90
Interplanetary Mission Design with Aero-Assisted Manoeuvers Multi-Objective Evolutive Optimization 89
Space System Design Automation Through a Fuzzy Multi-Criteria Decision Making Approach 89
Large Multi-Hinged Space System: a Parametric Stability Analysis 88
Multi-Disciplinary Optimisation for Space Vehicles During Aeroassisted Manoeuvres: an Evolutionary Algorithm Approach 86
Shape and Vibration Control of a Multibody Flexible Structure Using Recurrent Neural Networks 86
Scientific Use of the Sampler, Drill and Distribution Subsystem (SD2) 85
Dynamics and Control of 1g Rotating Two-Body Tethered Station 85
Lunar Orbital Dynamics by Finite Element in Time Method 85
Optimal Bi-Impulsive Earth-Moon Transfers 83
Modular Large Space Structures Dynamics 83
Equilibrium Configurations of a Large Multi-Hinged Space System 82
Totale 13.530
Salva come PNG Salva come JPEG
Categoria #
all - tutte 38.666
article - articoli 9.311
book - libri 0
conference - conferenze 27.831
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.524
Totale 77.332
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021608 0 0 0 0 0 0 100 145 60 124 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
2025/20264.009 1.077 1.057 431 565 304 334 241 0 0 0 0 0
Totale 14.602