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Planning
Wednesday, June 22, 2022
| Time | Event | (+) |
| 09:00 - 09:15 | Reception - Reception | |
| 09:15 - 10:00 | Opening ceremony - - | |
| 10:15 - 10:50 | Long-term numerical propagation for earth orbiting satellites - D. A. Vallado | |
| 10:50 - 11:15 | Coffee break | |
| 11:15 - 13:00 | Analytical, semi-analytical, and numerical propagation methods | (+) |
| 11:15 - 11:32 | › Bringing in break-up events within a space objects catalogue - A. Pastor, J. Siminski, G. Escribano, M. Sanjurjo-Rivo, D. Escobar | |
| 11:32 - 11:49 | › Efficient Numerical Solution of the Low-Thrust Lambert's problem - L. Dell'Elce, A.J. Rosengren | |
| 11:49 - 12:06 | › Flyby dynamical characterisation with Jacobian eigenvalues - A. Masat, C. Colombo, A. Boutonnet | |
| 12:06 - 12:23 | › Semi-analytical propagation of NEO binaries: the history of the Janus mission targets 1991 VH and 1996 FG3 - O. Fuentes-Muñoz, A. Meyer, D.J. Scheeres | |
| 12:23 - 12:40 | › Single-averaged analytical model for low-thrust collision avoidance manoeuvres - J.L. Gonzalo, C. Colombo | |
| 12:40 - 12:57 | › Dynamics of a Close Earth Satellite by Picard Iterations - M. Lara | |
| 13:00 - 14:20 | Lunch time | |
| 14:30 - 16:15 | Perturbation theory | (+) |
| 14:30 - 14:47 | › Statistical analysis of the long-term dynamical behavior of uncontrolled geostationary satellites near an unstable equilibrium point - [VIDEO] R. Flores, M. Pontani, E. Fantino | |
| 14:47 - 15:04 | › Improving long-term special perturbations efficiency for Low Earth Orbits - D. Amato, D.A. Vallado | |
| 15:04 - 15:21 | › Simultaneously Quasi-Critical and Quasi-Heliosynchronous Orbits - R.Vilhena de Moraes, M.L.Galhego da Costa, A.F.B.A.Prado, J.P.S. Carvalho | |
| 15:21 - 15:38 | › Semi-analytical computation of center-stable and center-unstable manifolds in the geostationary belt. - M. Barcelona, À. Haro, J-M. Mondelo | |
| 15:38 - 15:55 | › Validation of GTDS and DSST Standalone versions against precise orbit ephemerides - P. Cefola, J. Stratford, R. López, J.F. San-Juan | |
| 15:55 - 16:12 | › Remarks on The Super-integrability of Dynamical Systems - V. Martinusi | |
| 16:15 - 16:30 | Coffee break | |
| 16:30 - 18:30 | Resonances and chaos | (+) |
| 16:30 - 16:47 | › Iochroma asteroid family resonance perturbations - [VIDEO] A. Rosaev | |
| 16:47 - 17:04 | › A detailed dynamical model for inclination-only dependent lunisolar resonances. Effects on the ”eccentricity growth” mechanism. - E. Legnaro, C. Efthymiopoulos | |
| 17:04 - 17:21 | › An Arnold diffusion mechanism for the Galileo satellites - A. Pousse, M. Giralt, I. Baldomá, M. Guardia, E.M. Alessi | |
| 17:21 - 17:38 | › Fourier Expansion of the $J_2$ Potential as a Prelude to Resonant Orbit Control Theory - N. Nailhot, P. Gurfil | |
| 17:38 - 17:55 | › Lagrangian Descriptors for global dynamics - [VIDEO] J.Daquin, R. Pedenon-Orlanducci, M. Agaouglou, G. Garcıa-Sanchez, A.M.Mancho | |
| 17:55 - 18:12 | › Low energy interplanetary trajectories using multiple gravity assists - M. Werner, S. Ross | |
| 18:12 - 18:29 | › Lunar mean-motion and secular resonances - A.J. Rosengren, Di Wu, L. Dell'Elce |
Thursday, June 23, 2022
| Time | Event | (+) |
| 09:00 - 09:35 | Speech A natural perturbation treatment of the Molniya orbital behavior, based on the TLE data set - E. M. Alessi | |
| 09:35 - 10:30 | Hybrid and statistical methods | (+) |
| 09:35 - 09:52 | › Improving the force model of SGP4 using Neural Network - H. Carrillo, E. Segura, R. López, J.F. San-Juan | |
| 09:52 - 10:09 | › Apply the hybrid orbit propagator to the association problem in the GEO region - J.F. San-Juan, R. López, C. Yanez, M. Higueras | |
| 10:09 - 10:26 | › Manoeuvre detection based on S3TSR data - R. Vazquez, J.M. Montilla, J.C. Sanchez, J.Galan-Vioque, J. Rey, J. Siminski | |
| 10:30 - 10:45 | Coffee break | |
| 10:45 - 12:30 | Collision probability computation | (+) |
| 10:45 - 11:02 | › Analysing transport phenomena in orbital conjunctions - R. Molina, G. Escribano, M. Sanjurjo-Rivo | |
| 11:02 - 11:19 | › Astrodynamical methods for collision avoidance automation - J. Siminski, K. Merz, V. Schaus | |
| 11:19 - 11:36 | › Automation of the collision risk management from conjunction data message reception up to the decision-making - A. Petit, R. Lucken, S. Redel, F. Deleflie, V. Morand, F. Laporte | |
| 11:36 - 11:53 | › Covariance determination for uncertainty realism in collision probability estimates - A. Cano, A. Pastor, E. Arias, D. Sáez, J. Míguez, M.Sanjurjo-Rivo, D.Escobar | |
