Error Analysis of Satellite Formations in Near-Circular Low-Earth Orbits (AAS 03-651)
Sub-Optimal Formation Establishment and Reconfiguration Using Impulsive Control (AAS 03-590)
Formation Maintenance for Low Earth Near-Circular Orbits (AAS 03-652)
Modeling and Control of Satellite Formations in High Eccentricity Orbits (AAS 03-277)
Sigma Point Kalman Filters for Efficient Orbit Estimation (AAS 03-525)
An Evaluation and Comparison of Relative Motion Theories (AAS 03-567)
Formation Flying: Accommodating Non-Linearity and Eccentricity Perturbations (AAS 02-184)
The Characterization of Formation Flying Satellite Relative Motion Orbits (AAS 02-143)
Precise Onboard Ephemeris Propagation Method Using CW Frame and Multiple Compressions (AAS 02-134)
The Effect of the Periodic Covariance Variations on the Probability of Collision (AAS 02-118)
Effect of Atmospheric Density Uncertainty on Collision Probability (AAS 00-181)
The State Transition Matrix for Relative Motion of Formation Flying Satellites (AAS 02-186)
Dynamics and Control of Power Sail (AAS 01-230)
Impulsive Spacecraft Formation Flying Control to Establish Specific Mean Orbit Elements (AAS 00-113)
Dynamics and Control of Spacecraft Formations: Challenges and Some Solutions
Hill's Equations, Mean Orbital Elements, and Formation Flying of Satellites
Single Track Covariance for Space Surveillance Network Sensors