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

VASILE, MASSIMILIANO
 Distribuzione geografica
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Continente #
NA - Nord America 4.749
EU - Europa 2.608
AS - Asia 1.638
SA - Sud America 460
AF - Africa 53
Continente sconosciuto - Info sul continente non disponibili 6
OC - Oceania 2
Totale 9.516
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Nazione #
US - Stati Uniti d'America 4.647
RU - Federazione Russa 919
SG - Singapore 773
CN - Cina 467
IT - Italia 467
BR - Brasile 400
UA - Ucraina 288
SE - Svezia 218
DE - Germania 191
VN - Vietnam 150
GB - Regno Unito 128
FI - Finlandia 107
CA - Canada 73
IN - India 73
IE - Irlanda 65
AT - Austria 60
FR - Francia 50
NL - Olanda 35
JP - Giappone 26
KR - Corea 26
ES - Italia 23
AR - Argentina 22
HK - Hong Kong 21
BD - Bangladesh 18
BE - Belgio 18
MA - Marocco 18
JO - Giordania 13
MX - Messico 12
CI - Costa d'Avorio 11
IQ - Iraq 9
EC - Ecuador 8
PY - Paraguay 7
SA - Arabia Saudita 7
UY - Uruguay 7
ZA - Sudafrica 7
CO - Colombia 6
EU - Europa 6
PL - Polonia 6
RO - Romania 6
TR - Turchia 6
AZ - Azerbaigian 5
IL - Israele 5
LU - Lussemburgo 5
CH - Svizzera 4
CZ - Repubblica Ceca 4
PK - Pakistan 4
UZ - Uzbekistan 4
AM - Armenia 3
BJ - Benin 3
CL - Cile 3
GT - Guatemala 3
IR - Iran 3
JM - Giamaica 3
KE - Kenya 3
NP - Nepal 3
PT - Portogallo 3
RS - Serbia 3
TH - Thailandia 3
TW - Taiwan 3
VE - Venezuela 3
AE - Emirati Arabi Uniti 2
AL - Albania 2
AU - Australia 2
BO - Bolivia 2
DO - Repubblica Dominicana 2
DZ - Algeria 2
HN - Honduras 2
ID - Indonesia 2
LB - Libano 2
MW - Malawi 2
MY - Malesia 2
PA - Panama 2
PE - Perù 2
PH - Filippine 2
SN - Senegal 2
TT - Trinidad e Tobago 2
BG - Bulgaria 1
BH - Bahrain 1
BM - Bermuda 1
CD - Congo 1
CR - Costa Rica 1
CV - Capo Verde 1
CY - Cipro 1
EE - Estonia 1
EG - Egitto 1
ET - Etiopia 1
HU - Ungheria 1
KG - Kirghizistan 1
KZ - Kazakistan 1
LV - Lettonia 1
MD - Moldavia 1
NI - Nicaragua 1
OM - Oman 1
PS - Palestinian Territory 1
SI - Slovenia 1
TN - Tunisia 1
Totale 9.516
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Città #
Chandler 482
Singapore 463
Houston 402
Woodbridge 381
Ashburn 379
Santa Clara 338
Fairfield 327
Ann Arbor 316
Wilmington 220
Milan 198
Hefei 158
Jacksonville 156
Cambridge 126
Seattle 126
Dearborn 123
Moscow 109
Council Bluffs 108
Boardman 105
Beijing 87
Medford 76
Lawrence 69
Dublin 64
Los Angeles 61
Vienna 60
Ottawa 55
Dong Ket 51
Rome 48
Dallas 39
San Jose 36
San Diego 32
The Dalles 30
Buffalo 29
Ho Chi Minh City 26
Bovisio Masciago 25
São Paulo 24
Helsinki 23
Amsterdam 20
Redwood City 19
Tokyo 17
Hong Kong 16
Norwalk 15
Brussels 14
New York 14
Amman 13
London 13
Berlin 12
Abidjan 11
Columbus 11
Hanoi 11
Málaga 11
Rio de Janeiro 11
Seongnam 11
Seoul 11
Sassuolo 10
Turin 10
Belo Horizonte 9
Delft 9
Kenitra 9
New Delhi 9
Oldham 9
Brasília 8
Curitiba 8
Montreal 8
Auburn Hills 7
Dhaka 7
Frankfurt am Main 7
Guangzhou 7
Nanjing 7
Chicago 6
College Park 6
Des Moines 6
Harbin 6
Lafayette 6
Monza 6
Mumbai 6
Orem 6
Redondo Beach 6
Turku 6
Urbana 6
Atlanta 5
Aylesbury 5
Baku 5
Haiphong 5
Montevideo 5
Munich 5
Novara 5
Oakhurst 5
Shanghai 5
Stockholm 5
Tianjin 5
Bergamo 4
Brooklyn 4
Changsha 4
Chennai 4
Falkenstein 4
Glasgow 4
Hillsboro 4
Kolkata 4
Madrid 4
Petrolina 4
Totale 5.867
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Nome #
