20nd International Symposium on Space Flight Dynamics
São José dos Campos, Brazil, February 28 - March 4, 2011
The 22nd ISSFD was organized by INPE (Brazilian Institute for Space Research)
Monday - February 28, 2011
| Session 01 | Orbit Dynamics 1 (ODY1) |
| Chairmen: |
Jean-Paul Berthias (CNES); Hélio Koiti Kuga (INPE) |
| Final Commissioning of the PRISMA GPS Navigation System | |
|
Jeab-Sébastien Ardaens, DLR/GSOC, Germany |
|
| Analysis of Geostationary Transfer Orbit Long-Term Evolution and Lifetime | |
|
Alain Lamy, CNES, France |
|
| 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 |
|
| Dynamic Stabilization of L2 Periodic Orbits Using Attitude-Orbit Coupling Effects | |
|
Martin Lara, Real Observatorio de la Armada, Spain |
|
| Out of plane Autonomous Orbit Control | |
|
Éric Julien, CNES, France |
| Session 02 - | Formation Flying (FF) |
| Chairmen: |
Ralph Kahle (DLR/GSOC); A. F. Bertachini de A. Prado (INPE) |
| Monte Carlo Simulations of the Formation Flying Dynamics for the Magnetospheric Multiscale (MMS) Mission | |
|
Conrad Schiff, NASA GSFC, USA |
|
| Feasibility of Meteosat Third Generation Collocation Using a Single S-Band Tracking Station and Large Inclination Maneuvers | |
|
Pierluigi Righetti, EUMETSAT, Germany |
|
| Comparative Analysis Of Cartesian and Curvilinear Clohessy-Wiltshire Equations | |
| Frederik J. de Bruijn, Delft University of Technology, Netherlands |
|
| Proximity Operations Of On-Orbit Servicing Spacecraft Using An Eccentricity/Inclination Vector Separation | |
| J. Spurmann, DLR/GSOC, Germany |
|
| Relative Guidance of Formation Flying Mission Spacecraft: From Design to Flight Tests in FFIORD Mission | |
| Sophie Djalal, CNES, France |
| Session 03 | Interplanetary Mission Design 1 (IMD1) |
| Chairmen: |
Tomas Martin-Mur (NASA/JPL); Roberto Luiz Galski (INPE) |
| Trajectory Options for Solar Polar Region Observation Mission | |
| Yasuhiro Kawakatsu, JAXA, Japan |
|
| Sun Influence on Two-Impulsive Earth-to-Moon Transfers | |
| Sandro da Silva Fernandes, ITA, Brazil |
|
| Trajectory Design For BepiColombo Based On Navigation Requirements | |
| Rüdiger Jehn, ESA/ESOC, Germany |
|
| ASTER Mission : Stability Regions around the Triple Asteroid 2001 SN263 | |
| O.C. Winter, UNESP, Brazil |
|
| Jupiter Magnetospheric Orbiter Trajectory Design: Reaching High Inclination in the Jovian System | |
| Stefano Campagnola, JAXA, Japan |
|
| A study of the guidance method for the Small Solar Power Sail Demonstrator, IKAROS | |
| Masaki Nakamiya, JAXA, Japan |
| Tuesday - March 1, 2011 |
| Session 04 | Flight Dynamics Operations 1 (FDOP1) |
| Chairmen: |
Yasuhiro Kawakatsu (JAXA); Vivian Gomes (INPE) |
| TERRASAR-X / TANDEM-X Formation Control - First Results from Commissioning and Routine Operations | |
| Ralph Kahle, DLR, Germany |
|
| GOCE Flight Dynamics Operations from an Orbital Perspective | |
| Dirk Kuijper, Logica at ESA/ESOC, Germany |
|
| Operational Verification of the Flight Dynamics System for COMS Satellite | |
| Byoung-Sun Lee, ETRI and KARI, South Korea |
|
| Theos Orbit Maintenance: Assessment of 2 Years of Operations | |
| Pornthep Navakitkanok, GISTDA, Thailand |
| Session 05 | Orbit Dynamics 2 (ODY2) |
| Chairmen: |
Mark Beckman (NASA/GSFC); Valdemir Carrara (INPE) |
