An Evaluation and Comparison of Relative Motion Theories (AAS 03-567)
Angles-Only Orbit Updates for Low Earth Satellites (AAS 06-137)
Comparison of Optical and Radar Tracking for Catalog Maintenance (AAS 04-197)
Criteria for Best Configuration and Sub-Optimal Reconfiguration for MMS Mission (AAS 04-152)
Density Corrections for the NRLMSIS-00 Atmosphere Model (AAS 05-168)
Design and Control of Libration Point Satellite Formations (AAS 04-161)
Dynamics and Control of Power Sail (AAS 01-230)
Dynamics and Control of Spacecraft Formations: Challenges and Some Solutions
Effect of Atmospheric Density Uncertainty on Collision Probability (AAS 00-181)
Error Analysis of Satellite Formations in Near-Circular Low-Earth Orbits (AAS 03-651)
Formation Flying: Accommodating Non-Linearity and Eccentricity Perturbations (AAS 02-184)
Formation Maintenance for Low Earth Near-Circular Orbits (AAS 03-652)
High Accuracy Orbit Updates Using Angles-Only Data (AAS 04-198)
Hill's Equations, Mean Orbital Elements, and Formation Flying of Satellites
Improving Dynamic Calibration of the Atmosphere (AAS 07-185)
Improving Dynamic Calibration of the Atmosphere (AAS 07-185)
Impulsive Spacecraft Formation Flying Control to Establish Specific Mean Orbit Elements (AAS 00-113)
Maneuver Estimation Model for Relative Orbit Determination (AAS 05-405)
Modeling and Control of Satellite Formations in High Eccentricity Orbits (AAS 03-277)
Numerical Searches and Optimal Control of J2 Invariant Orbits (AAS 06-163)
Orbit Determination of a Tethered Satellite System Using Laser and Radar Tracking
Precise Onboard Ephemeris Propagation Method Using CW Frame and Multiple Compressions (AAS 02-134)
Real-Time Computations of Time-Optimal Magnetic Attitude Control (AAS 05-233)
Real-Time Outer and Inner Loop Optimal Control Using DIDO (AAS 05-353)
Results and Issues of Atmospheric Density Correction (AAS 04-305)
Sequential Attitude Estimation Using Particle Filters (AAS 05-265)
Sigma Particle Filtering for Nonlinear Dynamic Systems (AAS 05-266)
Sigma Point Kalman Filters for Efficient Orbit Estimation (AAS 03-525)
Single Track Covariance for Space Surveillance Network Sensors
Sub-Optimal Formation Establishment and Reconfiguration Using Impulsive Control (AAS 03-590)
The Characterization of Formation Flying Satellite Relative Motion Orbits (AAS 02-143)
The Effect of the Periodic Covariance Variations on the Probability of Collision (AAS 02-118)
The State Transition Matrix for Relative Motion of Formation Flying Satellites (AAS 02-186)
Three-Axis Magnetic Attitude Control Using Pseudospectral Control Law (AAS 05-417)
Validation and Application of Corrections to the NRLMSISE-00 Atmospheric Density Model (AAS 07-189)
Validation and Application of Corrections to the NRLMSISE-00 Atmospheric Density Model (AAS 07-189)