GAIAS, GABRIELLA VITTORIA MARIA
 Distribuzione geografica
Continente #
EU - Europa 5.643
NA - Nord America 3.905
AS - Asia 2.739
SA - Sud America 450
AF - Africa 127
OC - Oceania 35
Continente sconosciuto - Info sul continente non disponibili 2
Totale 12.901
Nazione #
US - Stati Uniti d'America 3.780
IT - Italia 2.143
RU - Federazione Russa 2.117
CN - Cina 736
SG - Singapore 734
BR - Brasile 371
VN - Vietnam 311
JP - Giappone 237
FR - Francia 220
KR - Corea 210
DE - Germania 201
GB - Regno Unito 153
FI - Finlandia 150
HK - Hong Kong 110
NL - Olanda 110
ES - Italia 105
AT - Austria 102
CA - Canada 95
IN - India 82
IE - Irlanda 79
CH - Svizzera 75
PH - Filippine 62
MA - Marocco 60
ID - Indonesia 47
SE - Svezia 44
UA - Ucraina 39
IR - Iran 36
AU - Australia 34
AR - Argentina 33
BD - Bangladesh 32
MX - Messico 23
BE - Belgio 21
PL - Polonia 21
TR - Turchia 21
TW - Taiwan 17
AE - Emirati Arabi Uniti 16
IQ - Iraq 16
PK - Pakistan 16
EC - Ecuador 14
CL - Cile 13
LU - Lussemburgo 13
ZA - Sudafrica 13
CI - Costa d'Avorio 12
EG - Egitto 11
JO - Giordania 10
GR - Grecia 8
MY - Malesia 7
NO - Norvegia 6
TN - Tunisia 6
VE - Venezuela 6
CO - Colombia 5
KE - Kenya 5
PT - Portogallo 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
BJ - Benin 3
BO - Bolivia 3
DZ - Algeria 3
EE - Estonia 3
HU - Ungheria 3
LB - Libano 3
RO - Romania 3
TH - Thailandia 3
UY - Uruguay 3
AO - Angola 2
CR - Costa Rica 2
ET - Etiopia 2
HR - Croazia 2
IL - Israele 2
MK - Macedonia 2
NG - Nigeria 2
NP - Nepal 2
PY - Paraguay 2
RS - Serbia 2
XK - ???statistics.table.value.countryCode.XK??? 2
BN - Brunei Darussalam 1
CY - Cipro 1
CZ - Repubblica Ceca 1
DK - Danimarca 1
DM - Dominica 1
DO - Repubblica Dominicana 1
GE - Georgia 1
HN - Honduras 1
KW - Kuwait 1
KZ - Kazakistan 1
MD - Moldavia 1
ML - Mali 1
MM - Myanmar 1
MW - Malawi 1
NZ - Nuova Zelanda 1
OM - Oman 1
PA - Panama 1
PR - Porto Rico 1
Totale 12.896
Città #
Milan 756
Ashburn 571
San Jose 538
Singapore 401
Santa Clara 301
Moscow 291
Chandler 270
Ciampino 236
Tokyo 182
Hefei 164
Seoul 163
The Dalles 162
Dallas 123
Helsinki 118
Beijing 113
Council Bluffs 111
Fairfield 109
Woodbridge 87
Vienna 86
Cambridge 81
Dublin 79
Málaga 72
Wilmington 72
Dong Ket 70
Bern 69
Rome 69
Lauterbourg 67
Boardman 66
Houston 64
Los Angeles 64
Ho Chi Minh City 61
Redwood City 60
Amsterdam 57
Lawrence 54
Ottawa 54
Hong Kong 53
Medford 53
Davao City 50
Seattle 50
Atlanta 48
Frankfurt am Main 43
Jakarta 42
Turin 42
Hanoi 38
London 37
New York 37
Kenitra 35
São Paulo 35
Ann Arbor 33
Cupertino 33
Central 29
North Charleston 26
Guangzhou 25
Naples 25
Orem 24
Dearborn 23
Giussano 22
Parma 22
Shanghai 21
Casablanca 20
Las Vegas 20
Buffalo 19
Crema 19
Boltiere 18
Falkenstein 18
Pedrengo 18
Hangzhou 17
San Diego 17
Chennai 16
Sydney 16
Jacksonville 15
Kent 15
Norwalk 15
Verona 15
Bengaluru 14
Bovisio Masciago 14
Brescia 14
Brussels 14
Paris 14
Phoenix 14
Bareggio 13
Bresso 13
Da Nang 13
Montreal 13
Munich 13
Rio de Janeiro 13
Abidjan 12
Busto Arsizio 12
Florence 12
Nanjing 12
Ojŏng-gu 12
Bremen 11
Buenos Aires 11
Reggio Emilia 11
Stanford 11
Toulouse 11
Chicago 10
Lecco 10
Madrid 10
Amman 9
Totale 7.261
Nome #
Safe Trajectory Design For Close Proximity Operations 355
Model of J2 perturbed satellite relative motion with time-varying differential drag 344
GNSS-based Navigation for a Remote Sensing Three-Satellite Formation Flying 341
Three Satellites Formation Flying: Deployment and Formation Acquisition Using Relative Orbital Elements 313
Rotational Control with Plume Impingement to Aid Rigid Capture of an Uncooperative Failed Satellite 312
