| Nome |
# |
|
Periodic motion around libration points in the Elliptic Restricted Three-Body Problem, file e0c31c0d-ad09-4599-e053-1705fe0aef77
|
661
|
|
Toward Self-Driving Interplanetary CubeSats: the ERC-Funded Project EXTREMA, file e0c31c12-2572-4599-e053-1705fe0aef77
|
392
|
|
Trajectory Design and Orbit Determination of Hera’s Milani CubeSat, file e0c31c11-9691-4599-e053-1705fe0aef77
|
327
|
|
N-body gravitational and contact dynamics for asteroid aggregation, file e0c31c0a-c7e2-4599-e053-1705fe0aef77
|
299
|
|
The EXTREMA Orbital Simulation Hub: a Facility for GNC Testing of Autonomous Interplanetary CubeSat, file e0c31c12-bd7e-4599-e053-1705fe0aef77
|
246
|
|
Suitable configurations for triangular formation flying about collinear libration points under the circular and elliptic restricted three-body problems, file e0c31c0c-763c-4599-e053-1705fe0aef77
|
219
|
|
Families of Bounded Orbits near Binary Asteroid 65803 Didymos, file e0c31c0c-ffa9-4599-e053-1705fe0aef77
|
211
|
|
Ballistic landing design on binary asteroids: the AIM case study, file e0c31c0d-c63f-4599-e053-1705fe0aef77
|
139
|
|
The Hera Milani Cubesat Mission, file e0c31c11-156e-4599-e053-1705fe0aef77
|
121
|
|
Mission Analysis and Navigation Assessment for Hera’s Milani CubeSat, file e0c31c12-eb06-4599-e053-1705fe0aef77
|
118
|
|
A parallel-GPU code for asteroid aggregation problems with angular particles, file e0c31c0f-3731-4599-e053-1705fe0aef77
|
117
|
|
Design of the Vision-Based GNC Subsystem of Hera’s Milani Mission, file 807a949b-e883-4c82-a855-1d280e47f6d3
|
109
|
|
Dynamical model of binary asteroid systems through patched three-body problems, file e0c31c0d-eb9d-4599-e053-1705fe0aef77
|
97
|
|
Trajectory Options for Hera’s Milani CubeSat Around (65803) Didymos, file e0c31c12-0540-4599-e053-1705fe0aef77
|
87
|
|
A New Environment to Simulate the Dynamics in the Close Proximity of Rubble-Pile Asteroids, file e0c31c0d-5a37-4599-e053-1705fe0aef77
|
50
|
|
Double Asteroid Redirection Test (DART): Structural and Dynamic Interactions between Asteroidal Elements of Binary Asteroid (65803) Didymos, file 200caca3-6ba2-475d-8d74-1c9c69d126a9
|
33
|
|
N-body simulations of rubble-pile aggregates with angular particles, file e0c31c10-06ea-4599-e053-1705fe0aef77
|
33
|
|
Dynamical Evolution of the Didymos−Dimorphos Binary Asteroid as Rubble Piles following the DART Impact, file 88c39d45-4c86-4829-a766-442ae3deb2f2
|
32
|
|
Preliminary mission profile of Hera’s Milani CubeSat, file e0c31c10-3422-4599-e053-1705fe0aef77
|
32
|
|
The role of fragment shapes in the simulations of asteroids as gravitational aggregates, file e0c31c0f-85bd-4599-e053-1705fe0aef77
|
31
|
|
Effects of Impact and Target Parameters on the Results of a Kinetic Impactor: Predictions for the Double Asteroid Redirection Test (DART) Mission, file 6fa1d08b-96a6-4f55-998a-1f34c4053d3f
|
26
|
|
A Code for the Study of Gravitational Aggregates with Non-Spherical Particles, file e0c31c0d-7c87-4599-e053-1705fe0aef77
|
24
|
|
GRAINS: a New Numerical Method for the Study of Gravitational Aggregates, file e0c31c0d-7c88-4599-e053-1705fe0aef77
