BERNELLI ZAZZERA, FRANCO
 Distribuzione geografica
Continente #
EU - Europa 24.380
NA - Nord America 18.748
AS - Asia 8.148
SA - Sud America 1.703
AF - Africa 307
OC - Oceania 42
Continente sconosciuto - Info sul continente non disponibili 19
Totale 53.347
Nazione #
US - Stati Uniti d'America 18.376
IT - Italia 15.338
RU - Federazione Russa 4.627
SG - Singapore 2.767
CN - Cina 2.371
BR - Brasile 1.470
VN - Vietnam 1.120
UA - Ucraina 696
GB - Regno Unito 580
DE - Germania 564
FI - Finlandia 443
FR - Francia 441
SE - Svezia 423
HK - Hong Kong 379
KR - Corea 364
AT - Austria 327
IE - Irlanda 282
CA - Canada 267
JP - Giappone 250
NL - Olanda 183
ES - Italia 165
IN - India 150
BD - Bangladesh 103
PH - Filippine 103
MA - Marocco 95
AR - Argentina 88
ID - Indonesia 84
BE - Belgio 76
TW - Taiwan 64
CH - Svizzera 61
TR - Turchia 61
ZA - Sudafrica 57
JO - Giordania 48
IQ - Iraq 46
MX - Messico 43
CI - Costa d'Avorio 39
PK - Pakistan 39
AU - Australia 33
PL - Polonia 32
PT - Portogallo 32
EC - Ecuador 31
DZ - Algeria 30
VE - Venezuela 29
UZ - Uzbekistan 27
RO - Romania 25
CO - Colombia 23
SA - Arabia Saudita 20
EG - Egitto 19
TH - Thailandia 18
EU - Europa 17
CL - Cile 16
IR - Iran 16
TN - Tunisia 16
PE - Perù 15
PY - Paraguay 15
AZ - Azerbaigian 14
KE - Kenya 14
DK - Danimarca 13
GR - Grecia 13
CZ - Repubblica Ceca 12
DO - Repubblica Dominicana 11
MY - Malesia 11
UY - Uruguay 11
AE - Emirati Arabi Uniti 10
BJ - Benin 10
LB - Libano 10
LT - Lituania 9
NP - Nepal 9
NZ - Nuova Zelanda 9
PA - Panama 9
IL - Israele 8
AL - Albania 7
CR - Costa Rica 7
KZ - Kazakistan 7
NO - Norvegia 7
PS - Palestinian Territory 7
GE - Georgia 6
JM - Giamaica 6
KG - Kirghizistan 6
GT - Guatemala 5
HN - Honduras 5
SN - Senegal 5
TT - Trinidad e Tobago 5
BO - Bolivia 4
BY - Bielorussia 4
ET - Etiopia 4
OM - Oman 4
QA - Qatar 4
AM - Armenia 3
BB - Barbados 3
CY - Cipro 3
GA - Gabon 3
HU - Ungheria 3
MD - Moldavia 3
MU - Mauritius 3
SV - El Salvador 3
SY - Repubblica araba siriana 3
BA - Bosnia-Erzegovina 2
BG - Bulgaria 2
BH - Bahrain 2
Totale 53.303
Città #
Milan 13.247
Ashburn 1.960
Fairfield 1.561
Singapore 1.464
Chandler 1.397
Woodbridge 1.363
San Jose 1.309
Houston 1.017
Ann Arbor 869
Santa Clara 763
Wilmington 738
Seattle 596
Moscow 573
Cambridge 534
Hefei 509
Beijing 450
Council Bluffs 423
Jacksonville 391
Boardman 386
The Dalles 367
Dearborn 346
Seoul 310
Vienna 309
Hong Kong 262
Los Angeles 251
Lawrence 245
Dublin 239
Lauterbourg 236
Ho Chi Minh City 228
North Charleston 209
Tokyo 204
Dallas 201
Helsinki 194
Ottawa 175
Rome 172
Dong Ket 164
Hanoi 161
Medford 147
Buffalo 131
São Paulo 115
Málaga 109
Amsterdam 103
Princeton 99
Des Moines 91
Zibido San Giacomo 86
Redwood City 85
San Diego 85
Bovisio Masciago 83
London 83
New York 81
Las Vegas 72
Shanghai 70
Davao City 62
Guangzhou 61
Brussels 58
Oldham 58
Jakarta 57
Frankfurt am Main 53
Hangzhou 52
Bern 51
Kenitra 51
Orem 49
Amman 46
Islington 45
Rio de Janeiro 44
Harbin 43
Nanjing 40
Da Nang 39
Abidjan 38
Taipei 38
Phoenix 37
Changsha 35
Belo Horizonte 34
Haiphong 34
Columbus 33
Montreal 31
Brooklyn 29
Chicago 29
Warsaw 28
Casablanca 26
Falkenstein 26
Giussano 26
Mumbai 26
Brasília 25
Busto Arsizio 25
Johannesburg 25
Munich 25
Robbiate 25
Tianjin 25
Turin 25
Boltiere 24
Florence 24
Norwalk 24
Atlanta 23
Zhengzhou 23
Boulder 22
Pedrengo 22
Tashkent 22
Fortaleza 21
Istanbul 21
Totale 36.943
Nome #
A High Order Method for Orbital Conjunctions Analysis: Monte Carlo Collision Probability Computation 489
A High Order Method for Orbital Conjunctions Analysis: Sensitivity to Initial Uncertainties 432
Low-Thrust Minimum-Fuel Optimization in the Circular Restricted Three-Body Problem 413
Combined Optimal Low-Thrust and Stable-Manifold Trajectories to the Earth-Moon Halo Orbits 398
A Method to Design Efficient Low-Energy, Low-Thrust Transfers to the Moon 394
Rigorous Global Optimization for Collision Risk Assessment on Perturbed Orbits 393
On-board telemetry monitoring via support vector machine with application to Philae solar generator 389
Solving Constrained Optimal Control Problems Using State-Dependent Factorization and Chebyshev Polynomials 382
Efficient Invariant-Manifold, Low-Thrust Planar Trajectories to the Moon 380
