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)
Sigma Point Kalman Filters for Efficient Orbit Estimation (AAS 03-525)
Formation Maintenance for Low Earth Near-Circular Orbits (AAS 03-652)
An Evaluation and Comparison of Relative Motion Theories (AAS 03-567)
Optimal Attitude Control for Coplanar Orbit Phasing Transfers (AAS 03-262)
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)
Third-Body Perturbation Effects on Satellite Formations (AAS 12-631)
State Transition Matrix for Relative Motion Including J~2 and Third-Body Perturbations (AAS 14-379)
A Boundary Value Problem Approach to Too-Short Arc Optical Track Association (AAS 14-201)
The Characterization of Formation Flying Satellite Relative Motion Orbits (AAS 02-143)
Modeling and Control of Satellite Formations in High Eccentricity Orbits (AAS 03-277)
Dynamics and Control of Power Sail (AAS 01-230)
A Curiously Outlandish Problem in Orbital Mechanics (AAS 01-430)
The State Transition Matrix for Relative Motion of Formation Flying Satellites (AAS 02-186)
Impulsive Spacecraft Formation Flying Control to Establish Specific Mean Orbit Elements (AAS 00-113)
Guaranteed Approach for Orbit Determination With Limited Measurements (AAS 13-706)
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
Time-Optimal Reorientation of Asymmetric Rigid Bodies (AAS 01-384)
Hill's Equations, Mean Orbital Elements, and Formation Flying of Satellites
Comparison of Covariance-Based Track Association Approaches With Simulated Radar Data (AAS 10-318)
Orbit Determination of a Tethered Satellite System Using Laser and Radar Tracking
Analytical Non-Linear Propagation of Uncertainty in the Two-Body Problem (AAS 11-202)
Single Track Covariance for Space Surveillance Network Sensors
Effect of Atmospheric Density Uncertainty on Collision Probability (AAS 00-181)
Optimal Solar Sail Trajectory Analysis for Interstellar Missions (AAS 12-234)
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
A Simple Technique for Low-Thrust High-Accuracy Trajectory Optimization (AAS 06-150)
Angles-Only Orbit Updates for Low Earth Satellites (AAS 06-137)