Dynamics and Control of Spacecraft Formations: Challenges and Some Solutions
Hill's Equations, Mean Orbital Elements, and Formation Flying of Satellites
Modeling and Control of Satellite Formations in High Eccentricity Orbits (AAS 03-277)
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)
Real-Time Outer and Inner Loop Optimal Control Using DIDO (AAS 05-353)
Sequential Attitude Estimation Using Particle Filters (AAS 05-265)
Sigma Particle Filtering for Nonlinear Dynamic Systems (AAS 05-266)
Three-Axis Magnetic Attitude Control Using Pseudospectral Control Law (AAS 05-417)
Maneuver Estimation Model for Relative Orbit Determination (AAS 05-405)
Single-Point Optimal Attitude Determination Using Modified Rodrigues Parameters (AAS 05-459)