Stability and Reconfiguration Analysis of a Circularly Spinning Two-Craft Coulomb Tether
Locally Power-Optimal Spacecraft Attitude Control for Redundant Reaction Wheel Cluster
Input Shaped Large Thrust Maneuver with a Tethered Debris Object
Local Debris Congestion in the Geosynchronous Environment with Population Augmentation
Stabilization of Satellite Motion Relative to a Coulomb Spacecraft Formation
Active Space Debris Charging for Contactless Electrostatic Disposal Maneuvers
AIAA-2004-5213 Angular Momentum Constraint for Coulomb Satellite Formation
FULL-LENGTH PAPERS - Hybrid Cartesian and Orbit Element Feedback Law for Formation Flying Spacecraft
FULL-LENGTH PAPERS - Singularity Avoidance Using Null Motion and Variable-Speed Control Moment Gyros
New Penalty Functions and Optimal Control Formulation for Spacecraft Attitude Control Problems