Current Development of the Precision Semianalytical Satellite Theory
REENTRY TIME PREDICTION USING ATMOSPHERIC DENSITY CORRECTIONS
Application of Sun-Synchronous Critically Inclined Orbits to Global Personal Communications Systems
Density Corrections for the NRLMSIS-00 Atmosphere Model (AAS 05-168)
Implementing a 50x50 Gravity Field Model in an Orbit Determination System (AAS 93-693)
Atmospheric Density Correction Using Two Line Element Sets as the Observation Data (AAS 03-626)
Results and Issues of Atmospheric Density Correction (AAS 04-305)
Elliptical Orbit Constellation- A New Paradigm for Higher Efficiency in Space Systems
Automated Station-Keeping for Satellite Constellations
Effect of Atmospheric Density Correction on Precision Orbit Determination (AAS 05-316)
Near-Real Time Atmospheric Density Correction Using NAVSPASUR Fence Observations (AAS 00-179)
Validation and Application of Corrections to the NRLMSISE-00 Atmospheric Density Model (AAS 07-189)