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

BIGGS, JAMES DOUGLAS
 Distribuzione geografica
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Continente #
NA - Nord America 6.805
EU - Europa 3.534
AS - Asia 747
AF - Africa 44
OC - Oceania 23
SA - Sud America 20
Continente sconosciuto - Info sul continente non disponibili 2
Totale 11.175
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Nazione #
US - Stati Uniti d'America 6.720
IT - Italia 2.521
CN - Cina 202
VN - Vietnam 188
ES - Italia 184
GB - Regno Unito 168
DE - Germania 119
SG - Singapore 111
FI - Finlandia 109
NL - Olanda 95
IE - Irlanda 84
CA - Canada 81
TR - Turchia 40
FR - Francia 38
JP - Giappone 38
SE - Svezia 38
JO - Giordania 33
IR - Iran 32
RU - Federazione Russa 32
PL - Polonia 29
AT - Austria 28
CI - Costa d'Avorio 26
IN - India 24
AU - Australia 23
UA - Ucraina 23
BE - Belgio 19
HK - Hong Kong 17
TW - Taiwan 16
GR - Grecia 13
KR - Corea 12
BR - Brasile 10
MA - Marocco 7
IL - Israele 6
LT - Lituania 6
LU - Lussemburgo 6
PH - Filippine 6
EG - Egitto 5
DK - Danimarca 4
ID - Indonesia 4
MO - Macao, regione amministrativa speciale della Cina 4
AE - Emirati Arabi Uniti 3
CH - Svizzera 3
CL - Cile 3
CZ - Repubblica Ceca 3
MU - Mauritius 3
MY - Malesia 3
PT - Portogallo 3
RO - Romania 3
SA - Arabia Saudita 3
AR - Argentina 2
CO - Colombia 2
EU - Europa 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
EE - Estonia 1
ET - Etiopia 1
HU - Ungheria 1
LC - Santa Lucia 1
NG - Nigeria 1
NO - Norvegia 1
PA - Panama 1
RS - Serbia 1
SK - Slovacchia (Repubblica Slovacca) 1
TH - Thailandia 1
Totale 11.175
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Città #
Fairfield 1.252
Milan 969
Woodbridge 801
Houston 612
Ashburn 520
Seattle 483
Wilmington 470
Cambridge 464
Ann Arbor 378
Chandler 361
Dearborn 157
Málaga 140
Dong Ket 119
Rome 99
Redwood City 88
Dublin 84
Beijing 79
Princeton 76
Lawrence 74
Zibido San Giacomo 73
Ottawa 64
Singapore 62
Bovisio Masciago 56
Fort Worth 56
Gavirate 56
San Diego 43
Medford 40
London 35
Amman 33
Helsinki 31
Vienna 28
Ciampino 27
Rho 27
Segrate 27
Abidjan 26
Des Moines 26
Monza 23
Dallas 22
Delft 21
Harbin 19
Madrid 17
Brussels 16
Istanbul 16
Shanghai 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
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
College Park 4
Freiburg 4
Indiana 4
Kunming 4
Modugno 4
Totale 8.489
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Nome #
Attitude Control for the LUMIO CubeSat in Deep Space 351
LUMIO: a Cubesat at Earth-Moon L2 348
LUMIO: Charazterizing Lunar Meteoroid Impacts with a CubeSat 247
Adaptive Attitude Tracking with Active Uncertainty Rejection 215
Attitude tracking with an adaptive sliding mode response to reaction wheel failure 212
System Design of LUMIO: a CubeSat at Earth-Moon l2 for Observing Lunar Meteoroid Impacts 209
Attitude guidance and tracking for spacecraft with two reaction wheels 206
Families of halo orbits in the elliptic restricted three-body problem for a solar sail with reflectivity control devices 180
LUMIO: an Autonomous CubeSat for Lunar Exploration 165
Motion planning on a class of 6-D Lie groups via a covering map 159
Orbit-Attitude Control in a Circular Restricted Three-Body Problem Using Distributed Reflectivity Devices 157
LUMIO: achieving autonomous operations for Lunar exploration with a CubeSat 156
Phase a Design of the LUMIO Spacecraft: a Cubesat for Observing and Characterizing Micro-Meteoroid Impacts on the Lunar far Side 155
Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems 148
Fixed-time near-optimal control for repointing maneuvers of a spacecraft with nonlinear terminal constraints 145
A singular adaptive attitude control with active disturbance rejection 143
A semi-analytic approach to spacecraft attitude guidance 141
Geometric attitude motion planning for spacecraft with pointing and actuator constraints 139
Adaptive fault-tolerant control of spacecraft attitude dynamics with actuator failures 136
Enhancing Station-Keeping Control With the Use of Extended State Observers 136
An efficient sub-optimal motion planning method for attitude manoeuvres 133
Fault-Tolerant Station-Keeping on Libration Point Orbits 132
A motion planning method for spacecraft attitude maneuvers using single polynomials 131
Finite-time relative orbit-attitude tracking control for multi-spacecraft with collision avoidance and changing network topologies 128
Near minimum-time trajectories for quadrotor UAVs in complex environments 123
Trajectory generation using sub-Riemannian curves for quadrotor UAVs 123
LUMIO CubeSat: toward a Lunar Situational Awareness 121
Control of solar sail periodic orbits in the elliptic three-body problem 119
LUMIO Cubesat: a Mission to Refine Meteoroid Population Knowledge 119
Analytic estimates and topological properties of the weak stability boundary 112
Analytical method for perturbed frozen orbit around an asteroid in highly inhomogeneous gravitational fields: A first approach 111
Semi-Analytic motion planning with actuator constraints on 3-D Lie groups 111
Predicting the Outcome of the LUMIO Lunar Cubesat 111
Path Planning Using Concatenated Analytically-Defined Trajectories for Quadrotor UAVs 110
Displaced geostationary orbit design using hybrid sail propulsion 109
Identification of new orbits to enable future mission opportunities for the human exploration of the Martian moon Phobos 108
