CRIS Current Research Information System

MODENINI, DARIO
 Distribuzione geografica
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Continente #
AS - Asia 5.146
NA - Nord America 4.393
EU - Europa 3.280
SA - Sud America 409
AF - Africa 286
OC - Oceania 13
Continente sconosciuto - Info sul continente non disponibili 1
Totale 13.528
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Nazione #
US - Stati Uniti d'America 4.284
IT - Italia 1.337
SG - Singapore 1.307
CN - Cina 1.291
VN - Vietnam 1.091
GB - Regno Unito 446
DE - Germania 328
HK - Hong Kong 318
BR - Brasile 280
JP - Giappone 249
FR - Francia 247
IN - India 205
BD - Bangladesh 204
KR - Corea 180
RU - Federazione Russa 169
SE - Svezia 138
IE - Irlanda 115
CI - Costa d'Avorio 108
NL - Olanda 103
CA - Canada 67
TG - Togo 58
BG - Bulgaria 55
FI - Finlandia 52
AR - Argentina 48
PH - Filippine 47
ZA - Sudafrica 45
ID - Indonesia 41
UA - Ucraina 39
AT - Austria 35
JO - Giordania 33
EE - Estonia 30
ES - Italia 30
PL - Polonia 29
TH - Thailandia 27
TR - Turchia 27
IQ - Iraq 25
MX - Messico 21
SC - Seychelles 21
TW - Taiwan 18
CL - Cile 16
DK - Danimarca 16
EC - Ecuador 16
SA - Arabia Saudita 16
CH - Svizzera 15
PE - Perù 15
BE - Belgio 13
CO - Colombia 13
GR - Grecia 13
AU - Australia 12
PK - Pakistan 11
HR - Croazia 10
MA - Marocco 10
UZ - Uzbekistan 10
EG - Egitto 9
PY - Paraguay 8
TN - Tunisia 8
JM - Giamaica 7
LT - Lituania 7
MY - Malesia 7
PT - Portogallo 7
RO - Romania 7
AE - Emirati Arabi Uniti 6
DZ - Algeria 6
SM - San Marino 6
VE - Venezuela 6
AZ - Azerbaigian 5
CZ - Repubblica Ceca 5
ET - Etiopia 5
LU - Lussemburgo 5
SK - Slovacchia (Repubblica Slovacca) 5
HU - Ungheria 4
NP - Nepal 4
UY - Uruguay 4
AL - Albania 3
BY - Bielorussia 3
DO - Repubblica Dominicana 3
HN - Honduras 3
IL - Israele 3
KE - Kenya 3
KW - Kuwait 3
LB - Libano 3
SI - Slovenia 3
SN - Senegal 3
AM - Armenia 2
BO - Bolivia 2
IR - Iran 2
KZ - Kazakistan 2
ME - Montenegro 2
NG - Nigeria 2
OM - Oman 2
SY - Repubblica araba siriana 2
TT - Trinidad e Tobago 2
YE - Yemen 2
ZM - Zambia 2
BB - Barbados 1
CM - Camerun 1
CR - Costa Rica 1
GH - Ghana 1
GT - Guatemala 1
KH - Cambogia 1
Totale 13.513
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Città #
Singapore 908
Santa Clara 395
Ashburn 384
Hefei 374
San Jose 366
Southend 342
Chandler 309
Hong Kong 292
Ho Chi Minh City 254
Bologna 252
Hanoi 215
Fairfield 193
Seoul 162
New York 144
Beijing 142
Woodbridge 113
Dublin 112
Dallas 109
Abidjan 108
Los Angeles 106
Seattle 105
Princeton 103
Wilmington 102
Boardman 100
Milan 100
Ann Arbor 94
Kagoya 82
Lauterbourg 78
Houston 75
Cambridge 70
São Paulo 70
Rome 66
Council Bluffs 64
Cesena 63
Lomé 58
Buffalo 57
Nanjing 56
Dong Ket 54
Sofia 52
Da Nang 48
Tokyo 48
Hangzhou 43
Osaka 42
Frankfurt am Main 40
Rimini 40
Haiphong 39
Turin 37
Westminster 37
Amman 33
Berlin 31
Forlì 31
Nuremberg 31
Bengaluru 30
Medford 30
Redondo Beach 30
Redwood City 30
Shanghai 29
Helsinki 27
Munich 27
Padova 27
Saint Petersburg 26
Chennai 25
Florence 24
Guangzhou 24
London 24
Vienna 24
Jinan 23
Jakarta 22
Chicago 21
Orem 21
San Francisco 21
Lappeenranta 19
Montreal 19
Moscow 19
Warsaw 18
Amsterdam 17
Atlanta 17
Brooklyn 17
Castel Maggiore 17
Ravenna 17
Toronto 17
Ferrara 16
Paris 16
San Diego 16
Biên Hòa 15
Copenhagen 15
Denver 15
Suzuka 15
Changsha 13
Dearborn 13
Des Moines 13
Hebei 13
Hải Dương 13
Zhengzhou 13
Bangkok 12
Naples 12
Parma 12
Salerno 12
Thái Nguyên 12
Tianjin 12
Totale 8.149
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Nome #
Achievement of the Planetary Defense Investigations of the Double Asteroid Redirection Test (DART) Mission 303
Aerodynamic assessment of a rotary entry vehicle for Mars landing: an experimental analysis 294
Large constellations of small satellites: A survey of near future challenges and missions 259
Preliminary orbital analysis for a CubeSat mission to the Didymos binary asteroid system 254
Evidence for multi-fragmentation and mass shedding of boulders on rubble-pile binary asteroid system (65803) Didymos 235
Attitude Sensor from Ellipsoid Observations: A Numerical and Experimental Validation 233
Automatic mass balancing system for a dynamic CubeSat attitude simulator: development and experimental validation 227
LICIACube - The Light Italian Cubesat for Imaging of Asteroids In support of the NASA DART mission towards asteroid (65803) Didymos 217
