CRIS Current Research Information System

MODENINI, DARIO
 Distribuzione geografica
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Continente #
AS - Asia 4.975
NA - Nord America 4.002
EU - Europa 3.125
SA - Sud America 353
AF - Africa 285
OC - Oceania 13
Continente sconosciuto - Info sul continente non disponibili 1
Totale 12.754
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Nazione #
US - Stati Uniti d'America 3.917
SG - Singapore 1.300
CN - Cina 1.285
IT - Italia 1.198
VN - Vietnam 1.089
GB - Regno Unito 443
DE - Germania 325
HK - Hong Kong 315
JP - Giappone 248
FR - Francia 247
BR - Brasile 227
IN - India 204
KR - Corea 180
RU - Federazione Russa 168
SE - Svezia 138
IE - Irlanda 115
CI - Costa d'Avorio 108
NL - Olanda 101
TG - Togo 58
BG - Bulgaria 55
BD - Bangladesh 54
CA - Canada 53
FI - Finlandia 52
AR - Argentina 48
PH - Filippine 47
ZA - Sudafrica 45
ID - Indonesia 41
UA - Ucraina 38
AT - Austria 35
JO - Giordania 33
EE - Estonia 30
ES - Italia 30
PL - Polonia 29
TH - Thailandia 27
TR - Turchia 27
IQ - Iraq 25
SC - Seychelles 20
MX - Messico 19
TW - Taiwan 18
DK - Danimarca 16
EC - Ecuador 16
SA - Arabia Saudita 16
CL - Cile 15
CH - Svizzera 14
PE - Perù 14
BE - Belgio 13
GR - Grecia 13
AU - Australia 12
CO - Colombia 12
HR - Croazia 10
MA - Marocco 10
PK - Pakistan 10
UZ - Uzbekistan 10
EG - Egitto 9
PY - Paraguay 8
TN - Tunisia 8
LT - Lituania 7
MY - Malesia 7
PT - Portogallo 7
AE - Emirati Arabi Uniti 6
DZ - Algeria 6
RO - Romania 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
SN - Senegal 3
AM - Armenia 2
BO - Bolivia 2
IR - Iran 2
JM - Giamaica 2
KZ - Kazakistan 2
NG - Nigeria 2
OM - Oman 2
SY - Repubblica araba siriana 2
TT - Trinidad e Tobago 2
YE - Yemen 2
ZM - Zambia 2
CM - Camerun 1
CR - Costa Rica 1
GH - Ghana 1
KH - Cambogia 1
LA - Repubblica Popolare Democratica del Laos 1
LV - Lettonia 1
LY - Libia 1
MD - Moldavia 1
Totale 12.743
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Città #
Singapore 902
Santa Clara 386
Hefei 374
San Jose 359
Southend 342
Chandler 309
Ashburn 298
Hong Kong 289
Ho Chi Minh City 254
Bologna 243
Hanoi 215
Fairfield 193
Seoul 162
Beijing 139
New York 125
Woodbridge 113
Dublin 112
Abidjan 108
Seattle 105
Princeton 103
Wilmington 102
Boardman 100
Ann Arbor 94
Dallas 88
Milan 84
Kagoya 82
Los Angeles 79
Lauterbourg 78
Houston 74
Cambridge 70
Cesena 63
Lomé 58
Nanjing 56
Council Bluffs 55
Dong Ket 54
Rome 52
Sofia 52
Da Nang 48
Tokyo 47
Buffalo 44
Hangzhou 43
Osaka 42
Frankfurt am Main 40
Haiphong 39
Turin 37
Westminster 37
Amman 33
Berlin 31
Bengaluru 30
Medford 30
Redondo Beach 30
Redwood City 30
Nuremberg 29
Rimini 28
Forlì 27
Helsinki 27
Munich 27
Padova 27
Shanghai 27
Saint Petersburg 26
Chennai 24
Guangzhou 24
Vienna 24
Jinan 23
Jakarta 22
London 21
São Paulo 21
Lappeenranta 19
Moscow 19
Chicago 18
Orem 18
Warsaw 18
Castel Maggiore 17
Ravenna 17
Ferrara 16
Paris 16
San Diego 16
San Francisco 16
Amsterdam 15
Atlanta 15
Biên Hòa 15
Copenhagen 15
Florence 15
Suzuka 15
Toronto 15
Brooklyn 14
Montreal 14
Changsha 13
Dearborn 13
Des Moines 13
Hebei 13
Hải Dương 13
Zhengzhou 13
Bangkok 12
Denver 12
Parma 12
Salerno 12
Thái Nguyên 12
Tianjin 12
Basingstoke 11
Totale 7.794
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Nome #
Aerodynamic assessment of a rotary entry vehicle for Mars landing: an experimental analysis 287
Preliminary orbital analysis for a CubeSat mission to the Didymos binary asteroid system 249
Large constellations of small satellites: A survey of near future challenges and missions 248
Automatic mass balancing system for a dynamic CubeSat attitude simulator: development and experimental validation 224
Attitude Sensor from Ellipsoid Observations: A Numerical and Experimental Validation 222
Evidence for multi-fragmentation and mass shedding of boulders on rubble-pile binary asteroid system (65803) Didymos 214
A DYNAMIC ATTITUDE TESTBED FOR CUBESATS 202
Attitude Determination from Ellipsoid Observations: A Modified Orthogonal Procrustes Problem 201
Deep Learning for Real-Time Satellite Pose Estimation on Tensor Processing Units 200
Five-Degree-of-Freedom Pose Estimation from an Imaged Ellipsoid of Revolution 198
