rootbrowseIAC-06C1session 55. Orbital DynamicsPapers1. New Method of the Analytic Periodic Solution for Spacecraft Formation in Elliptical Orbits2. Direct Density Correction Method: review of results3. Dynamics and Control of Low-Altitude Formations4. Station keeping strategy for geo satellites with low thrust electrical propulsion and limitations in the thrust direction. application to the conexpress project.5. General Dynamics in the Restricted Full Three-Body Problem6. India’s Lunar Mission (Chandrayaan- 1) Orbit Determination System7. Consider Covariance Sigma-Point Filtering Of Inertial Measurement Unit Data For Mars Reconnaissance Orbiter Spacecraft State Estimation During Aerobraking Operations8. Periodic Interplanetary Trajectories in a Restricted Coplanar Circular Two-Planet System9. Orbit Analysis of HAYABUSA around Asteroid ITOKAWA