kepassa2022 : Key Topics in Orbit Propagation Applied to Space Situational Awareness

Wed. 22

Thu. 23

Fri. 24

09:00

10:00

11:00

12:00

13:00

14:00

15:00

16:00

17:00

18:00

19:00

20:00

21:00

22:00

23:00

Reception

9:00 - 9:15 (15min)

Reception

Opening ceremony

9:15 - 10:00 (45min)

Opening ceremony

Long-term numerical propagation for earth orbiting satellites

10:15 - 10:50 (35min)

Long-term numerical propagation for earth orbiting satellites

D. A. Vallado

Coffee break

10:50 - 11:15 (25min)

Coffee break

Analytical, semi-analytical, and numerical propagation methods

11:15 - 13:00 (1h45)

Analytical, semi-analytical, and numerical propagation methods

› Bringing in break-up events within a space objects catalogue - A. Pastor, J. Siminski, G. Escribano, M. Sanjurjo-Rivo, D. Escobar 11:15-11:32 (17min)

› Efficient Numerical Solution of the Low-Thrust Lambert's problem - L. Dell'Elce, A.J. Rosengren 11:32-11:49 (17min)

› Flyby dynamical characterisation with Jacobian eigenvalues - A. Masat, C. Colombo, A. Boutonnet 11:49-12:06 (17min)

› 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 12:06-12:23 (17min)

› Single-averaged analytical model for low-thrust collision avoidance manoeuvres - J.L. Gonzalo, C. Colombo 12:23-12:40 (17min)

› Dynamics of a Close Earth Satellite by Picard Iterations - M. Lara 12:40-12:57 (17min)

Lunch time

13:00 - 14:20 (1h20)

Lunch time

Perturbation theory

14:30 - 16:15 (1h45)

Perturbation theory

› Statistical analysis of the long-term dynamical behavior of uncontrolled geostationary satellites near an unstable equilibrium point - [VIDEO] R. Flores, M. Pontani, E. Fantino 14:30-14:47 (17min)

› Improving long-term special perturbations efficiency for Low Earth Orbits - D. Amato, D.A. Vallado 14:47-15:04 (17min)

› 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 15:04-15:21 (17min)

› Semi-analytical computation of center-stable and center-unstable manifolds in the geostationary belt. - M. Barcelona, À. Haro, J-M. Mondelo 15:21-15:38 (17min)

› Validation of GTDS and DSST Standalone versions against precise orbit ephemerides - P. Cefola, J. Stratford, R. López, J.F. San-Juan 15:38-15:55 (17min)

› Remarks on The Super-integrability of Dynamical Systems - V. Martinusi 15:55-16:12 (17min)

Coffee break

16:15 - 16:30 (15min)

Coffee break

Resonances and chaos

16:30 - 18:30 (2h)

Resonances and chaos

› Iochroma asteroid family resonance perturbations - [VIDEO] A. Rosaev 16:30-16:47 (17min)

› A detailed dynamical model for inclination-only dependent lunisolar resonances. Effects on the ”eccentricity growth” mechanism. - E. Legnaro, C. Efthymiopoulos 16:47-17:04 (17min)

› An Arnold diffusion mechanism for the Galileo satellites - A. Pousse, M. Giralt, I. Baldomá, M. Guardia, E.M. Alessi 17:04-17:21 (17min)

› Fourier Expansion of the $J_2$ Potential as a Prelude to Resonant Orbit Control Theory - N. Nailhot, P. Gurfil 17:21-17:38 (17min)

› Lagrangian Descriptors for global dynamics - [VIDEO] J.Daquin, R. Pedenon-Orlanducci, M. Agaouglou, G. Garcıa-Sanchez, A.M.Mancho 17:38-17:55 (17min)

› Low energy interplanetary trajectories using multiple gravity assists - M. Werner, S. Ross 17:55-18:12 (17min)

› Lunar mean-motion and secular resonances - A.J. Rosengren, Di Wu, L. Dell'Elce 18:12-18:29 (17min)

Speech A natural perturbation treatment of the Molniya orbital behavior, based on the TLE data set

9:00 - 9:35 (35min)

Speech A natural perturbation treatment of the Molniya orbital behavior, based on the TLE data set

E. M. Alessi

Hybrid and statistical methods

9:35 - 10:30 (55min)

Hybrid and statistical methods

› Improving the force model of SGP4 using Neural Network - H. Carrillo, E. Segura, R. López, J.F. San-Juan 09:35-09:52 (17min)

› Apply the hybrid orbit propagator to the association problem in the GEO region - J.F. San-Juan, R. López, C. Yanez, M. Higueras 09:52-10:09 (17min)

› Manoeuvre detection based on S3TSR data - R. Vazquez, J.M. Montilla, J.C. Sanchez, J.Galan-Vioque, J. Rey, J. Siminski 10:09-10:26 (17min)

Coffee break

10:30 - 10:45 (15min)

Coffee break

Collision probability computation

10:45 - 12:30 (1h45)

