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

VASILE, MASSIMILIANO
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 3.821
EU - Europa 1.533
AS - Asia 548
SA - Sud America 20
AF - Africa 18
Continente sconosciuto - Info sul continente non disponibili 6
OC - Oceania 2
Totale 5.948
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 3.760
IT - Italia 430
UA - Ucraina 283
SG - Singapore 225
SE - Svezia 214
DE - Germania 172
CN - Cina 121
FI - Finlandia 101
GB - Regno Unito 100
VN - Vietnam 86
CA - Canada 58
IE - Irlanda 56
AT - Austria 51
IN - India 46
FR - Francia 34
NL - Olanda 27
JP - Giappone 23
BR - Brasile 19
BE - Belgio 18
ES - Italia 18
KR - Corea 15
CI - Costa d'Avorio 11
JO - Giordania 10
RU - Federazione Russa 8
EU - Europa 6
HK - Hong Kong 6
CH - Svizzera 4
LU - Lussemburgo 4
RO - Romania 4
BJ - Benin 3
IL - Israele 3
IR - Iran 3
PT - Portogallo 3
TR - Turchia 3
AU - Australia 2
AZ - Azerbaigian 2
CZ - Repubblica Ceca 2
GT - Guatemala 2
MW - Malawi 2
PH - Filippine 2
TH - Thailandia 2
BG - Bulgaria 1
CR - Costa Rica 1
EE - Estonia 1
EG - Egitto 1
MA - Marocco 1
PY - Paraguay 1
RS - Serbia 1
SA - Arabia Saudita 1
SI - Slovenia 1
Totale 5.948
Salva come PNG Salva come JPEG
Città #
Chandler 482
Houston 400
Woodbridge 381
Fairfield 327
Ann Arbor 316
Wilmington 220
Ashburn 174
Milan 173
Singapore 162
Santa Clara 160
Jacksonville 156
Cambridge 126
Seattle 126
Dearborn 123
Boardman 105
Medford 76
Lawrence 69
Beijing 60
Dublin 55
Ottawa 55
Dong Ket 51
Vienna 51
Rome 46
San Diego 32
Bovisio Masciago 25
Helsinki 22
Redwood City 19
Norwalk 15
Brussels 14
Tokyo 14
Amsterdam 13
Berlin 12
Abidjan 11
Málaga 11
Seongnam 11
Amman 10
Sassuolo 10
Delft 9
Oldham 9
Turin 8
Auburn Hills 7
Nanjing 7
College Park 6
Des Moines 6
Urbana 6
Aylesbury 5
Los Angeles 5
Novara 5
Oakhurst 5
Bergamo 4
Falkenstein 4
Glasgow 4
Guangzhou 4
Harbin 4
Kolkata 4
Lafayette 4
Redmond 4
Verona 4
Xian 4
Cotonou 3
Crema 3
Gunzenhausen 3
Hefei 3
Kowloon 3
Le Chesnay 3
London 3
Louvain 3
Madrid 3
Monza 3
Mountain View 3
Nanchang 3
New Delhi 3
New York 3
Osaka 3
Pordenone 3
Scafati 3
Shanghai 3
The Dalles 3
Tuscaloosa 3
Zanjan 3
Aduthurai 2
Ankara 2
Baku 2
Baotou 2
Biesenthal 2
Brno 2
Changsha 2
Chennai 2
Chiang Mai 2
Cologno Monzese 2
Farnham 2
Fort Worth 2
Guatemala City 2
Hattiesburg 2
Indiana 2
Italy 2
Kaluga 2
Kumar 2
Modena 2
Molteno 2
Totale 4.334
Salva come PNG Salva come JPEG
Nome #
An Approach to the Design of Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 178
Non Deterministic Planning with Evidence and Paradoxical Reasoning Theories 142
Autonomous Rover Control with Behavioral Algorithms and Neural Networks 141
Combining Two and Three-Body Dynamics for Low Energy Transfer Trajectories of Practical Interest 138
A Non-Deterministic Planner for Planetary Rover Autonomy 132
A multi-criteria assessment of deflection methods for dangerous NEOs 118
Approach to Model Interest for a Planetary Rover Through Dezert-Smarandache Theory 115
Attitude Dynamics of ESMO Satellite: Mass Expulsion Torques and Propellant Slosh Model 114
Earth-to-Moon Low Energy Transfers Targeting L-1 Hyperbolic Transit Orbits 113
Preliminary design of multiple gravity-assist trajectories 107
A comparative assessment of different deviation strategies for dangerous NEO 107
A Systematic-Heuristic Approach for Space Trajectory Design 106
Low-thrust-enabled highly-non-Keplerian orbits in support of future Mars exploration 106
Autonomous Navigation of a Rover for Planetary Exploration 104
A Hybrid Optimization of the Low Energy Interplanetary Transfers Associated to the Invariant Manifolds of the Restricted Three-Body Problem 104
Direct Multiphase Optimisation of Multiobjective Trajectory Design Problems 101
Space and ground based large scale solar power plants. A European perspective 101
Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 100
Preliminary design of Low-thrust multiple gravity-assist trajectories 98
Autonomous Landing Manoeuvre by Landmark Tracking Technique 94
Trajectory Design Combining Low-Thrust and Gravity Assist Manoeuvres 93
Prospects for space power work in Europe 91
Orpheus Project: a Study Proposal for a Mars ISRU Plant 91
Automated Reconfiguration Manoeuvres for Swarm Formation of Satellites 87
Design of Earth-Mars transfer trajectories using evolution-branching technique 87
Concepts for Near-Earth Asteroid Deflection Using Spacecraft with Advanced Nuclear and Solar Electric Propulsion Systems 87
Concepts for near-Earth asteroid deflection using spacecraft with advanced nuclear and solar electric propulsion systems 86
