ERCOLI, AMALIA
 Distribuzione geografica
Continente #
NA - Nord America 4.885
EU - Europa 2.757
AS - Asia 474
AF - Africa 19
OC - Oceania 8
SA - Sud America 7
Continente sconosciuto - Info sul continente non disponibili 5
Totale 8.155
Nazione #
US - Stati Uniti d'America 4.802
IT - Italia 910
UA - Ucraina 479
SE - Svezia 317
CN - Cina 270
DE - Germania 260
GB - Regno Unito 183
FI - Finlandia 153
AT - Austria 150
VN - Vietnam 96
IE - Irlanda 84
CA - Canada 79
FR - Francia 53
ES - Italia 51
NL - Olanda 45
BE - Belgio 28
KR - Corea 21
JP - Giappone 20
IN - India 19
CI - Costa d'Avorio 15
RU - Federazione Russa 13
TR - Turchia 13
JO - Giordania 9
AU - Australia 8
IR - Iran 8
BR - Brasile 7
RO - Romania 7
CH - Svizzera 5
EU - Europa 5
NO - Norvegia 5
GR - Grecia 4
LU - Lussemburgo 4
MX - Messico 3
PH - Filippine 3
SG - Singapore 3
TH - Thailandia 3
HK - Hong Kong 2
MU - Mauritius 2
MW - Malawi 2
MY - Malesia 2
PL - Polonia 2
AE - Emirati Arabi Uniti 1
BA - Bosnia-Erzegovina 1
HN - Honduras 1
ID - Indonesia 1
IQ - Iraq 1
PK - Pakistan 1
PT - Portogallo 1
RS - Serbia 1
SA - Arabia Saudita 1
SI - Slovenia 1
Totale 8.155
Città #
Woodbridge 633
Chandler 592
Houston 477
Fairfield 423
Ann Arbor 420
Milan 371
Wilmington 299
Jacksonville 263
Dearborn 217
Ashburn 208
Cambridge 162
Seattle 152
Vienna 149
Lawrence 115
Medford 115
Ottawa 75
Beijing 74
Dublin 74
Chongqing 54
Dong Ket 47
Málaga 47
Helsinki 38
Boardman 32
Bovisio Masciago 31
Amsterdam 24
Brussels 24
Des Moines 24
Zibido San Giacomo 23
Guangzhou 22
San Diego 22
Redwood City 20
Seongnam 17
Abidjan 15
Chengdu 15
Norwalk 13
Turin 13
Berlin 11
Delft 11
Harbin 11
Rome 11
Verona 11
Istanbul 10
Amman 9
Nanjing 9
Shanghai 9
Auburn Hills 8
Rho 8
Zhengzhou 8
Los Angeles 7
Oldham 7
Cornate 6
Hangzhou 6
Italy 6
London 6
Tokyo 6
Xian 6
Alcamo 5
Hebei 5
Hefei 5
Monza 5
Pescara 5
Segrate 5
Aylesbury 4
Breistein 4
Cinisello Balsamo 4
Columbus 4
Crema 4
Irvine 4
Kunming 4
Lafayette 4
Mountain View 4
Nanchang 4
Nova Milanese 4
San Giuliano 4
Vaprio D'adda 4
Varese 4
Ardgay 3
Athens 3
Brescia 3
Changchun 3
Dallas 3
Decatur 3
Duncan 3
Gunzenhausen 3
Jinan 3
Lucca 3
Marcon 3
Mexico 3
Miami 3
New York 3
Nice 3
Novara 3
Osnago 3
Philadelphia 3
Providence 3
Rossens 3
Scafati 3
Sydney 3
Tavagnasco 3
Thames Ditton 3
Totale 5.624
Nome #
Amalia Mission Lunar Rover - the Conceptual Design of the Team Italia Rover, Candidate for the Google Lunar x Prize Challenge 200
Scientific Use of the Sampler, Drill and Distribution Subsystem (SD2) 167
An Approach to the Design of Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 161
Aero-Gravity Assist Maneuvers: Controlled Dynamics Modeling and Optimization 148
A Drill-Soil System Modelization for Future Mars Exploration 147
Preliminary Design Global Optimization for Space Vehicles During Atmospheric Maneuvers 142
Rosetta Philae SD2 Drill System and Its Operation on 67p/Churyumov-Gerasimenko 138
Planning and implementation of the on-comet operations of the instrument SD2 onboard the lander Philae of Rosetta mission 138
A Multi-Attribute Decision Making Approach Toward Space System Design Automation Through a Fuzzy Logic-Based Analytic Hierarchical Process 133
Combining Two and Three-Body Dynamics for Low Energy Transfer Trajectories of Practical Interest 130
SD2 - a Cometary Soil Drill and Sampler Device 122
Space System Formation Planning and Scheduling: a Distributed Approach 118
Equilibrium Analysis of a Large Multi-Hinged Space System 116
Design of Robust Drag-Free Controllers with Given Structure 113
SD2: Technological/Scientific Instrument to Understand a Comet 107
Atmospheric Re-Entry Trajectory Tracking and Control for an Unmanned Space Vehicle with a Lyapunov Approach 103