An Approach to the Design of Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 265
Non Deterministic Planning with Evidence and Paradoxical Reasoning Theories 212
A Non-Deterministic Planner for Planetary Rover Autonomy 208
Autonomous Rover Control with Behavioral Algorithms and Neural Networks 206
Attitude Dynamics of ESMO Satellite: Mass Expulsion Torques and Propellant Slosh Model 192
Combining Two and Three-Body Dynamics for Low Energy Transfer Trajectories of Practical Interest 189
A multi-criteria assessment of deflection methods for dangerous NEOs 184
Approach to Model Interest for a Planetary Rover Through Dezert-Smarandache Theory 176
A comparative assessment of different deviation strategies for dangerous NEO 173
A Hybrid Optimization of the Low Energy Interplanetary Transfers Associated to the Invariant Manifolds of the Restricted Three-Body Problem 172
Autonomous Navigation of a Rover for Planetary Exploration 171
A Systematic-Heuristic Approach for Space Trajectory Design 169
Orpheus Project: a Study Proposal for a Mars ISRU Plant 156
Autonomous Navigation with Stereo Vision System for Planetary Exploration 153
Autonomous Landing Manoeuvre by Landmark Tracking Technique 153
Earth-to-Moon Low Energy Transfers Targeting L-1 Hyperbolic Transit Orbits 152
Low-thrust-enabled highly-non-Keplerian orbits in support of future Mars exploration 152
Automated Reconfiguration Manoeuvres for Swarm Formation of Satellites 151
Direct Multiphase Optimisation of Multiobjective Trajectory Design Problems 149
A Vision System for Autonomous Landing Manoeuvres 147
Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 144
Preliminary design of multiple gravity-assist trajectories 143
Agora: Mission to Demonstrate Technologies to Actively Remove Ariane Rocket Bodies 142
Preliminary design of Low-thrust multiple gravity-assist trajectories 140
A Tool for Preliminary Design of Low Thrust Gravity-Assist Trajectories 138
Reflexive Control of a Rover for Planetary Exploration with Artificial Neural Networks 135
In Situ Propellant Production on Mars 135
Design of Earth-Mars transfer trajectories using evolutionary-branching technique 134
Trajectory Design Combining Low-Thrust and Gravity Assist Manoeuvres 134
Prospects for space power work in Europe 130
Trajectory Optimization for a Mission to NEOs, Using Low-Thrust Propulsion and Gravity Assist 127
Comparison Between Cyclers and Stop-Over Cyclers for a Regular Earth-Mars Transportation System 123
Space and ground based large scale solar power plants. A European perspective 123
Autonomous Orbit Determination by Optical Devices 122
Design of Earth-Mars transfer trajectories using evolution-branching technique 122
Concepts for near-Earth asteroid deflection using spacecraft with advanced nuclear and solar electric propulsion systems 122
Optimal Trajectories for Lunar Landing Missions 121
Optimal Interplanetary Trajectories Using a Combination of Low-Thrust and Gravity Assist Manoeuvres 120
WISDOM: an Advanced Intelligent, Fault-Tolerant System for Autonomy in Risky Environments 119
Concepts for Near-Earth Asteroid Deflection Using Spacecraft with Advanced Nuclear and Solar Electric Propulsion Systems 114
Deep Space Autonomous Orbit Determination Using CCD 113
A global approach to optimal space trajectory design 113
