Orbit Determination of a Tethered Satellite System Using Laser and Radar Tracking
Single Track Covariance for Space Surveillance Network Sensors
Application of Optimal Periodic Control Theory to the Orbit Reboost Problem
Launch Period Analysis for the Jupiter Gravity Assist Opportunities to Pluto
Gravitational Effects of Earth in Optimizing Delta-V for Deflecting Earth-Crossing Asteroids
Impulsive Spacecraft Formation Flying Control to Establish Specific Mean Orbit Elements (AAS 00-113)
Dynamics and Control of Spacecraft Formations: Challenges and Some Solutions
Accuracy and Optimality of Direct Transcription Methods (AAS 00-205)
A Spectral Patching Method For Direct Trajectory Optimization
Hill's Equations, Mean Orbital Elements, and Formation Flying of Satellites
Effect of Atmospheric Density Uncertainty on Collision Probability (AAS 00-181)
Dynamics and Control of Power Sail (AAS 01-230)
A Curiously Outlandish Problem in Orbital Mechanics (AAS 01-430)
Time-Optimal Reorientation of Asymmetric Rigid Bodies (AAS 01-384)
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)