rootbrowseIAC-10C1session 11. Orbital DynamicsPapers1. analytic expansions of luni-solar gravity perturbations along rotating axes for trajectory optimization: part2: the multipliers system and simulations2. New Numerical Methods for Determining Periodic Orbits in the Circular Restricted Three-Body Problem3. extension of low thrust propulsion to the coplanar circular restricted four body problem with applications to future trojan asteroids missions4. On the low-energy transfers between icy moons of Jupiter5. Electric ?V in Solar Electric Propulsion (SEP) and Flyby for Near-Earth-Objects6. Short-Period Ballistic Out-of-Ecliptic Trajectories via Multiple Venus & Earth Swing-bys and VEGA-driven Multiple Earth Swing-bys7. Trajectory Evolution in Multi-Body Regimes with Applications in the Saturnian System8. accuracy analysis of orbit determination and prediction for low orbit lunar satellites9. Coulomb testbed force model verification for charged relative motion experiments10. Orbit Perturbations and Eccentricity Vector Control in Low-Altitude Moon Orbits11. How to Establish and Keep Orthogonal Constellation by Two Orbiters Under Perturbation12. Spacecraft Rendezvous Through Motion Camouflage