Table of Contents
Dynamics and Control for Surface Exploration of Small Bodies
ASC-1: Asteroid Missions and Asteroid Deflection • Monday, 18 August 2008 • 0900 hrs
Mirror Formation Control in the Vicinity of an Asteroid
ASC-1: Asteroid Missions and Asteroid Deflection • Monday, 18 August 2008 • 0900 hrs
Dynamics and Control of Gravity Tractor Spacecraft for Asteroid Deflection
ASC-1: Asteroid Missions and Asteroid Deflection • Monday, 18 August 2008 • 0900 hrs
Navigation Challenges of a Kinetic Energy Asteroid Deflection Spacecraft
ASC-1: Asteroid Missions and Asteroid Deflection • Monday, 18 August 2008 • 0900 hrs
Low-Thrust Trajectory Optimization Tool to Assess Options for Near-Earth Asteroid Deflection
ASC-1: Asteroid Missions and Asteroid Deflection • Monday, 18 August 2008 • 0900 hrs
Mission Design for a Kinetic-Energy Asteroid-Deflection Spacecraft
ASC-1: Asteroid Missions and Asteroid Deflection • Monday, 18 August 2008 • 0900 hrs
Spacecraft Formation Flying with an Earth-Crossing Object for Earth Impact Avoidance
ASC-1: Asteroid Missions and Asteroid Deflection • Monday, 18 August 2008 • 0900 hrs
Attitude Control on Two Wheels and No Gyros - The Past, Present, and Future of the TIMED Spacecraft
ASC-2: Attitude Dynamics and Control • Monday, 18 August 2008 • 0900 hrs
Locally Power-Optimal Spacecraft Attitude Control for Redundant Reaction Wheel Cluster
ASC-2: Attitude Dynamics and Control • Monday, 18 August 2008 • 0900 hrs
Spacecraft Attitude Sliding Mode Controller Using Reaction Wheels
ASC-2: Attitude Dynamics and Control • Monday, 18 August 2008 • 0900 hrs
Invariant Manifold Based Switching Control of Two-Dimensional Free-Flying Space Robot
ASC-2: Attitude Dynamics and Control • Monday, 18 August 2008 • 0900 hrs
Attitude Dynamics and Disturbances of the Advanced Land Observing Satellite (ALOS): Modeling, Identification, and Mitigation
ASC-2: Attitude Dynamics and Control • Monday, 18 August 2008 • 0900 hrs
Fine Pointing Performance of the STEREO Observatories
ASC-2: Attitude Dynamics and Control • Monday, 18 August 2008 • 0900 hrs
Attitude Determination by Magnetometer and Gyros During Eclipse
ASC-17: Attitude Sensing and Determination • Wednesday, 20 August 2008 • 0900 hrs
Development of a Low-Cost, Low-Power Attitude Determination System for a Nano-Satellite
ASC-17: Attitude Sensing and Determination • Wednesday, 20 August 2008 • 0900 hrs
Deterministic Relative Attitude Determination of Formation Flying Spacecraft
ASC-17: Attitude Sensing and Determination • Wednesday, 20 August 2008 • 0900 hrs
Orbital Express AVGS Validation and Calibration for Automated Rendezvous
ASC-17: Attitude Sensing and Determination • Wednesday, 20 August 2008 • 0900 hrs
A Practical Small Satellite Variable-Speed, Control Moment Gyroscope for Combined Energy Storage and Attitude Control
ASC-17: Attitude Sensing and Determination • Wednesday, 20 August 2008 • 0900 hrs
Navigational Use of Cassini Delta-V Telemetry
ASC-13: Cassini Mission • Tuesday, 19 August 2008 • 1400 hrs
Cassini Orbit Determination Results January 2006 - End of Prime Mission
ASC-13: Cassini Mission • Tuesday, 19 August 2008 • 1400 hrs
Communicating Navigation Data Inside the Cassini-Huygens Project: Visualizations and Tools
