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

ERCOLI, AMALIA
 Distribuzione geografica
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Continente #
NA - Nord America 7.932
EU - Europa 5.877
AS - Asia 3.106
SA - Sud America 696
AF - Africa 128
OC - Oceania 14
Continente sconosciuto - Info sul continente non disponibili 6
Totale 17.759
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Nazione #
US - Stati Uniti d'America 7.798
IT - Italia 2.158
RU - Federazione Russa 1.369
SG - Singapore 1.167
CN - Cina 999
BR - Brasile 607
UA - Ucraina 492
VN - Vietnam 383
SE - Svezia 328
DE - Germania 314
GB - Regno Unito 313
FI - Finlandia 203
FR - Francia 195
AT - Austria 159
KR - Corea 130
CA - Canada 98
IE - Irlanda 98
JP - Giappone 76
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 17.747
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Città #
Milan 1.559
Ashburn 682
Woodbridge 634
San Jose 629
Chandler 592
Singapore 590
Santa Clara 515
Houston 489
Fairfield 423
Ann Arbor 420
Wilmington 300
Jacksonville 264
Hefei 246
Dearborn 217
Moscow 186
Cambridge 162
Boardman 159
Council Bluffs 158
Vienna 154
Seattle 153
The Dalles 150
North Charleston 130
Beijing 128
Lawrence 115
Medford 115
Dallas 110
Seoul 105
Los Angeles 102
Lauterbourg 100
Dublin 86
Helsinki 84
London 78
Ottawa 76
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
New York 34
Amsterdam 33
Bovisio Masciago 31
Orem 28
Brussels 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
Brooklyn 16
Frankfurt am Main 16
Atlanta 15
Berlin 14
Columbus 14
Warsaw 14
Haiphong 13
Istanbul 13
Norwalk 13
Phoenix 13
Amman 12
Harbin 12
Kent 12
Ribeirão Preto 12
Rio de Janeiro 12
Tianjin 12
Belo Horizonte 11
Delft 11
Falkenstein 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
Chicago 8
Denver 8
Oldham 8
Rho 8
Can Tho 7
Glasgow 7
Totale 11.290
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Nome #
An Approach to the Design of Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 463
Combining Two and Three-Body Dynamics for Low Energy Transfer Trajectories of Practical Interest 368
Amalia Mission Lunar Rover - the Conceptual Design of the Team Italia Rover, Candidate for the Google Lunar x Prize Challenge 298
Optimal Bi-Impulsive Earth-Moon Transfers 255
A Multi-Attribute Decision Making Approach Toward Space System Design Automation Through a Fuzzy Logic-Based Analytic Hierarchical Process 249
A Drill-Soil System Modelization for Future Mars Exploration 246
On-Comet Power Production: the Case of Rosetta Lander Philae 244
Scientific Use of the Sampler, Drill and Distribution Subsystem (SD2) 244
Power Production for Small Body Landers: Post-Launch Activities on Philae's Power Subsystem 241
LILT Measurements on Silicon Solar Cells of Rosetta Lander Philae 240
Aero-Gravity Assist Maneuvers: Controlled Dynamics Modeling and Optimization 237
Solar Array Simulators for Low Power Space Missions 231
A New Nuclear Powered Cycler to Mars 227
Rosetta Philae SD2 Drill System and Its Operation on 67p/Churyumov-Gerasimenko 227
Preliminary Design Global Optimization for Space Vehicles During Atmospheric Maneuvers 215
Planning and implementation of the on-comet operations of the instrument SD2 onboard the lander Philae of Rosetta mission 211
A Fuzzy Logic MADM Approach Towards the Spacecraft Design Automation 199
SD2 - a Cometary Soil Drill and Sampler Device 198
A Nuclear Powered Cycler Mission to Mars 195
Lessons Learned from the SD2 Operations on the Comet 67/P 195
A Distributed Approach for Space System Formation Operation Autonomous Planning and Scheduling 193
Space System Formation Planning and Scheduling: a Distributed Approach 193
State Tracking and Control of a Lifted Autonomous Space Vehicle During the Atmospheric Re-Entry Phase: a Lyapunov Approach 192
SD2: Technological/Scientific Instrument to Understand a Comet 191
SD2 - How to Sample a Comet 189
En Route Toward a Comet 184
A Minimum Energy Robotic Arm for Mars Exploration 183
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 175
In-Orbit Technology Validation for a University Microsatellite 175
Rosetta Philae Sampling Drilling and Distribution Subsystem: Operation and Results from the First On-Comet Phase 175
A MADM Approach Towards Space System Design Automation by a Fuzzy-Logic Based Analytic Hierarchical Process 172
A Vision System for Autonomous Landing Manoeuvres 172
Distributed Planning and Scheduling for Space System Flotillas 169
MonteCarlo Techniques for Thermal Analysis. Design Margin Determination Using Reduced Models and Experimental Data 168
Aero-Gravity Assist Maneuvers for Interplanetary Missions: Controlled Dynamics Modelling and Optimization 168
Multiobjective Global Optimization of Space Mission Design Using Evolutionary Methods and Interval Analysis 168
Application of the Multibody Approach to the Control of Robotic Manipulators 167
Preliminary Design and Operations of Palamede Microsatellite 167
Long Term Space Program Scheduling and System Design Optimization 167
Lessons Learned from the SD2 Operations on the Comet 67/P 167
MonteCarlo Techniques in Space Thermal Analysis with Reduced Models: Design of Experiment and Statistic of Extremes Tools Applicability 166
A Possible in Orbit Relativistic Experiment Mission with Very Accurate S/C Relative Control 164
