| Monday - February 28, 2011 | |
| 08:30-10:10 | Registration |
| 10:10-11:30 | Openning |
| Session 01 | Orbit Dynamics 1 (ODY1) |
| Chairmen: | Jean-Paul Berthias (CNES); Hélio Koiti Kuga (INPE) |
| 10:30-10:50 | Final Commissioning of the PRISMA GPS Navigation System |
|
Jeab-Sébastien Ardaens, DLR/GSOC, Germany |
|
| 10:50-11:10 | Analysis of Geostationary Transfer Orbit Long-Term Evolution and Lifetime |
|
Alain Lamy, CNES, France |
|
| 11:10-11:30 | Autonomous Orbit Control Procedure, Using a Simplified GPS Navigator and a New Longitude Phase Drift Prediction Method, Applied to the CBERS Satellite |
|
Roberto Luiz Galski, INPE, Brazil |
|
| 11:30-11:50 | Dynamic Stabilization of L2 Periodic Orbits Using Attitude-Orbit Coupling Effects |
|
Martin Lara, Real Observatorio de la Armada, Spain |
|
| 11:50-12:10 | Out of plane Autonomous Orbit Control |
|
Éric Julien, CNES, France |
|
| 12:10-13:30 | Lunch |
| Session 02 - | Formation Flying (FF) |
| Chairmen: | Ralph Kahle (DLR/GSOC); A. F. Bertachini de A. Prado (INPE) |
| 13:30-13:50 | Monte Carlo Simulations of the Formation Flying Dynamics for the Magnetospheric Multiscale (MMS) Mission |
|
Conrad Schiff, NASA GSFC, USA |
|
| 13:50-14:10 | Feasibility of Meteosat Third Generation Collocation Using a Single S-Band Tracking Station and Large Inclination Maneuvers |
|
Pierluigi Righetti, EUMETSAT, Germany |
|
| 14:10-14:30 | Comparative Analysis Of Cartesian and Curvilinear Clohessy-Wiltshire Equations |
| Frederik J. de Bruijn, Delft University of Technology, Netherlands |
|
| 14:30-14:50 | Proximity Operations Of On-Orbit Servicing Spacecraft Using An Eccentricity/Inclination Vector Separation |
| J. Spurmann, DLR/GSOC, Germany |
|
| 14:50-15:10 | Relative Guidance of Formation Flying Mission Spacecraft: From Design to Flight Tests in FFIORD Mission |
| Sophie Djalal, CNES, France |
|
| 15:10-15:30 | Coffee-Break |
| Session 03 | Interplanetary Mission Design 1 (IMD1) |
| Chairmen: | Tomas Martin-Mur (NASA/JPL); Roberto Luiz Galski (INPE) |
| 15:30-15:50 | Trajectory Options for Solar Polar Region Observation Mission |
| Yasuhiro Kawakatsu, JAXA, Japan |
|
| 15:50-16:10 | Sun Influence on Two-Impulsive Earth-to-Moon Transfers |
| Sandro da Silva Fernandes, ITA, Brazil |
|
| 16:10-16:30 | Trajectory Design For BepiColombo Based On Navigation Requirements |
| Rüdiger Jehn, ESA/ESOC, Germany |
|
| 16:30-16:50 | ASTER Mission : Stability Regions around the Triple Asteroid 2001 SN263 |
| O.C. Winter, UNESP, Brazil |
|
| 16:50-17:10 | Jupiter Magnetospheric Orbiter Trajectory Design: Reaching High Inclination in the Jovian System |
| Stefano Campagnola, JAXA, Japan |
|
| 17:10-17:30 | A study of the guidance method for the Small Solar Power Sail Demonstrator, IKAROS |
| Masaki Nakamiya, JAXA, Japan |
|
| 20:00 | Coktail |
| Tuesday - March 1, 2011 |
| Session 04 | Flight Dynamics Operations 1 (FDOP1) |
| Chairmen: | Yasuhiro Kawakatsu (JAXA); Vivian Gomes (INPE) |
