Validation and Application of Corrections to the NRLMSISE-00 Atmospheric Density Model (AAS 07-189)
Validation and Application of Corrections to the NRLMSISE-00 Atmospheric Density Model (AAS 07-189)
Time-Optimal Reorientation of Asymmetric Rigid Bodies (AAS 01-384)
Three-Axis Magnetic Attitude Control Using Pseudospectral Control Law (AAS 05-417)
Third-Body Perturbation Effects on Satellite Formations (AAS 12-631)
The State Transition Matrix for Relative Motion of Formation Flying Satellites (AAS 02-186)
The Effect of the Periodic Covariance Variations on the Probability of Collision (AAS 02-118)
The Characterization of Formation Flying Satellite Relative Motion Orbits (AAS 02-143)
Sub-Optimal Formation Establishment and Reconfiguration Using Impulsive Control (AAS 03-590)
State Transition Matrix for Relative Motion Including J~2 and Third-Body Perturbations (AAS 14-379)
Singular Value Decomposition and Least Squares Orbit Determination (AAS 07-362)
Singularity-Free Optimal Steering of Control Moment Gyros (AAS 05-419)
Single Track Covariance for Space Surveillance Network Sensors
Sigma Point Kalman Filters for Efficient Orbit Estimation (AAS 03-525)
Sigma Particle Filtering for Nonlinear Dynamic Systems (AAS 05-266)
Sequential Attitude Estimation Using Particle Filters (AAS 05-265)
Results and Issues of Atmospheric Density Correction (AAS 04-305)
Real-Time Outer and Inner Loop Optimal Control Using DIDO (AAS 05-353)
Real-Time Computations of Time-Optimal Magnetic Attitude Control (AAS 05-233)
Pseudospectral Optimal Control on Arbitrary Grids (AAS 09-405)
Precise Onboard Ephemeris Propagation Method Using CW Frame and Multiple Compressions (AAS 02-134)
Orbit Determination of a Tethered Satellite System Using Laser and Radar Tracking
Optimal Solar Sail Trajectory Analysis for Interstellar Missions (AAS 12-234)
Optimal Attitude Control for Coplanar Orbit Phasing Transfers (AAS 03-262)
On the Fundamental Frequencies of Satellite Relative Motion and Control of Formations (AAS 07-427)
Numerical Searches and Optimal Control of J2 Invariant Orbits (AAS 06-163)
Modeling and Control of Satellite Formations in High Eccentricity Orbits (AAS 03-277)
Maneuver Estimation Model for Relative Orbit Determination (AAS 05-405)
Launch Period Analysis for the Jupiter Gravity Assist Opportunities to Pluto
Initialization of Real-Time Optimal Control (AAS 08-118)
Impulsive Spacecraft Formation Flying Control to Establish Specific Mean Orbit Elements (AAS 00-113)
Improving Dynamic Calibration of the Atmosphere (AAS 07-185)
Improving Dynamic Calibration of the Atmosphere (AAS 07-185)
Hill's Equations, Mean Orbital Elements, and Formation Flying of Satellites
High Accuracy Orbit Updates Using Angles-Only Data (AAS 04-198)
Guaranteed Approach for Orbit Determination With Limited Measurements (AAS 13-706)
Gravitational Effects of Earth in Optimizing Delta-V for Deflecting Earth-Crossing Asteroids
Formation Maintenance for Low Earth Near-Circular Orbits (AAS 03-652)
Formation Flying: Accommodating Non-Linearity and Eccentricity Perturbations (AAS 02-184)
Feedback Control for Formation Flying Maintenance Using State Transition Matrix (AAS 10-312)
Error Analysis of Satellite Formations in Near-Circular Low-Earth Orbits (AAS 03-651)