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)
 

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