| Nome |
# |
|
Trajectory Design in High-Fidelity Models, file e0c31c0c-a554-4599-e053-1705fe0aef77
|
490
|
|
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
|
|
LUMIO: A CubeSat to Monitor Micro-Meteroid Impacts on the Lunar Farside, file e0c31c12-3f91-4599-e053-1705fe0aef77
|
250
|
|
Design of the On-Board Image Processing of the Milani Mission, file e0c31c12-507b-4599-e053-1705fe0aef77
|
250
|
|
The EXTREMA Orbital Simulation Hub: a Facility for GNC Testing of Autonomous Interplanetary CubeSat, file e0c31c12-bd7e-4599-e053-1705fe0aef77
|
246
|
|
The Milani mission: overview and architecture of the optical-based GNC system, file e0c31c12-194d-4599-e053-1705fe0aef77
|
226
|
|
Target Selection for M-ARGO Interplanetary CubeSat, file e0c31c0f-d189-4599-e053-1705fe0aef77
|
177
|
|
Phase a Design of the LUMIO Spacecraft: a Cubesat for Observing and Characterizing Micro-Meteoroid Impacts on the Lunar far Side, file e0c31c0f-d18a-4599-e053-1705fe0aef77
|
164
|
|
SPESI: a Real-Time Space Environment Simulator for the EXTREMA Project, file b7df83a7-92d6-4bde-be95-454ccec108e5
|
153
|
|
Current Status of LUMIO: a Lunar CubeSat Mission at Earth-Moon L2, file e0c31c12-aafb-4599-e053-1705fe0aef77
|
152
|
|
Goal-Oriented Guidance Strategy for Binary Asteroid Exploration: Investigation of Different Metrics, file e8beafe7-44c5-4f43-9d7d-e0178b5a4959
|
127
|
|
LUMIO: A CubeSat for observing and characterizing micro-meteoroid impacts on the Lunar far side, file e0c31c12-63f2-4599-e053-1705fe0aef77
|
125
|
|
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
|
|
Convex Trajectory Optimization Using Thrust Regularization, file 0d3e087a-a626-457f-9497-7a8c8b7495ae
|
110
|
|
Design of the Vision-Based GNC Subsystem of Hera’s Milani Mission, file 807a949b-e883-4c82-a855-1d280e47f6d3
|
109
|
|
Design Challenges and Opportunities Offered by the LUMIO Spacecraft: a CubeSat for Observing and Characterizing Micro-Meteoroid Impacts on the Lunar Far Side, file e0c31c12-11aa-4599-e053-1705fe0aef77
|
105
|
|
Predicting the Outcome of the LUMIO Lunar Cubesat, file e0c31c0f-c9c6-4599-e053-1705fe0aef77
|
95
|
|
LUMIO Cubesat: a Mission to Refine Meteoroid Population Knowledge, file e0c31c11-367e-4599-e053-1705fe0aef77
|
95
|
|
Combined Convex and Direct Shooting Optimization for Low-Thrust Trajectory Generation with Analytical Thrust Profile, file 319b2806-5e95-44b5-9bb7-965577662448
|
91
|
|
Closed-Loop Guidance for Interplanetary CubeSats with Indirect Methods, file 32a3ac21-0d26-4c94-855e-cc01de27acd9
|
89
|
|
Analysis and Optimization of Robust Trajectories in Cislunar Environment with Application to the LUMIO Cubesat, file 2d48d3e3-4d83-436a-9529-12aebfb505d2
|
88
|
|
Trajectory Options for Hera’s Milani CubeSat Around (65803) Didymos, file e0c31c12-0540-4599-e053-1705fe0aef77
|
87
|
|
Current Status of LUMIO Mission: Characterizing Lunar Meteoroid Impacts with a CubeSat, file e0c31c11-ce35-4599-e053-1705fe0aef77
|
81
|
|
The Envelope of Reachable Asteroids of M-ARGO Interplanetary CubeSat, file e0c31c12-ce69-4599-e053-1705fe0aef77
|
76
|
|
Aeroballistic Capture at Mars: Modeling, Optimization, and Assessment, file e0c31c12-4fed-4599-e053-1705fe0aef77
|
73
|
|
Target-Based Guidance Method for Trajectories with Multiple Flybys, file 4af36dbe-9001-4e62-b1e6-f4cbff3b31c3
|
65
|
