Key Topics in Orbit Propagation Applied to Space Situational Awareness

›9:30 (30min)

Registration and welcome coffee

9:30 - 10:00 (30min)

Registration and welcome coffee

Welcome in Toulouse

›10:00 (30min)

Opening Session
SOC/LOC

10:00 - 10:30 (30min)

Opening Session

SOC/LOC

›10:30 (1h)

Plenary

10:30 - 11:30 (1h)

Plenary

› From the decameter to the millimeter accuracy in orbital dynamics. How ? For what Purpose ? - Florent Deleflie, IMCCE 10:30-11:30 (1h)

›11:30 (45min)

Orbit propagation comparisons
Florent Deleflie and Denis Hautesserres

11:30 - 12:15 (45min)

Orbit propagation comparisons

Florent Deleflie and Denis Hautesserres

› Coupling the nongravitational forces and modified Newton dynamics for cometary orbits - Lucie Maquet, Institut de Mécanique Céleste et de Calcul des Ephémérides 11:30-11:55 (25min)

› Orbit comparison tools - Florent Deleflie, Denis Hautesserres, Juan Felix San Juan 11:55-12:15 (20min)

›12:15 (10min)

Posters
Florent Deleflie

12:15 - 12:25 (10min)

Posters

Florent Deleflie

› The generalization of the Kepler equation: analytical solution - Rosario López, Center for Biomedical Research of La Rioja and University of La Rioja 12:15-12:20 (05min)

› Relative estimate of accuracy in orbit determination from a short tracklet. - Alessandro Vananti, Astronomical Institute, University of Bern - Thomas Schildknecht, Astronomical Institute, University of Bern 12:20-12:25 (05min)

›12:25 (1h35)

Lunch

12:25 - 14:00 (1h35)

Lunch

›14:00 (1h40)

Analytical and semi-analytical propagation methods
Alain Vienne

14:00 - 15:40 (1h40)

Analytical and semi-analytical propagation methods

Alain Vienne

› Linkage of very short arcs of observations with the two-body integrals - Baù Giulio, University of Pisa - Department of Mathematics 14:00-14:25 (25min)

› Libration Points in One Special Case of the Generalized RCP3B - Alexander Rodnikov, Bauman Moscow State Technical University 14:25-14:50 (25min)

› STOP - The Short-Term Orbit Propagator - Edwin Wnuk, Adam Mickiewicz University, Astronomical Observatory 14:50-15:15 (25min)

› Analysis of different types of perturbations in HEO objects trajectory prediction - Dorota Krużyńska, Astronomical Observatory Institute, Adam Mickiewicz University 15:15-15:40 (25min)

›15:40 (35min)

Coffee Break

15:40 - 16:15 (35min)

Coffee Break

›16:00 ()

Group Photo

16:00 - 16:00 ()

Group Photo

›16:15 (1h45)

Analytical and semi-analytical propagation methods
Juan Felix San Juan

16:15 - 18:00 (1h45)

Analytical and semi-analytical propagation methods

Juan Felix San Juan

› Generalized Logarithmic Helices for Low-Thrust Trajectory Design - Jesús Peláez, Space Dynamics Group - UPM 16:15-16:40 (25min)

› Analytical Method for Space Debris propagation - Daniel Casanova, Instituto Universitario de Matemáticas y Aplicaciones - Universidad de Zaragoza, Centro Universitario de la Defensa - Zaragoza 16:40-17:05 (25min)

› Intermediary LEO propagation including higher order zonal harmonics - Martin Lara, Denis Hautesserres, CNES 17:05-17:30 (25min)

› Orbit prediction of multiple satellites by using THEONA - Alexei Golikov, Keldysh Institute of Applied Mathematics, Russian Academy of Sciences 17:30-17:55 (25min)

›17:50 (10min)

Orbit propagation comparisons
Denis Hautesserres

17:50 - 18:00 (10min)

Orbit propagation comparisons

Denis Hautesserres

›17:55 (05min)

Concluding remarks, and posters presentation

17:55 - 18:00 (05min)

Concluding remarks, and posters presentation