RE.PUBLIC@POLIMI pubblicazioni di ricerca del Politecnico di Milano

BERNELLI ZAZZERA, FRANCO
 Distribuzione geografica
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Continente #
NA - Nord America 13.110
EU - Europa 7.071
AS - Asia 1.892
AF - Africa 77
SA - Sud America 71
OC - Oceania 25
Continente sconosciuto - Info sul continente non disponibili 18
Totale 22.264
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Nazione #
US - Stati Uniti d'America 12.903
IT - Italia 3.466
UA - Ucraina 676
SG - Singapore 540
CN - Cina 538
DE - Germania 438
SE - Svezia 400
FI - Finlandia 371
GB - Regno Unito 362
VN - Vietnam 345
AT - Austria 280
RU - Federazione Russa 276
IE - Irlanda 255
CA - Canada 196
ES - Italia 135
NL - Olanda 113
FR - Francia 101
PH - Filippine 74
HK - Hong Kong 72
IN - India 64
BR - Brasile 56
CH - Svizzera 56
BE - Belgio 54
ID - Indonesia 52
JP - Giappone 47
KR - Corea 39
JO - Giordania 34
CI - Costa d'Avorio 26
TW - Taiwan 22
AU - Australia 21
RO - Romania 20
DZ - Algeria 19
TR - Turchia 19
PT - Portogallo 18
EU - Europa 17
IR - Iran 11
PL - Polonia 11
BJ - Benin 10
DK - Danimarca 10
EG - Egitto 10
GR - Grecia 9
PE - Perù 9
PK - Pakistan 6
MX - Messico 5
MY - Malesia 5
NO - Norvegia 5
ZA - Sudafrica 5
AR - Argentina 4
AZ - Azerbaigian 4
IL - Israele 4
NZ - Nuova Zelanda 4
AE - Emirati Arabi Uniti 3
CZ - Repubblica Ceca 3
LT - Lituania 3
TH - Thailandia 3
TN - Tunisia 3
AM - Armenia 2
BG - Bulgaria 2
BY - Bielorussia 2
CR - Costa Rica 2
GT - Guatemala 2
IQ - Iraq 2
MA - Marocco 2
MU - Mauritius 2
SA - Arabia Saudita 2
BA - Bosnia-Erzegovina 1
BD - Bangladesh 1
EC - Ecuador 1
HN - Honduras 1
HR - Croazia 1
HU - Ungheria 1
KG - Kirghizistan 1
LU - Lussemburgo 1
PA - Panama 1
PY - Paraguay 1
QA - Qatar 1
SK - Slovacchia (Repubblica Slovacca) 1
SS - ???statistics.table.value.countryCode.SS??? 1
UZ - Uzbekistan 1
Totale 22.264
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Città #
Milan 1.592
Fairfield 1.550
Chandler 1.390
Woodbridge 1.361
Houston 997
Ann Arbor 855
Ashburn 740
Wilmington 734
Santa Clara 691
Seattle 579
Cambridge 530
Jacksonville 389
Singapore 378
Boardman 362
Dearborn 346
Vienna 274
Lawrence 244
Dublin 214
Beijing 180
Ottawa 174
Dong Ket 164
Rome 150
Medford 146
Helsinki 138
Málaga 109
Princeton 99
Des Moines 86
Zibido San Giacomo 86
Redwood City 85
Bovisio Masciago 83
San Diego 83
Amsterdam 72
Davao City 61
Oldham 57
Jakarta 52
Bern 51
Shanghai 40
Brussels 37
Nanjing 37
Harbin 35
Amman 34
Abidjan 26
Falkenstein 26
Giussano 26
London 25
Robbiate 25
Boltiere 24
Busto Arsizio 24
Norwalk 24
Boulder 22
Pedrengo 22
Guangzhou 21
Auburn Hills 19
Casaluce 19
Hefei 19
Hangzhou 18
Meda 18
Mountain View 18
Novosibirsk 18
Parma 18
Changsha 17
Menlo Park 17
Seongnam 17
Verona 17
Los Angeles 16
Pavia 16
Tokyo 16
Torino 16
Turin 16
Central 15
Florence 15
Segrate 15
Hong Kong 13
Lappeenranta 13
Mumbai 13
Ciampino 12
Istanbul 12
Novara 12
Varese 12
Zhengzhou 12
Besana in Brianza 11
Delft 11
Faro 11
New York 11
Phoenix 11
Rho 11
São Paulo 11
Bresso 10
Cotonou 10
Fidenza 10
Monza 10
Warsaw 10
Cornate 9
Dallas 9
Padova 9
Paris 9
Sassuolo 9
Bareggio 8
Falls Church 8
San Donato di Lecce 8
Totale 16.185
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Nome #
The H2020 ReDSHIFT Project: a Successful European Effort Towards Space Debris Mitigation 238
Adaptive Attitude Tracking with Active Uncertainty Rejection 232
Orbit Raising and De-Orbit for Coplanar Satellite Constellations with Low-Thrust Propulsion 208
High-order state transition polynomial with time expansion based on differential algebra 198
A High Order Method for Orbital Conjunctions Analysis: Monte Carlo Collision Probability Computation 196
Proposal for a EU quality label for aerospace education 194
A simple method to design non-collision relative orbits for close spacecraft formation flying 189
Comparative Assessment Of Different Constellation Geometries For Space-Based Application 187
Scientific Use of the Sampler, Drill and Distribution Subsystem (SD2) 181
A High Order Method for Orbital Conjunctions Analysis: Sensitivity to Initial Uncertainties 162
Distant Retrograde Orbits for space-based Near Earth Objects detection 162
