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

BIGGS, JAMES DOUGLAS
 Distribuzione geografica
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Continente #
NA - Nord America 7.568
EU - Europa 3.608
AS - Asia 972
AF - Africa 44
OC - Oceania 24
SA - Sud America 21
Continente sconosciuto - Info sul continente non disponibili 2
Totale 12.239
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Nazione #
US - Stati Uniti d'America 7.483
IT - Italia 2.527
SG - Singapore 263
CN - Cina 223
VN - Vietnam 188
ES - Italia 184
GB - Regno Unito 171
DE - Germania 143
FI - Finlandia 116
NL - Olanda 96
IE - Irlanda 86
CA - Canada 81
RU - Federazione Russa 49
ID - Indonesia 47
FR - Francia 41
TR - Turchia 41
JP - Giappone 39
SE - Svezia 38
JO - Giordania 33
IR - Iran 32
AT - Austria 30
PL - Polonia 29
CI - Costa d'Avorio 26
IN - India 24
AU - Australia 23
UA - Ucraina 23
BE - Belgio 19
TW - Taiwan 18
HK - Hong Kong 17
GR - Grecia 13
KR - Corea 13
DK - Danimarca 12
BR - Brasile 10
PH - Filippine 9
MA - Marocco 7
IL - Israele 6
LT - Lituania 6
LU - Lussemburgo 6
EG - Egitto 5
MO - Macao, regione amministrativa speciale della Cina 4
MY - Malesia 4
AE - Emirati Arabi Uniti 3
CH - Svizzera 3
CL - Cile 3
CZ - Repubblica Ceca 3
MU - Mauritius 3
PT - Portogallo 3
RO - Romania 3
SA - Arabia Saudita 3
AR - Argentina 2
CO - Colombia 2
EU - Europa 2
HU - Ungheria 2
MX - Messico 2
PE - Perù 2
PK - Pakistan 2
AZ - Azerbaigian 1
BD - Bangladesh 1
BG - Bulgaria 1
BO - Bolivia 1
DZ - Algeria 1
EC - Ecuador 1
EE - Estonia 1
ET - Etiopia 1
LC - Santa Lucia 1
NG - Nigeria 1
NO - Norvegia 1
NZ - Nuova Zelanda 1
PA - Panama 1
RS - Serbia 1
SK - Slovacchia (Repubblica Slovacca) 1
TH - Thailandia 1
Totale 12.239
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Città #
Fairfield 1.252
Milan 974
Woodbridge 801
Santa Clara 629
Houston 612
Ashburn 528
Seattle 483
Wilmington 470
Cambridge 464
Ann Arbor 378
Chandler 361
Singapore 204
Dearborn 157
Málaga 140
Dong Ket 119
Boardman 118
Rome 99
Redwood City 88
Dublin 86
Beijing 80
Princeton 76
Lawrence 74
Zibido San Giacomo 73
Ottawa 64
Bovisio Masciago 56
Fort Worth 56
Gavirate 56
Jakarta 46
San Diego 43
Medford 40
Helsinki 38
London 36
Amman 33
Vienna 28
Ciampino 27
Rho 27
Segrate 27
Abidjan 26
Des Moines 26
Monza 23
Dallas 22
Delft 21
Harbin 20
Shanghai 18
Falkenstein 17
Madrid 17
Brussels 16
Istanbul 16
Xian 16
Hangzhou 13
Torino 13
Mountain View 12
Oldham 12
Taipei 12
Amstelveen 11
Busto Garolfo 11
Norwalk 11
Fremont 10
Italy 10
Venegono Superiore 10
Athens 9
Bolu 9
Glasgow 9
Southampton 9
Tokyo 9
Turin 9
Casarile 8
Giussano 8
Guangzhou 8
Phoenix 8
Brookings 7
Marnate 7
Munich 7
Ankara 6
Bristol 6
Busto Arsizio 6
Cornate 6
Hong Kong 6
Los Angeles 6
New York 6
Padova 6
San Francisco 6
Tehran 6
Vilnius 6
Auburn Hills 5
Berlin 5
Bologna 5
Boulder 5
Bresso 5
Changsha 5
Davao City 5
Parma 5
Saint Petersburg 5
Sydney 5
Washington 5
Zhengzhou 5
Ariano Irpino 4
Atlanta 4
Barcelona 4
Cadoneghe 4
Totale 9.455
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Nome #
LUMIO: a Cubesat at Earth-Moon L2 361
Attitude Control for the LUMIO CubeSat in Deep Space 360
LUMIO: Charazterizing Lunar Meteoroid Impacts with a CubeSat 260
Adaptive Attitude Tracking with Active Uncertainty Rejection 232
System Design of LUMIO: a CubeSat at Earth-Moon l2 for Observing Lunar Meteoroid Impacts 223
Attitude tracking with an adaptive sliding mode response to reaction wheel failure 223
Attitude guidance and tracking for spacecraft with two reaction wheels 217
Families of halo orbits in the elliptic restricted three-body problem for a solar sail with reflectivity control devices 189
LUMIO: an Autonomous CubeSat for Lunar Exploration 177
Phase a Design of the LUMIO Spacecraft: a Cubesat for Observing and Characterizing Micro-Meteoroid Impacts on the Lunar far Side 172
LUMIO: achieving autonomous operations for Lunar exploration with a CubeSat 168