VADER: Probing the Dark Side of Dimorphos with LICIACube LUKE 216
Five-Degree-of-Freedom Pose Estimation from an Imaged Ellipsoid of Revolution 210
Deep Learning for Real-Time Satellite Pose Estimation on Tensor Processing Units 206
Attitude Determination from Ellipsoid Observations: A Modified Orthogonal Procrustes Problem 206
A DYNAMIC ATTITUDE TESTBED FOR CUBESATS 205
Estimating Soil Parameters From Hyperspectral Images: A benchmark dataset and the outcome of the HYPERVIEW challenge 197
ARMADA: Autorotation, Feasible Alternative to Traditional Martian Entry, Descent and Landing 195
Beyond current EDL Technologies on Mars: Evaluation of ARMADA Concepts 195
DustCube, a nanosatellite mission to binary asteroid 65803 Didymos as part of the ESA AIM mission 189
Rotary Wing Vehicle for Landing on Mars: The ARMADA Experience 184
An analytical approach to autonomous optical navigation for a CubeSat mission to a binary asteroid system 180
An autonomous optical navigation filter for a CubeSat mission to a binary asteroid system 180
Characterization of the DART Impact Ejecta Plume on Dimorphos from LICIACube Observations 178
Nanosatellite-class dynamic attitude simulator for hands-on aerospace control education 174
Expected Investigation of the (65803) Didymos–Dimorphos System Using the RGB Spectrophotometry Data Set from the LICIACube Unit Key Explorer (LUKE) Wide-angle Camera 173
Overview of AODCS for Nanosatellites and Expected Short-Term Evolution 171
Anticipated Geological Assessment of the (65803) Didymos–Dimorphos System, Target of the DART–LICIACube Mission 170
Gaussian deterministic recursive estimator with online tuning capabilities 164
A High Accuracy Horizon Sensor for Small Satellites 164
Design and Test of a Calibration System for Avalanche Photodiodes Used in X-Ray Compton Polarimeters for Space 163
The Dimorphos ejecta plume properties revealed by LICIACube 163
Terminal height estimation using a Fading Gaussian Deterministic filter 163
A SIMPLE METHOD FOR ACCURATE CENTER OF GRAVITY DETERMINATION OF SMALL SATELLITE PLATFORMS 163
Lithologies of Dimorphos revealed by boulder morphological classes 162
Measuring the mass of a main belt comet: Proteus mission 161
A dynamic testbed for nanosatellites attitude verification 159
The geology and evolution of the Near-Earth binary asteroid system (65803) Didymos 158
Fast boulder fracturing by thermal fatigue detected on stony asteroids 156
Radio Science Investigations with the Asteroid Impact Mission 155
Experimental verification of a simple method for accurate center of gravity determination of small satellite platforms 155
On-ground experimental verification of magnetic attitude control for nanosatellites 154
Development and testing of a milli-Newton high test peroxide monopropellant thruster 153
A Comparative Analysis of GPS-based Algorithms for Real-Time Navigation of Small Satellites 152
Preliminary Mission Analysis and Design of a Cubesat Mission to the Didymos Binary Asteroid System 152
Resonance locking in giant planets indicated by the rapid orbital expansion of Titan 152
Near-infrared Spectral Homogeneity of the Didymos System Before and After the DART Impact 150
Ground Segment Solutions for Small Satellites 150
CubeSat Ground Test Facility as a Tool for Collaborative Hands-On Education: The Joint Experience of the u3s and STAR Laboratories 149
SPACE ENGINEERING AND SMALL SATELLITES EDUCATIONAL ACTIVITIES AT UNIVERSITY OF BOLOGNA 149
Hybrid controller for global, robust, attitude stabilization of a magnetically actuated spacecraft 148
Automatic Balancing for Satellite Simulators with Mixed Mechanical and Magnetic Actuation 148
STANDALONE THREE-AXIS ATTITUDE DETERMINATION FROM EARTH IMAGES 145
Retrodictor-corrector filter 144
Verification Approaches for Nano- and Micro-Satellites 141
Two-line-element propagation improvement and uncertainty estimation using recurrent neural networks 140
Artificial Intelligence-Based Challenges as an Educational Tool in Aerospace Engineering: the u3S Laboratory Experience 138
Relations Between Collision Probability, Mahalanobis Distance, and Confidence Intervals for Conjunction Assessment 137
Pioneer 10 and 11 orbit determination analysis shows no discrepancy with Newton-Einstein laws of gravity 136
Updated Europa gravity field and interior structure from a reanalysis of Galileo tracking data 136
Elliptical ejecta of asteroid Dimorphos is due to its surface curvature 131
