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28-30 Oct 2015 Toulouse (France)
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Planning
Wednesday, October 28, 2015
| Time | Event | |
| 09:30 - 10:00 | Registration and welcome coffee - Welcome in Toulouse | |
| 10:00 - 10:30 | Opening Session - SOC/LOC | |
| 10:30 - 11:30 | Plenary | |
| 10:30 - 11:30 | › From the decameter to the millimeter accuracy in orbital dynamics. How ? For what Purpose ? - Florent Deleflie, IMCCE | |
| 11:30 - 12:15 | Orbit propagation comparisons - Florent Deleflie and Denis Hautesserres | |
| 11:30 - 11:55 | › Coupling the nongravitational forces and modified Newton dynamics for cometary orbits - Lucie Maquet, Institut de Mécanique Céleste et de Calcul des Ephémérides | |
| 11:55 - 12:15 | › Orbit comparison tools - Florent Deleflie, Denis Hautesserres, Juan Felix San Juan | |
| 12:15 - 12:25 | Posters - Florent Deleflie | |
| 12:15 - 12:20 | › The generalization of the Kepler equation: analytical solution - Rosario López, Center for Biomedical Research of La Rioja and University of La Rioja | |
| 12:20 - 12:25 | › 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 | |
| 12:25 - 14:00 | Lunch | |
| 14:00 - 15:40 | Analytical and semi-analytical propagation methods - Alain Vienne | |
| 14:00 - 14:25 | › Linkage of very short arcs of observations with the two-body integrals - Baù Giulio, University of Pisa - Department of Mathematics | |
| 14:25 - 14:50 | › Libration Points in One Special Case of the Generalized RCP3B - Alexander Rodnikov, Bauman Moscow State Technical University | |
| 14:50 - 15:15 | › STOP - The Short-Term Orbit Propagator - Edwin Wnuk, Adam Mickiewicz University, Astronomical Observatory | |
| 15:15 - 15:40 | › Analysis of different types of perturbations in HEO objects trajectory prediction - Dorota Krużyńska, Astronomical Observatory Institute, Adam Mickiewicz University | |
| 15:40 - 16:15 | Coffee Break | |
| 16:00 - 16:00 | Group Photo | |
| 16:15 - 18:00 | Analytical and semi-analytical propagation methods - Juan Felix San Juan | |
| 16:15 - 16:40 | › Generalized Logarithmic Helices for Low-Thrust Trajectory Design - Jesús Peláez, Space Dynamics Group - UPM | |
| 16:40 - 17:05 | › Analytical Method for Space Debris propagation - Daniel Casanova, Instituto Universitario de Matemáticas y Aplicaciones - Universidad de Zaragoza, Centro Universitario de la Defensa - Zaragoza | |
| 17:05 - 17:30 | › Intermediary LEO propagation including higher order zonal harmonics - Martin Lara, Denis Hautesserres, CNES | |
| 17:30 - 17:55 | › Orbit prediction of multiple satellites by using THEONA - Alexei Golikov, Keldysh Institute of Applied Mathematics, Russian Academy of Sciences | |
| 17:50 - 18:00 | Orbit propagation comparisons - Denis Hautesserres | |
| 17:55 - 18:00 | Concluding remarks, and posters presentation |
Thursday, October 29, 2015
| Time | Event | |
| 09:00 - 10:00 | Plenary | |
| 09:00 - 10:00 | › Uncertainty Quantification in Orbital Mechanics - Vasile Massimiliano, University of Strathclyde | |
| 10:00 - 10:05 | Discussions | |
| 10:05 - 10:30 | Propagation of uncertainties - Massimiliano Vasile | |
| 10:05 - 10:30 | › Using Taylor differential Algebra in Mission Analysis: Benefits and Drawbacks - Vincent Morand, CNES - Jean-Claude Berges, CNES | |
| 10:30 - 11:00 | Coffee break | |
| 11:00 - 12:15 | Propagation of uncertainties - Edwin Wnuk | |
| 11:00 - 11:25 | › A Hybrid Method for Uncertainty Propagation of Orbital Motion | |
