TECHNICAL NOTE - Accurate Orbit Determination from Short-Arc Dense Observational Data
Strategies for Near Earth Object Impact Hazard Mitigation (AAS 05-147)
Orbit Determination During High Thrust and Low Thrust Maneuvers (AAS 05-136)
Thrust Vector Control of the Jupiter Icy Moons Orbiter Spacecraft (AAS 05-114)
Preliminary Orbit Determination of a Tethered Satellite Using Angles-Only Measurements (AAS 05-228)
Mars Aerodynamic Entry Control Using Static Output Feedback and LPV Techniques (AAS 05-216)
Optimal Orbital Maneuvers Using Electrodynamic Tethers (AAS 05-206)