ASC-13: Cassini Mission • Tuesday, 19 August 2008 • 1400 hrs
Flyby Error Analysis Based on Contour Plots for the Cassini Tour
ASC-13: Cassini Mission • Tuesday, 19 August 2008 • 1400 hrs
In-Flight Modification ofthe Cassini Reference Trajectory
ASC-13: Cassini Mission • Tuesday, 19 August 2008 • 1400 hrs
Cassini-Huygens Maneuver Experience: Ending the Prime Mission
ASC-13: Cassini Mission • Tuesday, 19 August 2008 • 1400 hrs
Overview of the Cassini Extended Mission Trajectory
ASC-13: Cassini Mission • Tuesday, 19 August 2008 • 1400 hrs
Saturn Escape Options for Cassini Encore Missions
ASC-13: Cassini Mission • Tuesday, 19 August 2008 • 1400 hrs
Estimation of Nutation Time Constant Model Parameters for On-Axis Spinning Spacecraft
ASC-9: Dynamics and Control of Spinning Spacecraft • Tuesday, 19 August 2008 • 0900 hrs
Mission Experience Using New Attitude Tools for Spinning Spacecraft
ASC-9: Dynamics and Control of Spinning Spacecraft • Tuesday, 19 August 2008 • 0900 hrs
Design and Analysis of Passive Nutation Dampers for the RBSP Spacecraft
ASC-9: Dynamics and Control of Spinning Spacecraft • Tuesday, 19 August 2008 • 0900 hrs
A Practical Variable-Speed Control Moment Gyroscope Steering Law for Small Satellite Energy Storage and Attitude Control
ASC-9: Dynamics and Control of Spinning Spacecraft • Tuesday, 19 August 2008 • 0900 hrs
Advances in POST2 End-to-End Descent and Landing Simulation for the ALHAT Project
ASC-18: Entry, Descent, and Landing I • Wednesday, 20 August 2008 • 0900 hrs
Lunar Module Descent Mission Design
ASC-18: Entry, Descent, and Landing I • Wednesday, 20 August 2008 • 0900 hrs
Configuring the Deep Impact AutoNav System for Lunar, Comet and Mars Landing
ASC-18: Entry, Descent, and Landing I • Wednesday, 20 August 2008 • 0900 hrs
Optimal Precise Landing for Lunar Missions
ASC-18: Entry, Descent, and Landing I • Wednesday, 20 August 2008 • 0900 hrs
SuperSmart Parachute Deployment Algorithm for Mars Pinpoint Landing
ASC-18: Entry, Descent, and Landing I • Wednesday, 20 August 2008 • 0900 hrs
Desensitizing the Pin-Point Landing Trajectory on Mars
ASC-18: Entry, Descent, and Landing I • Wednesday, 20 August 2008 • 0900 hrs
Parametric Optimization and Guidance for an Aerogravity Assisted Atmospheric Sample Return From Mars and Venus
ASC-18: Entry, Descent, and Landing I • Wednesday, 20 August 2008 • 0900 hrs
Entry, Descent, and Landing Performance of the Mars Phoenix Lander
ASC-29: Entry, Descent, and Landing II • Thursday, 21 August 2008 • 1400 hrs
Multi-body Modeling and Simulation for the Mars Phoenix Lander Entry, Descent and Landing
ASC-29: Entry, Descent, and Landing II • Thursday, 21 August 2008 • 1400 hrs
Landing Site Dispersion Analysis and Statistical Assessment for the Mars Phoenix Lander
ASC-29: Entry, Descent, and Landing II • Thursday, 21 August 2008 • 1400 hrs
Entry, Descent, and Landing Operations Analysis for the Mars Phoenix Lander
ASC-29: Entry, Descent, and Landing II • Thursday, 21 August 2008 • 1400 hrs
Nonlinear Predictive Controller for Drag Tracking in Entry Guidance
ASC-29: Entry, Descent, and Landing II • Thursday, 21 August 2008 • 1400 hrs
