GAIAS, GABRIELLA VITTORIA MARIA
 Distribuzione geografica
Continente #
EU - Europa 5.583
NA - Nord America 3.716
AS - Asia 2.726
SA - Sud America 450
AF - Africa 126
OC - Oceania 35
Continente sconosciuto - Info sul continente non disponibili 2
Totale 12.638
Nazione #
US - Stati Uniti d'America 3.598
RU - Federazione Russa 2.117
IT - Italia 2.097
CN - Cina 735
SG - Singapore 733
BR - Brasile 371
VN - Vietnam 311
JP - Giappone 236
FR - Francia 219
KR - Corea 210
DE - Germania 191
GB - Regno Unito 153
FI - Finlandia 150
NL - Olanda 110
HK - Hong Kong 108
ES - Italia 104
AT - Austria 102
CA - Canada 90
IN - India 82
IE - Irlanda 79
CH - Svizzera 74
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 25
BE - Belgio 21
MX - Messico 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 6
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
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
MK - Macedonia 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 12.634
Città #
Milan 733
Ashburn 544
San Jose 488
Singapore 401
Santa Clara 301
Moscow 291
Chandler 270
Ciampino 236
Tokyo 182
Hefei 164
Seoul 163
The Dalles 162
Dallas 120
Helsinki 118
Beijing 113
Fairfield 109
Council Bluffs 98
Vienna 86
Woodbridge 86
Cambridge 81
Dublin 79
Málaga 72
Wilmington 72
Dong Ket 70
Bern 69
Lauterbourg 67
Boardman 66
Rome 66
Houston 62
Ho Chi Minh City 61
Los Angeles 60
Redwood City 60
Amsterdam 57
Lawrence 54
Ottawa 54
Medford 53
Hong Kong 51
Davao City 50
Seattle 50
Frankfurt am Main 43
Jakarta 42
Turin 41
Hanoi 38
London 36
Kenitra 35
São Paulo 35
Atlanta 34
Ann Arbor 33
Cupertino 33
New York 33
Central 29
North Charleston 26
Guangzhou 25
Naples 24
Dearborn 23
Orem 23
Giussano 22
Shanghai 21
Casablanca 20
Las Vegas 20
Crema 19
Boltiere 18
Falkenstein 18
Pedrengo 18
Hangzhou 17
San Diego 17
Chennai 16
Sydney 16
Buffalo 15
Jacksonville 15
Kent 15
Verona 15
Bengaluru 14
Bovisio Masciago 14
Brescia 14
Brussels 14
Norwalk 14
Paris 14
Bareggio 13
Bresso 13
Da Nang 13
Montreal 13
Rio de Janeiro 13
Abidjan 12
Busto Arsizio 12
Florence 12
Ojŏng-gu 12
Parma 12
Phoenix 12
Bremen 11
Buenos Aires 11
Nanjing 11
Reggio Emilia 11
Stanford 11
Toulouse 11
Chicago 10
Lecco 10
Madrid 10
Munich 10
Amman 9
Totale 7.090
Nome #
Safe Trajectory Design For Close Proximity Operations 348
GNSS-based Navigation for a Remote Sensing Three-Satellite Formation Flying 336
Model of J2 perturbed satellite relative motion with time-varying differential drag 326
Rotational Control with Plume Impingement to Aid Rigid Capture of an Uncooperative Failed Satellite 307
Analytical Framework for Precise Relative Motion in Low Earth Orbits 306
Three Satellites Formation Flying: Deployment and Formation Acquisition Using Relative Orbital Elements 305
Mission Analysis and Design for an Active Debris Removal Service for Large Constellations 302
Design of optimal low-thrust manoeuvres for remote sensing multi-satellite formation flying in low Earth orbit 284
Rendezvous and proximity operations design of an active debris removal service to a large constellation fleet 280
Mission analysis and guidance and control for the SpEye inspection CubeSat 275
Accurate Osculating/Mean Orbital Elements Conversions for Spaceborne Formation Flying 269
Formation Flying L-Band Aperture Synthesis: Design Challenges and Innovative Formation Architecture Concept 268
COMPASS: Control for orbit manoeuvring enhancing natural perturbations 263
A Simple Approach to Kinematic Inversion of Redundant Mechanisms 250
6-DoF Relative State and Parameters Estimation for Close-Range Navigation to Noncooperative Targets 245
Rendezvous and Proximity Operations Design of an Active Debris Removal Service to a Large Constellation Fleet 243
Mission Analysis and Guidance and Control for the SpEye inspection CubeSat 239
Precise Line-of-Sight Modelling for Angles-Only Relative Navigation 237
Extended Kalman filters for close-range navigation to noncooperative targets 233
Autonomous Optimal Absolute Orbit Keeping through Formation Flying Techniques 223
Design challenges and safety concept for the AVANTI experiment 210
Trajectory Design for Proximity Operations: The Relative Orbital Elements’ Perspective 210
From GRACE to AVANTI: 15 Years of formation-flying experience at DLR 200
Enabling strategies for safe proximity operations to uncooperative and non-collaborative objects in Low Earth Orbit 195
Spaceborne autonomous vision-based navigation system for AVANTI 189
Guidance and Control for Safe Contactless Plume Impingement Operations to Detumble an Uncooperative Spacecraft 185
Safe Guidance Scheme for Proximity Operations Forced Motion 184
Fast Angles-Only Initial Relative Orbit Determination for Onboard Application 177
