rootbrowseIAC-09C1session 22. Orbital Dynamics (1)Papers1. departure / swingby window expansion for gravity capture around the moon via the combination of the solar tidal force with the low thrust propulsion2. On Ballistic Acquisition of Short Period Out-Of-Ecliptic Trajectories3. State Transition Matrix Approximation with Geometry Preservation for General Perturbed Orbits4. Identification of Families of Periodic Orbits Above/Below the Solar Sail Earth-Moon Libration Points5. A reduced model for efficient multiple gravity assist trajectory design6. Analysis of a family of periodic orbits around Mars in the framework of restricted three-body problem7. Low-cost Mission to NEO Binary 1999 KW48. Non-Keplerian orbits using low thrust, high Isp propulsion systems9. General relativistic effects on solar sail trajectories near the sun10. A Study on the Distribution of Dust Particles Trapped into a Horseshoe Orbit11. survey of research on lambert’s problem