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Tether Design Considerations for Large Thrust Debris De-Orbit Burns (AAS 14-443)
Touchless Electrostatic Three-Dimensional Detumbling of Large GEO Debris (AAS 14-378)
Discretized Input Shaping for a Large Thrust Tethered Debris Object (AAS 14-446)
Longitude-Dependent Effects of Fragmentation Events in the Geosynchronous Orbit Regime (AAS 14-321)
Characterizing Localized Debris Congestion in the Geosynchronous Orbit Regime (AAS 14-322)
Stabilization of Satellite Motion Relative to a Coulomb Spacecraft Formation
Relative Orbit Geometry Through Classical Orbit Element Differences
Hybrid Control of Orbit Normal and Along-Track 2-Craft Coulomb Tethers (AAS 07-193)
Hybrid Control of Orbit Normal and Along-Track 2-Craft Coulomb Tethers (AAS 07-193)
Spacecraft Attitude Control Using Symmetric Stereographic Orientation Parameters (AAS 07-182)
Spacecraft Attitude Control Using Symmetric Stereographic Orientation Parameters (AAS 07-182)
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
Invariant Shape Solutions of Spinning Three Craft Coulomb Tether Problem (AAS 06-228)
Reconfiguration of a 2-Craft Coulomb Tether (AAS 06-229)
Coulomb Spacecraft Voltage Study Due to Differential Orbital Perturbations (AAS 06-123)
Static Equilibrium Configurations in GEO Coulomb Spacecraft Formations (AAS 05-104)
Linear Dynamics and Stability Analysis of a Coulomb Tether Formation (AAS 05-204)
Nonsingular Attitude Filtering Using Modified Rodrigues Parameters (AAS 09-130)
Stabilization of Satellite Motion Relative to a Coulomb Spacecraft Formation (AAS 04-259)
Partial Disk Tracking Using Visual Snakes: Application to Spacecraft Pose Estimation (AAS 09-124)
Electrostatic Spacecraft Collision Avoidance Using Piece-Wise Constant Charges (AAS 09-184)
One-Dimensional Testbed for Coulomb Controlled Spacecraft (AAS 09-115)
Open-Loop Electrostatic Spacecraft Collision Avoidance Using Patched Conics Analysis (AAS 08-207)
Orbit-Nadir Aligned Coulomb Tether Reconfiguration Analysis (AAS 08-149)
Linear Stability and Shape Analysis of Spinning Three-Craft Coulomb Formations (AAS 11-225)
Adaptive External Torque Estimation by Means of Tracking a Lyapunov Function
An Instantaneous Eigenstructure Quasi-Coordinate Formulation for Nonlinear Multibody Dynamics
J~2 Invariant Relative Orbits for Spacecraft Formations
Feedback Control Law for Variable Speed Control Moment Gyros
Impulsive Spacecraft Formation Flying Control to Establish Specific Mean Orbit Elements (AAS 00-113)
MATLAB Toolbox for Rigid Body Kinematics