| 11:53 - 12:10 | › Deep learning for all-vs-all conjunction detection - E. Stevenson, V. Rodriguez-Fernandez, H. Urrutxua, D. Camacho | |
| 12:10 - 12:27 | › Fast Orbit Propagation for Conjunction Screening - A. Rivero, C. Bombardelli, R. Vázquez | |
| 12:30 - 14:00 | Lunch time | |
| 14:00 - 15:45 | Uncertainty quantification and propagation | (+) |
| 14:17 - 14:34 | › A convex optimisation-based approach to detect and estimate manoeuvres - L. Pirovano, R. Armellin | |
| 14:34 - 14:51 | › Assessment of uncertainty propagation techniques to study the topology of the space resident population - M. Romano, T. Carletti, A. Lemaitre, J. Daquin | |
| 14:51 - 15:08 | › Cislunar Space Domain Awareness: Improved characterization and uncertainty quantification - P. Machuca, A.J. Rosengren | |
| 15:08 - 15:25 | › Combining Taylor polynomials and multifidelity dynamics for the efficient propagation of uncertainties in orbital mechanics - A. Fossà, R. Armellin, E. Delande, M. Losacco, F. Sanfedino | |
| 15:25 - 15:42 | › Non-linear Set Propagation with Generalised Equinoctial Orbital Elements - M. Hallgarten La Casta, L. Sánchez Fernandez-Mellado, D. Amato, M. Vasile | |
| 15:45 - 16:05 | Coffee break | |
| 16:05 - 17:50 | Mission design | (+) |
| 16:05 - 16:22 | › Disposal Options below the GEO protected region - [VIDEO] D.K. Skoulidou, S. Lemmens | |
| 16:22 - 16:39 | › Preliminary analysis of an active debris removal mission for large constellations: A Constraint Programming methodology - A. Barea, J.L. Gonzalo, C. Colombo, H. Urrutxua | |
| 16:39 - 16:56 | › GPU-assisted search for low-cost transfers between whiskered tori, with applications to resonance transfers in a restricted 4-body model - B. Kumar, R. Anderson, R. de la Llave | |
| 16:56 - 17:13 | › Shape-based low-thrust trajectory optimization enhanced via orthogonal functions, collocation and regularization - S. Cuevas del Valle, H. Urrutxua, P. Solano-López | |
| 17:13 - 17:30 | › Orbit Transfer using Theory of Functional Connections via change of variables - [VIDEO] A. Kardec de Almeida Junior, A.F.B.A. Prado, D. Mortari | |
| 17:30 - 17:47 | › On optimal trajectories of solar sails - [VIDEO] A. Herasimenka | |
| 21:00 - 23:55 | Cocktail and Gala Dinner at Delicatto Restaurant (Bus 20:30 h) |
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Friday, June 24, 2022
| Time | Event | (+) |
| 10:05 - 11:30 | Perturbation modeling and integration | (+) |
| 10:05 - 10:22 | › Dynamical geometry associated with the collision manifold in the circular restricted three-body problem - J. Fitzgerald, S. Ross | |
| 10:22 - 10:39 | › Canonical Modeling of The Solar Radiation Pressure Perturbation - N. Vegh, V. Martinusi | |
| 10:39 - 10:56 | › CUDA implementation of the first derivative of the gravity potential - C. Rubio, J. Gonzalo, J. Siminski, A. Escapa | |
| 10:56 - 11:13 | › CUDAjectory: a GPU-based software for massive parallel orbit propagation - [VIDEO] A.F. Inno, C. Colombo, A. Masat, L. Bucci, F. Renk | |
| 11:13 - 11:30 | › Time integrator for second order in time problems - B. Bujanda, A. Duque | |
| 11:30 - 11:50 | Coffee break | |
| 11:50 - 13:15 | Relative dynamics | (+) |
| 11:50 - 12:07 | › A Curvilinear Generalization of the Yamanaka-Ankersen State Transition Matrix - A. Martínez-Cacho, C. Bombardelli | |
| 12:07 - 12:24 | › Influence of Apophis' spin axis variations on a spacecraft during the 2029 close approach with Earth - S. Aljbaae, A.F.B.A. Prado, J. Souchay, V. Carruba | |
| 12:24 - 12:41 | › Formation design selection based on time and cost of reset - D. Menzio, A. Mahfouz, F. Dalla Vedova, H. Voos | |
| 12:41 - 12:58 | › A Closer Look at Two-Line Elements Data - A. Ciccarelli, C. Bombardelli | |
| 13:00 - 13:15 | KePASSA Closing | |
| 13:15 - 14:45 | Lunch time | |
| 18:00 - 23:00 |
Solar de Samaniego Winery + Laguardia Tour - Cost: 70 € including Bus + activities. The organization of these activities (bus, winnery, tour guide, tapas...) depends on the number of people interested. Write an email to rosario.lopez@unirioja.es no later than June, 9. Bus at 17:15 h AC hotel, 17:30 h at Fuente de Murrieta 18:00 - 1 hour-visit (museum and winery). Ends with a taste of 2 wines and tapas. 19:30 - 1 hour-visit (Laguardia and calado -old underground winery-). Ends with a taste o wine. Tapas in Laguardia in its festivity of St. Juan Return: at 23:00/23:30 h |
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