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

GAIAS, GABRIELLA VITTORIA MARIA
 Distribuzione geografica
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Continente #
EU - Europa 5.906
NA - Nord America 4.317
AS - Asia 2.795
SA - Sud America 458
AF - Africa 128
Continente sconosciuto - Info sul continente non disponibili 95
OC - Oceania 35
Totale 13.734
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Nazione #
US - Stati Uniti d'America 4.157
IT - Italia 2.388
RU - Federazione Russa 2.117
SG - Singapore 740
CN - Cina 739
BR - Brasile 375
VN - Vietnam 341
JP - Giappone 243
FR - Francia 223
KR - Corea 211
DE - Germania 206
GB - Regno Unito 153
FI - Finlandia 150
NL - Olanda 113
CA - Canada 112
HK - Hong Kong 110
ES - Italia 109
AT - Austria 102
IN - India 84
IE - Irlanda 79
CH - Svizzera 75
PH - Filippine 62
MA - Marocco 60
ID - Indonesia 48
SE - Svezia 44
UA - Ucraina 39
IR - Iran 38
AU - Australia 34
BD - Bangladesh 34
AR - Argentina 33
MX - Messico 25
TR - Turchia 24
BE - Belgio 21
PL - Polonia 21
TW - Taiwan 17
AE - Emirati Arabi Uniti 16
IQ - Iraq 16
PK - Pakistan 16
CL - Cile 14
EC - Ecuador 14
LU - Lussemburgo 13
ZA - Sudafrica 13
CI - Costa d'Avorio 12
EG - Egitto 11
JO - Giordania 10
GR - Grecia 8
MY - Malesia 7
VE - Venezuela 7
CO - Colombia 6
CR - Costa Rica 6
NO - Norvegia 6
PT - Portogallo 6
TN - Tunisia 6
KE - Kenya 5
SA - Arabia Saudita 5
AL - Albania 4
BG - Bulgaria 4
BH - Bahrain 4
LK - Sri Lanka 4
LT - Lituania 4
SN - Senegal 4
UZ - Uzbekistan 4
AZ - Azerbaigian 3
BB - Barbados 3
BJ - Benin 3
BO - Bolivia 3
DZ - Algeria 3
EE - Estonia 3
HN - Honduras 3
HU - Ungheria 3
JM - Giamaica 3
LB - Libano 3
PY - Paraguay 3
RO - Romania 3
TH - Thailandia 3
UY - Uruguay 3
XK - ???statistics.table.value.countryCode.XK??? 3
AO - Angola 2
ET - Etiopia 2
HR - Croazia 2
IL - Israele 2
MK - Macedonia 2
NG - Nigeria 2
NP - Nepal 2
RS - Serbia 2
SC - Seychelles 2
TT - Trinidad e Tobago 2
BA - Bosnia-Erzegovina 1
BN - Brunei Darussalam 1
CY - Cipro 1
CZ - Repubblica Ceca 1
DK - Danimarca 1
DM - Dominica 1
DO - Repubblica Dominicana 1
GE - Georgia 1
GT - Guatemala 1
IS - Islanda 1
KW - Kuwait 1
KZ - Kazakistan 1
MD - Moldavia 1
Totale 13.630
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Città #
Milan 846
Ashburn 618
San Jose 565
Singapore 406
Santa Clara 323
Moscow 291
Chandler 270
Ciampino 236
Tokyo 183
Hefei 164
Seoul 164
The Dalles 163
Council Bluffs 159
Dallas 125
Helsinki 118
Beijing 114
Rome 113
Fairfield 109
Woodbridge 87
Vienna 86
Cambridge 81
Dublin 80
Boardman 74
Ho Chi Minh City 73
Málaga 72
Wilmington 72
Dong Ket 70
Bern 69
Lauterbourg 67
Los Angeles 67
Houston 66
Redwood City 60
Amsterdam 57
Lawrence 54
Ottawa 54
Turin 54
Hong Kong 53
Medford 53
Davao City 50
Seattle 50
Atlanta 49
Frankfurt am Main 46
Hanoi 46
Jakarta 42
New York 38
London 37
Ann Arbor 35
Kenitra 35
São Paulo 35
Cupertino 33
Naples 31
Central 29
North Charleston 27
Guangzhou 25
Orem 24
Dearborn 23
Parma 23
Giussano 22
Buffalo 21
Shanghai 21
Casablanca 20
Las Vegas 20
Crema 19
Boltiere 18
Falkenstein 18
Pedrengo 18
Da Nang 17
Hangzhou 17
Phoenix 17
San Diego 17
Bengaluru 16
Chennai 16
Jacksonville 16
Sydney 16
Verona 16
Chicago 15
Kent 15
Norwalk 15
Bovisio Masciago 14
Brescia 14
Brussels 14
Paris 14
Rio de Janeiro 14
Bareggio 13
Bologna 13
Bresso 13
Montreal 13
Munich 13
Abidjan 12
Brooklyn 12
Busto Arsizio 12
Florence 12
Fremont 12
Nanjing 12
Ojŏng-gu 12
Reggio Emilia 12
Bremen 11
Buenos Aires 11
San Francisco 11
Stanford 11
Totale 7.639
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Nome #
Model of J2 perturbed satellite relative motion with time-varying differential drag 379
Safe Trajectory Design For Close Proximity Operations 369
GNSS-based Navigation for a Remote Sensing Three-Satellite Formation Flying 345
