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

GAIAS, GABRIELLA VITTORIA MARIA
 Distribuzione geografica
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Continente #
EU - Europa 5.208
NA - Nord America 2.875
AS - Asia 1.977
SA - Sud America 403
AF - Africa 106
OC - Oceania 33
Continente sconosciuto - Info sul continente non disponibili 1
Totale 10.603
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Nazione #
US - Stati Uniti d'America 2.777
RU - Federazione Russa 2.115
IT - Italia 1.954
SG - Singapore 634
CN - Cina 569
BR - Brasile 348
VN - Vietnam 177
DE - Germania 165
FI - Finlandia 135
FR - Francia 129
JP - Giappone 110
GB - Regno Unito 102
ES - Italia 100
AT - Austria 96
NL - Olanda 96
HK - Hong Kong 85
KR - Corea 76
CA - Canada 75
CH - Svizzera 74
IN - India 72
IE - Irlanda 70
PH - Filippine 59
MA - Marocco 56
ID - Indonesia 46
SE - Svezia 43
IR - Iran 36
UA - Ucraina 36
AU - Australia 32
AR - Argentina 27
BE - Belgio 21
PL - Polonia 20
MX - Messico 19
TR - Turchia 19
BD - Bangladesh 16
LU - Lussemburgo 13
CI - Costa d'Avorio 12
PK - Pakistan 12
TW - Taiwan 11
IQ - Iraq 10
ZA - Sudafrica 10
EC - Ecuador 9
JO - Giordania 9
CL - Cile 8
EG - Egitto 8
GR - Grecia 8
AE - Emirati Arabi Uniti 7
PT - Portogallo 5
SA - Arabia Saudita 5
BH - Bahrain 4
LK - Sri Lanka 4
NO - Norvegia 4
VE - Venezuela 4
BJ - Benin 3
DZ - Algeria 3
EE - Estonia 3
HU - Ungheria 3
KE - Kenya 3
LB - Libano 3
LT - Lituania 3
MY - Malesia 3
RO - Romania 3
TN - Tunisia 3
UY - Uruguay 3
UZ - Uzbekistan 3
AL - Albania 2
AZ - Azerbaigian 2
BG - Bulgaria 2
BO - Bolivia 2
CO - Colombia 2
ET - Etiopia 2
HR - Croazia 2
IL - Israele 2
SN - Senegal 2
AO - Angola 1
BN - Brunei Darussalam 1
CR - Costa Rica 1
DK - Danimarca 1
DM - Dominica 1
DO - Repubblica Dominicana 1
KZ - Kazakistan 1
MD - Moldavia 1
MK - Macedonia 1
MW - Malawi 1
NG - Nigeria 1
NZ - Nuova Zelanda 1
OM - Oman 1
PA - Panama 1
RS - Serbia 1
TG - Togo 1
XK - ???statistics.table.value.countryCode.XK??? 1
Totale 10.603
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Città #
Milan 674
Ashburn 412
Singapore 333
Santa Clara 299
Moscow 291
Chandler 270
Ciampino 236
Hefei 163
San Jose 122
Fairfield 109
Helsinki 103
Dallas 102
Beijing 98
Woodbridge 86
Council Bluffs 82
Vienna 80
Málaga 72
Wilmington 72
Dong Ket 70
Dublin 70
Bern 69
Boardman 66
Rome 66
Houston 62
Redwood City 60
Tokyo 60
Lawrence 54
Medford 53
Ottawa 53
Los Angeles 52
Davao City 50
Seattle 49
Amsterdam 48
Cambridge 45
Jakarta 42
Kenitra 35
São Paulo 34
Ann Arbor 33
Cupertino 33
Frankfurt am Main 32
Seoul 31
Hong Kong 30
London 30
Central 29
Turin 29
New York 28
Dearborn 23
Naples 23
Giussano 22
The Dalles 21
Casablanca 19
Crema 19
Boltiere 18
Guangzhou 18
Ho Chi Minh City 18
Pedrengo 18
Falkenstein 17
San Diego 17
Jacksonville 15
Kent 15
Verona 15
Bengaluru 14
Bovisio Masciago 14
Brussels 14
Chennai 14
Norwalk 14
Orem 14
Sydney 14
Bareggio 13
Bresso 13
Buffalo 13
Rio de Janeiro 13
Abidjan 12
Brescia 12
Hangzhou 12
Hanoi 12
Ojŏng-gu 12
Shanghai 12
Buenos Aires 11
Nanjing 11
Reggio Emilia 11
Stanford 11
Toulouse 11
Bremen 10
Lecco 10
Paris 10
Amman 9
Atlanta 9
Brooklyn 9
Lappeenranta 9
Parma 9
Pavia 9
Phoenix 9
Piacenza 9
Redmond 9
Rubiana 9
Xian 9
Busto Arsizio 8
Nuremberg 8
Bologna 7
Totale 5.624
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Nome #
GNSS-based Navigation for a Remote Sensing Three-Satellite Formation Flying 301
Safe Trajectory Design For Close Proximity Operations 291
Analytical Framework for Precise Relative Motion in Low Earth Orbits 278