| Relative Navigation for the TanDEM-X mission and evaluation with DEM calibration results | |
| Martin Wermuth, DLR/GSOC, Germany |
|
| Asymptotic Solution for the Orbit Motion Under Constant Tangential Acceleration | |
| Claudio Bombardelli, TUM , Spain |
|
| Artificial Satellites Dynamics: Resonant Effects | |
| Jarbas Cordeiro Sampaio, UNESP, Brazil |
| Wednesday - March 2, 2011 |
| Session 06 | Interplanetary Navigation (IN) |
| Chairmen: |
Jürgen Fertig (ESA/ESOC); Ulisses Thadeu Vieira Guedes (INPE) |
| Navigation Strategies for Primitive Solar System Body Rendezvous and Proximity Operations | |
| Kenneth Getzandanner, NASA GSFC, USA |
|
| Solar Sail Force Modeling for Spinning Solar Sail Using the Radiometric Tracking Data | |
| Tomohiro Yamaguchi, The Grad. Univ. for Adv.Studies, Japan |
|
| Mars Science Laboratory Interplanetary Navigaton Analysis | |
| T. J. Martin-Mur, JPL/CIT, USA |
|
| Effects of the Initial Conditions in a Swing-By of a Cloud of Particles | |
| V. M. Gomes, INPE, Brazil |
| Session 07 | Attitude Dynamics 1 (AD1) |
| Chairmen: |
Hélio Koiti Kuga (INPE); Othon Cabo Winter (UNESP) |
| Spin Stabilized Satellite's Attitude Propagation with Quaternions | |
| Maria C.Zanardi, UNESP, Brazil |
|
| Bringing Realistic Attitude Sequence Modeling to Non-Experts | |
| Véronique Pommier-Maurussane, CS Comm. & Systèmes, France |
|
| Attitude Simulation Software to Support Brazilian Space Missions | |
| Valdemir Carrara, INPE, Brazil |
|
| In-Flight Characterisation of CRYOSAT-2 Reaction Control System | |
| Stefano Pessina, Terma GmbH c/o ESA/ESOC, Germany |
|
| Spin Stabilized Satellite's Attitude Analytical Prediction | |
| Maria C.Zanardi, UNESP, Brazil |
| Session 08 | Colision Risk and Space Debris (CR&SD) |
| Chairmen: |
Rodolpho Vilhena de Moraes (UNIFESP); A. F. Bertachini de A. Prado (INPE) |
| Handling of Conjunction Warnings in EUMETSAT Flight Dynamics | |
| P. Righetti, EUMETSAT, German |
|
| Efficient All Vs. All Collision Risk Analyses | |
| Diego Escobar, GMV, Spain |
|
| Collision Risk Assessment and Operational Experiences for LEO Satellites at GSOC | |
| Saika Aida, DLR/GSOC, Germany |
|
| Search for the Disposal Orbits with a Given Lifetime for a Near-Polar Space Debris | |
| Yu. F. Kolyuka, Mission Control Center, Russia |
|
| Dynamics of Ion-Beam-Propelled Space Debris | |
| Claudio Bombardelli, Tech.University of Madrid, Spain |
| Session 09 | Mission Design (MD) |
| Chairmen: |
Jürgen Fertig (ESA/ESOC); Roberto Vieira da Fonseca Lopes (INPE) |
| Meteosat Third Generation Navigation Approach | |
| Hilda Kinter, EUMETSAT, Germany |
|
| High Performance Satellite Dynamics and Control Simulation for Multi-Purpose Application | |
| Ivanka Pelivan, DLR, Germany |
|
| Alignment of the THEMIS Extended Mission with the Magnetospheric Neutral Sheet | |
| Sabine Frey, University of California, USA |
| Thusday - March 3, 2011 |
| Session 10 | Orbit Determination (OD) |
| Chairmen: |
Ralph Kahle (DLR/GSOC); Alexander Sukhanov (IKI) |
| Automated Operational Multi-Tracking High Precision Orbit Determination for LEO Missions | |
| Jaime Fernández, GMV, Spain |
|
| Robustness Assessment Between Sigma Point and Extended Kalman Filter for Orbit Determination | |
| P. C. P. M. Pardal, INPE, Brazil |
|
| Comparison of Angles only Initial Orbit Determination Algorithms for Space Debris Cataloguing | |