Rotational Control with Plume Impingement to Aid Rigid Capture of an Uncooperative Failed Satellite 332
Analytical Framework for Precise Relative Motion in Low Earth Orbits 320
Three Satellites Formation Flying: Deployment and Formation Acquisition Using Relative Orbital Elements 320
Mission Analysis and Design for an Active Debris Removal Service for Large Constellations 319
Rendezvous and proximity operations design of an active debris removal service to a large constellation fleet 291
Mission analysis and guidance and control for the SpEye inspection CubeSat 291
Design of optimal low-thrust manoeuvres for remote sensing multi-satellite formation flying in low Earth orbit 289
Formation Flying L-Band Aperture Synthesis: Design Challenges and Innovative Formation Architecture Concept 285
Accurate Osculating/Mean Orbital Elements Conversions for Spaceborne Formation Flying 276
COMPASS: Control for orbit manoeuvring enhancing natural perturbations 269
6-DoF Relative State and Parameters Estimation for Close-Range Navigation to Noncooperative Targets 267
A Simple Approach to Kinematic Inversion of Redundant Mechanisms 261
Rendezvous and Proximity Operations Design of an Active Debris Removal Service to a Large Constellation Fleet 253
Mission Analysis and Guidance and Control for the SpEye inspection CubeSat 249
Precise Line-of-Sight Modelling for Angles-Only Relative Navigation 247
Extended Kalman filters for close-range navigation to noncooperative targets 243
Autonomous Optimal Absolute Orbit Keeping through Formation Flying Techniques 240
Design challenges and safety concept for the AVANTI experiment 235
Trajectory Design for Proximity Operations: The Relative Orbital Elements’ Perspective 222
Safe Guidance Scheme for Proximity Operations Forced Motion 212
From GRACE to AVANTI: 15 Years of formation-flying experience at DLR 211
Enabling strategies for safe proximity operations to uncooperative and non-collaborative objects in Low Earth Orbit 210
Spaceborne autonomous vision-based navigation system for AVANTI 200
Guidance and Control for Safe Contactless Plume Impingement Operations to Detumble an Uncooperative Spacecraft 198
Angles-only navigation to a noncooperative satellite using relative orbital elements 194
Fast Angles-Only Initial Relative Orbit Determination for Onboard Application 185
Angles-only relative orbit determination in low earth orbit 183
Safety in Forced Motion Guidance for Proximity Operations Based on Relative Orbital Elements 180
Angles-only relative navigation activities during AVANTI 171
Long Term Space Program Scheduling and System Design Optimization 169
Design Challenges and Safety Concept for the AVANTI Experiment 168
Safe picosatellite release from a small satellite carrier 167
Angles-Only Relative Orbit Determination during the AVANTI Experiment 166
Semi-Analytical Framework for Precise Relative Motion in Low Earth Orbits 165
A numerical approach to the problem of angles-only initial relative orbit determination in low earth orbit 165
Flight demonstration of autonomous noncooperative rendezvous in low earth orbit 162
The Fine Resolution Explorer for Salinity, Carbon and Hydrology (FRESCH): A Satellite Mission to Study Ocean-Land-Ice Interfaces 160
Impulsive maneuvers for formation reconfiguration using relative orbital elements 151
InSAR Microsatellite Formation Preliminary Design Optimization 147
Flight demonstration of spaceborne real-time angles-only navigation to a noncooperative target in low earth orbit 146
A Far Range Image Processing Method for Autonomous Tracking of an Uncooperative Target 146
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 144
Precise Line-of-Sight Modelling for Angles-Only Relative Navigation 144