Nonlinear orbital uncertainty propagation with differential algebra and Gaussian mixture model 162
On-board telemetry monitoring via support vector machine with application to Philae solar generator 161
Combined Optimal Low-Thrust and Stable-Manifold Trajectories to the Earth-Moon Halo Orbits 160
Region-confined restoration method for motion-blurred star image of the star sensor under dynamic conditions 160
Rigorous Global Optimization for Collision Risk Assessment on Perturbed Orbits 159
Experimental Characterization of Power Dissipation of Battery Cells for Space Environment 157
Active Flutter Suppression Using Recurrent Neural Networks 156
Propagation of Large Uncertainty Sets in Orbital Dynamics by Automatic Domain Splitting 155
High Order Optimal Feedback Control of Space Trajectories with Bounded Control 153
Rosetta Philae SD2 Drill System and Its Operation on 67p/Churyumov-Gerasimenko 149
Planning and implementation of the on-comet operations of the instrument SD2 onboard the lander Philae of Rosetta mission 149
Solving Constrained Optimal Control Problems Using State-Dependent Factorization and Chebyshev Polynomials 149
Gravity Assist Space Pruning Based on Differential Algebra 147
Autonomous Rover Control with Behavioral Algorithms and Neural Networks 144
Efficient Invariant-Manifold, Low-Thrust Planar Trajectories to the Moon 144
High Order Optimal Control of Space Trajectories with Uncertain Boundary Conditions 141
Optimal Selection of the Coefficient Matrix in State-Dependent Control Methods 140
Embodied and Evolved Dynamical Neural Networks for Robust Planetary Navigation 139
The PERSEUS Project to Promote Excellence in Aerospace Education 139
Mars Garden: an Engineered Greenhouse for a Sustainable Residence on Mars 137
Multi-criteria design of continuous global coverage Walker and Street-of-Coverage constellations through property assessment 136
Low-Thrust Minimum-Fuel Optimization in the Circular Restricted Three-Body Problem 135
Asteroid Close Encounters Characterization Using Differential Algebra: the Case of Apophis 132
Radially Accelerated Optimal Feedback Orbits in Central Gravity Field with Linear Drag 131
Low-Energy, Low-Thrust Transfers to the Moon 131
A Method to Design Efficient Low-Energy, Low-Thrust Transfers to the Moon 131
Analytical Solution of Optimal Feedback Control for Radially Accelerated Orbits 131
Attitude Dynamics of ESMO Satellite: Mass Expulsion Torques and Propellant Slosh Model 130
ReDSHIFT: A Global Approach to Space Debris Mitigation 130
Vibration Suppression of Flexible-Link Manipulator by PZT Actuators and Sensors 129
Robust Trajectory and Attitude Control of a Flexible Launcher 128
Earth-Mars Transfers with Ballistic Escape and Low-Thrust Capture 128
An Automatic Domain Splitting Technique to Propagate Uncertainties in Highly Nonlinear Orbital Dynamics 128
Optimization of Low-Thrust Trajectories for Formation Flying with Parallel Multiple Shooting 125
Experiments on Command Shaping Control of a Manipulator with Flexible Links 125
Two ASRE approaches with application to spacecraft coulomb formations 123
High Minimum Inter-Execution Time Sigmoid Event-Triggered Control for Spacecraft Attitude Tracking With Actuator Saturation 122
Global Optimization of Interplanetary Transfers with Deep Space Maneuvers Using Differential Algebra 122
Spacecraft Magnetic Attitude Control Using Approximating Sequence Riccati Equations 121
Active Space Debris Removal by a Hybrid Propulsion Module 120
Optimal Low-Thrust Invariant Manifold Trajectories via Attainable Sets 120
Attitude-Correlated Frames Algorithms to Improve the Attitude Accuracy of the Star Tracker Under Highly Dynamic Conditions 118
Autonomous Navigation of a Rover for Planetary Exploration 117
High-Order State Transition Polynomial with Time Expansion Based on Differential Algebra 117
Earth-to-Moon Low Energy Transfers Targeting L-1 Hyperbolic Transit Orbits 115
Visual Servoing Control System for Lightweight Robotic Manipulator 113
GPS Attitude Determination by Kalman Filtering: Simulation of Multipath Rejection 113
Formation Flight Optimization Using Extremum Seeking Feedback 113
