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TECHNICAL NOTE - Dynamics and Orbit Determination of Tethered Satellite Systems
Reorientations of Asymmetric Spacecraft Using Two or More Impulses
Nonlinear Attitude Motion of Asymmetric Spacecraft Containing Symmetric Rotors
Multibody Modeling of Communications Satellite Dynamics for Ground-Based Simulation
Large Angle Maneuver of Asymmetric Spacecraft Using Solutions to the Impulsive Reorientation Problem
Impulsive Reorientations of Asymmetric Spacecraft - Characteristics of the Motion (AAS 94-107)
Fixed-Time Reorientations of Rigid Bodies and Lambert's Problem
Dynamics and Orbit Determination of Tethered Satellite Systems