Autonomous Navigation with Stereo Vision System for Planetary Exploration 85
Design of Earth-Mars transfer trajectories using evolutionary-branching technique 84
Optimal Trajectories for Lunar Landing Missions 84
A Vision System for Autonomous Landing Manoeuvres 84
Design of low-thrust trajectories for the exploration of the outer solar system 84
Trajectory Optimization for a Mission to NEOs, Using Low-Thrust Propulsion and Gravity Assist 82
Comparison Between Cyclers and Stop-Over Cyclers for a Regular Earth-Mars Transportation System 80
Reflexive Control of a Rover for Planetary Exploration with Artificial Neural Networks 80
In Situ Propellant Production on Mars 79
Autonomous Orbit Determination by Optical Devices 78
Optimal Interplanetary Trajectories Using a Combination of Low-Thrust and Gravity Assist Manoeuvres 78
Agora: Mission to Demonstrate Technologies to Actively Remove Ariane Rocket Bodies 76
Preliminary Analysis of Low-Thrust Gravity Assist Trajectories by an Inverse Method and a Global Optimization Technique 71
Evolution of the Concurrent Design Process Under Uncertainties 71
Robust Optimisation of Trajectories Intercepting Dangerous NEO 71
Deep Space Autonomous Orbit Determination Using CCD Cameras 68
Combining Low-Thrust and Gravity Assist Manoeuvres to Reach Planet Mercury 68
Optimizing Low-Thrust and Gravity Assist Maneuvers to Design Interplanetary Trajectories 68
A Tool for Preliminary Design of Low Thrust Gravity-Assist Trajectories 68
Probabilistic Optimisation Applied to to Spacecraft Rendezvous on Keplerian Orbits 65
A global approach to optimal space trajectory design 65
Robustness Optimisation of Aerocapture Trajectories Design Using a Hybrid Co-Evolutionary Approach 65
Optimal trajectories for NEO deflection 63
Interplanetary and Lunar Transfers Using Libration Points 62
WISDOM: an Advanced Intelligent, Fault-Tolerant System for Autonomy in Risky Environments 61
Electric Propulsion Options for a Probe to Europa 60
Economical Earth-Moon Transfers: a Quality Study 59
Combining Evolutionary Programs and Gradient Methods for WSB Transfer Optimisation 59
Autonomous Control of a Rover for Planetary Exploration based on Behavioral Algorithms 58
New Algorithm for Attitude Determination Using GPS Signals 54
Advanced Trajectory Options for the Exploration of the Pluto-Charon System 54
Effectiveness of GNSS disposal strategies 54
Options for a mission to Pluto and beyond 53
Direct Averaging for Multiple Revolution Trajectory Optimisation 52
Low Thrust Interplanetary Transfers Through Invariant Manifolds and an Evolutionary Neurocontrol 52
Assessment of an Integrated Space-Terrestrial, Solar-Based Euro-Asian Energy System 51
Roles of Solar Power from Space for Europe: Space Exploration and Combinations with Terrestral Solar Plants Concepts 50
Optimal Attitude Trajectory Manoeuvre for Moon Landing 49
End-of-life disposal concepts for Libration Point and Highly Elliptical Orbit missions 49
Targeting a Heliocentric Orbit Combining Low-Thrust Propulsion and Gravity Assist Maneuvers 47
Lunar Orbital Dynamics by Finite Element in Time Method 46
A global optimization algorithm for space trajectory design 44
Trajectory optimization for the Hevelius - Lunar Microsatellite Mission 42
Preliminary analysis of interplanetary trajectories with aerogravity and gravity assist manoeuvres 42
Space Trajectory Optimisation in a Concurrent Design Environment: Results and Related Issues 41
Direct Lunar Descent Optimisation by Finite Elements in Time Approach 40
Robotic Systems for Active Debris Removal: Equipments, State-of-the-Art, and Concept Architecture of the Rendez Vous and Capture (RVC) Control System 40
Halo orbit determination in the mission analysis of the Hevelius - Lunar microsatellite mission 37
Interception and deviation of near earth objects via solar collector strategy 36
On the Solution of Interplanetary Trajectory Design Problems by Global Optimisation Methods 34
Mission analysis of Hevelius - Lunar microsatellite mission 28
Totale 6.012
Salva come PNG Salva come JPEG
Categoria #
all - tutte 16.857
article - articoli 3.179
book - libri 0
conference - conferenze 12.804
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 874
Totale 33.714
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/2020818 0 0 0 0 136 126 147 70 118 53 138 30
2020/2021818 70 38 61 35 84 69 67 72 41 88 54 139
2021/2022654 29 87 20 44 87 19 22 23 41 48 91 143
2022/2023799 143 103 70 88 52 107 10 54 96 28 42 6
2023/2024343 34 67 15 36 25 29 28 0 44 11 5 49
2024/2025499 17 105 37 42 298 0 0 0 0 0 0 0
Totale 6.012