Momentum transfer from the DART mission kinetic impact on asteroid Dimorphos 130
Optimal blade pitch profile for an autorotative entry vehicle 130
STARS - Standalone Three-axis Attitude Reconstruction Sensor 128
DART Impact Ejecta Plume Evolution: Implications for Dimorphos 128
Investigating Vision Transformers for Bridging Domain Gap in Satellite Pose Estimation 127
Experimental Aerodynamic Characterization of a Rotary Entry Vehicle for Mars Landing 126
Systems Design and Performance of Cold Gas Microthruster for Microsatellite Attitude Control 122
High-speed Boulders and the Debris Field in DART Ejecta 121
Heat transfer measurements in a supersonic wind tunnel through inverse temperature data reduction: application to a backward facing step 120
On-board precise GPS navigation solution for small satellite missions 120
Two-Leg Deep Space Relay Architectures: Performance, Challenges, and Perspectives 120
Ground and Space Hardware for Interplanetary Communication Networks 117
Experimental investigation of a supersonic backward facing step flow 117
The Unusual Brightness Phase Curve of (65803) Didymos 117
Re-examination of Pioneer 10 tracking data including spacecraft thermal modeling 116
The Italian microsatellite mission LICIACube as an enabler for innovative strategies in interplanetary exploration and planetary defense 114
Spectral Rotational Characterization of the Didymos System prior to the DART Impact* 112
The SSDC Role in the LICIACube Mission: Data Management and the MATISSE Tool 112
Planet–sun sensor revisited 111
A solution to spacecraft position and attitude determination from an imaged ellipsoid 107
Lessons learnt from operating ESEO Educational Spacecraft 103
CUSP: a two CubeSats constellation for space weather and solar flares x-ray polarimetry 95
Deep learning-based spacecraft pose estimation with the fail-safe fallback mechanism 88
Analytic solution for perturbed Keplerian motion under small acceleration using averaging theory 81
Efficient Close-Range Navigation Around a Known Uncooperative Resident Space Object 78
The INNOVATOR CubeSat Mission and the development of its intersatellite link transceiver (ISL‐T) 71
BOPAS: The Bologna Observatory Pipeline for Astrometry of Satellites 66
A comparison of spacecraft collision detection strategies using a virtual conjunction dataset 65
The multiphysics analysis, design, and testing of CUSP, a CubeSat mission for space weather and solar flares x-ray polarimetry 64
The Italian microsatellite mission LICIACube as an enabler for innovative strategies in Interplanetary Exploration and Planetary Defense 62
Exploring Stochastic Variational Gaussian Processes for Trustworthy Monocular Pose Estimation in Space 55
Publisher Correction: Resonance locking in giant planets indicated by the rapid orbital expansion of Titan (Nature Astronomy, (2020), 10.1038/s41550-020-1120-5) 54
Solar Flare Hard X-ray Polarimetry with the CUbesat Solar Polarimeter (CUSP) mission 51
The multiphysics analysis and design of CUSP, a two CubeSat constellation for space weather and solar flares X-ray polarimetry 50
Development and calibration of a measurement system for the characterization of avalanche photodiodes prospectively used as sensors in X-ray Compton polarimeters for space 50
Prototype Development and Calibration of the CUbesat Solar Polarimeter (CUSP) 42
The CUbesat Solar Polarimeter (CUSP) mission overview 33
The evaluation of the CUSP scientific performance by a GEANT4 Monte Carlo simulation 32
The CUbesat Solar Polarimeter (CUSP): mission overview II 32
Study of the HV power supply modules for the CUbesat Solar Polarimeter (CUSP) 30
Characterization of avalanche photodiodes (APDs) for the CUbesat Solar Polarimeter (CUSP) mission 29
3D Reconstruction of DART Ejecta at Dimorphos Reveals an Anisotropic, Filamentary Structure 11
Totale 13.879
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Categoria #
all - tutte 38.927
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 38.927
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022964 71 35 54 40 118 55 42 90 76 34 158 191
2022/20231.404 146 182 96 164 95 107 51 100 247 58 74 84
2023/2024675 44 75 32 63 54 132 58 38 37 50 40 52
2024/20252.619 142 333 252 182 525 144 184 93 52 121 169 422
2025/20266.216 352 627 575 362 540 264 463 248 1.227 655 358 545
2026/202785 85 0 0 0 0 0 0 0 0 0 0 0
Totale 13.879