Low Thrust Interplanetary Transfers Through Invariant Manifolds and an Evolutionary Neurocontrol 112
Assessment of an Integrated Space-Terrestrial, Solar-Based Euro-Asian Energy System 111
Autonomous Control of a Rover for Planetary Exploration based on Behavioral Algorithms 110
Interplanetary and Lunar Transfers Using Libration Points 108
Optimizing Low-Thrust and Gravity Assist Maneuvers to Design Interplanetary Trajectories 108
New Algorithm for Attitude Determination Using GPS Signals 108
Advanced Trajectory Options for the Exploration of the Pluto-Charon System 107
Combining Low-Thrust and Gravity Assist Manoeuvres to Reach Planet Mercury 106
Evolution of the Concurrent Design Process Under Uncertainties 105
Design of low-thrust trajectories for the exploration of the outer solar system 104
Preliminary Analysis of Low-Thrust Gravity Assist Trajectories by an Inverse Method and a Global Optimization Technique 101
Robustness Optimisation of Aerocapture Trajectories Design Using a Hybrid Co-Evolutionary Approach 99
Probabilistic Optimisation Applied to to Spacecraft Rendezvous on Keplerian Orbits 98
A global optimization algorithm for space trajectory design 98
Economical Earth-Moon Transfers: a Quality Study 96
Robust Optimisation of Trajectories Intercepting Dangerous NEO 92
Combining Evolutionary Programs and Gradient Methods for WSB Transfer Optimisation 91
Optimal trajectories for NEO deflection 91
Electric Propulsion Options for a Probe to Europa 88
Roles of Solar Power from Space for Europe: Space Exploration and Combinations with Terrestral Solar Plants Concepts 87
Targeting a Heliocentric Orbit Combining Low-Thrust Propulsion and Gravity Assist Maneuvers 86
Effectiveness of GNSS disposal strategies 85
Lunar Orbital Dynamics by Finite Element in Time Method 85
End-of-life disposal concepts for Libration Point and Highly Elliptical Orbit missions 83
Direct Averaging for Multiple Revolution Trajectory Optimisation 82
Options for a mission to Pluto and beyond 81
Optimal Attitude Trajectory Manoeuvre for Moon Landing 81
Direct Lunar Descent Optimisation by Finite Elements in Time Approach 80
Trajectory optimization for the Hevelius - Lunar Microsatellite Mission 77
Space Trajectory Optimisation in a Concurrent Design Environment: Results and Related Issues 76
Robotic Systems for Active Debris Removal: Equipments, State-of-the-Art, and Concept Architecture of the Rendez Vous and Capture (RVC) Control System 72
Interception and deviation of near earth objects via solar collector strategy 68
Preliminary analysis of interplanetary trajectories with aerogravity and gravity assist manoeuvres 66
Halo orbit determination in the mission analysis of the Hevelius - Lunar microsatellite mission 65
Mission analysis of Hevelius - Lunar microsatellite mission 65
On the Solution of Interplanetary Trajectory Design Problems by Global Optimisation Methods 64
Totale 9.580
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Categoria #
all - tutte 26.638
article - articoli 4.754
book - libri 0
conference - conferenze 20.520
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.364
Totale 53.276
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021461 0 0 0 0 0 0 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
2024/20251.525 17 105 37 42 307 205 101 139 189 46 193 144
2025/20262.542 734 719 299 328 174 180 108 0 0 0 0 0
Totale 9.580