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

VASILE, MASSIMILIANO
 Distribuzione geografica
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Continente #
NA - Nord America 4.637
EU - Europa 2.600
AS - Asia 1.507
SA - Sud America 457
AF - Africa 42
Continente sconosciuto - Info sul continente non disponibili 6
OC - Oceania 2
Totale 9.251
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Nazione #
US - Stati Uniti d'America 4.540
RU - Federazione Russa 919
SG - Singapore 663
IT - Italia 465
CN - Cina 450
BR - Brasile 398
UA - Ucraina 288
SE - Svezia 218
DE - Germania 191
VN - Vietnam 150
GB - Regno Unito 125
FI - Finlandia 107
IN - India 71
CA - Canada 70
IE - Irlanda 65
AT - Austria 60
FR - Francia 50
NL - Olanda 35
JP - Giappone 26
KR - Corea 26
AR - Argentina 22
ES - Italia 22
HK - Hong Kong 20
BD - Bangladesh 18
BE - Belgio 18
JO - Giordania 13
CI - Costa d'Avorio 11
MX - Messico 10
MA - Marocco 9
EC - Ecuador 8
IQ - Iraq 8
SA - Arabia Saudita 7
UY - Uruguay 7
CO - Colombia 6
EU - Europa 6
PY - Paraguay 6
RO - Romania 6
TR - Turchia 6
AZ - Azerbaigian 5
IL - Israele 5
LU - Lussemburgo 5
ZA - Sudafrica 5
CH - Svizzera 4
CZ - Repubblica Ceca 4
PK - Pakistan 4
PL - Polonia 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 9.251
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Città #
Chandler 482
Singapore 420
Houston 400
Woodbridge 381
Ashburn 357
Santa Clara 337
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 86
Medford 76
Lawrence 69
Dublin 64
Vienna 60
Los Angeles 56
Ottawa 55
Dong Ket 51
Rome 48
Dallas 39
San Diego 32
The Dalles 30
Buffalo 29
Ho Chi Minh City 26
Bovisio Masciago 25
Helsinki 23
São Paulo 23
Amsterdam 20
Redwood City 19
Tokyo 17
Hong Kong 15
Norwalk 15
Brussels 14
Amman 13
Berlin 12
London 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
New Delhi 9
New York 9
Oldham 9
Brasília 8
Curitiba 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
Redondo Beach 6
Turku 6
Urbana 6
Aylesbury 5
Baku 5
Haiphong 5
Montevideo 5
Montreal 5
Munich 5
Novara 5
Oakhurst 5
Stockholm 5
Tianjin 5
Bergamo 4
Changsha 4
Chennai 4
Falkenstein 4
Glasgow 4
Hillsboro 4
Kolkata 4
Madrid 4
Mumbai 4
Petrolina 4
Redmond 4
Ribeirão Preto 4
Salvador 4
Shanghai 4
Shijiazhuang 4
Tashkent 4
Totale 5.739
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Nome #
An Approach to the Design of Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 258
Non Deterministic Planning with Evidence and Paradoxical Reasoning Theories 208
Autonomous Rover Control with Behavioral Algorithms and Neural Networks 202
A Non-Deterministic Planner for Planetary Rover Autonomy 199
Attitude Dynamics of ESMO Satellite: Mass Expulsion Torques and Propellant Slosh Model 185
Combining Two and Three-Body Dynamics for Low Energy Transfer Trajectories of Practical Interest 183
A multi-criteria assessment of deflection methods for dangerous NEOs 174
Approach to Model Interest for a Planetary Rover Through Dezert-Smarandache Theory 168
A comparative assessment of different deviation strategies for dangerous NEO 166
A Systematic-Heuristic Approach for Space Trajectory Design 164
A Hybrid Optimization of the Low Energy Interplanetary Transfers Associated to the Invariant Manifolds of the Restricted Three-Body Problem 164
Autonomous Navigation of a Rover for Planetary Exploration 163
Orpheus Project: a Study Proposal for a Mars ISRU Plant 149
Earth-to-Moon Low Energy Transfers Targeting L-1 Hyperbolic Transit Orbits 149
Direct Multiphase Optimisation of Multiobjective Trajectory Design Problems 148
Low-thrust-enabled highly-non-Keplerian orbits in support of future Mars exploration 148
Autonomous Navigation with Stereo Vision System for Planetary Exploration 146
Autonomous Landing Manoeuvre by Landmark Tracking Technique 146
Automated Reconfiguration Manoeuvres for Swarm Formation of Satellites 145
Low Energy Interplanetary Transfers Exploiting Invariant Manifolds of the Restricted Three-Body Problem 142
Preliminary design of multiple gravity-assist trajectories 141
A Vision System for Autonomous Landing Manoeuvres 141
Preliminary design of Low-thrust multiple gravity-assist trajectories 137
Agora: Mission to Demonstrate Technologies to Actively Remove Ariane Rocket Bodies 137
Reflexive Control of a Rover for Planetary Exploration with Artificial Neural Networks 131
Trajectory Design Combining Low-Thrust and Gravity Assist Manoeuvres 131
A Tool for Preliminary Design of Low Thrust Gravity-Assist Trajectories 131
Design of Earth-Mars transfer trajectories using evolutionary-branching technique 129