|
24
|
|
Applied Trajectory Design for CubeSat Close-Proximity Operations around Asteroids: The Milani Case, file 250b15d5-5f93-471d-9aa7-a2ce159fc4bc
|
22
|
|
Pre-encounter Predictions of DART Impact Ejecta Behavior and Observability, file 62343993-43da-438a-bedd-87ce98d85fa4
|
22
|
|
Predictions for the Dynamical States of the Didymos System before and after the Planned DART Impact, file ab256edf-990d-4d20-acc8-55b6a4fe2f28
|
19
|
|
Interior of top-shaped asteroids with cohesionless surface, file b79c7b84-3f25-495a-94ae-e3060c677fbc
|
16
|
|
Ejecta Formation, Early Collisional Processes, and Dynamical Evolution after the DART Impact on Dimorphos, file bb7333f0-cf03-4ed2-b29b-37c9959fbb2d
|
15
|
|
The Orbital Regime Index: a Comprehensive Parameter to Determine Orbital Regions Around Minor Bodies, file dbeb2be4-94b4-460a-bac2-713aa9c90697
|
14
|
|
After DART: Using the First Full-scale Test of a Kinetic Impactor to Inform a Future Planetary Defense Mission, file d70808b0-fff1-49ac-af2f-87fd9c33a22c
|
12
|
|
Momentum Transfer from the DART Mission Kinetic Impact on Asteroid Dimorphos, file 2dad8b3a-a5ee-4edc-b446-8539b0a94ba0
|
11
|
|
Successful Kinetic Impact into an Asteroid for Planetary Defense, file c604a00c-a893-429c-abe8-96624f8bc989
|
11
|
|
Libration-induced Orbit Period Variations Following the DART Impact, file eddd7f1a-928b-4bea-8355-4f6f339ec104
|
11
|
|
NASA’s Double Asteroid Redirection Test (DART): Mutual Orbital Period Change Due to Reshaping in the Near-Earth Binary Asteroid System (65803) Didymos, file aeaf54f4-595f-42c8-9c8e-7046ae19cf20
|
9
|
|
A new method for identifying dynamical transitions in rubble-pile asteroid scenarios, file 3d7a32d9-1e69-4c03-a59b-ef2c572b0135
|
8
|
|
The ERC-Funded EXTREMA Project: Achieving Self-Driving Interplanetary CubeSats, file c312c551-cdab-4c68-b5bb-854520e6a397
|
8
|
|
Ejecta Evolution Following a Planned Impact into an Asteroid: The First Five Weeks, file 92f645f9-80cc-4ba1-9888-3fd962ac4045
|
7
|
|
Ejecta from the DART-produced active asteroid Dimorphos, file c93575d3-70dc-4b7a-9dce-bf5643b0a410
|
6
|
|
Characterization of the Ejecta from the NASA/DART Impact on Dimorphos: Observations and Monte Carlo Models, file 4c80dade-95c6-4dd3-8021-acf0c8700b99
|
5
|
|
Global Optimization of Relative Configurations Between Spacecraft Near Lagrangian Point Orbits, file e0c31c08-deff-4599-e053-1705fe0aef77
|
5
|
|
The effect of a rocky terrain for CubeSat landing on asteroid surfaces, file 1f422244-869a-4ea9-9b08-98d9409456a1
|
3
|
|
Guidance and Control design for CubeSat small body landing using discrete firings of sliding mode control, file b24a3a7e-0442-4bfb-82cd-988794af978a
|
3
|
|
Optimal Configurations for Nanosatellite Formation Flying in Binary Asteroid Environment, file e0c31c0b-4cb2-4599-e053-1705fe0aef77
|
3
|
|
Periodic motion around libration points in the Elliptic Restricted Three-Body Problem, file e0c31c0c-83fe-4599-e053-1705fe0aef77
|
3
|
|