| 11:25 - 11:50 | › Uncertainty Propagation in orbital mechanics based on Tchebycheff polynomial expansions - Chiara Tardioli, Department of Mechanical & Aerospace Engineering, University of Strathclyde | |
| 11:50 - 12:15 | › Uncertainty propagation in asteroid deflection demonstration missions: NEOTωIST - Daniel HESTROFFER, IMCCE/Paris observatory | |
| 12:15 - 14:00 | Lunch | |
| 14:00 - 16:30 | Earth's space environment - Martin Lara | |
| 14:00 - 14:25 | › Accurate uncontrolled atmospheric reentry using Taylor algebra - Emmanuel Bignon, Thales Services | |
| 14:25 - 14:50 | › 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 | |
| 14:50 - 15:15 | › Density approach to debris propagation - Francesca Letizia, University of Southampton | |
| 15:15 - 15:40 | › Astrometric observations of satellites and space debris using Poznań Spectroscopic Telescope 2 in Arizona - Mikołaj Krużyński, Astronomical Observatory, Adam Mickiewicz University | |
| 15:40 - 16:05 | › 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 | |
| 16:05 - 16:30 | › 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 | |
| 16:30 - 17:00 | Coffee break | |
| 17:00 - 17:50 | Equations of motion and stability | |
| 17:00 - 17:25 | › Stochastic Modeling in Astronomy - Frédéric Pierret, Institut de Mécanique Céleste et de Calcul des Ephémérides | |
| 17:25 - 17:50 | › Vectorial Elements for Orbit Propagation and the Computation of Dynamical Stability Maps - Ioannis Gkolias, University of Rome "Tor Vergata" | |
| 20:00 - 23:30 | Banquet |
Friday, October 30, 2015
| Time | Event | |
| 09:00 - 10:00 | Plenary | |
| 09:00 - 10:00 | › 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 | |
| 10:00 - 10:05 | Discussions | |
| 10:05 - 10:30 | New generation of propagation methods - Martin Lara | |
| 10:05 - 10:30 | › KS variables in rotating reference fram. Application to satellite dynamics. - Krzysztof Langner, Astronomical Observatory of Adam Mickiewicz University (POLAND) | |
| 10:30 - 11:00 | Coffee break | |
| 11:00 - 12:15 | New generation of propagation methods - Roberto Armellin | |
| 11:00 - 11:25 | › Building Hybrid Orbit Propagators using Interpolation Techniques - Iván Pérez, Scientific Computing Group (GRUCACI), University of La Rioja | |
| 11:25 - 11:50 | › Hybrid SGP4 orbit propagator. First approach - Juan Félix San-Juan, University of La Rioja | |
| 11:50 - 12:15 | › The High Order Transfer Map Method for Perturbed Keplerian Motion - Alexander Wittig, ESA Advanced Concepts Team | |
| 12:15 - 14:00 | Lunch | |
| 14:00 - 14:50 | New generation of propagation methods - Roberto Armellin | |
| 14:00 - 14:25 | › Domain splitting in Jet Transport flow propagation - Daniel Pérez-Palau - Universitat de Barcelona | |
| 14:25 - 14:50 | › Numerical criteria for the definition of dynamical regimes in interplanetary orbit propagation - Davide Amato, Space Dynamics Group - UPM | |
| 14:50 - 15:30 | Coffee break | |
| 15:00 - 15:00 | Group photo | |
| 15:30 - 16:45 | Software packages for orbit propagation - Denis Hautesserres | |
| 15:30 - 15:55 | › An efficient code to solve the Kepler equation - Virginia Raposo-Pulido, Space Dynamics Group - UPM | |
| 15:55 - 16:20 | › Repeating ground-track orbit corrections and their applications in satellite constellations. - David Arnas, Centro Universitario de la Defensa - Zaragoza | |
| 16:20 - 16:45 | › The Differential Algebra Space Toolbox - roberto armellin, Universidad de La Rioja | |
| 16:45 - 17:00 | Concluding remarks - Denis Hautesserres and SOC/LOC |
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