Stochastic Analysis in Space Engineering: a Survay of Existing Tools and Methodologies for Thermal Analysis 103
Lessons Learned from the SD2 Operations on the Comet 67/P 100
Lessons Learned from the SD2 Operations on the Comet 67/P 100
A New Nuclear Powered Cycler to Mars 98
Preliminary Spacecraft Design: Genetic Algorithms and AHP to Support the Concurrent Process Approach 98
Multiobjective Global Optimization of Space Mission Design Using Evolutionary Methods and Interval Analysis 98
Interplanetary Mission Design with Aero-Assisted Manoeuvres Multi-Objective Evolutive Optimization 98
A Nuclear Powered Cycler Mission to Mars 98
Spacecraft Design as a Multi-Criteria Decision-Making 94
High-Order Robust Guidance of Interplanetary Trajectories Based on Differential Algebra 94
Optimal Formation Flying Reconfiguration and Station Keeping Maneuvers Using Low Thrust Propulsion 93
SD2 - How to Sample a Comet 92
Rosetta Philae Sampling Drilling and Distribution Subsystem: Operation and Results from the First On-Comet Phase 92
Project PALAMEDE at Politecnico di Milano: a Real Satellite to Teach Satellites Design Techniques 89
Large Multi-Hinged Space Systems: a Parametric Stability Analysis 88
State Tracking and Control of a Lifted Autonomous Space Vehicle During the Atmospheric Re-Entry Phase: a Lyapunov Approach 86
A Fuzzy Logic MADM Approach Towards the Spacecraft Design Automation 85
Preliminary Design and Operations of Palamede Microsatellite 84
In-Orbit Technology Validation for a University Microsatellite 82
MonteCarlo Techniques for Thermal Analysis. Design Margin Determination Using Reduced Models and Experimental Data 81
Space Probe Multidisciplinary Design During Atmospheric Phases 81
A Minimum Energy Robotic Arm for Mars Exploration 80
Fuzzy Inductive Reasoning and Possibilistic Logic for Space Systems Failure Smart Detection and Identification 79
Composites and Smart Materials for Structural Space Applications: a Review 76
Distributed Planning and Scheduling for Space System Flotillas 76
A Vision System for Autonomous Landing Manoeuvres 76
A Distributed Approach for Space System Formation Operation Autonomous Planning and Scheduling 75
En Route Toward a Comet 75
Montecarlo Techiniques for Thermal Analysis of Space Vehicles: Practical Examples of Robustness Determination in Preliminary Design 75
MonteCarlo Techniques in Space Thermal Analysis with Reduced Models: Design of Experiment and Statistic of Extremes Tools Applicability 74
Fuzzy Logic in Spacecraft Design 74
Industria aerospaziale italiana: le attività in ambito spazio di Galileo Avionica s.p.a. 73
A MADM Approach Towards Space System Design Automation by a Fuzzy-Logic Based Analytic Hierarchical Process 70
Aero-Gravity Assist Maneuvers for Interplanetary Missions: Controlled Dynamics Modelling and Optimization 70
Aero-Gravity Assist Manoeuvres Within Preliminary Interplanetary Mission Design: a Multi-Objective Evolutive Algorithm Approach 69
Spacecraft Design Automation with Fuzzy Multiple Criteria Decision Making 67
Long Term Space Program Scheduling and System Design Optimization 67
Globalisation of Aerospace Engineering Education 66
Atmospheric Re-Entry Vehicles: a Lyapunov Approach to Track and Control the System States 64
Fuzzy Logic and Decisional Processes Towards a Space System Activity Autonomous Scheduler 64
SD2-Sampler, Drill and Distribution System 64
Modified Discrete-Time Velocity Feedback for Vibration Suppression of a LSS Laboratory Model 63
SD2: How to Drill a Comet 63
Sampler, Drill and Distribution System for in Situ Analysis of a Cometary Nucleus 60
A Tool for Preliminary Design of Low Thrust Gravity-Assist Trajectories 60
