rootbrowseIAC-20C1session VPVP. Virtual Presentations - IAF ASTRODYNAMICS SYMPOSIUMPapers1. Attitude Control and Determination Accuracy Study of Small Satellite with Limited Set of Sensors. capability analysis for manipulator-actuated integrated translational and rotational control strategy of spacecraft. J2-perturbed low-energy orbits around Enceladus. Development of an Unscented Kalman Filter for the validation of the European Space Agency candidate mission Asteroid Impact Mission’s optical navigation strategy up to Hardware In the Loop. Orbital stability analysis around the primary of a binary asteroid system. Chandrayaan-2: Orbit Maneuver Operations. regularized analytical orbit theory with solar radiation pressure. FULL - BODY RELATIVE SPACECRAFT MOTION. A MINIMAL PARAMETERIZATION USING CAYLEY-LIKE TRANSFORM. Initial Orbit Improvement and Best Observation Time Window Determination Based-on Angles-Only Measurements. Satellite Repositioning Maneuver Detection in Geosynchronous Orbit Using Two-line Element (TLE) Data