CHIESA, Sergio
 Distribuzione geografica
Continente #
EU - Europa 15.645
NA - Nord America 12.841
AS - Asia 7.536
SA - Sud America 594
AF - Africa 118
OC - Oceania 40
Continente sconosciuto - Info sul continente non disponibili 1
Totale 36.775
Nazione #
US - Stati Uniti d'America 12.676
IT - Italia 4.161
DE - Germania 2.966
GB - Regno Unito 2.199
FR - Francia 2.150
CN - Cina 2.094
SG - Singapore 2.016
VN - Vietnam 1.353
UA - Ucraina 1.132
RU - Federazione Russa 880
KR - Corea 490
NL - Olanda 480
BR - Brasile 473
TR - Turchia 401
HK - Hong Kong 332
SE - Svezia 331
IE - Irlanda 304
CH - Svizzera 228
IN - India 224
FI - Finlandia 198
AT - Austria 191
CA - Canada 114
JP - Giappone 104
ES - Italia 63
PH - Filippine 59
BE - Belgio 51
IR - Iran 50
AP - ???statistics.table.value.countryCode.AP??? 49
JO - Giordania 45
MY - Malesia 43
TH - Thailandia 42
IL - Israele 41
IQ - Iraq 38
ID - Indonesia 36
PL - Polonia 36
BD - Bangladesh 35
EU - Europa 34
AR - Argentina 32
AU - Australia 32
PK - Pakistan 30
TW - Taiwan 30
RO - Romania 29
MX - Messico 28
ZA - Sudafrica 27
MA - Marocco 25
BY - Bielorussia 20
EC - Ecuador 19
GR - Grecia 18
CL - Cile 16
BG - Bulgaria 14
PT - Portogallo 14
DZ - Algeria 13
VE - Venezuela 13
CZ - Repubblica Ceca 12
CO - Colombia 11
EG - Egitto 11
KZ - Kazakistan 11
LV - Lettonia 11
PE - Perù 11
SA - Arabia Saudita 11
AE - Emirati Arabi Uniti 10
NG - Nigeria 10
UZ - Uzbekistan 10
LT - Lituania 9
NP - Nepal 9
EE - Estonia 8
LU - Lussemburgo 8
UY - Uruguay 8
KE - Kenya 7
PY - Paraguay 7
TN - Tunisia 7
AM - Armenia 6
AZ - Azerbaigian 5
JM - Giamaica 5
NO - Norvegia 5
NZ - Nuova Zelanda 5
OM - Oman 5
SK - Slovacchia (Repubblica Slovacca) 5
SN - Senegal 5
HR - Croazia 4
RS - Serbia 4
AL - Albania 3
BO - Bolivia 3
BW - Botswana 3
CI - Costa d'Avorio 3
DK - Danimarca 3
DO - Repubblica Dominicana 3
HN - Honduras 3
HU - Ungheria 3
LB - Libano 3
MD - Moldavia 3
ME - Montenegro 3
NI - Nicaragua 3
QA - Qatar 3
ET - Etiopia 2
GT - Guatemala 2
KH - Cambogia 2
NA - Namibia 2
PA - Panama 2
PS - Palestinian Territory 2
Totale 36.750
Città #
Ashburn 3.724
Southend 1.897
Seattle 1.171
Singapore 996
Turin 810
San Jose 602
Chandler 533
Beijing 512
Jacksonville 499
Princeton 440
Fairfield 386
Ho Chi Minh City 386
Boardman 323
Hanoi 317
Santa Clara 293
Izmir 284
Dublin 283
San Ramon 278
Berlin 276
Hong Kong 275
Ann Arbor 265
Frankfurt 233
Milan 213
Hangzhou 198
Bern 192
Woodbridge 189
Zhengzhou 188
San Donato Milanese 185
Bologna 184
Shanghai 181
Helsinki 167
Wilmington 158
Houston 157
Rome 154
Chicago 151
Herkenbosch 149
Lauterbourg 144
Cambridge 143
Torino 138
Katy 136
Vienna 135
Buffalo 132
Los Angeles 126
Zaporozhye 126
Seoul 124
Saint Petersburg 119
Pennsylvania Furnace 117
Baltimore 108
Dallas 106
Overberg 94
Des Moines 92
Moscow 92
Monopoli 89
Amsterdam 85
Padua 80
Council Bluffs 71
San Francisco 67
Paris 64
North Bergen 56
Munich 52
Redwood City 52
Shenzhen 50
Atlanta 49
Boise 49
Putian 49
Da Nang 48
Guangzhou 48
Bremen 44
Frankfurt am Main 44
Mountain View 43
Brussels 42
Haiphong 42
Malatya 42
Naples 40
Wuhan 39
London 38
New York 36
Toronto 36
São Paulo 35
Dearborn 34
Tokyo 34
Xian 34
Madrid 33
Piscataway 33
Arlington 32
Hamburg 31
Kiev 31
Norwalk 30
Yubileyny 29
Las Vegas 28
Austin 24
Florence 24
Montreal 24
Nanjing 24
Hefei 23
Jakarta 23
Nuremberg 23
Orem 23
Columbus 22
Istanbul 22
Totale 21.152
Nome #
ASTRID - AIRCRAFT ON BOARD SYSTEMS SIZING AND TRADE-OFF ANALYSIS IN INITIAL DESIGN 1.237
Active space debris removal by a hybrid propulsion module 630
Rational and affordable concepts of Landing Gear for small reentry vehicle demonstrators 534
UAV Logistic Support Definition 526
About Feasibility of a 5th generation Light Fighter Aircraft 525
Mini-uav remote control: a case study at Politecnico di Torino 488
Hypothesis for Hypersonic Flight development 485
Diesel Engine Application on AEW&C Turboprop Effectiveness-Cost Assessment 479
SISTEMA DI PROPULSIONE PER VELIVOLO E METODO DI CONTROLLO DEL SISTEMA DI PROPULSIONE PER VELIVOLO 460
AUGMENTED GNSS FOR PRECISION APPROACH OF UNMANNED AERIAL VEHICLE: RISKS AND SAFETY ANALYSIS 420
About Feasibility of 5th Generation Light Fighter Aircraft 407