Model of J2 perturbed satellite relative motion with time-varying differential drag 278
Rotational Control with Plume Impingement to Aid Rigid Capture of an Uncooperative Failed Satellite 271
Mission Analysis and Design for an Active Debris Removal Service for Large Constellations 270
Three Satellites Formation Flying: Deployment and Formation Acquisition Using Relative Orbital Elements 266
Accurate Osculating/Mean Orbital Elements Conversions for Spaceborne Formation Flying 249
Design of optimal low-thrust manoeuvres for remote sensing multi-satellite formation flying in low Earth orbit 246
Mission analysis and guidance and control for the SpEye inspection CubeSat 237
COMPASS: Control for orbit manoeuvring enhancing natural perturbations 233
Rendezvous and proximity operations design of an active debris removal service to a large constellation fleet 231
Formation Flying L-Band Aperture Synthesis: Design Challenges and Innovative Formation Architecture Concept 231
6-DoF Relative State and Parameters Estimation for Close-Range Navigation to Noncooperative Targets 228
A Simple Approach to Kinematic Inversion of Redundant Mechanisms 227
Rendezvous and Proximity Operations Design of an Active Debris Removal Service to a Large Constellation Fleet 224
Precise Line-of-Sight Modelling for Angles-Only Relative Navigation 216
Mission Analysis and Guidance and Control for the SpEye inspection CubeSat 206
Autonomous Optimal Absolute Orbit Keeping through Formation Flying Techniques 194
Extended Kalman filters for close-range navigation to noncooperative targets 192
Trajectory Design for Proximity Operations: The Relative Orbital Elements’ Perspective 188
Design challenges and safety concept for the AVANTI experiment 184
From GRACE to AVANTI: 15 Years of formation-flying experience at DLR 178
Spaceborne autonomous vision-based navigation system for AVANTI 161
Fast Angles-Only Initial Relative Orbit Determination for Onboard Application 157
Guidance and Control for Safe Contactless Plume Impingement Operations to Detumble an Uncooperative Spacecraft 153
Safe Guidance Scheme for Proximity Operations Forced Motion 152
Safety in Forced Motion Guidance for Proximity Operations Based on Relative Orbital Elements 151
Enabling strategies for safe proximity operations to uncooperative and non-collaborative objects in Low Earth Orbit 149
Angles-only relative navigation activities during AVANTI 149
Angles-only navigation to a noncooperative satellite using relative orbital elements 148
Long Term Space Program Scheduling and System Design Optimization 145
Angles-only relative orbit determination in low earth orbit 144
Design Challenges and Safety Concept for the AVANTI Experiment 141
Angles-Only Relative Orbit Determination during the AVANTI Experiment 139
Semi-Analytical Framework for Precise Relative Motion in Low Earth Orbits 137
A numerical approach to the problem of angles-only initial relative orbit determination in low earth orbit 129
Precise Line-of-Sight Modelling for Angles-Only Relative Navigation 123
InSAR Microsatellite Formation Preliminary Design Optimization 122
Trajectory Optimization for the Proximity Rendezvous Operation Considering the Relative Navigation Error 120
Flight demonstration of autonomous noncooperative rendezvous in low earth orbit 119
Angles-only navigation to a non-cooperative satellite using relative orbital elements 118
Employing Sequential Convex Programming to Solve a Class of Optimal Control Problems with a Minimum Control Input Magnitude Constraint: Formation Reconfiguration Using Low-Thrust as a Case Study 117
