Trajectory Accuracy Assessment During Intrack Thrusting Using Energy Integrals (AAS 94-155)
Stochastic Clock Model for Definitive Sequential Orbit Determination
Solution to the Geocentric Lambert Boundary Value Problem for a Complete Force Field (AAS 93-752)
Sherman's Theorem: Solutions to the Multidimensional Nonlinear Real-Time Problems (AAS 05-451)
Orbit Determination Solution to Non-Markov Gravity Error Problem (AAS 94-176)
Estimation of Instantaneous Maneuvers Using a Fixed Interval Smoother (AAS 03-518)
Close Approach Spacecraft Maneuver Criterion (AAS 99-393)