|
A Hybrid Stochastic-Deterministic Integrator for Spacecraft Dynamics with Uncertainty, file 437bb479-000b-450b-8ec4-609d1c7fc079
|
59
|
|
LUMIO CubeSat: Toward a Lunar Situational Awareness, file e0c31c0e-5414-4599-e053-1705fe0aef77
|
48
|
|
The Image Processing of Milani: Challenges After DART Impact, file 6fb2edca-61e5-4cb0-a367-1d52ca90a22c
|
47
|
|
Design of Operational Compliant Trajectories Through a Homotopic Direct Collocation Algorithm, file 33c615d1-fab0-4adf-a31e-671730a002d2
|
38
|
|
Preliminary mission profile of Hera’s Milani CubeSat, file e0c31c10-3422-4599-e053-1705fe0aef77
|
32
|
|
Applied Trajectory Design for CubeSat Close-Proximity Operations around Asteroids: The Milani Case, file 250b15d5-5f93-471d-9aa7-a2ce159fc4bc
|
22
|
|
A Homotopic Direct Collocation Approach for Operational-Compliant Trajectory Design, file 4b5e5a9d-e093-427d-9cc9-3a1b5e17154c
|
18
|
|
The Orbital Regime Index: a Comprehensive Parameter to Determine Orbital Regions Around Minor Bodies, file dbeb2be4-94b4-460a-bac2-713aa9c90697
|
14
|
|
An Indirect Formulation of Operational Compliant Low-Thrust Trajectories, file a7647505-7489-4e9a-abc2-0c91f9ef4d85
|
9
|
|
LUMIO CubeSat: toward a Lunar Situational Awareness, file e0c31c0e-57de-4599-e053-1705fe0aef77
|
9
|
|
The ERC-Funded EXTREMA Project: Achieving Self-Driving Interplanetary CubeSats, file c312c551-cdab-4c68-b5bb-854520e6a397
|
8
|
|
Characterization of the Ejecta from the NASA/DART Impact on Dimorphos: Observations and Monte Carlo Models, file 4c80dade-95c6-4dd3-8021-acf0c8700b99
|
5
|
|
Analysis, Design, and Optimization of Robust Trajectories in Cislunar Environment for Limited-Capability Spacecraft, file bba645c0-cc58-4fb7-bde0-cc1e6d318bca
|
5
|
|
Modeling and Optimization of Aero-Ballistic Capture, file e0c31c0c-bd44-4599-e053-1705fe0aef77
|
5
|
|
Envelop of reachable asteroids by M-ARGO CubeSat, file e0c31c10-dcb8-4599-e053-1705fe0aef77
|
4
|
|
Achievement of the Planetary Defense Investigations of the Double Asteroid Redirection Test (DART) Mission, file 7d1dc513-017b-43c3-b778-f38fcdc326e8
|
2
|
|
Characterization of Gauss–Markov stochastic sequences for mission analysis, file aead1f8f-b38b-492d-8379-49a981bfdb86
|
2
|
|
Synthesis of Ballistic Capture Corridors at Mars via Polynomial Chaos Expansion, file af57d3a9-8cd6-4a32-9e71-7c2f7cdbb180
|
2
|
|
Dedicated Mission to the Sun-Earth Saddle Point: a Feasibility Assessment, file e0c31c0c-f762-4599-e053-1705fe0aef77
|
2
|
|
Envelop of reachable asteroids by M-ARGO CubeSat, file e0c31c11-1b21-4599-e053-1705fe0aef77
|
2
|
|
Convex Trajectory Optimization Using Thrust Regularization, file 1813b118-62a5-4f7f-b99c-ede566a30cec
|
1
|
|
An Indirect Formulation of Operational Compliant Low-Thrust Trajectories, file 34414449-c187-46c9-b978-9b6bc3608ff0
|
1
|
|
Target-Based Guidance Method for Trajectories with Multiple Flybys, file 72b884bc-2235-449a-8ea9-4f33a20a531c
|
1
|
|
Initial Trajectory Assessment of a low-thrust option for the RAMSES Mission to (99942) Apophis, file d9d3bc99-fc4d-4b74-811a-ee21c0d8a38e
|
1
|
|
Meteoroids detection with the LUMIO lunar CubeSat, file df3fc9fd-2e7a-43c7-805d-2590fc73e08c
|
1
|
|
The Milani mission: overview and architecture of the optical-based GNC system, file e0c31c11-d46e-4599-e053-1705fe0aef77
|
1
|
| Totale |
4.821 |