Fault Tolerant Control Allocation for Mars Entry Vehicle using Adaptive Control
ASC-29: Entry, Descent, and Landing II • Thursday, 21 August 2008 • 1400 hrs
Multiple Model Adaptive Estimation for Inertial Navigation During Mars Entry
ASC-29: Entry, Descent, and Landing II • Thursday, 21 August 2008 • 1400 hrs
Mars Phoenix Entry, Descent, and Landing Simulation Design and Modeling Analysis
ASC-29: Entry, Descent, and Landing II • Thursday, 21 August 2008 • 1400 hrs
A Quadrature Based Method of Moments for Nonlinear Filtering
ASC-10: Estimation and Orbit Determination Theory • Tuesday, 19 August 2008 • 0900 hrs
Estimating Small-Body Gravity Field from Shape Model and Navigation Data
ASC-10: Estimation and Orbit Determination Theory • Tuesday, 19 August 2008 • 0900 hrs
Estimating Geometric Aspects of Relative Satellite Motion Using Angles-Only Measurements
ASC-10: Estimation and Orbit Determination Theory • Tuesday, 19 August 2008 • 0900 hrs
Linearized Relative State Estimation & Data Association for Orbit Determination of Clustered Geosynchronous Satellites
ASC-10: Estimation and Orbit Determination Theory • Tuesday, 19 August 2008 • 0900 hrs
Local Estimators for Multiple Spacecraft Formation Flying
ASC-10: Estimation and Orbit Determination Theory • Tuesday, 19 August 2008 • 0900 hrs
Relative Motion Estimator for the Shuttle Radar Topography Mission
ASC-10: Estimation and Orbit Determination Theory • Tuesday, 19 August 2008 • 0900 hrs
Stability and Control of Relative Equilibria of Three-Spacecraft Magnetically Tethered Systems
ASC-30: Formation Flying • Thursday, 21 August 2008 • 1400 hrs
Effects of Satellite Dimensions in the Solar Pressure Formulation for Formation Flying
ASC-30: Formation Flying • Thursday, 21 August 2008 • 1400 hrs
Formation Design and Sensitivity Analysis for the Magnetospheric Multiscale Mission (MMS)
ASC-30: Formation Flying • Thursday, 21 August 2008 • 1400 hrs
A Comparative Analysis of Control Techniques for Formation Flying Spacecraft in an Earth/Moon-Sun L2 Centered LISSAJOUS Orbit
ASC-30: Formation Flying • Thursday, 21 August 2008 • 1400 hrs
Formation Maintenance and Fuel Balancing for Satellites with Implusive Control
ASC-30: Formation Flying • Thursday, 21 August 2008 • 1400 hrs
Triangle Formation Design in Eccentric Orbits Using Pseudospectral Optimal Control
ASC-30: Formation Flying • Thursday, 21 August 2008 • 1400 hrs
Two-Craft Coulomb-Force Formation Dynamics and Stability Analysis with Debye Length Characteristics
ASC-30: Formation Flying • Thursday, 21 August 2008 • 1400 hrs
Electric Propulsion System Selection Process for Interplanetary Missions
ASC-31: Interplanetary Trajectory Design and Optimization • Thursday, 21 August 2008 • 1400 hrs
Algorithm for Low-Thrust Optimal Interplanetary Transfers with Escape and Capture Phases
ASC-31: Interplanetary Trajectory Design and Optimization • Thursday, 21 August 2008 • 1400 hrs
Application of Differential Transformation Based Algorithm to Find Optimal Interplanetary Low-Thrust Transfers
ASC-31: Interplanetary Trajectory Design and Optimization • Thursday, 21 August 2008 • 1400 hrs
Trajectory Design of Solar Probe+ Using Multiple Venus Gravity Assists
