Nome |
# |
Rendezvous in Lunar Near Rectilinear Halo Orbits, file e0c31c0c-37d1-4599-e053-1705fe0aef77
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509
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Cislunar Non-Keplerian Orbits Rendezvous & Docking: 6DOF Guidance and Control, file e0c31c0c-3370-4599-e053-1705fe0aef77
|
497
|
Fully magnetic attitude control subsystem for picosat platforms, file e0c31c0d-a98f-4599-e053-1705fe0aef77
|
430
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Technologies And Facilities For The AIV/AIT Phase Of Nanosatellites ADCS Subsystems: HERMES As An Applicative Case, file e0c31c11-d1cc-4599-e053-1705fe0aef77
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420
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H.E.R.M.E.S.: a CubeSat Based Constellation for the New Generation of Multi-Messenger Astrophysics, file e0c31c10-05ab-4599-e053-1705fe0aef77
|
224
|
Localisation of gamma-ray bursts from the combined SpIRIT+HERMES-TP/SP nano-satellite constellation, file e3495973-2620-4104-8d0d-7920bc4b30c9
|
212
|
An Effective Sensor Architecture for Full-Attitude Determination in the HERMES Nano-Satellites, file 7431ce28-ebbe-4449-90e6-712b321e46b3
|
195
|
Fault Tolerant Attitude and Orbit Determination System for Small Satellite Platforms, file e0c31c12-2a71-4599-e053-1705fe0aef77
|
188
|
A Spacecraft Attitude Determination and Control Algorithm for Solar Arrays Pointing Leveraging Sun Angle and Angular Rates Measurements, file e0c31c12-0426-4599-e053-1705fe0aef77
|
168
|
Floquet modes and stability analysis of periodic orbit-attitude solutions along Earth–Moon halo orbits, file e0c31c11-94b9-4599-e053-1705fe0aef77
|
150
|
GrailQuest and HERMES: hunting for gravitational wave electromagnetic counterparts and probing space-time quantum foam, file e0c31c10-cd8e-4599-e053-1705fe0aef77
|
123
|
Integrated vibration suppression attitude control for flexible spacecrafts with internal liquid sloshing, file e0c31c11-24d3-4599-e053-1705fe0aef77
|
86
|
Enhancing Technologies and Operations for Service Transportation in Cislunar Environment, file e0c31c11-eb1b-4599-e053-1705fe0aef77
|
85
|
Oxygen Extraction from Lunar Soil Oxides: on Ground Experiments and Numerical Modelling for Thermal Reduction Processes, file 9950d1ea-9764-4a8e-baf5-8630c5092770
|
84
|
Guidance, navigation and control for 6DOF rendezvous in Cislunar multi-body environment, file e0c31c11-19b6-4599-e053-1705fe0aef77
|
82
|
The payload data handling unit (PDHU) on-board the HERMES-TP and HERMES-SP CubeSat missions, file e0c31c10-aadb-4599-e053-1705fe0aef77
|
78
|
Dynamical analysis of rendezvous and docking with very large space infrastructures in non-Keplerian orbits, file e0c31c0d-a99c-4599-e053-1705fe0aef77
|
76
|
A Finite State Machine Approach to Nano-Satellite SW Design: the HERMES Case Study, file 14e8f0ec-af7c-48ba-8c4d-c82921f0b46f
|
71
|
Preliminary results on the dynamics of large and flexible space structures in Halo orbits, file e0c31c0d-b2ff-4599-e053-1705fe0aef77
|
70
|
Sky visibility analysis for astrophysical data return maximization in HERMES constellation, file e0c31c0f-f0b0-4599-e053-1705fe0aef77
|
54
|
Characterisation of 6DOF natural and controlled relative dynamics in cislunar space, file e0c31c10-837d-4599-e053-1705fe0aef77
|
43
|
Lunar Oxygen Production System Study and Equipment Breadboarding, file a9db337e-d816-458d-b034-ab07be300b9d
|
37
|
Solid-Gas Carbothermal Reduction for Water Production from Lunar Regolith Simulant: Experimental Results, file d12b2eb1-120f-4051-b05b-a20f8994c9c8
|
33
|
Flat-Sat Facility for Processor-In-the-loop Verification and Testing of Nanosatellite ADCS, file a03eca45-953f-4b7f-bf93-94ab04b9fbf0
|
24
|