| 08:30-08:50 | TERRASAR-X / TANDEM-X Formation Control - First Results from Commissioning and Routine Operations |
| Ralph Kahle, DLR, German |
|
| 08:50-09:10 | GOCE Flight Dynamics Operations from an Orbital Perspective |
| Dirk Kuijper, Logica at ESA/ESOC, Germany |
|
| 09:10-09:30 | Operational Verification of the Flight Dynamics System for COMS Satellite |
| Byoung-Sun Lee, ETRI and KARI, South Korea |
|
| 09:30-09:50 | Theos Orbit Maintenance: Assessment of 2 Years of Operations |
| Pornthep Navakitkanok, GISTDA, Thailand |
|
| 09:50-10:10 | Coffee-Break |
| Session 05 | Orbit Dynamics 2 (ODY2) |
| Chairmen: | Mark Beckman (NASA/GSFC); Valdemir Carrara (INPE) |
| 10:10-10:50 | Relative Navigation for the TanDEM-X mission and evaluation with DEM calibration results |
| Martin Wermuth, DLR/GSOC, Germany |
|
| 10:30-10:50 | Asymptotic Solution for the Orbit Motion Under Constant Tangential Acceleration |
| Claudio Bombardelli, TUM , Spain |
|
| 10:50-11:10 | Artificial Satellites Dynamics: Resonant Effects |
| Jarbas Cordeiro Sampaio, UNESP, Brazil |
|
| 11:10-12:10 | Free Time |
| 12:10-13:30 | Lunch |
| 13:30 ... | Free Time |
| Wednesday - March 2, 2011 |
| Session 06 | Interplanetary Navigation (IN) |
| Chairmen: | Jürgen Fertig (ESA/ESOC); Ulisses Thadeu Vieira Guedes (INPE) |
| 08:30-08:50 | Navigation Strategies for Primitive Solar System Body Rendezvous and Proximity Operations |
| Kenneth Getzandanner, NASA GSFC, USA |
|
| 08:50-09:10 | Solar Sail Force Modeling for Spinning Solar Sail Using the Radiometric Tracking Data |
| Tomohiro Yamaguchi, The Grad. Univ. for Adv.Studies, Japan |
|
| 09:10-09:30 | Mars Science Laboratory Interplanetary Navigaton Analysis |
| T. J. Martin-Mur, JPL/CIT, USA |
|
| 09:30-09:50 | Effects of the Initial Conditions in a Swing-By of a Cloud of Particles |
| V. M. Gomes, INPE, Brazil |
|
| 09:50-10:10 | Coffee-Break |
| Session 07 | Attitude Dynamics 1 (AD1) |
| Chairmen: | Hélio Koiti Kuga (INPE); Othon Cabo Winter (UNESP) |
| 10:10-10:30 | Spin Stabilized Satellite's Attitude Propagation with Quaternions |
| Maria C.Zanardi, UNESP, Brazil |
|
| 10:30-10:50 | Bringing Realistic Attitude Sequence Modeling to Non-Experts |
| Véronique Pommier-Maurussane, CS Comm. & Systèmes, France |
|
| 10:50-11:10 | Attitude Simulation Software to Support Brazilian Space Missions |
| Valdemir Carrara, INPE, Brazil |
|
| 11:10-11:30 | In-Flight Characterisation of CRYOSAT-2 Reaction Control System |
| Stefano Pessina, Terma GmbH c/o ESA/ESOC, Germany |
|
| 11:30-11:50 | Spin Stabilized Satellite's Attitude Analytical Prediction |
| Maria C.Zanardi, UNESP, Brazil |
|
| 11:50-12:10 | Free Time |
| 12:10-13:30 | Lunch |
| Session 08 | Colision Risk and Space Debris (CR&SD) |
| Chairmen: | Rodolpho Vilhena de Moraes (UNIFESP); A. F. Bertachini de A. Prado (INPE) |
| 13:30-13:50 | Handling of Conjunction Warnings in EUMETSAT Flight Dynamics |