LICIACube - The Light Italian Cubesat for Imaging of Asteroids In support of the NASA DART mission towards asteroid (65803) Didymos 198
Beyond current EDL Technologies on Mars: Evaluation of ARMADA Concepts 192
Achievement of the Planetary Defense Investigations of the Double Asteroid Redirection Test (DART) Mission 190
ARMADA: Autorotation, Feasible Alternative to Traditional Martian Entry, Descent and Landing 187
Estimating Soil Parameters From Hyperspectral Images: A benchmark dataset and the outcome of the HYPERVIEW challenge 186
Rotary Wing Vehicle for Landing on Mars: The ARMADA Experience 181
An analytical approach to autonomous optical navigation for a CubeSat mission to a binary asteroid system 178
An autonomous optical navigation filter for a CubeSat mission to a binary asteroid system 178
Characterization of the DART Impact Ejecta Plume on Dimorphos from LICIACube Observations 175
VADER: Probing the Dark Side of Dimorphos with LICIACube LUKE 173
Nanosatellite-class dynamic attitude simulator for hands-on aerospace control education 173
Anticipated Geological Assessment of the (65803) Didymos–Dimorphos System, Target of the DART–LICIACube Mission 168
Expected Investigation of the (65803) Didymos–Dimorphos System Using the RGB Spectrophotometry Data Set from the LICIACube Unit Key Explorer (LUKE) Wide-angle Camera 166
Overview of AODCS for Nanosatellites and Expected Short-Term Evolution 166
Gaussian deterministic recursive estimator with online tuning capabilities 162
A SIMPLE METHOD FOR ACCURATE CENTER OF GRAVITY DETERMINATION OF SMALL SATELLITE PLATFORMS 162
The Dimorphos ejecta plume properties revealed by LICIACube 160
Terminal height estimation using a Fading Gaussian Deterministic filter 160
A High Accuracy Horizon Sensor for Small Satellites 160
Measuring the mass of a main belt comet: Proteus mission 159
DustCube, a nanosatellite mission to binary asteroid 65803 Didymos as part of the ESA AIM mission 156
A dynamic testbed for nanosatellites attitude verification 156
Fast boulder fracturing by thermal fatigue detected on stony asteroids 154
Radio Science Investigations with the Asteroid Impact Mission 154
Design and Test of a Calibration System for Avalanche Photodiodes Used in X-Ray Compton Polarimeters for Space 152
Development and testing of a milli-Newton high test peroxide monopropellant thruster 152
Experimental verification of a simple method for accurate center of gravity determination of small satellite platforms 152
A Comparative Analysis of GPS-based Algorithms for Real-Time Navigation of Small Satellites 151
On-ground experimental verification of magnetic attitude control for nanosatellites 150
Resonance locking in giant planets indicated by the rapid orbital expansion of Titan 149
Near-infrared Spectral Homogeneity of the Didymos System Before and After the DART Impact 148
SPACE ENGINEERING AND SMALL SATELLITES EDUCATIONAL ACTIVITIES AT UNIVERSITY OF BOLOGNA 148
Preliminary Mission Analysis and Design of a Cubesat Mission to the Didymos Binary Asteroid System 148
Hybrid controller for global, robust, attitude stabilization of a magnetically actuated spacecraft 147
Ground Segment Solutions for Small Satellites 147
Automatic Balancing for Satellite Simulators with Mixed Mechanical and Magnetic Actuation 147
CubeSat Ground Test Facility as a Tool for Collaborative Hands-On Education: The Joint Experience of the u3s and STAR Laboratories 145
The geology and evolution of the Near-Earth binary asteroid system (65803) Didymos 143
Retrodictor-corrector filter 143
STANDALONE THREE-AXIS ATTITUDE DETERMINATION FROM EARTH IMAGES 142
Lithologies of Dimorphos revealed by boulder morphological classes 140
Verification Approaches for Nano- and Micro-Satellites 139
Two-line-element propagation improvement and uncertainty estimation using recurrent neural networks 139
Artificial Intelligence-Based Challenges as an Educational Tool in Aerospace Engineering: the u3S Laboratory Experience 136
Relations Between Collision Probability, Mahalanobis Distance, and Confidence Intervals for Conjunction Assessment 134
Pioneer 10 and 11 orbit determination analysis shows no discrepancy with Newton-Einstein laws of gravity 133
Updated Europa gravity field and interior structure from a reanalysis of Galileo tracking data 131