ASC-31: Interplanetary Trajectory Design and Optimization • Thursday, 21 August 2008 • 1400 hrs
Trajectory Optimization for a Mission to Neptune and Triton
ASC-31: Interplanetary Trajectory Design and Optimization • Thursday, 21 August 2008 • 1400 hrs
Maneuver Design Strategy Enables Precise Targeting of the First MESSENGER Mercury Flyby
ASC-31: Interplanetary Trajectory Design and Optimization • Thursday, 21 August 2008 • 1400 hrs
Planetary Protection Trajectory Analysis for the Juno Mission
ASC-31: Interplanetary Trajectory Design and Optimization • Thursday, 21 August 2008 • 1400 hrs
Launch Period Development for the Juno Mission to Jupiter
ASC-31: Interplanetary Trajectory Design and Optimization • Thursday, 21 August 2008 • 1400 hrs
Mars Reconnaissance Orbiter Navigation During the Primary Science Phase
ASC-5: Missions to Mars • Monday, 18 August 2008 • 1400 hrs
Elliptical Parking Orbits for Mars Sample Return
ASC-5: Missions to Mars • Monday, 18 August 2008 • 1400 hrs
Enhancements on the Convex Programming Based Powered Descent Guidance Algorithm for Mars Landing
ASC-5: Missions to Mars • Monday, 18 August 2008 • 1400 hrs
Effects of Atmospheric Phenomena on Mars Science Laboratory Entry Performance
ASC-5: Missions to Mars • Monday, 18 August 2008 • 1400 hrs
Thermal Protection Tradeoffs for Ballute versus Aeroshell Entry and Descent at Mars
ASC-5: Missions to Mars • Monday, 18 August 2008 • 1400 hrs
Quasi-Synchronous Orbits Around Phobos in the Context of a Phobos Sample Return Mission
ASC-5: Missions to Mars • Monday, 18 August 2008 • 1400 hrs
Iterated Analytical Solution to the Restricted Problem of Three Bodies
ASC-6: N-Body and 3-Body Dynamics and Missions • Monday, 18 August 2008 • 1400 hrs
Stability Mapping of Distant Retrograde Orbits and Transports in the Circular Restricted Three-Body Problem
ASC-6: N-Body and 3-Body Dynamics and Missions • Monday, 18 August 2008 • 1400 hrs
Dynamically Relevant Local Coordinates for Halo Orbits
ASC-6: N-Body and 3-Body Dynamics and Missions • Monday, 18 August 2008 • 1400 hrs
Families of Cycler Trajectories in the Earth-Moon System
ASC-6: N-Body and 3-Body Dynamics and Missions • Monday, 18 August 2008 • 1400 hrs
Actuator Constrained Optimal Control of Formations Near the Libration Points
ASC-6: N-Body and 3-Body Dynamics and Missions • Monday, 18 August 2008 • 1400 hrs
Spacecraft Trajectory Design Strategies Based on Close Encounters with a Smaller Primary in a 4-Body Model
ASC-6: N-Body and 3-Body Dynamics and Missions • Monday, 18 August 2008 • 1400 hrs
NASA's Planned Return to the Moon: Global Access and Anytime Return Requirement Implications on the Lunar Orbit Insertion Burns
ASC-6: N-Body and 3-Body Dynamics and Missions • Monday, 18 August 2008 • 1400 hrs
Fusion Tracking Filter for the Flight Safety System of a Space Launch Vehicle
ASC-32: Operational Orbit Determination and Debris • Thursday, 21 August 2008 • 1400 hrs
The Use of GMSEC Architecture for Multi-Mission Flight Dynamics Orbit and Attitude Support
ASC-32: Operational Orbit Determination and Debris • Thursday, 21 August 2008 • 1400 hrs
Reconstruction of the Voyager 2 Neptune Encounter in the ICRF System
ASC-32: Operational Orbit Determination and Debris • Thursday, 21 August 2008 • 1400 hrs
