CINECA IRIS Institutional Research Information System

GALATOLO, ROBERTO
 Distribuzione geografica
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Continente #
NA - Nord America 15.647
AS - Asia 9.469
EU - Europa 8.180
SA - Sud America 956
AF - Africa 293
OC - Oceania 22
Continente sconosciuto - Info sul continente non disponibili 13
Totale 34.580
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Nazione #
US - Stati Uniti d'America 15.013
IT - Italia 3.289
SG - Singapore 2.873
CN - Cina 2.854
HK - Hong Kong 1.396
SE - Svezia 1.118
BR - Brasile 786
DE - Germania 733
BG - Bulgaria 641
VN - Vietnam 632
CA - Canada 526
UA - Ucraina 436
KR - Corea 413
GB - Regno Unito 402
FI - Finlandia 401
TR - Turchia 368
FR - Francia 339
RU - Federazione Russa 298
JP - Giappone 285
IN - India 206
CH - Svizzera 169
CI - Costa d'Avorio 135
BD - Bangladesh 83
BE - Belgio 75
IQ - Iraq 70
NL - Olanda 62
AR - Argentina 59
MX - Messico 51
SA - Arabia Saudita 47
PL - Polonia 40
PK - Pakistan 39
ZA - Sudafrica 38
EC - Ecuador 33
AT - Austria 29
ES - Italia 27
KE - Kenya 26
UZ - Uzbekistan 25
ID - Indonesia 24
GR - Grecia 23
MA - Marocco 20
VE - Venezuela 19
IR - Iran 18
PH - Filippine 17
CO - Colombia 16
NP - Nepal 15
AU - Australia 14
JO - Giordania 14
EG - Egitto 13
IE - Irlanda 13
AL - Albania 12
DZ - Algeria 12
EU - Europa 12
JM - Giamaica 12
AE - Emirati Arabi Uniti 11
PT - Portogallo 11
TW - Taiwan 11
CL - Cile 10
CZ - Repubblica Ceca 10
LT - Lituania 10
PY - Paraguay 10
TN - Tunisia 10
BJ - Benin 9
OM - Oman 9
SN - Senegal 9
UY - Uruguay 9
CR - Costa Rica 8
IL - Israele 8
MY - Malesia 8
PE - Perù 8
BB - Barbados 7
NZ - Nuova Zelanda 7
RS - Serbia 7
TT - Trinidad e Tobago 7
DO - Repubblica Dominicana 6
ET - Etiopia 6
NO - Norvegia 6
RO - Romania 6
DK - Danimarca 5
LB - Libano 5
LK - Sri Lanka 5
AM - Armenia 4
KZ - Kazakistan 4
PA - Panama 4
PS - Palestinian Territory 4
SI - Slovenia 4
AO - Angola 3
BO - Bolivia 3
GT - Guatemala 3
GY - Guiana 3
HN - Honduras 3
HU - Ungheria 3
KG - Kirghizistan 3
LA - Repubblica Popolare Democratica del Laos 3
MD - Moldavia 3
TH - Thailandia 3
BW - Botswana 2
BZ - Belize 2
EE - Estonia 2
HR - Croazia 2
KW - Kuwait 2
Totale 34.549
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Città #
Singapore 1.660
Hong Kong 1.359
Chandler 1.300
Ashburn 1.292
Woodbridge 1.260
Ann Arbor 1.235
Dallas 1.134
Santa Clara 1.079
Houston 849
San Jose 827
Serra 769
Sofia 639
Milan 597
Beijing 557
Shanghai 556
Jacksonville 550
Hefei 526
Ottawa 452
New York 425
Seoul 389
Fairfield 361
Boardman 322
Princeton 252
Lawrence 240
Tokyo 237
Lauterbourg 217
Wilmington 208
Los Angeles 207
Des Moines 199
Nanjing 196
Izmir 169
Bern 150
Seattle 149
Rome 143
Cambridge 137
Dearborn 137
Abidjan 135
Medford 134
Ho Chi Minh City 130
Helsinki 114
Istanbul 107
Jüchen 106
Hanoi 100
Nanchang 95
Buffalo 91
Redondo Beach 88
Council Bluffs 85
Dong Ket 85
Boulder 84
Pisa 83
Florence 70
Munich 69
Orem 69
Lancaster 63
São Paulo 59
Kunming 58
Redwood City 56
Frankfurt am Main 50
Ogden 44
Pune 43
Shenyang 42
Changsha 41
Düsseldorf 39
Falls Church 38
Brussels 37
Guangzhou 36
Hebei 35
Brasília 34
Rio de Janeiro 34
Baghdad 32
Auburn Hills 31
Jiaxing 30
Chennai 29
Columbus 29
San Diego 29
The Dalles 29
Turin 28
Turku 28
Lucca 27
Tianjin 27
Alessandria 25
Norwalk 24
Hangzhou 23
London 23
Riyadh 23
Tashkent 23
Ankara 22
Livorno 22
Phoenix 22
Verona 22
Warsaw 22
Da Nang 21
Falkenstein 21
Manchester 21
Vienna 21
Dhaka 20
Indiana 20
Nairobi 20
Jinan 19
Torino 19
Totale 23.885
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Nome #
Condition monitoring of a morphing laminate with MFC piezoelectric patches via model-based approach 463
Introduzione all’ambiente di simulazione Modelica-Dymola ed esempi di modellizzazione di sistemi multifisici 452
Development and experimental validation of a Sense-and-Avoid System for a mini-UAV 431
Fault-Tolerant Control of a Three-Phase Permanent Magnet Synchronous Motor for Lightweight UAV Propellers via Central Point Drive 249
Fatigue crack growth of multiple interacting cracks: Analytical models and experimental validation 226
Conflict detection and resolution algorithms for UAVs collision avoidance 226
Modelling and control design of a novel robotic membrane 225
Phenomenological Description of the Fatigue Crack Growth Test Results in IN718 Corner Crack Specimens for Brite Euram Programme BE-3379, Report n. 17 221
Fractographic and microstructural analysis of fatigue crack growth in a Ti-6Al-4V fan disc forging 219