Hypothesis about cost-effective unmanned offensive airplane vehicles 405
Applied design methodology for lunar rover elastic wheel 400
Autonomous take-off and landing for unmanned aircraft system: Risk and safety analysis 393
L’avamprogetto dei velivoli 373
Feasibility Study of a Technological Demonstrator of Reduced Size for Sub-Orbital Flight 371
UAV BASED ADVANCED MONITORING SYSTEM: FLEET AND LOGISTIC SYSTEM SIZING BY OBJECT BASED MODEL AND MONTE-CARLO SIMULATION 361
BENEFITS AND TECHNOLOGICAL IMPACTS OF THE FUTURE ATM SCENARIO FOR CIVIL AND MILITARY AIRCRAFT 360
Design, Development and Test of Engineering Models of Tethered Nanosatellites to Observe the Solar Corona 358
Innovative solutions for light, very light and unmanned aircraft Preliminary design and Life Cycle Cost estimation 354
Applying interoperability to the validation of embedded systems design in aeronautics 351
STATUS AND PERSPECTIVES OF HYPERSONIC SYSTEMS AND TECHNOLOGIES WITH EMPHASIS ON THE ROLE OF SUB-ORBITAL FLIGHT 345
Linear quadratic control for quadrotors UAVs dynamics and formation flight 343
Feasibility Study of small Satellite Launcher Vehicle launched from atmospheric Carrier Aircraft 342
Utilizzo di CAD 3D parametrico per studi di configurazione e Digital Mock-up nel progetto concettuale 342
GENERAL METHODOLOGY FOR DEMONSTRATION MISSION DESIGN 336
AVIONIC DESIGN FOR CIVIL-MILITARY INTEROPERABILITY IN SINGLE EUROPEAN SKY 333
The SAVE project: hypothesis and investigation strategies for alternative energy based systems for MALE UAV 327
Heuristic and exact techniques for aircraft maintenance scheduling 325
Active debris multi-removal mission concept based on hybrid propulsion 319
Fattibilita' di conversione 'All Electric' per attuali velivoli da trasporto regionale 316
Experimental Investigation of in-flight performances for and aircraft air-conditioning prototype based on carbon dioxide as working fluid 316
Velivolo cargo di grandissime dimensioni: sviluppo del progetto e sperimentazione didattica 314
Active space debris removal by hybrid engine module 314
Turbojet Steady State and Transient Analytical Model Development and Validation 313
Methodology for an integrated definition of a system and its subsystems: the case-study of an airplane and its subsystems 308
Active debris removal space mission concepts based on hybrid propulsion 308
Nuovo Sistema di Generazione Elettrica a 270 Vdc a Bordo dei Velivoli e macchine elettriche “Switched Reluctance”; attività al Politecnico di Torino 307
Design of an U.A.V. controller based on the open source platform Arduino 306
Contribution To R.A.M.S estimation in early design phases of unmanned aerial vehicles - UAVs 305
Towards an effective interoperability of models within the 'Systems Engineering' applied to aeronautics 305
Affidabilità, Sicurezza e Manutenzione nel Progetto dei Sistemi 304
Zonal safety analysis in aircraft conceptual design: application to SAvE aircraft 301
SESAR AND MILITARY: TOWARDS ATM INTEGRATION 301
Design of all electric secondary power system for future advanced MALE UAV 300
SUPPORT AND MAINTENANCE STRATEGIES FOR FUTURE, INNOVATIVE AND LARGELY WIDESPREAD AIR PERSONAL TRANSPORTATION SYSTEMS 300
Affordable technological demonstrator for hypersonic flight 297
CONTRIBUTIONS FROM EDUCATIONAL ACTIVITIES TO RESEARCHES ABOUT HYBRID PROPULSION OPPORTUNITIES FOR LIGHT AIRCAFT 297
Hybrid configuration – Advanced A.P.U. concept for future turboprop 297
FEASIBILITY STUDY OF SMALL SATELLITES LAUNCHER VEHICLE LAUNCHED FROM ATMOSPHERIC CARRIER AIRCRAFT 296
Results of the first edition of the International Master SEEDS 296
Design of all electric secondary power system for future advanced MALE UAV 295
Low cost indoor navigation system for autonomous vehicle 294
Cubesat development at Politecnico di Torino: the e-st@r program 289
A small-Scale Low-Cost Technology Demonstrator of a reusable Launch Vehicle 286
Concept for Very Low Cost Technology Demonstrator for Hypersonic Vehicles (VeLCHyD) 285
Affordable space tourism transatmospheric plane 279
A System of Systems Approach for the Concurrent Design of Space Missions 276
