Abstract Book:

Presentations

Dates

9:00 – 9:50 | Registration |

9:15 – 10:00 | Opening |

10:15 – 11:00 | Plenary: Hodei Urrutxua Regularization and Error Propagation in Orbit Predictions |

11:00 – 11:20 | Coffee break |

11:20 – 11:40 | C. Bombardelli, G. Falco, D. Amato and A. RosengrenMeasuring space occupancy of LEO satellites |

11:40 – 12:00 | A. Petit and D. CasanovaComparison of several methods used to create a synthetic population of the space debris in the GEO region |

12:00 – 12:20 | A. Barea, H. Urrutxua and Luis Cadarso Optimal large-scale object selection and trajectory planning for active space debris removal missions |

12:20 – 12:40 | E.M. Klein and Y. Yang Laser/matter interaction modelling for space debris removal |

12:40 – 13:00 | R. Vilhena de Moraes, J.P.S. Carvalho, C.M. Gonçalves and A.F.B.A. Prado Orbital evolution of space debris around the Earth: solar sail, an alternative to remove space debris |

13:00 – 14:30 | Lunch break |

14:30 – 14:50 | R. Domínguez, N. Sánchez-Ortiz, P. Quiles and D. OlivieroDrivers for the cataloguing of space objects |

14:50 – 15:10 | A. Vananti and T. SchilknechtDistance between Keplerian orbits in the correlation of short arc radar tracks |

15:10 – 15:30 | A. Pastor, D. Escobar, M. Sanjurjo-Rivo and A. Águeda Initial orbit determination methods for track-to-track association |

15:30 – 15:50 | A. Díez, A. Pastor, S. López, A. Souto, P. García and D. Escobar Covariance determination from operational orbits and sensor data |

15:50 – 16:10 | Coffee break |

16:10 – 16:30 | J. SiminskiMixed-model orbit determination for closely-spaced objects |

16:30 – 16:50 | G. Baù, H. Ma, D. Bracali Cioci and G.F. GronchiAn IOD method for LEO objects observed by radar |

16:50 – 17:10 | L. Pirovano and R. ArmellinProbabilistic data association as intersection of orbit sets |

17:10 – 17:30 | M.A. Vázquez, J. López-Santiago, M. Sanjurjo-Rivo and J. Míguez A particle filtering method for the opportunistic update of a space debris catalogue |

17:30 – 18:00 | Software competition (D. Hautesserres / R. Armellin / J.F. San-Juan) |

09:00 – 09:45 | Plenary: Lamberto Dell’Elce Multi-Phase Averaging of Time-Optimal Low-Thrust Transfers (in collaboration with J.-B.Caillau and J.-B. Pomet) |

09:45 – 10:05 | H. Namazyfard, A.J. Rosengren, D. Amato, C. Bombardelli and L. Dell’ElceAccurate recovery of ephemerides from TLEs of resonant orbits |

10:05 – 10:25 | M. Nugnes and C. ColomboIntroduction to a Keplerian-orbital-element-based optimisation approach via differential dynamic programming |

10:25 – 10:45 | Coffee break |

10:45 – 11:05 | T. Nie and P. Gurﬁl On propagation of lunar frozen orbits |

11:05 – 11:25 | R. Armellin, D. Gondelach, A. Wittig and Y. He High order transfer map method: theory and applications |

11:25 – 11:45 | A. Wittig and H. UrrutxuaDifferential Algebra propagators for the orbital prediction of space debris |

11:45 – 12:05 | P. Bartram, H. Urrutxua and A. Wittig The performance of multistep collocation methods on problems in Astrodynamics |

12:05 – 12:25 | J. Hernando-Ayuso, C. Bombardelli and G. Baù Orbit uncertainty propagation in Dromo variables with a time element |

12:25 – 14:00 | Lunch break |

14:00 – 14:20 | D. McKnight, K. Molloy, S. Speaks and C. O’HaraMachine Learning exercise for MCMA conjunction prediction improvements |