Co-Simulation for Design, Optimization and Analysis of All-Electric Aircraft Systems 217
Short fatigue crack growth behaviour in Ti-6Al-4V 215
Modellizzazione di attuatori servoidraulici per comandi primari di volo, con servovalvole ad azionamento diretto (DDV) 213
Multi-hole probe and elaboration algorithms for the reconstruction of the air data parameters 209
Short crack observations in Ti-6Al-4V under constant amplitude loading 199
OBJECT-ORIENTED MODELLING OF FLIGHT CONTROL ACTUATION SYSTEMS FOR POWER ABSORPTION ASSESSMENT 198
Compression tests on stiffened bonded panels 197
Fatigue Crack Growth Test Results on Corner Crack Specimens for Brite Euram Programme BE3379: Effect of the Complex Loading Sequences in IN718, Report n. 16 193
A solution to detect and avoid conflicts for civil remotely piloted aircraft systems into non-segregated airspaces 191
Air Data Computation in Fly By Wire Flight Control Systems 190
OBJECT DETECTION AND TRACKING ALGORITHMS BASED ON KLT FEATURE TRACKER FOR A SENSE AND AVOID SYSTEM 189
Compression tests on bonded stiffened panels built by Aeritalia G.V.T 187
Impact of Safety Requirements on the Weight of Civil Unmanned Aerial Vehicles 186
Experimental assessment of the dynamic stiffness of a fault-tolerant fly-by-wire hydraulic actuator 184
Air Data Computation Using Neural Networks 183
Compression tests on stiffened panels built by Aeritalia G.V.T 181
Fractographic and microstructural analysis of fatigue crack growth in a Ti-6Al-4V fan disc forging 181
An AHRS Based on a Kalman Filter for the Integration of Inertial, Magnetometric and GPS Data 181
Electro-mechanical actuator for helicopter landing gear extension/retraction: experimental study and dynamic model validation 181
Model-based prognostic health-management algorithms for the freeplay identification in electromechanical flight control actuators 180
Fault-Tolerant Control of a Dual-Stator PMSM for the Full-Electric Propulsion of a Lightweight Fixed-Wing UAV 179
Crack propagation under constant amplitude and spectrum loading in a nichel based superalloy 175
Prediction of fatigue crack growth in a Ti-6Al-4V fan disk forging under spectrum loading 173
Model-based health-monitoring of an electro-mechanical actuator for unmanned aerial system flight controls 173
CONTROLLO AMBIENTALE CON MINI AERIAL VEHICLE PROGETTO SIMONA/MAV 172
Novel approach to fault-tolerant control of inter-turn short circuits in permanent magnet synchronous motors for UAV propellers 171
Crack propagation under constant amplitude and spectrum loading in a nichel based superalloy 171
Crack closure measurements under spectrum loading 171
Influence of turning parameters on the high-temperature fatigue performance of Inconel 718 superalloy 171
High temperature fatigue crack propagation on Waspalloy material under spectrum loading 170
AW149 Actuator Closed-Loop Control Design 169
Programma di Calcolo MVP-CARD: Acquisizione ed Elaborazione di Immagini. Manuale d'Uso e Manuale del Programmatore 168
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 165
Power Absorption Characterisation of Electro-Mechanical Flight Control Actuators via Detailed System Modelling 165
Applicabilità dei criteri Damage Tolerance al progetto dei dischi di turbina di motori per aviazione 164
BRITE EURAM BE-3379, Task 3: The Potential Drop Technique for Crack Monitoring on Rotating Disks: Experimental check of the Calibration Curves, Report n. 11 164
Wind identification via Kalman filter for aircraft flow angles calibration 164
Sul progetto a fatica dei dischi di turbina dei motori aeronautici di nuova generazione 163
La sperimentazione a fatica in aeronautica e il suo ruolo nella affidabilità delle strutture 163
Robust force control in a hydraulic workbench for flight actuators 162
Residual Strenght Tests on Stiffened Panels (GLARE Material) 161
Prediction of fatigue crack growth in Ti-6Al-4V engine disk material under the loading sequence Turbistan 160
Full-Scale crack propagation test on spinning turbine disks using the potential drop technique 160
Calcolo degli errori del sistema Dati Aria in Flow Fail Mode (alfa, beta nose boom) 160
Crack propagation from artificial defects in typical engine disk materials; interpretation of experimental results by means of 3D J Integral 159
Significance of short fatigue cracks for aircraft and crack growth data for 2024-T3 aluminium alloy 158
Caratterizzazione della fase di propagazione di fessure per fatica ad alta temperatura nelle superleghe a base nickel AP1 e AF115 156