A Space Engineering Summer School for European Students: Training on a Real Space Project 163
Preliminary Spacecraft Design: Genetic Algorithms and AHP to Support the Concurrent Process Approach 162
Interplanetary Mission Design with Aero-Assisted Manoeuvres Multi-Objective Evolutive Optimization 162
A Tool for Preliminary Design of Low Thrust Gravity-Assist Trajectories 162
Aero-Gravity Assist Manoeuvres Within Preliminary Interplanetary Mission Design: a Multi-Objective Evolutive Algorithm Approach 162
Optimal Formation Flying Reconfiguration and Station Keeping Maneuvers Using Low Thrust Propulsion 161
Design of Robust Drag-Free Controllers with Given Structure 161
Project PALAMEDE at Politecnico di Milano: a Real Satellite to Teach Satellites Design Techniques 160
Spacecraft Design as a Multi-Criteria Decision-Making 158
Fuzzy Inductive Reasoning and Possibilistic Logic for Space Systems Failure Smart Detection and Identification 158
Space Probe Multidisciplinary Design During Atmospheric Phases 157
Montecarlo Techiniques for Thermal Analysis of Space Vehicles: Practical Examples of Robustness Determination in Preliminary Design 157
SD2-Sampler, Drill and Distribution System 156
Large Multi-Hinged Space Systems: a Parametric Stability Analysis 155
Stochastic Analysis in Space Engineering: a Survay of Existing Tools and Methodologies for Thermal Analysis 152
High-Order Robust Guidance of Interplanetary Trajectories Based on Differential Algebra 151
"Spazio per tutti" : A Hands-On Experience toward Space Engineering 150
Fuzzy Logic and Decisional Processes Towards a Space System Activity Autonomous Scheduler 146
SD2: How to Drill a Comet 142
Sampler, Drill and Distribution System for in Situ Analysis of a Cometary Nucleus 140
Rosetta Mission: On-Comet Operation Planning for the Sampler, Drill and Distribution Subsystem 138
Extremely Accurate Line of Sight Control Between a Pointing and a Target Spacecraft 133
Fuzzy Logic in Spacecraft Design 133
Sampler, Drill and Distribution System for Cometary Soil Analysis 132
Rosetta Mission : the Solar Array Photovoltaic Assembly 131
Composites and Smart Materials for Structural Space Applications: a Review 130
Industria aerospaziale italiana: le attività in ambito spazio di Galileo Avionica s.p.a. 130
Spacecraft Attitude Control for Extremely Accurate Line of Sight Pointing 128
Feedback Dynamic Compensation via Multibody Models and Applications to Robot Control 127
An Educational Hands-On Experience Toward Space Engineering: "Spazio per Tutti" 123
Optimal Trajectory Generation and Control for Reconfiguration Maneuvers of Formation Flying Using Low-Thrust Propulsion 122
Space System Activity Scheduling Automation: a Decisional Theory Approach 121
Fuzzy Logic and Predicate Calculus to Automate the Spacecraft Activity Scheduling 119
Atmospheric Re-Entry Vehicles: a Lyapunov Approach to Track and Control the System States 119
Concurrent Processes Within Preliminary Spacecraft Design: an Autonomous Decisional Support Based on a Genetic Algorithms and Analytic Hierarchical Process 119
Globalisation of Aerospace Engineering Education 116
Mars Dust Devil Test Facility 116
Attitude Maneuvers of a Flexible Space Station by Means of Deployable Tethers 115
The Sample Drill and Distribution Subsystem of the Rosetta Lander 115
Modified Discrete-Time Velocity Feedback for Vibration Suppression of a LSS Laboratory Model 113
Spacecraft Design Automation with Fuzzy Multiple Criteria Decision Making 112
Particular Aspects of the Forced Response of Finite-Dimensional Modular Structures 111
Decisional Methods in Supporting Space System Design Processes 110
Experiment Proposal for the Detection of Possible Photons Trajectory Perturbation Caused by Maxwellian Fields 110
Robust Aero-Gravity Assisted Maneuvers for a Multi-Objective Interplanetary Trajectory Design Optimization 110
Italian Partecipation in the Mars Exploration Program 109
Interplanetary Mission Design with Aero-Assisted Manoeuvers Multi-Objective Evolutive Optimization 109
Equilibrium of a Large Multi-Hinged Space Sistems 108
Multi-Criteria Optimization for Space Mission Design: a New Approach 108
Multi-Criteria Design Optimization of a Space System with a Fuzzy Logic Approach 108
Economical Earth-Moon Transfers: a Quality Study 106
Interplanetary Mission Design with Aero-Assisted Manoeuvers Multi-Objective Evolutive Optimization 106
Scientific Use of the Sampler, Drill and Distribution Subsystem (SD2) 106
Space System Design Automation Through a Fuzzy Multi-Criteria Decision Making Approach 105
Shape and Vibration Control of a Multibody Flexible Structure Using Recurrent Neural Networks 105
Dynamics and Control of 1g Rotating Space Station 105
Lunar Orbital Dynamics by Finite Element in Time Method 105
Totale 16.457
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Categoria #
all - tutte 45.256
article - articoli 10.428
book - libri 0
conference - conferenze 33.069
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.759
Totale 90.512
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021116 0 0 0 0 0 0 0 0 0 0 0 116
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
2025/20267.241 1.077 1.057 431 565 304 334 930 353 715 859 421 195
Totale 17.834