Kaguya Orbit Determination from JPL
ASC-32: Operational Orbit Determination and Debris • Thursday, 21 August 2008 • 1400 hrs
Orbit Determination During Spacecraft Emergencies with Sparse Tracking Data: THEMIS and TDRS-3 Lessons Learned
ASC-32: Operational Orbit Determination and Debris • Thursday, 21 August 2008 • 1400 hrs
Consequences of Debris Events in Geosynchronous Orbit
ASC-32: Operational Orbit Determination and Debris • Thursday, 21 August 2008 • 1400 hrs
Lifetime Reduction for Highly Inclined, Highly Eccentric Disposal Orbits by Changing Inclination
ASC-32: Operational Orbit Determination and Debris • Thursday, 21 August 2008 • 1400 hrs
Identification of Solid Rocket Motor Retro-Burns in the LDEF IDE Impact Data
ASC-32: Operational Orbit Determination and Debris • Thursday, 21 August 2008 • 1400 hrs
Stellar Positioning System Part I: Applying Ancient Theory to a Modern World
ASC-14: Optical Navigation • Tuesday, 19 August 2008 • 1400 hrs
Stellar Positioning System Part II: Overcoming Error During Implementation
ASC-14: Optical Navigation • Tuesday, 19 August 2008 • 1400 hrs
LinCov Analysis of an Automated Celestial Inertial Navigation Approach for GEO Satellites
ASC-14: Optical Navigation • Tuesday, 19 August 2008 • 1400 hrs
Autonomous Mid-Course Navigation for Lunar Return
ASC-14: Optical Navigation • Tuesday, 19 August 2008 • 1400 hrs
Celestial Navigation (CelNav): Lunar Surface Navigation
ASC-14: Optical Navigation • Tuesday, 19 August 2008 • 1400 hrs
Optical Navigation for Lunar Transportation Systems Contingency Scenarios
ASC-14: Optical Navigation • Tuesday, 19 August 2008 • 1400 hrs
Navigation for the MESSENGER Mission's First Mercury Encounter
ASC-14: Optical Navigation • Tuesday, 19 August 2008 • 1400 hrs
A Statistical Analysis of Spacecraft Maneuvers for a Deep Space Mission
ASC-25: Orbit Maneuvers and Maintenance • Thursday, 21 August 2008 • 0900 hrs
Maneuvers for Maximal Changes to Orbital Geometry
ASC-25: Orbit Maneuvers and Maintenance • Thursday, 21 August 2008 • 0900 hrs
Autonomous Orbit Maintenance Law for LEO Sun Synchronous, Earth Repeating Satellites with Electric Propulsion System
ASC-25: Orbit Maneuvers and Maintenance • Thursday, 21 August 2008 • 0900 hrs
Mutual Interactions Between Drag Make-Up and Mean Local Time Maneuver Designs
ASC-25: Orbit Maneuvers and Maintenance • Thursday, 21 August 2008 • 0900 hrs
Landsat 5 World Reference System Error Investigation
ASC-25: Orbit Maneuvers and Maintenance • Thursday, 21 August 2008 • 0900 hrs
Effects of Libration on General Electrodynamic Tether Orbital Maneuvers
ASC-25: Orbit Maneuvers and Maintenance • Thursday, 21 August 2008 • 0900 hrs
AstroHD: Astrodynamics Modeling With a Distinctly Digital Flavor
ASC-21: Orbit Perturbations • Wednesday, 20 August 2008 • 1400 hrs
Progress in Modeling the Sources of Error in Orbital Predictions
ASC-21: Orbit Perturbations • Wednesday, 20 August 2008 • 1400 hrs
A Symplectic Keplerian Map for Perturbed Two-Body Dynamics
ASC-21: Orbit Perturbations • Wednesday, 20 August 2008 • 1400 hrs
Stability of Highly Elliptical Orbits at the Moon
ASC-21: Orbit Perturbations • Wednesday, 20 August 2008 • 1400 hrs
