› 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)
› 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)
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)
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)
› A Hybrid Method for Uncertainty Propagation of Orbital Motion -
11:00-11:25 (25min)
› Uncertainty Propagation in orbital mechanics based on Tchebycheff polynomial expansions - Chiara Tardioli, Department of Mechanical & Aerospace Engineering, University of Strathclyde
11:25-11:50 (25min)
› Uncertainty propagation in asteroid deflection demonstration missions: NEOTωIST - Daniel HESTROFFER, IMCCE/Paris observatory
11:50-12:15 (25min)
› Accurate uncontrolled atmospheric reentry using Taylor algebra - Emmanuel Bignon, Thales Services
14:00-14:25 (25min)
› Implementation of the atmospheric drag in numerical propagators to study the space debris population in the LEO region - Alexis Petit, FRIA PhD Student, Department of Mathematics, University of Namur
14:25-14:50 (25min)
› Density approach to debris propagation - Francesca Letizia, University of Southampton
14:50-15:15 (25min)
› Astrometric observations of satellites and space debris using Poznań Spectroscopic Telescope 2 in Arizona - Mikołaj Krużyński, Astronomical Observatory, Adam Mickiewicz University
15:15-15:40 (25min)
› A study of the time complexity of an Elitist Genetic Algorithm used for associating optical observations of MEO and GEO Space Debris - Michiel Zittersteijn, Astronomical Institute of the University of Bern
15:40-16:05 (25min)
› Using the evaluation of maneuvers in the propagation of the active space objects movement in order to mitigate the risk of collisions - Andrey Baranov, Keldysh Institute of Applied Mathematics, Russian Academy of Sciences
16:05-16:30 (25min)
› Stochastic Modeling in Astronomy - Frédéric Pierret, Institut de Mécanique Céleste et de Calcul des Ephémérides
17:00-17:25 (25min)
› Vectorial Elements for Orbit Propagation and the Computation of Dynamical Stability Maps - Ioannis Gkolias, University of Rome "Tor Vergata"
17:25-17:50 (25min)
› Earth satellite's dynamics from the Delta(v) point of view - Martin Lara, Space Dynamics Group, Polytechnic University of Madrid - UPM, Grupo de Cálculo Científico, Universidad de La Rioja
09:00-10:00 (1h)
› KS variables in rotating reference fram. Application to satellite dynamics. - Krzysztof Langner, Astronomical Observatory of Adam Mickiewicz University (POLAND)
10:05-10:30 (25min)
› Building Hybrid Orbit Propagators using Interpolation Techniques - Iván Pérez, Scientific Computing Group (GRUCACI), University of La Rioja
11:00-11:25 (25min)
› Hybrid SGP4 orbit propagator. First approach - Juan Félix San-Juan, University of La Rioja
11:25-11:50 (25min)
› The High Order Transfer Map Method for Perturbed Keplerian Motion - Alexander Wittig, ESA Advanced Concepts Team
11:50-12:15 (25min)
› Domain splitting in Jet Transport flow propagation -
14:00-14:25 (25min)
› Numerical criteria for the definition of dynamical regimes in interplanetary orbit propagation - Davide Amato, Space Dynamics Group - UPM
14:25-14:50 (25min)
› An efficient code to solve the Kepler equation - Virginia Raposo-Pulido, Space Dynamics Group - UPM
15:30-15:55 (25min)
› Repeating ground-track orbit corrections and their applications in satellite constellations. - David Arnas, Centro Universitario de la Defensa - Zaragoza
15:55-16:20 (25min)
› The Differential Algebra Space Toolbox - roberto armellin, Universidad de La Rioja
16:20-16:45 (25min)