BRITE EURAM BE-3379, Task 3: The Potential Drop Technique for Crack Monitoring on Rotating Disks 155
BRITE EURAM BE-3379, Task 3: The Potential Drop Technique for Crack Monitoring on Rotating Disks: Experimental Results of the Spinning Test, Report n. 19 155
Fatigue Threshold and Fracture Toughness Automatic Testing at High Temperature 154
EMA motor control loop 154
Smart air-data probe for fault-tolerant flow measurements 154
Fault-Tolerant Procedures for Air Data Elaboration 152
Development of a Flight Management System Within the UAV - SCAUT Project 152
Caratterizzazione della fase di propagazione di fessure per fatica ad alta temperatura in presenza di carichi ad ampiezza costante e ad ampiezza variabile sulla superlega Waspalloy 151
Caratterizzazione della fase di propagazione di fessure per fatica nella lega IN100 alla temperatura di 450 °C 151
ANALISI CFD PER LA CARATTERIZZAZIONE DEL FLUSSO IN UNA SERVOVALVOLA ELETTROIDRAULICA 150
Multibody analysis and design of an electromechanical system simulating hyperelastic membranes 150
Characterisation of the Extension/Retraction Dynamics of Electrically Powered Landing Gears 149
null 149
SENSE AND AVOID SYSTEM FOR A MINI UAV BASED ON DATA FUSION BETWEEN ELECTRO-OPTICAL AND RADAR SENSORS 148
Fatigue Crack Propagation in Residual Stress Field of Welded Plates 147
Traffic-Separation and Collision-Avoidance Strategy to Promote Civil Applications of UAVs 147
Test di Fatica Oligociclica in Temperatura: Risultati ottenuti dai provini del Lotto 4 147
Experiments and model predictions for fatigue crack propagation in riveted lap-joints with multiple site damage 147
Applicability of the commonly used fracture mechanics tools to the prediction of the residual strength of Glare 146
Turbine disks: Lifing against defects and materials development 145
Modello linearizzato della dinamica di un attuatore servoidraulico asimmetrico per aerofreno 145
Power absorption assessment of flight control actuation systems via object-oriented modelling 145
Hybrid thermo-electric propulsion system for climbing performance enhancement of lightweight fixed-wing UAVs 145
L'analisi dell'immagine nella sperimentazione a fatica 143
Fatigue Crack Growth Threshold at High Temperature on Engine Disk Superalloys 143
Climbing performance enhancement of small fixed-wing UAVs via hybrid electric propulsion 143
Propagazione di fessure per fatica ad alta temperatura nella superlega a base nickel IN718 su provini corner crack e compact tension 142
Attività del Dipartimento di Ingegneria Aerospaziale dell’Università di Pisa nell’Ambito del Progetto UAV-SCAUT 142
Modellizzazione di attuatori servoidraulici lineari per la movimentazione delle superfici primarie dei velivoli e progettazione del controllo di posizione 142
Short crack growth in the lap joints: experimental and numerical results 142
Crack closure measurements under spectrum loading 139
Attivita’ del Dipartimento di Ingegneria Aerospaziale di Pisa nel Settore dei miniUAV 139
Modelling and Simulation of a Fault-tolerant Electrical Motor for Aerospace Servovalves with Modelica 139
Fatigue Problems in the Design of Fuselage Panels in Glare 138
Real-Time Hardware-in-the-loop Simulation of Fly-by-Wire Flight Control Systems 138
Caratterizzazione della fase di propagazione di fessure per fatica nella lega IN-718 alla temperatura di 450 °C 137
An AHRS Based on a Kalmann Filter for the Integration of Inertial, Magnetometric and GPS Data 137
Progetto Vulcano 127. Determinazione dei punti di impatto per le avarie maggiormente critiche del dimostratore Dim_1374_03 (ROLLCTRL) 137
Multi-variable aircraft directional control with anti-skid differential brakes 137
Problematiche tipiche della sperimentazione a fatica in alta temperatura 136
EMAS control loop 136
Simulazione SW completa del Flight Control System 136
An Experimental and Numerical Analysis of Multi-Site Damaged Butt-Joints 136
Test di fatica oligociclica in temperatura: messa a punto dell’attrezzatura e procedura di prova 136
Totale 17.410
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Categoria #
all - tutte 86.288
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 86.288
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021347 0 0 0 0 0 0 0 0 0 0 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
2024/20257.671 61 342 136 331 809 713 541 365 712 1.037 969 1.655
2025/20267.737 480 1.743 781 436 739 792 1.167 329 402 688 180 0
Totale 34.886