Hamilton-Jacobi Modelling of Relative Motion for Formation Flying
The Two-Step Optimal Estimator and Example Applications (AAS 00-002)
Relative Spacecraft Motion: A Hamiltonian Approach to Eccentricity Perturbations (AAS 04-294)
Bounded, Periodic Relative Motion Using Canonical Epicyclic Orbital Elements (AAS 05-186)
Optimal Out-of-the-Ecliptic Trajectories for Space-borne Observatories (AAS 01-162)
Optimal Out-of-the-Ecliptic Trajectories for Space-borne Observatories (AAS 01-162)
Hovercraft Satellite Simulation Test-Bed (AAS 04-300)
Satellite Attitude Estimation Using a Two-Step Optimal Estimator (AAS 02-002)
Low Earth Orbit Constellation Design Using the Earth-Moon L1 Point (AAS 04-248)
Optimization of an Occulter-Based Extrasolar-Planet-lmaging Mission
Nonlinear Modeling and Control of Spacecraft Relative Motion in the Configuration Space (AAS 03-108)