"Safety by zonal analysis in aircraft conceptual design: application to SAvE project" 275
A Modeling Framework for the Concurrent Design of Complex Space Systems 272
Future-oriented C4ISTAR applications. UAS versus manned aircraft. Merit analysis to consider performance/cost aspects 271
The double-fuselage layout: a possible way to reduce development costs for new high capacity aircraft 270
All electric Secondary Power System for future advancedMALE UAV 268
Risk Analysis: Sample Application To a Totally New Aircraft Design 267
Volo ipersonico per l’accesso allo Spazio: passato, presente e futuro 267
Unmanned Sea vehicles for Harbor Patrolling: Low-Cost Solutions to Enhance Coastal Security 267
MALE UAV and its systems as basis of future definitions 265
Virtual and flying models for aircraft development 260
Turbojet Analytical Model Development and Validation 260
MARGARET: A PERSONAL TRANSPORTATION AIRCRAFT OF TOMORROW USED TODAY FOR COLLABORATION AMONG UNIVERSITIES 258
Sulla previsione di costi, sicurezza, affidabilità e entità della manutenzione in avamprogetto 257
Support and Maintenance Strategies for Future, Innovative and Largely Widespread Air Personal Transportation Systems 255
Studio di fattibilità per un dimostratore tecnologico estremamente economico di velivoli ipersonici 253
Possible hybrid propulsion configuration for transport jet aircraft 251
Algoritmi per il controllo di flotte di piccole piattaforme aerospaziali e verifica sperimentale 251
Reusable launch vehicle conceptual design structural study 249
PiCPoT program: lessons learned 248
POSSIBLE HYBRID PROPULSION CONFIGURATION FOR TRANSPORT JET AIRCRAFT 248
Regional turboprop conversion for AEW&C purposes supposing auxiliary engine installation – Technical and economical analysis 245
Il diesel in aeronautica: problematiche e prospettive 243
Experimental assessment of not pneumatic wheel for lunar rover technological demonstrator 241
The educational experience at Politecnico di Torino to develop and increase the capability in aircraft layout comprehension and definition 240
Conceptual design and structural analysis: an integrated approach via FEM 235
PROGETTO “VIBRISSA”, DIMOSTRATORE TECNOLOGICO PER UNA PARTICOLARE MODALITA’ DI GUIDA E NAVIGAZIONE PER ROBOT INDOOR: “SEGUIRE IL MURO” 234
A Parametric Approach to the Concurrent Design of Complex Systems 234
Supporto alla definizione di Sistemi, a livello concettuale, mediante strumenti di modellazione e simulazione 233
System programmable logic controller computer aided development procedure 222
Hypersonic Aircraft Conceptual Design Methodology 221
Cambiamenti globali dell’architettura di un velivolo: una via per lo sviluppo dell’avamprogetto 221
New hypothesis about hypersonic technological demonstrators based on standard air-to-air missiles 219
Mini UAV Remote Control: a case at Politecnico di Torino 218
AN ACADEMIC EXPERIENCE ABOUT AIRCRAFT DESIGN: AFFORDABLE ADVANCED JET TRAINER 217
Safety by zonal analysis at a very early phase of system design 216
The weight estimation in aerospace engineering at the Polytechnic of Turin 215
SISTEMI ROBOTICI PER CONTROLLO E VIGILANZA INDOOR: IL PROGETTO “ARGO” 215
VeLCHyD: Very Low Cost Hypersonic Demonstrator for a complete orbit re-entry mission 214
Modelli in scala per la sperimentazione delle possibilità di volo su Marte 210
PiCPoT program: lessons learned 207
Fattibilità di dimostratore tecnologico di ridotti dimensioni e costi, per veicoli spaziali non pilotati 205
Tethered nano-satellites to observe the solar corona 204
Totale 31.455
Categoria #
all - tutte 96.507
article - articoli 25.189
book - libri 1.687
conference - conferenze 64.556
curatela - curatele 0
other - altro 897
patent - brevetti 954
selected - selezionate 0
volume - volumi 3.224
Totale 193.014


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021184 0 0 0 0 0 0 0 0 0 0 147 37
2021/20221.156 43 122 10 104 32 78 38 36 43 44 252 354
2022/20232.267 192 372 55 157 242 328 203 117 236 12 126 227
2023/2024985 34 74 29 78 101 80 62 40 21 166 102 198
2024/20252.927 78 388 224 291 253 266 72 143 509 175 231 297
2025/20266.653 472 330 398 576 506 507 1.048 472 1.472 863 9 0
Totale 36.894