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
The K-Vector ND and its Application to Building a Non-Dimensional Star Identification Catalog
Closed-Loop Control of Satellite Formations Using a Quasi-Rigid Body Formulation
A Dynamical Systems Analysis of Resonant Flybys: Ballistic Case
Terrain-Relative and Beacon-Relative Navigation for Lunar Powered Descent and Landing
Optimal Out-Of-Ecliptic Orbits for Short-Term Space-Borne Infrared Telescope Missions
Modified Chebyshev-Picard Iteration Methods for Orbit Propagation
Near-Earth Asteroid Flyby Survey Mission Using Solar Sailing Technology
Design of Optimal Low-Thrust Lunar Pole-Sitter Missions
Deep Resonant GPS-Dynamics Due to the Geopotential