Motion planning on a class of 6-D Lie groups via a covering map 168
Orbit-Attitude Control in a Circular Restricted Three-Body Problem Using Distributed Reflectivity Devices 166
Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems 157
Fixed-time near-optimal control for repointing maneuvers of a spacecraft with nonlinear terminal constraints 157
A motion planning method for spacecraft attitude maneuvers using single polynomials 156
A singular adaptive attitude control with active disturbance rejection 155
A semi-analytic approach to spacecraft attitude guidance 151
Geometric attitude motion planning for spacecraft with pointing and actuator constraints 148
Adaptive fault-tolerant control of spacecraft attitude dynamics with actuator failures 146
Enhancing Station-Keeping Control With the Use of Extended State Observers 146
An efficient sub-optimal motion planning method for attitude manoeuvres 142
Fault-Tolerant Station-Keeping on Libration Point Orbits 141
Finite-time relative orbit-attitude tracking control for multi-spacecraft with collision avoidance and changing network topologies 137
LUMIO Cubesat: a Mission to Refine Meteoroid Population Knowledge 137
LUMIO CubeSat: toward a Lunar Situational Awareness 134
Trajectory generation using sub-Riemannian curves for quadrotor UAVs 132
Near minimum-time trajectories for quadrotor UAVs in complex environments 131
Predicting the Outcome of the LUMIO Lunar Cubesat 130
Control of solar sail periodic orbits in the elliptic three-body problem 126
Integrated guidance and control for solar sail station-keeping with optical degradation 126
Analytical method for perturbed frozen orbit around an asteroid in highly inhomogeneous gravitational fields: A first approach 124
Path Planning Using Concatenated Analytically-Defined Trajectories for Quadrotor UAVs 123
Analytic estimates and topological properties of the weak stability boundary 122
Semi-Analytic motion planning with actuator constraints on 3-D Lie groups 119
Displaced geostationary orbit design using hybrid sail propulsion 118
Identification of new orbits to enable future mission opportunities for the human exploration of the Martian moon Phobos 117
The geometry of optimal control solutions on some six dimensional lie groups 116
Dynamical systems techniques for designing libration point orbits in proximity of highly-inhomogeneous planetary satellites: Application to the Mars-Phobos elliptic three-body problem with additional gravity harmonics 116
Time-delayed autosynchronous swarm control 115
Natural motion around the Martian moon Phobos: the dynamical substitutes of the Libration Point Orbits in an elliptic three-body problem with gravity harmonics 114
Lyapunov characteristic exponent maps for multi-body space systems analysis 114
Path planning for simple wheeled robots: Sub-Riemannian and elastic curves on SE(2) 113
Design of an attitude stabilization electromagnetic module for detumbling uncooperative targets 113
Analytic perturbative theories in highly inhomogeneous gravitational fields 112
Singularities of optimal control problems on some 6-D lie groups 112
A quaternion-based attitude tracking controller for robotic systems 111
Optimal De-Tumbling of Spacecraft with Four Thrusters 111
Optimal geometric motion planning for a spin-stabilized spacecraft 111
Low-thrust-enabled highly-non-Keplerian orbits in support of future Mars exploration 110
Planning rigid body motions using elastic curves 108
Rigid Body Trajectories in Different 6D Spaces 108
Displaced geostationary orbits using hybrid low-thrust propulsion 106
Survey of highly-non-Keplerian orbits with low-thrust propulsion 105
Solar sail formation flying for deep-space remote sensing 104
Design of optimal earth pole-sitter transfers using low-thrust propulsion 103
Planning natural repointing manoeuvres for nano-spacecraft 103
Integrating Hamiltonian systems defined on the Lie groups SO(4) and SO(1,3) 100