High Order Optimal Feedback Control of Space Trajectories with Bounded Control 379
Earth-Mars Transfers with Ballistic Escape and Low-Thrust Capture 365
Optimal Selection of the Coefficient Matrix in State-Dependent Control Methods 362
Optimal Low-Thrust Invariant Manifold Trajectories via Attainable Sets 360
Gravity Assist Space Pruning Based on Differential Algebra 357
A Hybrid Optimization of the Low Energy Interplanetary Transfers Associated to the Invariant Manifolds of the Restricted Three-Body Problem 355
Low-Energy, Low-Thrust Transfers to the Moon 352
Collision Avoidance Maneuver Design Based on Multi-Objective Optimization 351
Transfers to Distant Periodic Orbits Around the Moon via Their Invariant Manifolds 349
Two ASRE approaches with application to spacecraft coulomb formations 343
Analytical Solution of Optimal Feedback Control for Radially Accelerated Orbits 342
Radially Accelerated Optimal Feedback Orbits in Central Gravity Field with Linear Drag 337
Global Optimization of Interplanetary Transfers with Deep Space Maneuvers Using Differential Algebra 335
A Hybrid Propulsion Approach to Design Earth-to-Moon Transfers with Ballistic Capture 332
The H2020 ReDSHIFT Project: a Successful European Effort Towards Space Debris Mitigation 328
Adaptive Attitude Tracking with Active Uncertainty Rejection 327
Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 326
Erratum to: Constructing Ballistic Capture Orbits in the Real Solar System Model 325
Earth-to-Moon Low Energy Transfers Targeting L-1 Hyperbolic Transit Orbits 324
A Multidisciplinary Approach to Landing Site Selection for Small-Body Missions 323
Approximate Solutions to Nonlinear Optimal Control Problems in Astrodynamics 320
Computing Collision Probability Using Differential Algebra and Advanced Monte Carlo Methods 316
Orbit Raising and De-Orbit for Coplanar Satellite Constellations with Low-Thrust Propulsion 314
Low-Thrust Minimum Fuel Optimization in the Circular Restricted Three-Body Model 314
Exploiting Distant Periodic Orbits and Their Invariant Manifolds to Design Novel Space Trajectories to the Moon 313
Constructing Ballistic Capture Orbits in the Real Solar System Model 313
High Order Algorithms for the Management of Uncertainties with Applications in Space Situational Awareness 312
Numerical Methods for Low-Energy Low-Thrust Sun-Perturbed Earth-to-Moon Trajectory Design 311
A Method to Design Sun-Perturbed Earth-To-moon Low-Thrust Transfers with Ballistic Capture 307
An Exploration of Numerical Methods for Low-Thrust Trajectory Optimization in n-Body Models 305
A Method to Solve Nonlinear Optimal Control Problems in Astrodynamics 304
Controlled Drug Delivery in Cancer Immunotherapy: Stability, Optimization, and Montecarlo Analysis 302
Scheduled input shaping based attitude agile control for flexible spacecraft with vibration suppression 298
Invariant-Manifold, Low-Thrust Transfers to Low Mars Orbits 298
Analysis of Options to Enhance the Performance of New Space Economy Downstream Services 298
On-Board Telemetry Monitoring via Support Vector Machine with Application to Philae Solar Generator 296
Computation of Collision Probabilities Based on Special Perturbations and High Order Methods 295
Proposal for a EU quality label for aerospace education 295
Numerical Methods to Design Low-Energy, Low-Thrust Sun-Perturbed Transfers to the Moon 294
Efficient Invariant-Manifold, Low-Thrust Planar Trajectories to the Moon 294
Low-Thrust, Invariant-Manifolds Trajectories to Halo Orbits 292
Feedback Optimal Control in Low-Thrust Interplanetary Trajectory Design 290
Collision Risk Assessment for Perturbed Orbits Via Rigorous Global Optimization 289
Analytical Solution of the Feedback Optimal Control in Low-Thrust Transfers 288
Multi-criteria design of continuous global coverage Walker and Street-of-Coverage constellations through property assessment 288
High Minimum Inter-Execution Time Sigmoid Event-Triggered Control for Spacecraft Attitude Tracking With Actuator Saturation 287
The Role of Dynamical Models in Ballistic Capture: the Perturbed Sun-Planet Case 287
Interplanetary and Lunar Transfers Using Libration Points 286
Simulation of Low-Intensity, Low-Temperature Solar Arrays with Software and Hardware Tools 286