Collision probability computation

› Analysing transport phenomena in orbital conjunctions - R. Molina, G. Escribano, M. Sanjurjo-Rivo 10:45-11:02 (17min)

› Astrodynamical methods for collision avoidance automation - J. Siminski, K. Merz, V. Schaus 11:02-11:19 (17min)

› 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 11:19-11:36 (17min)

› Covariance determination for uncertainty realism in collision probability estimates - A. Cano, A. Pastor, E. Arias, D. Sáez, J. Míguez, M.Sanjurjo-Rivo, D.Escobar 11:36-11:53 (17min)

› Deep learning for all-vs-all conjunction detection - E. Stevenson, V. Rodriguez-Fernandez, H. Urrutxua, D. Camacho 11:53-12:10 (17min)

› Fast Orbit Propagation for Conjunction Screening - A. Rivero, C. Bombardelli, R. Vázquez 12:10-12:27 (17min)

Lunch time

12:30 - 14:00 (1h30)

Lunch time

Uncertainty quantification and propagation

14:00 - 15:45 (1h45)

Uncertainty quantification and propagation

› A convex optimisation-based approach to detect and estimate manoeuvres - L. Pirovano, R. Armellin 14:17-14:34 (17min)

› Assessment of uncertainty propagation techniques to study the topology of the space resident population - M. Romano, T. Carletti, A. Lemaitre, J. Daquin 14:34-14:51 (17min)

› Cislunar Space Domain Awareness: Improved characterization and uncertainty quantification - P. Machuca, A.J. Rosengren 14:51-15:08 (17min)

› 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 15:08-15:25 (17min)

› Non-linear Set Propagation with Generalised Equinoctial Orbital Elements - M. Hallgarten La Casta, L. Sánchez Fernandez-Mellado, D. Amato, M. Vasile 15:25-15:42 (17min)

Coffee break

15:45 - 16:05 (20min)

Coffee break

Mission design

16:05 - 17:50 (1h45)

Mission design

› Disposal Options below the GEO protected region - [VIDEO] D.K. Skoulidou, S. Lemmens 16:05-16:22 (17min)

› Preliminary analysis of an active debris removal mission for large constellations: A Constraint Programming methodology - A. Barea, J.L. Gonzalo, C. Colombo, H. Urrutxua 16:22-16:39 (17min)

› 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 16:39-16:56 (17min)

› Shape-based low-thrust trajectory optimization enhanced via orthogonal functions, collocation and regularization - S. Cuevas del Valle, H. Urrutxua, P. Solano-López 16:56-17:13 (17min)

› Orbit Transfer using Theory of Functional Connections via change of variables - [VIDEO] A. Kardec de Almeida Junior, A.F.B.A. Prado, D. Mortari 17:13-17:30 (17min)

› On optimal trajectories of solar sails - [VIDEO] A. Herasimenka 17:30-17:47 (17min)

Cocktail and Gala Dinner at Delicatto Restaurant (Bus 20:30 h)

21:00 - 23:55 (2h55)

Cocktail and Gala Dinner at Delicatto Restaurant (Bus 20:30 h)

https://kepassa2022.sciencesconf.org/data/program/Social_activities_KePASSA_22.pdf

Perturbation modeling and integration

10:05 - 11:30 (1h25)

Perturbation modeling and integration

› Dynamical geometry associated with the collision manifold in the circular restricted three-body problem - J. Fitzgerald, S. Ross 10:05-10:22 (17min)

› Canonical Modeling of The Solar Radiation Pressure Perturbation - N. Vegh, V. Martinusi 10:22-10:39 (17min)

› CUDA implementation of the first derivative of the gravity potential - C. Rubio, J. Gonzalo, J. Siminski, A. Escapa 10:39-10:56 (17min)

› CUDAjectory: a GPU-based software for massive parallel orbit propagation - [VIDEO] A.F. Inno, C. Colombo, A. Masat, L. Bucci, F. Renk 10:56-11:13 (17min)

› Time integrator for second order in time problems - B. Bujanda, A. Duque 11:13-11:30 (17min)

Coffee break

11:30 - 11:50 (20min)

Coffee break

Relative dynamics
KePASSA Closing

11:50 - 13:15 (1h25)

Relative dynamics

› A Curvilinear Generalization of the Yamanaka-Ankersen State Transition Matrix - A. Martínez-Cacho, C. Bombardelli 11:50-12:07 (17min)

› 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 12:07-12:24 (17min)

› Formation design selection based on time and cost of reset - D. Menzio, A. Mahfouz, F. Dalla Vedova, H. Voos 12:24-12:41 (17min)

› A Closer Look at Two-Line Elements Data - A. Ciccarelli, C. Bombardelli 12:41-12:58 (17min)

13:00 - 13:15 (15min)

KePASSA Closing

Lunch time

13:15 - 14:45 (1h30)

Lunch time

Solar de Samaniego Winery + Laguardia Tour

18:00 - 23:00 (5h)

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

https://kepassa2022.sciencesconf.org/data/program/Social_activities_KePASSA22.pdf