Characteristics and Advantages in Using the Eulerian Orbital Elements for Modelling the Satellites' Formation Flying 116
A Far Range Image Processing Method for Autonomous Tracking of an Uncooperative Target 114
The Fine Resolution Explorer for Salinity, Carbon and Hydrology (FRESCH): A Satellite Mission to Study Ocean-Land-Ice Interfaces 112
Impulsive maneuvers for formation reconfiguration using relative orbital elements 110
Flight demonstration of spaceborne real-time angles-only navigation to a noncooperative target in low earth orbit 109
In-orbit experience and lessons learned from the AVANTI experiment 104
Delta-V-optimal centralized guidance strategy for under-actuated N-satellite formations 103
Flight Demonstration of Spaceborne Real-Time Angles-Only Navigation to a Noncooperative Target in Low Earth Orbit 102
Generalised multi-impulsive manoeuvres for optimum spacecraft rendezvous in near-circular orbit 101
The AVANTI Experiment: Flight Results 94
Safe picosatellite release from a small satellite carrier 93
Visual trajectory reconstruction of a cubesat after deployment 93
Formation Flying: Relative Orbits' Modelling and Control Through Eulerian Orbital Elements 92
Low-thrust under-actuated satellite formation guidance and control strategies 86
The Autonomous Vision Approach Navigation and Target Identification (AVANTI) Experiment: Objectives and Design 83
Noncooperative rendezvous using angles-only optical navigation: System design and flight results 82
Fuel-Optimal Formation Reconfiguration by Means of Unidirectional Low-Thrust Propulsion System 82
In-Orbit Experience and Lessons Learned from the AVANTI Experiment 81
SpEye: a CubeSat Technology Demonstration Mission for On-Orbit Inspection and Formation-Flying 79
Paving the Way for Future On-Orbit-Servicing Missions: the AVANTI Experiment 77
Flight Demonstration of Non-Cooperative Rendezvous using Optical Navigation 72
Preliminary Design Optimization of a Microsatellite Formation Flying for Radar Interferometric Applications 70
Operational Concept of a Picosatellite Release from a LEO Satellite 68
Integrated Solution for Rapid Development of Complex GNC Software 68
Formation Flying Testbed at DLR's German Space Operations Center (GSOC) 67
Generalized Multi-Impulsive Maneuvers for Optimum Spacecraft Rendezvous 61
Hardware-in-the-loop Multi-satellite Simulator for Proximity Operations 55
Safe release of a picosatellite from a small satellite carrier in low Earth orbit 55
A Swarm-Driven Solution for Space Debris Removal: Inspection, Capturing, and Controlled De-Orbiting 39
Collision Risk Assessment and Avoidance Methods for Safe Autonomous Proximity Operations 10
Space Eye (SpEye): Preliminary Design of an On-Orbit Inspection and Formation-Flying Demonstration 9
Safety Concept of Proximity Operations in Low Earth Orbit: The SpEye CubeSat Mission 8
Totale 10.688
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Categoria #
all - tutte 26.971
article - articoli 10.413
book - libri 0
conference - conferenze 16.066
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 53.450
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021491 0 0 0 0 0 0 35 39 77 42 132 166
2021/2022833 27 43 45 55 96 97 41 119 75 51 69 115
2022/2023965 128 82 53 85 98 103 26 54 100 97 48 91
2023/2024583 20 66 28 31 54 27 106 23 53 68 39 68
2024/20252.805 186 27 89 76 582 219 153 128 279 141 210 715
2025/20263.818 1.311 849 371 378 339 320 250 0 0 0 0 0
Totale 10.688