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 108
Lyapunov characteristic exponent maps for multi-body space systems analysis 106
Time-delayed autosynchronous swarm control 106
The geometry of optimal control solutions on some six dimensional lie groups 106
Natural motion around the Martian moon Phobos: the dynamical substitutes of the Libration Point Orbits in an elliptic three-body problem with gravity harmonics 105
Path planning for simple wheeled robots: Sub-Riemannian and elastic curves on SE(2) 105
Integrated guidance and control for solar sail station-keeping with optical degradation 105
Design of an attitude stabilization electromagnetic module for detumbling uncooperative targets 104
Singularities of optimal control problems on some 6-D lie groups 104
Analytic perturbative theories in highly inhomogeneous gravitational fields 103
A quaternion-based attitude tracking controller for robotic systems 102
Low-thrust-enabled highly-non-Keplerian orbits in support of future Mars exploration 100
Planning rigid body motions using elastic curves 100
Optimal De-Tumbling of Spacecraft with Four Thrusters 100
Optimal geometric motion planning for a spin-stabilized spacecraft 100
Rigid Body Trajectories in Different 6D Spaces 99
Survey of highly-non-Keplerian orbits with low-thrust propulsion 97
Displaced geostationary orbits using hybrid low-thrust propulsion 97
Solar sail formation flying for deep-space remote sensing 96
Design of optimal earth pole-sitter transfers using low-thrust propulsion 95
Planning natural repointing manoeuvres for nano-spacecraft 94
Low-thrust propulsion in a coplanar circular restricted four body problem 91
Integrating Hamiltonian systems defined on the Lie groups SO(4) and SO(1,3) 91
Identification of new orbits to enable future missions for the exploration of the martian moon phobos 91
Optimal kinematic control of an autonomous underwater vehicle 90
An analysis of dissipation functions in swarming systems 90
Heteroclinic optimal control solutions for attitude motion planning 90
Integrable quadratic hamiltonians on the euclidean group of motions 89
Dynamical analysis of an orbiting three-rigid-body system 89
Near time-minimal earth to L1 transfers for low-thrust spacecraft 88
A new approach to the solution of free rigid body motion for attitude maneuvers 85
Extended-State-Observer Based Event-Triggered Orbit-Attitude Tracking for Low-Thrust Spacecraft 85
Mission analysis and systems design of a near-term and far-term pole-sitter mission 84
Optimal attitude motion planner for large slew maneuvers using a shape-based method 83
Closed form solution for p-curves in SO(4) 80
Neural-network-based optimal attitude control using four impulsive thrusters 79
Analytical low-jerk reorientation maneuvers for multi-body spacecraft structures 79
Identification of new orbits to enable future mission opportunities for the human exploration of the Martian Moon Phobos 78
Time-delayed feedback control in astrodynamics 78
An optimal gains matrix for time-delay feedback control 78
Optimal under-actuated kinematic motion planning on the Epsilon-group 77
On the Sophisticated Orbit Design of the Lunar Meteoroid Impacts Observer CubeSat 75
Adaptive fault-tolerant control for longitudinal motion of supercavitating vehicles 74
New periodic orbits in the solar sail three-body problem 73
Optimal path planning for nonholonomic robotic systems via parametric optimisation 73
Mission analysis and systems design of a near-term and far-term pole-sitter mission 71
An exponentially fast attitude tracking controller on the rotation group 68
Quadratic Hamiltonians on non-Euclidean spaces of arbitrary constant curvature 65
Integrating control systems defined on the frame bundles of the space forms 65
Design of optimal earth pole-sitter transfers using low-thrust propulsion 65
Finite-time attitude set-point tracking for thrust-vectoring spacecraft rendezvous 64
Developing and Analysing an Electromechanical Model of a Bio-Inspired Flapping Wing Mini UAV 60
Control of a Thrust-Vectoring CubeSat Using a Single Variable-Speed Control Moment Gyroscope 59
Passive orbit control for space-based geo-engineering 58
An Application of Adaptive Fault-Tolerant Control to Nano-Spacecraft 57
Singularities of optimal attitude motions 57
Relative Orbit-Attitude Tracking for Spacecraft Using Adaptive Fast Terminal Sliding Mode Control 55
Stabilizing periodic orbits above the Ecliptic plane in the solar sail 3-body problem 53
Integrable Hamiltonian systems defined on the Lie groups SO(3) and SU(2): an application to the attitude control of a spacecraft 52
Observer-based control for spacecraft electromagnetic docking 51
Post-capture attitude control with prescribed performance 49
An inverse dynamics approach to the guidance of spacecraft in close proximity of tumbling debris 49
Computationally light attitude controls for resource limited nano-spacecraft 47
Attitude motion planning for a spin stabilised disk sail 46
Totale 10.862
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Categoria #
all - tutte 120.143
article - articoli 14.281
book - libri 0
conference - conferenze 93.812
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 11.871
Totale 240.107
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20203.519 377 222 137 277 501 473 342 347 364 167 192 120
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
2024/20253 3 0 0 0 0 0 0 0 0 0 0 0
Totale 11.321