GALATOLO, ROBERTO
 Distribuzione geografica
Continente #
NA - Nord America 10.016
EU - Europa 6.764
AS - Asia 2.216
AF - Africa 150
SA - Sud America 38
OC - Oceania 16
Continente sconosciuto - Info sul continente non disponibili 12
Totale 19.212
Nazione #
US - Stati Uniti d'America 9.553
IT - Italia 3.021
CN - Cina 1.208
SE - Svezia 1.106
BG - Bulgaria 639
DE - Germania 529
CA - Canada 457
UA - Ucraina 424
SG - Singapore 288
GB - Regno Unito 262
FI - Finlandia 257
VN - Vietnam 234
TR - Turchia 206
CH - Svizzera 161
CI - Costa d'Avorio 134
RU - Federazione Russa 90
FR - Francia 75
HK - Hong Kong 73
BE - Belgio 72
JP - Giappone 67
IN - India 57
KR - Corea 28
AT - Austria 22
BR - Brasile 19
GR - Grecia 16
PL - Polonia 15
NL - Olanda 14
IR - Iran 13
ES - Italia 12
EU - Europa 12
EC - Ecuador 11
PK - Pakistan 11
AU - Australia 10
PT - Portogallo 9
TW - Taiwan 9
CZ - Repubblica Ceca 8
AL - Albania 7
MX - Messico 6
NZ - Nuova Zelanda 6
DK - Danimarca 5
DZ - Algeria 5
ID - Indonesia 5
CO - Colombia 4
MY - Malesia 4
RO - Romania 4
RS - Serbia 4
SN - Senegal 4
EG - Egitto 3
IE - Irlanda 3
IL - Israele 3
NO - Norvegia 3
PE - Perù 3
AE - Emirati Arabi Uniti 2
HR - Croazia 2
PH - Filippine 2
SC - Seychelles 2
TH - Thailandia 2
ZA - Sudafrica 2
CL - Cile 1
EE - Estonia 1
HU - Ungheria 1
KH - Cambogia 1
KZ - Kazakistan 1
LV - Lettonia 1
MD - Moldavia 1
SA - Arabia Saudita 1
SY - Repubblica araba siriana 1
Totale 19.212
Città #
Chandler 1.300
Woodbridge 1.259
Ann Arbor 1.235
Houston 843
Serra 768
Sofia 638
Milan 570
Jacksonville 549
Beijing 454
Ottawa 448
New York 388
Fairfield 361
Ashburn 273
Princeton 252
Lawrence 240
Wilmington 208
Des Moines 196
Nanjing 195
Izmir 168
Bern 150
Seattle 145
Cambridge 137
Dearborn 136
Abidjan 134
Medford 133
Singapore 124
Rome 114
Jüchen 106
Nanchang 95
Dong Ket 85
Boulder 84
Pisa 73
Lancaster 63
Florence 62
Boardman 60
Hong Kong 59
Kunming 57
Redwood City 56
Ogden 44
Shenyang 42
Changsha 40
Pune 40
Falls Church 38
Hebei 35
Brussels 34
Auburn Hills 31
Jiaxing 30
Tokyo 30
Hefei 29
Guangzhou 28
Los Angeles 28
San Diego 28
Tianjin 26
Alessandria 25
Norwalk 24
Düsseldorf 22
Hangzhou 22
Indiana 20
Shanghai 20
Lucca 19
Torino 19
Verona 19
Jinan 18
Livorno 18
Vienna 18
Phoenix 16
Washington 15
Bologna 14
Nürnberg 14
Turin 14
Istanbul 13
Caserta 12
Orange 12
Palermo 12
Tagliacozzo 12
Guayaquil 11
Chengdu 10
Duncan 10
Frankfurt am Main 10
Perugia 10
Bari 9
Castelnuovo Bormida 9
Centro 9
Ningbo 9
Scherpenheuvel 9
Brindisi 8
Cascina 8
Naples 8
Parma 8
Seoul 8
Zhengzhou 8
Genova 7
Lanzhou 7
Marseille 7
Taipei 7
Tirana 7
Meudon 6
Padova 6
Pistoia 6
Tappahannock 6
Totale 13.302
Nome #
Introduzione all’ambiente di simulazione Modelica-Dymola ed esempi di modellizzazione di sistemi multifisici 255
Modellizzazione di attuatori servoidraulici per comandi primari di volo, con servovalvole ad azionamento diretto (DDV) 162
Multi-hole probe and elaboration algorithms for the reconstruction of the air data parameters 162
null 149
Conflict detection and resolution algorithms for UAVs collision avoidance 148
Fatigue crack growth of multiple interacting cracks: Analytical models and experimental validation 140
Experimental assessment of the dynamic stiffness of a fault-tolerant fly-by-wire hydraulic actuator 138
A solution to detect and avoid conflicts for civil remotely piloted aircraft systems into non-segregated airspaces 135
Modelling and control design of a novel robotic membrane 134
Fractographic and microstructural analysis of fatigue crack growth in a Ti-6Al-4V fan disc forging 132
Phenomenological Description of the Fatigue Crack Growth Test Results in IN718 Corner Crack Specimens for Brite Euram Programme BE-3379, Report n. 17 132
Air Data Computation in Fly By Wire Flight Control Systems 132