Delta-V-optimal centralized guidance strategy for under-actuated N-satellite formations 143
Angles-only navigation to a non-cooperative satellite using relative orbital elements 143
Trajectory Optimization for the Proximity Rendezvous Operation Considering the Relative Navigation Error 141
In-orbit experience and lessons learned from the AVANTI experiment 136
Characteristics and Advantages in Using the Eulerian Orbital Elements for Modelling the Satellites' Formation Flying 134
Generalised multi-impulsive manoeuvres for optimum spacecraft rendezvous in near-circular orbit 128
Low-thrust under-actuated satellite formation guidance and control strategies 125
Formation Flying: Relative Orbits' Modelling and Control Through Eulerian Orbital Elements 123
Flight Demonstration of Spaceborne Real-Time Angles-Only Navigation to a Noncooperative Target in Low Earth Orbit 123
Visual trajectory reconstruction of a cubesat after deployment 120
Noncooperative rendezvous using angles-only optical navigation: System design and flight results 118
The Autonomous Vision Approach Navigation and Target Identification (AVANTI) Experiment: Objectives and Design 116
SpEye: a CubeSat Technology Demonstration Mission for On-Orbit Inspection and Formation-Flying 115
Fuel-Optimal Formation Reconfiguration by Means of Unidirectional Low-Thrust Propulsion System 115
The AVANTI Experiment: Flight Results 113
In-Orbit Experience and Lessons Learned from the AVANTI Experiment 101
Formation Flying Testbed at DLR's German Space Operations Center (GSOC) 97
Paving the Way for Future On-Orbit-Servicing Missions: the AVANTI Experiment 97
A Swarm-Driven Solution for Space Debris Removal: Inspection, Capturing, and Controlled De-Orbiting 95
Flight Demonstration of Non-Cooperative Rendezvous using Optical Navigation 94
Operational Concept of a Picosatellite Release from a LEO Satellite 91
Preliminary Design Optimization of a Microsatellite Formation Flying for Radar Interferometric Applications 90
Collision Risk Assessment and Avoidance Methods for Safe Autonomous Proximity Operations 89
Generalized Multi-Impulsive Maneuvers for Optimum Spacecraft Rendezvous 87
Safe release of a picosatellite from a small satellite carrier in low Earth orbit 85
Integrated Solution for Rapid Development of Complex GNC Software 82
Hardware-in-the-loop Multi-satellite Simulator for Proximity Operations 75
Space Eye (SpEye): Preliminary Design of an On-Orbit Inspection and Formation-Flying Demonstration 58
Safety Concept of Proximity Operations in Low Earth Orbit: The SpEye CubeSat Mission 57
Modelling and Simulation of GNSS Observables for Spacecraft Navigation 46
Towards Robust Angles-Only Relative Orbit Navigation: Assessing Key Modelling Factors Using Batch Least Squares Filtering 42
Perturbed Relative Trajectory Design for on-orbit Servicing to Uncooperative Targets in Geostationary Orbits 36
Fast and Accurate Relative Orbit Determination via Angles-Only Batch Unscented Filtering 24
Incidence Angle Optimization for Formation-Flying Across-Track SAR Interferometry 21
A Finite State Machine Guidance Architecture for Autonomous Rendezvous with Arbitrarily Elliptic Targets 20
Autonomous GNSS-based Relative Navigation for Distributed Earth Observation Missions using Adaptive Extended Kalman Filter 8
Totale 13.734
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Categoria #
all - tutte 33.829
article - articoli 12.970
book - libri 0
conference - conferenze 20.279
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 67.078
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022806 0 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
2025/20266.505 1.311 849 371 378 339 320 945 380 405 607 201 399
2026/2027359 186 173 0 0 0 0 0 0 0 0 0 0
Totale 13.734