14:20 – 14:40 | J.L. Gonzalo, C. Colombo and P. Di LiziaDrag- and SRP-induced effects in uncertainty evolution for close approaches |

14:40 – 15:00 | M. Romano, C. Colombo and J.M. Sánchez Line sampling procedure for extensive planetary protection analysis |

15:00 – 15:20 | N. Reiland, A.J. Rosengren and C. Bombardelli Assessing collision risk using brute-force numerical simulations |

15:20 – 15:40 | R. García-PelayoProbability of collision between a rectangular cuboid and small debris |

15:40 – 16:00 | Coffee break |

16:00 – 16:15 | E.M. AlessiThe ReDSHIFT software tool for passive debris mitigation. The ReDSHIFT Team |

16:15 – 16:30 | N. Sánchez-Ortiz, R. Domínguez, J. Nomen and S. PessinaSSA tools and techniques supporting satellite flight dynamics activities |

16:30 – 16:45 | A. Lozano, R. Sánchez and J.J. Negrete Application of SAPO, the GMV’s Semi-Analytical Orbit Propagator, in flight dynamics operational tools |

16:45 – 17:00 | A. MorselliSINTOP: a numerical orbit propagator for satellite operations |

17:00 – 17:15 | I. Pérez, R. López, E. Vergara, M. San-Martín, E. Segura and H. CarrilloHOPE: Hybrid Orbit Propagator Environment |

17:15 – 17:30 | F. Deleflie, L. Sagnières, A. Petit, D. Hautesserres and M. Capderou Atmospheric reentry predictions with SATlight/STELA from TLE time series. Application on the Tiangong-1 reentry |

17:30 – 17:45 | P.J. Cefola, J.F. San-Juan and R. López Validation of the DSST C/C++ version |

17:45 – 18:00 | A. Wittig, V. Vanick, R. Penn, J. Castle and J. TylerSpace AR: augmented and virtual reality devices for Astrodynamics visualization |

**21:00 Gala Dinner: **Restaurante Herventia. Location: Portales, 61

09:30 – 10:15 | Plenary: Guillermo Ortega Overview and Future of Design for Demise Activities at the European Space Agency |

10:15 – 10:35 | N. Miguel and C. ColomboAveraged attitude and orbit dynamics of a planar Earth-orbiting helio-stable solar sail |

10:35 – 10:55 | P. Izzo, L. Dell’Elce, P. Gurfil and A.J. RosengrenTransformation between mean and osculating elements in the presence of lunisolar perturbations |

10:55 – 11:15 | A.J. Rosengren and M. Lara Averaging the Legendre polynomials for third-body and zonal harmonics perturbations |

11:15 – 11:35 | M. Sansottera, A.-S. Libert, U. Locatelli and A. Giorgilli Long-term evolution of extrasolar systems via normal forms |

11:35 – 11:55 | Coffee break |

11:55 – 12:15 | E.M. Alessi, C. Colombo and A. RossiPhase space description of the dynamics due to the coupled effect of the planetary oblateness and the solar radiation pressure perturbations |

12:15 – 12:35 | D. Hautesserres1st-order secular resonances and L-K mechanism for lunar perturbations in SSTO orbits |

12:35 – 12:55 | J. Daquin, I. Gkolias and C. Efthymiopoulos Diving into the 2g + h resonance |

12:55 – 13:15 | M. Duroyon, J. Daquin and J. Pérez The integrated autocorrelation function as a dynamical chaos indicator |

13:15 – 13:35 | A. Zlenko, I. RyabikovaRepresentations of the force function of two rigid bodies in canonical variables |

13:35 – 13:55 | I. Gkolias, M. Lara and C. ColomboIntegrable approximations for the coupled interaction of the zonal and lunisolar perturbations for Earth satellites |

13:55 – 14:00 | Closing (F. Deleflie / R. Armellin) |

14:00 – 15:30 | Lunch break |