Editorial: Astrodynamics, guidance, navigation and control in chaotic multi-body environments, file d63e660e-2bf8-4ed5-83d5-352d43eca36b
|
23
|
Integrated Magnetic Management of Stored Angular Momentum in Autonomous Attitude Control Systems, file 95c7d7b5-78ef-4e1c-a0d5-611e7cfb8db7
|
22
|
HERMES Constellation: a New Paradigm for Multi-Messenger Astrophysics with CubeSats, file 2da5e3ed-cd6d-45db-aa2e-6fc6cff1fa09
|
13
|
Terrestrial demonstrator for a low-temperature carbothermal reduction process on lunar regolith simulant: Design and AIV activities, file 2fba204c-56a3-4387-86ec-f2972d1229f8
|
11
|
Rendezvous in Lunar Near Rectilinear Halo Orbits, file 6a31a486-3297-4f8b-839d-a39221472a6c
|
10
|
Semi-Analytical Approach to Fasten Complex and Flexible Pointing Strategies Definition for Nanosatellite Clusters: the HERMES Mission Case from Design to Flight, file e0c31c0e-714a-4599-e053-1705fe0aef77
|
9
|
Dynamical analysis of rendezvous and docking with very large space infrastructures in non-Keplerian orbits, file e0c31c0c-0219-4599-e053-1705fe0aef77
|
8
|
Dynamical Analysis of Rendezvous and Docking with Very Large Space Infrastructures in Non-Keplerian Orbits, file e0c31c09-9994-4599-e053-1705fe0aef77
|
7
|
Characterisation of 6DOF natural and controlled relative dynamics in cislunar space, file e0c31c10-cd13-4599-e053-1705fe0aef77
|
7
|
Preliminary results on the dynamics of large and flexible space structures in Halo orbits, file e0c31c0a-7ed6-4599-e053-1705fe0aef77
|
6
|
Lunar ISRU Ground Prototype for the Demonstration of Oxygen Extraction from Lunar Regolith, file 7cac1105-3e9d-4636-b199-5285d6a7ff5d
|
5
|
e.INSPECTOR: Multi-Spectral Imaging the VESPA Debris in Preparation to Active Removal, file da17faf4-69ce-48a1-ab91-3c770c8c2d45
|
5
|
The HERMES-technologic and scientific pathfinder, file e0c31c11-e1c3-4599-e053-1705fe0aef77
|
4
|
Dynamics and Control of Modular and Extended Space Structures in Cislunar Environment, file e0c31c0b-f442-4599-e053-1705fe0aef77
|
3
|
Terrestrial demonstrator for a low-temperature carbothermal reduction process on lunar regolith simulant: Design and AIV activities, file 063d43c9-4043-46af-bec2-0a71018536ad
|
2
|
HERMES Mission Software: from Design to Implementation of the Finite State Machine, file 37504af9-60fd-4129-9b48-80ddb212a6b9
|
2
|
Scaled Lunar ISRU Pilot Plant for Oxygen Extraction through Carbothermal Reduction: the ORACLE Payload, file 6c766231-c585-4285-8a76-5cc0a39c2939
|
2
|
Preliminary Results on the Dynamics of Large and Flexible Space Structures in Halo Orbits, file e0c31c0a-3254-4599-e053-1705fe0aef77
|
2
|
ARMONIA: Feasibility Study on Aerobots in Martian Atmosphere to Enhance Science Return, file e0c31c0a-a30c-4599-e053-1705fe0aef77
|
2
|
Assembly and operations for a cislunar orbit space station, file e0c31c0c-4175-4599-e053-1705fe0aef77
|
2
|
Sky visibility analysis for astrophysical data return maximization in HERMES constellation, file e0c31c0f-e990-4599-e053-1705fe0aef77
|
2
|
Guidance, navigation and control for 6DOF rendezvous in Cislunar multi-body environment, file e0c31c11-2d63-4599-e053-1705fe0aef77
|
2
|
Coupled Dynamics Analysis Around Asteroids by Means of Accurate Shape and Perturbations Modeling, file e0c31c08-de6d-4599-e053-1705fe0aef77
|
1
|
GTOC8: Results and Methods of POLIMI-UPM, file e0c31c09-336e-4599-e053-1705fe0aef77
|
1
|
Fully magnetic attitude control subsystem for picosat platforms, file e0c31c0d-a992-4599-e053-1705fe0aef77
|
1
|
Characterization of 6DOF Natural and Controlled Relative Dynamics in Cislunar Space, file e0c31c0e-6fb9-4599-e053-1705fe0aef77
|
1
|
Rendezvous in Lunar Near Rectilinear Halo Orbits, file e19672b5-07a6-4470-8e87-8bbc686d99f2
|
1
|
Totale |
4.093 |