| P. Righetti, EUMETSAT, German |
|
| 13:50-14:10 | Efficient All Vs. All Collision Risk Analyses |
| Diego Escobar, GMV, Spain |
|
| 14:10-14:30 | Collision Risk Assessment and Operational Experiences for LEO Satellites at GSOC |
| Saika Aida, DLR/GSOC, Germany |
|
| 14:30-14:50 | Search for the Disposal Orbits with a Given Lifetime for a Near-Polar Space Debris |
| Yu. F. Kolyuka, Mission Control Center, Russia |
|
| 14:50-15:10 | Dynamics of Ion-Beam-Propelled Space Debris |
| Claudio Bombardelli, Tech.University of Madrid, Spain |
|
| 15:10-15:30 | Coffee-Break |
| Session 09 | Mission Design (MD) |
| Chairmen: | Jürgen Fertig (ESA/ESOC); Roberto Vieira da Fonseca Lopes (INPE) |
| 15:30-15:50 | Meteosat Third Generation Navigation Approach |
| Hilda Kinter, EUMETSAT, Germany |
|
| 15:50-16:10 | High Performance Satellite Dynamics and Control Simulation for Multi-Purpose Application |
| Ivanka Pelivan, DLR, Germany |
|
| 16:10-16:30 | Alignment of the THEMIS Extended Mission with the Magnetospheric Neutral Sheet |
| Sabine Frey, University of California, USA |
|
| 16:30-17:30 | Free Time | 20:00 | Symposium Dinner |
| Thusday - March 3, 2011 |
| Session 10 | Orbit Determination (OD) |
| Chairmen: | Ralph Kahle (DLR/GSOC); Alexander Sukhanov (IKI) |
| 08:30-08:50 | Automated Operational Multi-Tracking High Precision Orbit Determination for LEO Missions |
| Jaime Fernández, GMV, Spain |
|
| 08:50-09:10 | Robustness Assessment Between Sigma Point and Extended Kalman Filter for Orbit Determination |
| P. C. P. M. Pardal, INPE, Brazil |
|
| 09:10-09:30 | Comparison of Angles only Initial Orbit Determination Algorithms for Space Debris Cataloguing |
| Fran Martinez Fadrique, GMV, Spain |
|
| 09:30-09:50 | A Batch-Sequential Filter for the Orbit Determination of the BepiColombo Radio Science Experiment |
| Antonio Genova, Un. di Roma La Sapienza, Italy |
|
| 09:50-10:10 | Coffee Break |
| Session 11 | Attitude Dynamics 2 (AD2) |
| Chairmen: | Jürgen Fertig (ESA/ESOC); Valdemir Carrara (INPE) |
| 10:10-10:30 | Venus Express Solar Arrays Rotation Experiments to Measure Atmospheric Density |
| Lorenzo Arona, ESA/ESOC, Germany |
|
| 10:30-10:50 | Analysis of Albedo Effects on Coarse Sun Direction Determination Algorithms |
| R.V. da F. Lopes, INPE, Brazil |
|
| 10:50-11:10 | New Eumetsat Polar System Attitude Monitoring Software |
| P. G. Sánchez, GMV, Spain |
|
| 11:10-11:30 | Probabilistic Motion Estimation for Near Real-Time Navigation and Landing on Small Celestial Bodies |
| Cedric Cocaud, University of Tokyo, Japan |
|
| 11:30-11:50 | Magnetospheric Multiscale (MMS) Mission Attitude Ground System Design |
| Joseph Sedlak, A.I.Solutions,Inc - USA |
|
| 11:50-12:10 | Unscented Kalman Filter for Spacecraft Attitude Estimation Using Quaternions and Euler Angles |
| Roberta Veloso Garcia, INPE - Brazil |
|
| 12:10-13:30 | Lunch |
| Session 12 | Orbit Dynamics 3 (OD3) |
