Iodine Electric Propulsion System Thrust Validation: From Numerical Modeling to In-Space Testing
On-Line Mass Estimation for a Tethered Space Debris During Post-Capture and Retrieval (AAS 14-451)
Lidar and Optical-Based Autonomous Navigation for Small Body Proximity Operations (AAS 14-420)
State Transition Matrix for Relative Motion Including J~2 and Third-Body Perturbations (AAS 14-379)
Longitude-Dependent Effects of Fragmentation Events in the Geosynchronous Orbit Regime (AAS 14-321)
Attitude Estimation Via Lidar Altimetry and a Particle Filter (AAS 14-301)
Preliminary Determination of the Geocentric Earth Flyby Path of Asteroid 2012 DA14 (AAS 14-288)
Sequential Orbit Determination Using Satellite Laser Ranging (AAS 14-287)
A Boundary Value Problem Approach to Too-Short Arc Optical Track Association (AAS 14-201)
Tether Design Considerations for Large Thrust Debris De-Orbit Burns (AAS 14-443)
Uncertainty Quantification for Angles-Only Initial Orbit Determination (AAS 14-434)
Utilization of Uncertainty Information in Angles-Only Initial Orbit Determination (AAS 14-431)
Spacecraft Swarm Finite-Thrust Cooperative Control for Common Orbit Convergence (AAS 14-380)
Techniques for Designing Many-Revolution, Electric-Propulsion Trajectories (AAS 14-373)
Orbit Design and Navigation Through the End of Messenger's Extended Mission at Mercury (AAS 14-369)
Solar Sailing Apophis Rendezvous Mission With Fuel-Fixed Delta-V (AAS 14-353)
Satellite Breakup Debris Cloud Characterization (AAS 14-329)
Bilinear Observer/Kalman Filter Identification (AAS 14-307)
Gyro-Free Rigid Body Attitude Stabilization Using Only Vector Measurements on SO(3) (AAS 14-300)
Mapping To Compensate Radial Geometrical Distortion In Pin-Hole Cameras (AAS 14-297)
Bezier Description of Space Trajectories (AAS 14-294)
Explore Europa by the Jovian Magnetic Lorentz Force (AAS 14-269)
The Adaptive Entry Guidance Based on 3D Obtainable Space Concept (AAS 14-250)
Fault Detection and Isolation Strategy for Redundant Inertial Measurement Units (AAS 14-246)
Near Optimal Feedback Guidance Design and the Planar Restricted Three-Body Problem (AAS 14-238)
Estimation for Satellite Collision Probabilities Using Importance Sampling (AAS 14-203)
A Navigator's Journey (AAS 14-473)
External Torques Affecting the Attitude Motion of a Mercury Orbiter (AAS 14-452)
Determining Orbits That Can be Controlled by Natural Forces (AAS 14-426)
End-of-Life Earth Re-Entry for Highly Elliptical Orbits: The Integral Mission (AAS 14-325)
Forced Precession Orbit Departing From Keplerian Orbit Under Continuous Normal Thrust (AAS 14-265)
A Non-Singular Keplerian Differential State Transition Matrix (AAS 14-213)
Enabling the Use of Rotating Platforms for Orbit Determination Applications (AAS 14-206)