PPKBZ9 $$\mathcal{A}, \mathcal{S}\mathcal{A}$$ Two Orbit Propagators Based on an Analytical Theory
Closed-Loop Time-Optimal Attitude Maneuvering of Magnetically Actuated Spacecraft
Modified Chebyshev-Picard Iteration Methods for Solution of Boundary Value Problems
Spacecraft Formation Design and Control in Keplerian Elliptic Orbits
Information Theoretic Weighting for Robust Star Centroiding
Earth Satellite Perturbation Theories as Approximate KAM Tori
A Study of the Achievable Geosynchronous Angles-Only Orbit Estimation Accuracy
Attitude Motion of a Spinning Spacecraft with Fuel Sloshing and Nutation Damping