In Situ Propellant Production on Mars 129
Prospects for space power work in Europe 128
Trajectory Optimization for a Mission to NEOs, Using Low-Thrust Propulsion and Gravity Assist 125
Space and ground based large scale solar power plants. A European perspective 123
Comparison Between Cyclers and Stop-Over Cyclers for a Regular Earth-Mars Transportation System 121
Design of Earth-Mars transfer trajectories using evolution-branching technique 120
Concepts for near-Earth asteroid deflection using spacecraft with advanced nuclear and solar electric propulsion systems 120
Optimal Trajectories for Lunar Landing Missions 120
Autonomous Orbit Determination by Optical Devices 119
Optimal Interplanetary Trajectories Using a Combination of Low-Thrust and Gravity Assist Manoeuvres 119
WISDOM: an Advanced Intelligent, Fault-Tolerant System for Autonomy in Risky Environments 115
Concepts for Near-Earth Asteroid Deflection Using Spacecraft with Advanced Nuclear and Solar Electric Propulsion Systems 113
Deep Space Autonomous Orbit Determination Using CCD 112
A global approach to optimal space trajectory design 110
Low Thrust Interplanetary Transfers Through Invariant Manifolds and an Evolutionary Neurocontrol 110
Interplanetary and Lunar Transfers Using Libration Points 107
Optimizing Low-Thrust and Gravity Assist Maneuvers to Design Interplanetary Trajectories 105
Autonomous Control of a Rover for Planetary Exploration based on Behavioral Algorithms 105
New Algorithm for Attitude Determination Using GPS Signals 104
Assessment of an Integrated Space-Terrestrial, Solar-Based Euro-Asian Energy System 104
Evolution of the Concurrent Design Process Under Uncertainties 103
Advanced Trajectory Options for the Exploration of the Pluto-Charon System 103
Design of low-thrust trajectories for the exploration of the outer solar system 103
Combining Low-Thrust and Gravity Assist Manoeuvres to Reach Planet Mercury 102
Preliminary Analysis of Low-Thrust Gravity Assist Trajectories by an Inverse Method and a Global Optimization Technique 100
Robustness Optimisation of Aerocapture Trajectories Design Using a Hybrid Co-Evolutionary Approach 98
Probabilistic Optimisation Applied to to Spacecraft Rendezvous on Keplerian Orbits 97
Economical Earth-Moon Transfers: a Quality Study 94
A global optimization algorithm for space trajectory design 94
Robust Optimisation of Trajectories Intercepting Dangerous NEO 91
Optimal trajectories for NEO deflection 90
Combining Evolutionary Programs and Gradient Methods for WSB Transfer Optimisation 87
Electric Propulsion Options for a Probe to Europa 86
Roles of Solar Power from Space for Europe: Space Exploration and Combinations with Terrestral Solar Plants Concepts 85
Targeting a Heliocentric Orbit Combining Low-Thrust Propulsion and Gravity Assist Maneuvers 84
Effectiveness of GNSS disposal strategies 84
End-of-life disposal concepts for Libration Point and Highly Elliptical Orbit missions 82
Lunar Orbital Dynamics by Finite Element in Time Method 81
Direct Averaging for Multiple Revolution Trajectory Optimisation 79
Options for a mission to Pluto and beyond 79
Optimal Attitude Trajectory Manoeuvre for Moon Landing 79
Trajectory optimization for the Hevelius - Lunar Microsatellite Mission 76
Space Trajectory Optimisation in a Concurrent Design Environment: Results and Related Issues 76
Direct Lunar Descent Optimisation by Finite Elements in Time Approach 75
Robotic Systems for Active Debris Removal: Equipments, State-of-the-Art, and Concept Architecture of the Rendez Vous and Capture (RVC) Control System 71
Interception and deviation of near earth objects via solar collector strategy 67
Halo orbit determination in the mission analysis of the Hevelius - Lunar microsatellite mission 65
Preliminary analysis of interplanetary trajectories with aerogravity and gravity assist manoeuvres 65
Mission analysis of Hevelius - Lunar microsatellite mission 63
On the Solution of Interplanetary Trajectory Design Problems by Global Optimisation Methods 62
Totale 9.315
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Categoria #
all - tutte 25.985
article - articoli 4.650
book - libri 0
conference - conferenze 20.017
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.318
Totale 51.970
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021530 0 0 0 0 0 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
2024/20251.525 17 105 37 42 307 205 101 139 189 46 193 144
2025/20262.277 734 719 299 328 174 23 0 0 0 0 0 0
Totale 9.315