Impact of Safety Requirements on the Weight of Civil Unmanned Aerial Vehicles 130
Air Data Computation Using Neural Networks 130
AW149 Actuator Closed-Loop Control Design 128
OBJECT-ORIENTED MODELLING OF FLIGHT CONTROL ACTUATION SYSTEMS FOR POWER ABSORPTION ASSESSMENT 124
Short crack observations in Ti-6Al-4V under constant amplitude loading 122
Compression tests on bonded stiffened panels built by Aeritalia G.V.T 121
Short fatigue crack growth behaviour in Ti-6Al-4V 121
null 121
Electro-mechanical actuator for helicopter landing gear extension/retraction: experimental study and dynamic model validation 117
CONTROLLO AMBIENTALE CON MINI AERIAL VEHICLE PROGETTO SIMONA/MAV 116
Co-Simulation for Design, Optimization and Analysis of All-Electric Aircraft Systems 116
Compression tests on stiffened bonded panels 115
Fractographic and microstructural analysis of fatigue crack growth in a Ti-6Al-4V fan disc forging 115
null 114
null 113
Robust force control in a hydraulic workbench for flight actuators 112
null 112
Fatigue Crack Growth Test Results on Corner Crack Specimens for Brite Euram Programme BE3379: Effect of the Complex Loading Sequences in IN718, Report n. 16 111
Residual Strenght Tests on Stiffened Panels (GLARE Material) 108
Model-based health-monitoring of an electro-mechanical actuator for unmanned aerial system flight controls 108
Compression tests on stiffened panels built by Aeritalia G.V.T 107
Crack closure measurements under spectrum loading 107
An AHRS Based on a Kalman Filter for the Integration of Inertial, Magnetometric and GPS Data 106
null 106
Influence of turning parameters on the high-temperature fatigue performance of Inconel 718 superalloy 106
Wind identification via Kalman filter for aircraft flow angles calibration 106
Fault-Tolerant Procedures for Air Data Elaboration 103
Crack propagation under constant amplitude and spectrum loading in a nichel based superalloy 102
null 102
Significance of short fatigue cracks for aircraft and crack growth data for 2024-T3 aluminium alloy 100
ANALISI CFD PER LA CARATTERIZZAZIONE DEL FLUSSO IN UNA SERVOVALVOLA ELETTROIDRAULICA 100
EMA motor control loop 99
null 99
Full-Scale crack propagation test on spinning turbine disks using the potential drop technique 98
null 98
null 97
Power Absorption Characterisation of Electro-Mechanical Flight Control Actuators via Detailed System Modelling 96
BRITE EURAM BE-3379, Task 3: The Potential Drop Technique for Crack Monitoring on Rotating Disks: Experimental check of the Calibration Curves, Report n. 11 95
Crack propagation from artificial defects in typical engine disk materials; interpretation of experimental results by means of 3D J Integral 94
Crack propagation under constant amplitude and spectrum loading in a nichel based superalloy 94
Test di Fatica Oligociclica in Temperatura: Risultati ottenuti dai provini del Lotto 4 93
EMAS control loop 92
High temperature fatigue crack propagation on Waspalloy material under spectrum loading 91
La sperimentazione a fatica in aeronautica e il suo ruolo nella affidabilità delle strutture 91
Prediction of fatigue crack growth in a Ti-6Al-4V fan disk forging under spectrum loading 91
Modellizzazione di attuatori servoidraulici lineari per la movimentazione delle superfici primarie dei velivoli e progettazione del controllo di posizione 91
Modelling and Simulation of a Fault-tolerant Electrical Motor for Aerospace Servovalves with Modelica 91
Model-based prognostic health-management algorithms for the freeplay identification in electromechanical flight control actuators 91
BRITE EURAM BE-3379, Task 3: The Potential Drop Technique for Crack Monitoring on Rotating Disks: Experimental Results of the Spinning Test, Report n. 19 90
Programma di Calcolo MVP-CARD: Acquisizione ed Elaborazione di Immagini. Manuale d'Uso e Manuale del Programmatore 90