| Fran Martinez Fadrique, GMV, Spain |
|
| A Batch-Sequential Filter for the Orbit Determination of the BepiColombo Radio Science Experiment | |
| Antonio Genova, Un. di Roma La Sapienza, Italy |
| Session 11 | Attitude Dynamics 2 (AD2) |
| Chairmen: |
Jürgen Fertig (ESA/ESOC); Valdemir Carrara (INPE) |
| Venus Express Solar Arrays Rotation Experiments to Measure Atmospheric Density | |
| Lorenzo Arona, ESA/ESOC, Germany |
|
| Analysis of Albedo Effects on Coarse Sun Direction Determination Algorithms | |
| R.V. da F. Lopes, INPE, Brazil |
|
| New Eumetsat Polar System Attitude Monitoring Software | |
| P. G. Sánchez, GMV, Spain |
|
| Probabilistic Motion Estimation for Near Real-Time Navigation and Landing on Small Celestial Bodies | |
| Cedric Cocaud, University of Tokyo, Japan |
|
| Magnetospheric Multiscale (MMS) Mission Attitude Ground System Design | |
| Joseph Sedlak, A.I.Solutions,Inc - USA |
|
| Unscented Kalman Filter for Spacecraft Attitude Estimation Using Quaternions and Euler Angles | |
| Roberta Veloso Garcia, INPE - Brazil |
| Session 12 | Orbit Dynamics 3 (OD3) |
| Chairmen: |
Mark Beckman (NASA/GSFC); Sandro da Silva Fernandes (ITA) |
| Adaptive Scheme for Accurate Orbit Propagation | |
| Giulio Baù, Un. of Padova, Italy |
|
| Long term orbit propagation techniques developed in the frame of the French Space Act | |
| Hubert Fraysse, CNES, France |
|
| De-Orbiting Satellites in LEO Orbit Using Solar Sails | |
| Danielle Romagnoli, DLR, Germany |
|
| A Study of the Effects of a Close Approach Between a Planet and a Particle | |
| J. K. S. Formiga, FATEC, Brazil |
|
| Precision On-Board Orbit Model for Attitude Control of the Advanced Land Observing Satellite (ALOS) | |
| Takanori Iwata, JAXA, Japan |
| Session 13 | Optimization (OPT) |
| Chairmen: |
Jean-Paul Berthias (CNES); A. F. Bertachini de A. Prado (INPE) |
| Study of Integration Schemes Suited for the Long-Term Extrapolation | |
| Julie Anton, ISAE, France |
|
| Preliminary Design of Satellite Constellations for a Brazilian Regional Positioning System by Means of an Evolutionary Optimization Algorithm | |
| Roberto Luiz Galski, INPE, Brazil |
|
| Extending Propagation with User-Defined Equations, Applications to Optimization and Partial Derivatives Computation | |
| Véronique Pommier-Maurussane, CS Comm. & Systèmes, France |
|
| Optimization of Low-Thrust Transfers Between Given Orbits in a Perturbed Gravity Field | |
| Alexander Sukhanov, IKI, Russia |
|
| Flyby for Optimal Solutions for Near-Earth Asteroid | |
| Denilson P. S. Santos, INPE, Brazil |
|
| 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) |
| CRYOSAT-2: From LEOP to Acquisition of the Reference Orbit | |
| Miguel Angel Martin Serrano, VCS AG at ESA/ESOC, Germany |
|
| ALSAT-2A Transfer and First Year Operations | |
| Mohamed Kameche, CTS/ASAL, Algeria |
|
| High Gain Antenna Calibration on Three Spacecraft | |
| Joseph A. Hashmall, A.I. Solutions, Inc, USA |
| 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 |
|
| Research on Launch Vehicle Interface for Interplanetary Mission | |
| Yasuhiro Saito, JAXA, Japan |
|
| Small Hypothetical Satellites and Dust Particles near Nix and Hydra: Implications for the New Horizons Mission | |
| Silvia Maria Giuliatti Winter, UNESP, Brazil |