Low-thrust propulsion in a coplanar circular restricted four body problem 99
Identification of new orbits to enable future missions for the exploration of the martian moon phobos 99
An analysis of dissipation functions in swarming systems 99
Optimal kinematic control of an autonomous underwater vehicle 98
Heteroclinic optimal control solutions for attitude motion planning 98
Integrable quadratic hamiltonians on the euclidean group of motions 97
Dynamical analysis of an orbiting three-rigid-body system 97
Near time-minimal earth to L1 transfers for low-thrust spacecraft 97
A new approach to the solution of free rigid body motion for attitude maneuvers 95
Extended-State-Observer Based Event-Triggered Orbit-Attitude Tracking for Low-Thrust Spacecraft 94
Neural-network-based optimal attitude control using four impulsive thrusters 94
Adaptive fault-tolerant control for longitudinal motion of supercavitating vehicles 94
Mission analysis and systems design of a near-term and far-term pole-sitter mission 93
Optimal attitude motion planner for large slew maneuvers using a shape-based method 91
Analytical low-jerk reorientation maneuvers for multi-body spacecraft structures 89
Closed form solution for p-curves in SO(4) 88
An optimal gains matrix for time-delay feedback control 87
Identification of new orbits to enable future mission opportunities for the human exploration of the Martian Moon Phobos 86
Time-delayed feedback control in astrodynamics 86
Optimal under-actuated kinematic motion planning on the Epsilon-group 86
On the Sophisticated Orbit Design of the Lunar Meteoroid Impacts Observer CubeSat 85
New periodic orbits in the solar sail three-body problem 81
Optimal path planning for nonholonomic robotic systems via parametric optimisation 81
Mission analysis and systems design of a near-term and far-term pole-sitter mission 79
An exponentially fast attitude tracking controller on the rotation group 78
Design of optimal earth pole-sitter transfers using low-thrust propulsion 74
Quadratic Hamiltonians on non-Euclidean spaces of arbitrary constant curvature 73
Finite-time attitude set-point tracking for thrust-vectoring spacecraft rendezvous 73
Integrating control systems defined on the frame bundles of the space forms 72
Developing and Analysing an Electromechanical Model of a Bio-Inspired Flapping Wing Mini UAV 71
Control of a Thrust-Vectoring CubeSat Using a Single Variable-Speed Control Moment Gyroscope 68
An Application of Adaptive Fault-Tolerant Control to Nano-Spacecraft 66
Relative Orbit-Attitude Tracking for Spacecraft Using Adaptive Fast Terminal Sliding Mode Control 66
Passive orbit control for space-based geo-engineering 66
Singularities of optimal attitude motions 65
Stabilizing periodic orbits above the Ecliptic plane in the solar sail 3-body problem 63
Integrable Hamiltonian systems defined on the Lie groups SO(3) and SU(2): an application to the attitude control of a spacecraft 61
An inverse dynamics approach to the guidance of spacecraft in close proximity of tumbling debris 61
Observer-based control for spacecraft electromagnetic docking 60
Post-capture attitude control with prescribed performance 58
Attitude motion planning for a spin stabilised disk sail 55
Computationally light attitude controls for resource limited nano-spacecraft 55
Totale 11.874
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Categoria #
all - tutte 124.823
article - articoli 16.383
book - libri 0
conference - conferenze 96.237
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 11.968
Totale 249.411
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20202.005 0 0 0 0 0 473 342 347 364 167 192 120
2020/20211.747 142 82 135 144 123 180 66 154 138 148 138 297
2021/20221.163 67 150 108 51 94 58 63 112 68 56 152 184
2022/20231.075 165 103 58 114 94 125 26 66 112 153 49 10
2023/2024499 31 95 24 36 17 56 19 6 4 82 13 116
2024/20251.067 13 118 33 32 609 262 0 0 0 0 0 0
Totale 12.385