rootbrowseIAC-05C1session PP. Poster Session on AstrodynamicsPapers2. Route Theory for Optimal Design of Satellite Constellations to Minimize Revisit Time in Low Earth Orbits3. On Inherent Information Redundancy in Vector Measuring Attitude Determination Methods4. Attitude Determination for the student satellite nCubeII: Kalman Filter5. Command shaping for a flexible satellite platform controlled by advanced fly-wheels systems6. Attitude control of the ESEO satellite7. Inflatable Gravity Gradient Boom8. Coordinated control of satellites: the attitude case9. A study of actuator configurations for the ESEO satellite10. Thruster actuation algorithms for scientific space missions12. Reaction wheels development at Stork Aerospace13. Minimum energy control law for satellite reorientation by two wheels.14. Optimal Motion Planning and Tracking Control for a Flexible Manipulator15. A Practical Operation Strategy for an Electrodynamic Tether System 16. Dynamics of Membrane Deployment for Tether-Controlled Spinning Solar Sail18. An efficient optimization method to deal with global RLV (ascent and branching) trajectories20. The Pioneer Anomaly in the Context of Non-Newtonian Gravity23. A Design of a Mission to Neptune using Close Approaches24. Turn over Problem of Tether Satellite System25. Observability of measurement bias for nonlinear systems arising from satellite autonomous navigation and attitude determination 27. Feasibility Study of Robotic Servicing for the Hubble Space Telescope28. A New Approach for Spacecraft Rendezvous and Fly-Around Control on Elliptic Orbits