Fatigue Threshold and Fracture Toughness Automatic Testing at High Temperature 90
Smart air-data probe for fault-tolerant flow measurements 90
Modello linearizzato della dinamica di un attuatore servoidraulico asimmetrico per aerofreno 89
State-Of-The-Art Study on Ema Technology 89
AW149 Actuator Simulation: Actuator Model Adaptation 89
Prediction of fatigue crack growth in Ti-6Al-4V engine disk material under the loading sequence Turbistan 88
Applicability of the commonly used fracture mechanics tools to the prediction of the residual strength of Glare 88
Real-Time Hardware-in-the-loop Simulation of Fly-by-Wire Flight Control Systems 88
null 88
OBJECT DETECTION AND TRACKING ALGORITHMS BASED ON KLT FEATURE TRACKER FOR A SENSE AND AVOID SYSTEM 88
Development of a Flight Management System Within the UAV - SCAUT Project 87
An AHRS Based on a Kalmann Filter for the Integration of Inertial, Magnetometric and GPS Data 87
null 87
Simulation and Experiments for the Study of a Fault-Tolerant Hydraulic Actuator for Fly-By-Wire Helicopters 86
Progetto Vulcano 127. Determinazione dei punti di impatto per le avarie maggiormente critiche del dimostratore Dim_1374_03 (ROLLCTRL) 86
Test di fatica oligociclica in temperatura: messa a punto dell’attrezzatura e procedura di prova 86
Fatigue Crack Propagation in Residual Stress Field of Welded Plates 84
Characterisation of the Extension/Retraction Dynamics of Electrically Powered Landing Gears 84
Power absorption assessment of flight control actuation systems via object-oriented modelling 84
Test di Fatica Oligociclica in Temperatura: Risultati ottenuti dai provini del Lotto 2 84
Applicazione dei materiali Powder Metal nella costruzione dei dischi di turbina dei motori aeronautici; stato attuale delle conoscenze e impostazione di un programma di ricerca 83
BRITE EURAM BE-3379, Task 3: The Potential Drop Technique for Crack Monitoring on Rotating Disks 83
Procedure e modelli per la simulazione dei dati-aria 83
Sviluppo di una sonda multi-pressione e di algoritmi di elaborazione per la ricostruzione dei parametri di volo 83
Sviluppo di una sonda multi-pressione e di algoritmi di elaborazione per la ricostruzione dei parametri di volo 83
Fatigue Crack Growth Threshold at High Temperature on Engine Disk Superalloys 82
Analisi delle prestazioni di una sonda multifunzione per il rilevamento dei dati-aria 82
Simulazione SW completa del Flight Control System 82
AW149 De-Risk Actuator: Rotary Ddv Model Development And Validation 82
AW149 De-Risk Actuator: Actuator Model Development And Validation 82
Test di Fatica Oligociclica in Temperatura: Risultati ottenuti dai provini del Lotto 3 82
null 82
Caratterizzazione della fase di propagazione di fessure per fatica ad alta temperatura nelle superleghe a base nickel AP1 e AF115 81
L'analisi dell'immagine nella sperimentazione a fatica 81
GRA AEA WP3.2 - Questionnaire on methods and tools for Energy Management v.2 81
Traffic-Separation and Collision-Avoidance Strategy to Promote Civil Applications of UAVs 81
Multibody analysis and design of an electromechanical system simulating hyperelastic membranes 81
Attività del Dipartimento di Ingegneria Aerospaziale dell’Università di Pisa nell’Ambito del Progetto UAV-SCAUT 80
Totale 10.315
Categoria #
all - tutte 44.862
article - articoli 0
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 44.862


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20202.809 357 303 569 115 198 213 251 92 203 184 280 44
2020/20211.400 131 42 129 54 187 59 113 135 103 100 74 273
2021/20222.540 35 224 52 111 519 449 71 108 145 72 118 636
2022/20233.153 370 329 295 338 378 479 29 231 487 11 157 49
2023/20242.568 389 282 320 147 343 435 114 95 71 47 81 244
2024/202528 28 0 0 0 0 0 0 0 0 0 0 0
Totale 19.506