Analytical Framework for Precise Relative Motion in Low Earth Orbits 308
Mission Analysis and Design for an Active Debris Removal Service for Large Constellations 307
Design of optimal low-thrust manoeuvres for remote sensing multi-satellite formation flying in low Earth orbit 285
Rendezvous and proximity operations design of an active debris removal service to a large constellation fleet 282
Mission analysis and guidance and control for the SpEye inspection CubeSat 281
Formation Flying L-Band Aperture Synthesis: Design Challenges and Innovative Formation Architecture Concept 272
Accurate Osculating/Mean Orbital Elements Conversions for Spaceborne Formation Flying 271
COMPASS: Control for orbit manoeuvring enhancing natural perturbations 264
A Simple Approach to Kinematic Inversion of Redundant Mechanisms 254
6-DoF Relative State and Parameters Estimation for Close-Range Navigation to Noncooperative Targets 250
Rendezvous and Proximity Operations Design of an Active Debris Removal Service to a Large Constellation Fleet 244
Precise Line-of-Sight Modelling for Angles-Only Relative Navigation 241
Mission Analysis and Guidance and Control for the SpEye inspection CubeSat 240
Extended Kalman filters for close-range navigation to noncooperative targets 239
Autonomous Optimal Absolute Orbit Keeping through Formation Flying Techniques 226
Design challenges and safety concept for the AVANTI experiment 223
Trajectory Design for Proximity Operations: The Relative Orbital Elements’ Perspective 210
Enabling strategies for safe proximity operations to uncooperative and non-collaborative objects in Low Earth Orbit 201
From GRACE to AVANTI: 15 Years of formation-flying experience at DLR 201
Spaceborne autonomous vision-based navigation system for AVANTI 191
Safe Guidance Scheme for Proximity Operations Forced Motion 190
Guidance and Control for Safe Contactless Plume Impingement Operations to Detumble an Uncooperative Spacecraft 185
Angles-only navigation to a noncooperative satellite using relative orbital elements 185
Fast Angles-Only Initial Relative Orbit Determination for Onboard Application 179
Safety in Forced Motion Guidance for Proximity Operations Based on Relative Orbital Elements 175
Angles-only relative orbit determination in low earth orbit 173
Angles-only relative navigation activities during AVANTI 169
Long Term Space Program Scheduling and System Design Optimization 167
Design Challenges and Safety Concept for the AVANTI Experiment 165
Angles-Only Relative Orbit Determination during the AVANTI Experiment 159
Semi-Analytical Framework for Precise Relative Motion in Low Earth Orbits 155
A numerical approach to the problem of angles-only initial relative orbit determination in low earth orbit 155
Flight demonstration of autonomous noncooperative rendezvous in low earth orbit 153
The Fine Resolution Explorer for Salinity, Carbon and Hydrology (FRESCH): A Satellite Mission to Study Ocean-Land-Ice Interfaces 152
Safe picosatellite release from a small satellite carrier 149
Impulsive maneuvers for formation reconfiguration using relative orbital elements 145
Precise Line-of-Sight Modelling for Angles-Only Relative Navigation 142
Trajectory Optimization for the Proximity Rendezvous Operation Considering the Relative Navigation Error 140
Angles-only navigation to a non-cooperative satellite using relative orbital elements 140
A Far Range Image Processing Method for Autonomous Tracking of an Uncooperative Target 138
InSAR Microsatellite Formation Preliminary Design Optimization 137