| Chairmen: | Mark Beckman (NASA/GSFC); Sandro da Silva Fernandes (ITA) |
| 13:30-13:50 | Adaptive Scheme for Accurate Orbit Propagation |
| Giulio Baù, Un. of Padova, Italy |
|
| 13:50-14:10 | Long term orbit propagation techniques developed in the frame of the French Space Act |
| Hubert Fraysse, CNES, France |
|
| 14:10-14:30 | De-Orbiting Satellites in LEO Orbit Using Solar Sails |
| Danielle Romagnoli, DLR, Germany |
|
| 14:30-14:50 | A Study of the Effects of a Close Approach Between a Planet and a Particle |
| J. K. S. Formiga, FATEC, Brazil |
|
| 14:50-15:10 | Precision On-Board Orbit Model for Attitude Control of the Advanced Land Observing Satellite (ALOS) |
| Takanori Iwata, JAXA, Japan |
|
| 15:10-15:30 | Coffee Break |
| Session 13 | Optimization (OPT) |
| Chairmen: | Jean-Paul Berthias (CNES); A. F. Bertachini de A. Prado (INPE) |
| 15:30-15:50 | Study of Integration Schemes Suited for the Long-Term Extrapolation |
| Julie Anton, ISAE, France |
|
| 15:50-16:10 | Preliminary Design of Satellite Constellations for a Brazilian Regional Positioning System by Means of an Evolutionary Optimization Algorithm |
| Roberto Luiz Galski, INPE, Brazil |
|
| 16:10-16:30 | Extending Propagation with User-Defined Equations, Applications to Optimization and Partial Derivatives Computation |
| Véronique Pommier-Maurussane, CS Comm. & Systèmes, France |
|
| 16:30-16:50 | Optimization of Low-Thrust Transfers Between Given Orbits in a Perturbed Gravity Field |
| Alexander Sukhanov, IKI, Russia |
|
| 16:50-17:10 | Flyby for Optimal Solutions for Near-Earth Asteroid |
| Denilson P. S. Santos, INPE, Brazil |
|
| 17:10-17:30 | Algorithm for Automated Global Optimization of Low and High Thrust Spacecraft Trajectories in a Time Changing Environment |
| Bostjan Eferl, Eferl & co., Slovenia |
| Friday - March 4, 2011 |
| Session 14 | Flight Dynamics Operations 2 (FDOP2) |
| Chairmen: | Yasuhiro Kawakatsu (JAXA); Hélio Koiti Kuga (INPE) |
| 08:30-08:50 | CRYOSAT-2: From LEOP to Acquisition of the Reference Orbit |
| Miguel Angel Martin Serrano, VCS AG at ESA/ESOC, Germany |
|
| 08:50-09:10 | ALSAT-2A Transfer and First Year Operations |
| Mohamed Kameche, CTS/ASAL, Algeria |
|
| 09:10-09:30 | High Gain Antenna Calibration on Three Spacecraft |
| Joseph A. Hashmall, A.I. Solutions, Inc, USA |
|
| 09:30-09:50 | Coffee Break |
| Session 15 | Interplanetary Mission Design 2 (IMD2) |
| Chairmen: | Tomas Martin-Mur (NASA/JPL); Vivian Gomes (INPE) |
| 09:50-10:10 | Short-Period Ballistic Out-of-Ecliptic Trajectories via Multiple Venus & Earth Swing-Bys And Vega-Driven Multiple Earth Swing-Bys |
| Jun'ichiro Kawaguchi, JAXA, Japan |
|
| 10:10-10:50 | Research on Launch Vehicle Interface for Interplanetary Mission |
| Yasuhiro Saito, JAXA, Japan |
|
| 10:30-10:50 | Small Hypothetical Satellites and Dust Particles near Nix and Hydra: Implications for the New Horizons Mission |
| Silvia Maria Giuliatti Winter, UNESP, Brazil |