Orbit Determination of a Tethered Satellite System Using Laser and Radar Tracking
Single Track Covariance for Space Surveillance Network Sensors
Modeling Catastrophic Decay Orbits Through Perigee
Estimating Atmosphere Density Variations to Improve LEO Orbit Prediction Accuracy
Orbit Determination for Medium-Altitude Eccentric Orbits Using GPS
Optimal Station Keeping Strategies Via Parallel Genetic Algorithms
Impulsive Spacecraft Formation Flying Control to Establish Specific Mean Orbit Elements (AAS 00-113)
Dynamics and Control of Spacecraft Formations: Challenges and Some Solutions
Near-Real Time Atmospheric Density Correction Using NAVSPASUR Fence Observations (AAS 00-179)
Hill's Equations, Mean Orbital Elements, and Formation Flying of Satellites
Effect of Atmospheric Density Uncertainty on Collision Probability (AAS 00-181)
Atmospheric Density Correction Using Space Catalog Data (AAS 01-481)
Dynamics and Control of Power Sail (AAS 01-230)
Formation Flying: Accommodating Non-Linearity and Eccentricity Perturbations (AAS 02-184)
The Effect of the Periodic Covariance Variations on the Probability of Collision (AAS 02-118)
Precise Onboard Ephemeris Propagation Method Using CW Frame and Multiple Compressions (AAS 02-134)