Momentum transfer from the DART mission kinetic impact on asteroid Dimorphos 128
STARS - Standalone Three-axis Attitude Reconstruction Sensor 126
Optimal blade pitch profile for an autorotative entry vehicle 126
DART Impact Ejecta Plume Evolution: Implications for Dimorphos 124
Experimental Aerodynamic Characterization of a Rotary Entry Vehicle for Mars Landing 123
Elliptical ejecta of asteroid Dimorphos is due to its surface curvature 122
Systems Design and Performance of Cold Gas Microthruster for Microsatellite Attitude Control 120
Heat transfer measurements in a supersonic wind tunnel through inverse temperature data reduction: application to a backward facing step 117
On-board precise GPS navigation solution for small satellite missions 117
Two-Leg Deep Space Relay Architectures: Performance, Challenges, and Perspectives 117
Re-examination of Pioneer 10 tracking data including spacecraft thermal modeling 114
Experimental investigation of a supersonic backward facing step flow 111
Investigating Vision Transformers for Bridging Domain Gap in Satellite Pose Estimation 110
High-speed Boulders and the Debris Field in DART Ejecta 110
The SSDC Role in the LICIACube Mission: Data Management and the MATISSE Tool 107
Spectral Rotational Characterization of the Didymos System prior to the DART Impact* 106
A solution to spacecraft position and attitude determination from an imaged ellipsoid 105
Ground and Space Hardware for Interplanetary Communication Networks 104
Planet–sun sensor revisited 104
Lessons learnt from operating ESEO Educational Spacecraft 101
The Unusual Brightness Phase Curve of (65803) Didymos 101
The Italian microsatellite mission LICIACube as an enabler for innovative strategies in interplanetary exploration and planetary defense 99
CUSP: a two CubeSats constellation for space weather and solar flares x-ray polarimetry 94
Analytic solution for perturbed Keplerian motion under small acceleration using averaging theory 80
Efficient Close-Range Navigation Around a Known Uncooperative Resident Space Object 75
The Italian microsatellite mission LICIACube as an enabler for innovative strategies in Interplanetary Exploration and Planetary Defense 59
Deep learning-based spacecraft pose estimation with the fail-safe fallback mechanism 58
The INNOVATOR CubeSat Mission and the development of its intersatellite link transceiver (ISL‐T) 56
Publisher Correction: Resonance locking in giant planets indicated by the rapid orbital expansion of Titan (Nature Astronomy, (2020), 10.1038/s41550-020-1120-5) 53
Exploring Stochastic Variational Gaussian Processes for Trustworthy Monocular Pose Estimation in Space 50
A comparison of spacecraft collision detection strategies using a virtual conjunction dataset 48
The multiphysics analysis and design of CUSP, a two CubeSat constellation for space weather and solar flares X-ray polarimetry 46
Development and calibration of a measurement system for the characterization of avalanche photodiodes prospectively used as sensors in X-ray Compton polarimeters for space 43
Prototype Development and Calibration of the CUbesat Solar Polarimeter (CUSP) 40
BOPAS: The Bologna Observatory Pipeline for Astrometry of Satellites 40
Solar Flare Hard X-ray Polarimetry with the CUbesat Solar Polarimeter (CUSP) mission 33
The CUbesat Solar Polarimeter (CUSP) mission overview 31
The multiphysics analysis, design, and testing of CUSP, a CubeSat mission for space weather and solar flares x-ray polarimetry 31
The evaluation of the CUSP scientific performance by a GEANT4 Monte Carlo simulation 30
The CUbesat Solar Polarimeter (CUSP): mission overview II 29
Study of the HV power supply modules for the CUbesat Solar Polarimeter (CUSP) 29
Characterization of avalanche photodiodes (APDs) for the CUbesat Solar Polarimeter (CUSP) mission 28
Totale 13.100
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Categoria #
all - tutte 36.540
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 36.540
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021231 0 0 0 0 0 0 0 0 0 0 39 192
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
2025/20265.522 352 627 575 362 540 264 463 248 1.227 655 209 0
Totale 13.100