Comparative Assessment Of Different Constellation Geometries For Space-Based Application 284
High-order state transition polynomial with time expansion based on differential algebra 282
Analysis of Ballistic Capture Orbits in the Real N-Body Problem 278
Dynamical Systems, Optimal Control and Space Trajectory Design 276
A simple method to design non-collision relative orbits for close spacecraft formation flying 276
Feedback Optimal Control in Low-Thrust Interplanetary Trajectory Design with Drag 274
Orbit Determination of Space Debris Using a Bi-static Radar Configuration with a Multiple-Beam Receiver 269
Analytical Solution of the Feedback Optimal Control in Low-Thrust Transfers 268
Nonlinear orbital uncertainty propagation with differential algebra and Gaussian mixture model 267
Optimal Low-Thrust Station Keeping of Geostationary Satellites 259
High Order Optimal Feedback Control of Low-Thrust Orbital Transfers with Saturating Actuators 257
Active Flutter Suppression Using Recurrent Neural Networks 252
Attainable Sets in Space Mission Design: a Method to Define Low-Thrust, Invariant Manifold Trajectories 252
Simulation of Low-Intensity, Low-Temperature Solar Arrays with Software and Hardware Tools 251
Philae Attitude Determination Through Nonlinear Optimal Identication of Solar Arrays Telemetry 251
Hybrid Propulsion Transfers to the Moon 249
Asteroid Close Encounters Characterization Using Differential Algebra: the Case of Apophis 244
Scientific Use of the Sampler, Drill and Distribution Subsystem (SD2) 244
Enhancing Planetary Exploration by Using Hybrid Propulsion Transfers 241
On-Comet Power Production: the Case of Rosetta Lander Philae 240
Numerical Approximation of Invariant Manifolds in the Restricted Three-Body Problem 239
Propagation of Large Uncertainty Sets in Orbital Dynamics by Automatic Domain Splitting 238
Power Production for Small Body Landers: Post-Launch Activities on Philae's Power Subsystem 237
Distant Retrograde Orbits for space-based Near Earth Objects detection 236
An Automatic Domain Splitting Technique to Propagate Uncertainties in Highly Nonlinear Orbital Dynamics 236
Autonomous Rover Control with Behavioral Algorithms and Neural Networks 235
Experimental Characterization of Power Dissipation of Battery Cells for Space Environment 234
Solution of a Class of Optimal Feedback Control Problems 231
ReDSHIFT: A Global Approach to Space Debris Mitigation 228
Active Space Debris Removal by a Hybrid Propulsion Module 227
Solar Array Simulators for Low Power Space Missions 227
Rosetta Philae SD2 Drill System and Its Operation on 67p/Churyumov-Gerasimenko 227
On-Comet Attitude Reconstruction of Rosetta Lander Philae Through Solar Arrays Telemetry 223
Attitude Dynamics of ESMO Satellite: Mass Expulsion Torques and Propellant Slosh Model 221
Vibration Suppression of Flexible-Link Manipulator by PZT Actuators and Sensors 221
Robust Trajectory and Attitude Control of a Flexible Launcher 217
A Multiobjective Experiment for Innovative Researches in Space Robotic Systems Onboard the Space Station 216
Design and Modal Analysis of a Large Deployable Solar Sail System Based on Flasher Origami Structure and CFRP Boom 215
Re-entry predictions of space debris for collision avoidance with air traffic 215
Mars Garden: an Engineered Greenhouse for a Sustainable Residence on Mars 215
Distributed Optimization Method for Spacecraft Attitude Control and Vibration Suppression 212
Region-confined restoration method for motion-blurred star image of the star sensor under dynamic conditions 212
Totale 29.410
Categoria #
all - tutte 147.286
article - articoli 71.430
book - libri 0
conference - conferenze 72.937
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 2.919
Totale 294.572


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021398 0 0 0 0 0 0 0 0 0 0 0 398
2021/20222.300 90 277 98 236 282 94 101 136 143 172 207 464
2022/20232.962 395 291 212 376 249 358 56 201 332 187 193 112
2023/20241.624 92 265 67 154 128 109 193 58 163 114 56 225
2024/20256.192 180 136 188 194 1.132 487 312 491 753 371 683 1.265
2025/202627.188 3.040 2.635 1.014 1.414 864 803 2.299 1.123 5.527 3.503 3.432 1.534
Totale 53.542