‹ Wednesday, June 12, 2024 › | |
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›8:30 (30min)
8:30 - 9:00 (30min)
Reception
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›9:00 (30min)
9:00 - 9:30 (30min)
Opening ceremony
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›9:40 (50min)
Plenary: Automated Saturn Moon Tour Design for Ocean Worlds Exploration
Joan-Pau Sánchez Cuartielles. Professeur ISAE-SUPAERO in Astrodynamics and Mission Design, École nationale supérieure de l'aéronautique et de l'espace Toulouse, France 9:40 - 10:30 (50min)
Plenary: Automated Saturn Moon Tour Design for Ocean Worlds Exploration
Joan-Pau Sánchez Cuartielles. Professeur ISAE-SUPAERO in Astrodynamics and Mission Design, École nationale supérieure de l'aéronautique et de l'espace Toulouse, France
›10:30 (30min)
10:30 - 11:00 (30min)
Coffee break
›11:00 (1h20)
11:00 - 12:20 (1h20)
Space debris and end-of-life disposal dynamics
Joan-Pau Sánchez Cuartielles
› Cis-lunar monitoring activities: astrodynamics challenges
- Jan Siminski, European Space Operations Center. Coauthor: Emiliano Cordelli
11:00-11:20 (20min)
› Secular dynamics of Earth and Moon satellites
- Edoardo Legnaro, Dipartimento di Matematica [Genova]
11:20-11:40 (20min)
› Methods for improved robustness in batch orbit estimation and propagation
- Lorenzo Porcelli, GMV. Coauthors: Alejandro Cano Sánchez, Pau Gago, Loris Carlo Quadri, Diego Escobar
11:40-12:00 (20min)
› Hybrid solutions to the association problem in the GEO region
- Juan Félix San-Juan, Scientific Computing & Technological Innovation (SCoTIC), University of La Rioja. R. López, C. Yanez, I. Pérez y M. Higueras
12:00-12:20 (20min)
›13:00 (1h30)
13:00 - 14:30 (1h30)
Lunch
›14:40 (1h)
14:40 - 15:40 (1h)
Constellations and formation flying
David Vallado
› Robust Metric for Spacecraft Collision Risk Assessment
- Yema Paul, Institut Supérieur de l'Aéronautique et de l'Espace - Joan-Pau Sanchez Cuartielles, Institut Supérieur de l'Aéronautique et de l'Espace
14:40-15:00 (20min)
› A Dynamical Model for an Efficient Multi-target Tracking of Orbital Constellations
- Manuel Sanjurjo-Rivo, Universidad Carlos III de Madrid. Coauthor: Sergio Cuevas del Valle, Emmanuel Delande
15:00-15:20 (20min)
› Employing Sequential Convex Programming to Solve a Class of Optimal Control Problems with a Minimum Control Input Magnitude Constraint: Formation Reconfiguration Using Low-Thrust as a Case Study
- Ahmed Mahfouz, Interdisciplinary Centre for Security, Reliability and Trust [Luxembourg]. Coauthors: Gabriella Gaias, Florio Dalla Vedova, Holger Voos
15:20-15:40 (20min)
›15:40 (20min)
15:40 - 16:00 (20min)
Coffee break
›16:00 (1h40)
16:00 - 17:40 (1h40)
Uncertainty propagation
Manuel Sanjurjo Rivo
› Cislunar initial orbit determination using measurement and sensor centric admissible regions
- Queenique Dinh, University of Colorado Boulder. Coauthors: Daniel Scheeres, Marcus Holzinger
16:00-16:20 (20min)
› Shape constraints for phase space structures in hamiltonian systems
- Oliver Boodram, University of Colorado Boulder. Coauthor: Daniel Scheeres
16:20-16:40 (20min)
› Covariance realism improvement with GRAVES radar measurements in orbit estimation and propagation
- Alejandro Cano Sánchez, Universidad Carlos III de Madrid [Madrid], GMV. Coauthors: Manuel Sanjurjo-Rivo, Joaquín Míguez, Diego Escobar, Valentin Baral, Emmanuel Delande
16:40-17:00 (20min)
› Uncertainty Propagation of Generalized Bernoulli Folded von Mises Distribution Defined on Local Orbital Elements in Three-Body Problems
- Ryne Beeson, Princeton University
17:00-17:20 (20min)
› Quadratic Model for Analytical Uncertainty Propagation
- Alicia Martínez Cacho, Universidad Politécnica de Madrid. Coauthor: Claudio Bombardelli
17:20-17:40 (20min)
›17:40 (20min)
17:40 - 18:00 (20min)
Asteroids and propagation in the Solar system
Manuel Sanjurjo Rivo
› Gradient based reachability analysis for goal-oriented guidance. Application to Eros proximity operations
- Antonio Rizza, Dipartimento di Scienze e Tecnologie Aerospaziali [Milano]. Coauthor: Francesco Topputo,
17:40-18:00 (20min)
›19:45 (15min)
19:45 - 20:00 (15min)
Meeting point
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›20:00 (3h30)
20:00 - 23:30 (3h30)
Gala Dinner
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Session | Speech | Logistics | Break | Tour |