Safety in Forced Motion Guidance for Proximity Operations Based on Relative Orbital Elements 175
Angles-only navigation to a noncooperative satellite using relative orbital elements 173
Angles-only relative navigation activities during AVANTI 166
Angles-only relative orbit determination in low earth orbit 164
Design Challenges and Safety Concept for the AVANTI Experiment 163
Long Term Space Program Scheduling and System Design Optimization 161
Angles-Only Relative Orbit Determination during the AVANTI Experiment 156
Semi-Analytical Framework for Precise Relative Motion in Low Earth Orbits 155
Safe picosatellite release from a small satellite carrier 149
A numerical approach to the problem of angles-only initial relative orbit determination in low earth orbit 149
Flight demonstration of autonomous noncooperative rendezvous in low earth orbit 147
The Fine Resolution Explorer for Salinity, Carbon and Hydrology (FRESCH): A Satellite Mission to Study Ocean-Land-Ice Interfaces 146
Precise Line-of-Sight Modelling for Angles-Only Relative Navigation 141
Trajectory Optimization for the Proximity Rendezvous Operation Considering the Relative Navigation Error 140
Impulsive maneuvers for formation reconfiguration using relative orbital elements 138
Angles-only navigation to a non-cooperative satellite using relative orbital elements 137
A Far Range Image Processing Method for Autonomous Tracking of an Uncooperative Target 136
InSAR Microsatellite Formation Preliminary Design Optimization 135
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 134
Delta-V-optimal centralized guidance strategy for under-actuated N-satellite formations 134
Characteristics and Advantages in Using the Eulerian Orbital Elements for Modelling the Satellites' Formation Flying 130
Flight demonstration of spaceborne real-time angles-only navigation to a noncooperative target in low earth orbit 130
In-orbit experience and lessons learned from the AVANTI experiment 126
Flight Demonstration of Spaceborne Real-Time Angles-Only Navigation to a Noncooperative Target in Low Earth Orbit 116
Formation Flying: Relative Orbits' Modelling and Control Through Eulerian Orbital Elements 115
Visual trajectory reconstruction of a cubesat after deployment 114
Low-thrust under-actuated satellite formation guidance and control strategies 113
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 108
The AVANTI Experiment: Flight Results 108
Fuel-Optimal Formation Reconfiguration by Means of Unidirectional Low-Thrust Propulsion System 106
SpEye: a CubeSat Technology Demonstration Mission for On-Orbit Inspection and Formation-Flying 104
The Autonomous Vision Approach Navigation and Target Identification (AVANTI) Experiment: Objectives and Design 100
In-Orbit Experience and Lessons Learned from the AVANTI Experiment 97
Paving the Way for Future On-Orbit-Servicing Missions: the AVANTI Experiment 92
Formation Flying Testbed at DLR's German Space Operations Center (GSOC) 91
Flight Demonstration of Non-Cooperative Rendezvous using Optical Navigation 86
Operational Concept of a Picosatellite Release from a LEO Satellite 83
Preliminary Design Optimization of a Microsatellite Formation Flying for Radar Interferometric Applications 81
Generalized Multi-Impulsive Maneuvers for Optimum Spacecraft Rendezvous 81
A Swarm-Driven Solution for Space Debris Removal: Inspection, Capturing, and Controlled De-Orbiting 80
Integrated Solution for Rapid Development of Complex GNC Software 80
Safe release of a picosatellite from a small satellite carrier in low Earth orbit 79
Hardware-in-the-loop Multi-satellite Simulator for Proximity Operations 70
Collision Risk Assessment and Avoidance Methods for Safe Autonomous Proximity Operations 63
Space Eye (SpEye): Preliminary Design of an On-Orbit Inspection and Formation-Flying Demonstration 44
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 26
Perturbed Relative Trajectory Design for on-orbit Servicing to Uncooperative Targets in Geostationary Orbits 24
Modelling and Simulation of GNSS Observables for Spacecraft Navigation 23
Incidence Angle Optimization for Formation-Flying Across-Track SAR Interferometry 10
A Finite State Machine Guidance Architecture for Autonomous Rendezvous with Arbitrarily Elliptic Targets 8
Totale 12.728
Categoria #
all - tutte 29.952
article - articoli 11.511
book - libri 0
conference - conferenze 17.904
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 59.367


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021340 0 0 0 0 0 0 0 0 0 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
2025/20265.858 1.311 849 371 378 339 320 945 380 405 560 0 0
Totale 12.728