Achievement of the Planetary Defense Investigations of the Double Asteroid Redirection Test (DART) Mission, file 7d1dc513-017b-43c3-b778-f38fcdc326e8
|
2
|
|
Free Tumbling Objects Attitude Control via Contactless Chaser Authority Exploiting a Formation Flying Architecture, file e0c31c08-544b-4599-e053-1705fe0aef77
|
2
|
|
Suitable configurations for triangular formation flying about collinear libration points under the circular and elliptic restricted three-body problems, file e0c31c0c-763d-4599-e053-1705fe0aef77
|
2
|
|
Direct N-body Simulations of Satellite Formation around Small Asteroids: Insights from DART’s Encounter with the Didymos System, file a3f1b5cf-8a31-4ab9-b9a0-d583734842fb
|
1
|
|
Initial Trajectory Assessment of a low-thrust option for the RAMSES Mission to (99942) Apophis, file d9d3bc99-fc4d-4b74-811a-ee21c0d8a38e
|
1
|
|
Formation Flying Dynamics in Circular Restricted Three-Body Problem and Applications to Binary Asteroid Systems, file e0c31c08-2d5b-4599-e053-1705fe0aef77
|
1
|
|
Design Drivers for Formation Flying Near Collinear Libration Points in the Circular and Elliptic Restricted Three-Body Problems, file e0c31c08-4fe4-4599-e053-1705fe0aef77
|
1
|
|
MASCOT-2 Landing Opportunities Using Three-Body Solutions for Asteroid Impact Mission, file e0c31c08-d5c4-4599-e053-1705fe0aef77
|
1
|
|
Coupled Dynamics Analysis Around Asteroids by Means of Accurate Shape and Perturbations Modeling, file e0c31c08-de6d-4599-e053-1705fe0aef77
|
1
|
|
Dynamical model of binary asteroid systems through patched three-body problems, file e0c31c09-9c1e-4599-e053-1705fe0aef77
|
1
|
|
Optimization of Triangular Formation Flying Configurations Under the Circular and Elliptic Three-Body Problem Dynamics Modelling, file e0c31c09-db0d-4599-e053-1705fe0aef77
|
1
|
|
The Asteroid Impact Mission: Consolidated Mission Analysis and Scientific Payload Operations at Binary Asteroid Didymos, file e0c31c09-e639-4599-e053-1705fe0aef77
|
1
|
|
ESA’s Asteroid Impact Mission: Mission Analysis and Payload Operations State of the Art, file e0c31c09-e79e-4599-e053-1705fe0aef77
|
1
|
|
Coupling High Fidelity Body Modeling with Non-Keplerian Dynamics to Design Aim-Mascot-2 Landing Trajectories on Didymos Binary Asteroid, file e0c31c09-e79f-4599-e053-1705fe0aef77
|
1
|
|
Small Celestial Bodies Model Refinement by Means of N-Body Gravitational Dynamics, file e0c31c0a-4ccb-4599-e053-1705fe0aef77
|
1
|
|
Trajectory Design About Binary Asteroids Through Coupled Three Body Problems, file e0c31c0a-c1fc-4599-e053-1705fe0aef77
|
1
|
|
Formation Flying and Relative Dynamics Under the Circular Restricted Three-Body Problem Formulation, file e0c31c0a-cc98-4599-e053-1705fe0aef77
|
1
|
|
Families of Bounded Orbits near Binary Asteroid 65803 Didymos, file e0c31c0c-cce6-4599-e053-1705fe0aef77
|
1
|
|
The role of fragment shapes in the simulations of asteroids as gravitational aggregates, file e0c31c0f-58c8-4599-e053-1705fe0aef77
|
1
|
|
Modeling and Simulation of Milani CubeSat Contact Motion on the Surface of the Secondary Asteroid of Didymos Binary System, file e0c31c12-aa83-4599-e053-1705fe0aef77
|
1
|
| Totale |
3.664 |