Space System Activity Scheduling Automation: a Decisional Theory Approach 59
Application of the Multibody Approach to the Control of Robotic Manipulators 59
A Possible in Orbit Relativistic Experiment Mission with Very Accurate S/C Relative Control 57
Fuzzy Logic and Predicate Calculus to Automate the Spacecraft Activity Scheduling 57
Rosetta Mission : the Solar Array Photovoltaic Assembly 57
Italian Partecipation in the Mars Exploration Program 56
Optimal Trajectory Generation and Control for Reconfiguration Maneuvers of Formation Flying Using Low-Thrust Propulsion 56
Rosetta Mission: On-Comet Operation Planning for the Sampler, Drill and Distribution Subsystem 56
Equilibrium of a Large Multi-Hinged Space Sistems 55
Experiment Proposal for the Detection of Possible Photons Trajectory Perturbation Caused by Maxwellian Fields 55
Spacecraft Attitude Control for Extremely Accurate Line of Sight Pointing 54
Concurrent Processes Within Preliminary Spacecraft Design: an Autonomous Decisional Support Based on a Genetic Algorithms and Analytic Hierarchical Process 53
Extremely Accurate Line of Sight Control Between a Pointing and a Target Spacecraft 53
Decisional Methods in Supporting Space System Design Processes 53
Attitude Maneuvers of a Flexible Space Station by Means of Deployable Tethers 53
Space System Design Automation Through a Fuzzy Multi-Criteria Decision Making Approach 53
Sampler, Drill and Distribution System for Cometary Soil Analysis 53
Economical Earth-Moon Transfers: a Quality Study 52
A Space Engineering Summer School for European Students: Training on a Real Space Project 52
Interplanetary Mission Design with Aero-Assisted Manoeuvers Multi-Objective Evolutive Optimization 51
Scientific Use of the Sampler, Drill and Distribution Subsystem (SD2) 51
Multi-Criteria Design Optimization of a Space System with a Fuzzy Logic Approach 51
Particular Aspects of the Forced Response of Finite-Dimensional Modular Structures 50
Large Multi-Hinged Space System: a Parametric Stability Analysis 48
Multi-Criteria Optimization for Space Mission Design: a New Approach 48
Optimal Bi-Impulsive Earth-Moon Transfers 48
"Spazio per tutti" : A Hands-On Experience toward Space Engineering 46
Interplanetary Mission Design with Aero-Assisted Manoeuvers Multi-Objective Evolutive Optimization 46
An Educational Hands-On Experience Toward Space Engineering: "Spazio per Tutti" 45
Feedback Dynamic Compensation via Multibody Models and Applications to Robot Control 44
Shape and Vibration Control of a Multibody Flexible Structure Using Recurrent Neural Networks 44
The Sample Drill and Distribution Subsystem of the Rosetta Lander 44
Optimal Attitude Trajectory Manoeuvre for Moon Landing 43
Robust Aero-Gravity Assisted Maneuvers for a Multi-Objective Interplanetary Trajectory Design Optimization 43
Re-Entry Phase of an Unmanned Lifted Vehicle: 3-D Attitude Dynamics Control with a Lyapunov Approach 42
Modular Large Space Structures Dynamics 42
Multi-Disciplinary Optimisation for Space Vehicles During Aeroassisted Manoeuvres: an Evolutionary Algorithm Approach 40
Lunar Orbital Dynamics by Finite Element in Time Method 40
Mars Dust Devil Test Facility 38
Totale 7.744
Categoria #
all - tutte 19.145
article - articoli 5.156
book - libri 0
conference - conferenze 13.308
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 681
Totale 38.290


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019322 0 0 0 0 0 0 0 0 0 0 164 158
2019/20201.601 137 154 32 114 175 189 205 95 202 56 187 55
2020/20211.163 112 34 111 72 125 101 100 145 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
2023/2024540 46 111 26 51 31 39 36 27 127 46 0 0
Totale 8.230