Virtual Exploration by Computing Global Families of Trajectories with Supercomputers (AAS 05-220)
Venus and Mars Gravity-Assist Trajectories to Jupiter Using Nuclear Electric Propulsion (AAS 05-112)
Using HANDS to Augment AFSCN Tracking (AAS 05-137)
Trust, Risk & Aerospace Software: Balance and Optimization (AAS 05-202)
Transforming Space Surveillance to Meet Today's Space Superiority Needs (AAS 05-201)
Trajectory Design and Maneuver Strategy for the MESSENGER Mission to Mercury (AAS 05-173)
Trajectories Leaving a Sphere in the Restricted 3-Body Problem (AAS 05-221)
Thrust Vector Control of the Jupiter Icy Moons Orbiter Spacecraft (AAS 05-114)
The Validation of SimFence - A Simulation of the Air Force Space Surveillance System (AAS 05-126)
Tethered Satellite Identification with Mixed Observation Data (AAS 05-229)
TECHNICAL NOTE - Accurate Orbit Determination from Short-Arc Dense Observational Data
Synodic and Relative Flower Constellations with Applications to Planetary Explorations (AAS 05-151)
Streets of Coverage Constellations to Minimize Revisit Time in Low Earth Orbit (AAS 05-154)
Strategies for Near Earth Object Impact Hazard Mitigation (AAS 05-147)
Static Equilibrium Configurations in GEO Coulomb Spacecraft Formations (AAS 05-104)
Speed and Accuracy Tests of the Variable-Step Stoermer-Cowell Integrator (AAS 05-172)
Space Standards, Rules, Innovation, and Inhibition (AAS 05-198)
Satellite Constellation Design for Earth Observation (AAS 05-148)
Safe or Emergency Fault Protection Approaches for Spacecraft (AAS 05-212)
Root Locus Analysis of Higher Order Repetitive Control (AAS 05-230)
Refinements to the Q-Law for Low-Thrust Orbit Transfers (AAS 05-162)
Recovery from a Period of Missed Thrust During a Low-Thrust Mission to Jupiter (AAS 05-177)
Reconnaissance Problem Using Genetic Algorithms (AAS 05-184)
Real-Time Computations of Time-Optimal Magnetic Attitude Control (AAS 05-233)
Public Risk Assessment of Off-Nominal Genesis Entries (AAS 05-224)
Primer Vector Optimization: Force Model Considerations (AAS 05-183)
Preliminary Orbit Determination of a Tethered Satellite Using Angles-Only Measurements (AAS 05-228)
Orbit Mechanics About Planetary Satellites Including Higher Order Gravity Fields (AAS 05-190)
Orbit Determination Results for the Cassini Titan-A Flyby (AAS 05-113)
Orbit Determination During High Thrust and Low Thrust Maneuvers (AAS 05-136)
Optimal Orbital Maneuvers Using Electrodynamic Tethers (AAS 05-206)
Optimal Low-Thrust Reconfiguration for Satellites in Formation (AAS 05-101)
Optimal Formation Control for Imaging and Fuel Usage (AAS 05-160)
Optimal Control of the Deployment/Retrieval of a Spinning Tethered Formation (AAS 05-207)
Optimal Configuration of Spacecraft Formations Via a Gauss Pseudospectral Method (AAS 05-103)