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 136
Flight demonstration of spaceborne real-time angles-only navigation to a noncooperative target in low earth orbit 136
Delta-V-optimal centralized guidance strategy for under-actuated N-satellite formations 135
Characteristics and Advantages in Using the Eulerian Orbital Elements for Modelling the Satellites' Formation Flying 132
In-orbit experience and lessons learned from the AVANTI experiment 131
Formation Flying: Relative Orbits' Modelling and Control Through Eulerian Orbital Elements 118
Flight Demonstration of Spaceborne Real-Time Angles-Only Navigation to a Noncooperative Target in Low Earth Orbit 117
Low-thrust under-actuated satellite formation guidance and control strategies 116
Visual trajectory reconstruction of a cubesat after deployment 116
Generalised multi-impulsive manoeuvres for optimum spacecraft rendezvous in near-circular orbit 111
Noncooperative rendezvous using angles-only optical navigation: System design and flight results 109
The AVANTI Experiment: Flight Results 108
SpEye: a CubeSat Technology Demonstration Mission for On-Orbit Inspection and Formation-Flying 107
Fuel-Optimal Formation Reconfiguration by Means of Unidirectional Low-Thrust Propulsion System 106
The Autonomous Vision Approach Navigation and Target Identification (AVANTI) Experiment: Objectives and Design 103
In-Orbit Experience and Lessons Learned from the AVANTI Experiment 98
Paving the Way for Future On-Orbit-Servicing Missions: the AVANTI Experiment 93
Formation Flying Testbed at DLR's German Space Operations Center (GSOC) 92
Flight Demonstration of Non-Cooperative Rendezvous using Optical Navigation 89
Preliminary Design Optimization of a Microsatellite Formation Flying for Radar Interferometric Applications 87
Operational Concept of a Picosatellite Release from a LEO Satellite 85
A Swarm-Driven Solution for Space Debris Removal: Inspection, Capturing, and Controlled De-Orbiting 82
Generalized Multi-Impulsive Maneuvers for Optimum Spacecraft Rendezvous 82
Integrated Solution for Rapid Development of Complex GNC Software 81
Safe release of a picosatellite from a small satellite carrier in low Earth orbit 81
Hardware-in-the-loop Multi-satellite Simulator for Proximity Operations 71
Collision Risk Assessment and Avoidance Methods for Safe Autonomous Proximity Operations 65
Space Eye (SpEye): Preliminary Design of an On-Orbit Inspection and Formation-Flying Demonstration 46
Safety Concept of Proximity Operations in Low Earth Orbit: The SpEye CubeSat Mission 41
Towards Robust Angles-Only Relative Orbit Navigation: Assessing Key Modelling Factors Using Batch Least Squares Filtering 31
Modelling and Simulation of GNSS Observables for Spacecraft Navigation 30
Perturbed Relative Trajectory Design for on-orbit Servicing to Uncooperative Targets in Geostationary Orbits 25
Incidence Angle Optimization for Formation-Flying Across-Track SAR Interferometry 11
A Finite State Machine Guidance Architecture for Autonomous Rendezvous with Arbitrarily Elliptic Targets 9
Fast and Accurate Relative Orbit Determination via Angles-Only Batch Unscented Filtering 4
Totale 12.992
Categoria #
all - tutte 31.206
article - articoli 11.993
book - libri 0
conference - conferenze 18.665
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 61.864


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021166 0 0 0 0 0 0 0 0 0 0 0 166
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
2025/20266.122 1.311 849 371 378 339 320 945 380 405 607 201 16
Totale 12.992