Transfers to Distant Periodic Orbits Around the Moon via Their Invariant Manifolds 113
Low-thrust planar transfer for co-planar low Earth orbit satellites considering self-induced collision avoidance 113
Optimal Path Planning for Planetary Exploration Rovers based on Artificial Vision System for Environment Reconstruction 112
Nonlinear Control of Formation Flying with State Constraints 112
Inverse Dynamics of Aircraft via Reduced-Order Shooting Methods 111
A Visual Servoing Control System for Lightweight Robotic Manipulator 111
Control of a Legged Rover for Planetary Exploration Using Embedded and Evolved Dynamical Recurrent Artificial Neural Networks 111
Lessons Learned from the SD2 Operations on the Comet 67/P 111
Optimization of Low-Thrust Reconfiguration Maneuvers for Spacecraft Flying in Formation 110
Lessons Learned from the SD2 Operations on the Comet 67/P 110
Rosetta Philae Sampling Drilling and Distribution Subsystem: Operation and Results from the First On-Comet Phase 108
Realization and Control of a Prototype of Legged Rover for Planetary Exploration 108
Approximate Solutions to Nonlinear Optimal Control Problems in Astrodynamics 107
Design and testing of an active damping system for the reduction of vibrations induced by a rotating device on the ISS 107
Performance Analysis of the Attitude-Correlated Frames Approach for Star Sensors 107
A Hybrid Optimization of the Low Energy Interplanetary Transfers Associated to the Invariant Manifolds of the Restricted Three-Body Problem 106
Control of Formation Flight Via Extremum Seeking 105
Wavefront Interferometric Technique for Accurate Spacecraft Relative Attitude Determination 104
Collision Avoidance Maneuver Design Based on Multi-Objective Optimization 104
Direct Multiphase Optimisation of Multiobjective Trajectory Design Problems 103
SD2 - How to Sample a Comet 103
Sliding Mode Control of a Large Flexible Space Structure 103
Adaptive Control of Space Structures via Recurrent Neural Networks 103
Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 102
N.E.Me.Sys: a Planetary Legged Rover Controlled with Dynamical Artificial Neural Networks 100
Erratum to: Constructing Ballistic Capture Orbits in the Real Solar System Model 100
Design and Optimization of a Nonlinear Lyapunov based Attitude Control Law for Rigid Spacecraft 100
Project PALAMEDE at Politecnico di Milano: a Real Satellite to Teach Satellites Design Techniques 98
Attitude Determination and Control System for Palamede Microsatellite 98
Optimal Trajectory Design for SIMONE Mission Study 97
Alta Scuola Politecnica: an Ongoing Experiment in the Multidisciplinary Education of Top Students Towards Innovation in Engineering, Architecture and Design 96
Failure Detection by Signal Similarity Measurement of Brushless DC Motors 96
Preliminary Design and Operations of Palamede Microsatellite 95
In-Orbit Technology Validation for a University Microsatellite 95
Trajectory Design Combining Low-Thrust and Gravity Assist Manoeuvres 95
Constructing Ballistic Capture Orbits in the Real Solar System Model 94
Active Control of Tether Satellites Via Boom Rotation: a Proof of Concept Experiment 94
Computing Collision Probability Using Differential Algebra and Advanced Monte Carlo Methods 93
Controlled Drug Delivery in Cancer Immunotherapy: Stability, Optimization, and Montecarlo Analysis 93
Comment on "New Design Method for Pulse-Width Modulation Control Systems Via Digital Redesign" 92
Re-entry predictions of space debris for collision avoidance with air traffic 90
Totale 12.842
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Categoria #
all - tutte 89.028
article - articoli 50.427
book - libri 0
conference - conferenze 37.089
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.512
Totale 178.056
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20202.050 0 0 0 0 0 0 519 325 482 186 414 124
2020/20212.511 239 118 234 105 205 200 183 265 189 225 150 398
2021/20222.293 90 277 98 236 280 94 101 135 142 172 205 463
2022/20232.949 394 289 212 374 247 357 56 201 328 187 192 112
2023/20241.621 92 264 67 154 128 109 193 58 162 114 56 224
2024/20252.375 180 135 188 194 1.129 483 66 0 0 0 0 0
Totale 22.451