Decade-Scale GPS Orbit Evolution and Third Body Perturbations
ASC-21: Orbit Perturbations • Wednesday, 20 August 2008 • 1400 hrs
Detecting Body Tides and Librations of Europa with an Altimetric Exploration Mission
ASC-26: Orbit Perturbations in a Non-Earth Environment • Thursday, 21 August 2008 • 0900 hrs
Improved force modeling on Mars-Orbiting spacecraft
ASC-26: Orbit Perturbations in a Non-Earth Environment • Thursday, 21 August 2008 • 0900 hrs
Spacecraft Dynamics in the Vicinity of a Comet in a Rotating Frame
ASC-26: Orbit Perturbations in a Non-Earth Environment • Thursday, 21 August 2008 • 0900 hrs
Characterization of Spacecraft and Debris Trajectory Stability within Binary Asteroid Systems
ASC-26: Orbit Perturbations in a Non-Earth Environment • Thursday, 21 August 2008 • 0900 hrs
Structure Preserving Approximations of Conservative Forces for Application to Small Body Dynamics
ASC-26: Orbit Perturbations in a Non-Earth Environment • Thursday, 21 August 2008 • 0900 hrs
Dynamics of Lorentz Spacecraft with Application to a Mission to Enceladus
ASC-26: Orbit Perturbations in a Non-Earth Environment • Thursday, 21 August 2008 • 0900 hrs
Titan Explorer
ASC-22: Planetary Moon Mission Design and Optimization • Wednesday, 20 August 2008 • 1400 hrs
On the Design of an Enceladus Science Orbit
ASC-22: Planetary Moon Mission Design and Optimization • Wednesday, 20 August 2008 • 1400 hrs
The Lunar Polesitter
ASC-22: Planetary Moon Mission Design and Optimization • Wednesday, 20 August 2008 • 1400 hrs
Fuel-Optimal Design of Moon-Earth Trajectories Using Legendre Pseudospectral Method
ASC-22: Planetary Moon Mission Design and Optimization • Wednesday, 20 August 2008 • 1400 hrs
Indirect Optimization of Low Earth Orbit to Low Lunar Orbit Transfers
ASC-22: Planetary Moon Mission Design and Optimization • Wednesday, 20 August 2008 • 1400 hrs
Transit from Low Earth Orbit to Lunar Orbit: One Month's Velocity Change (Delta-V) Requirements and a Sensitivity Study
ASC-22: Planetary Moon Mission Design and Optimization • Wednesday, 20 August 2008 • 1400 hrs
Analysis of Lorentz Spacecraft Motion about Earth Using the Hill-Clohessy-Wiltshire Equations
ASC-15: Relative Motion and Rendezvous Missions • Tuesday, 19 August 2008 • 1400 hrs
Propagation of the Relative Satellite Motion in a Formation in the Presence of Gravitational Perturbations
ASC-15: Relative Motion and Rendezvous Missions • Tuesday, 19 August 2008 • 1400 hrs
A Quaternionic Exact Solution to the Relative Orbital Motion
ASC-15: Relative Motion and Rendezvous Missions • Tuesday, 19 August 2008 • 1400 hrs
Analysis of Automated Rendezvous and Docking Operations
ASC-15: Relative Motion and Rendezvous Missions • Tuesday, 19 August 2008 • 1400 hrs
HTV Guidance, Navigation and Control System Design for Safe Robotics Capture
ASC-15: Relative Motion and Rendezvous Missions • Tuesday, 19 August 2008 • 1400 hrs
Orbital Express Autonomous Rendezvous and Capture Flight Operations, Part 2 of 2: AR&C Exercise 4,5, and End-Of-Life
ASC-15: Relative Motion and Rendezvous Missions • Tuesday, 19 August 2008 • 1400 hrs
Static Formations Using Momentum Exchange Between Satellites
ASC-15: Relative Motion and Rendezvous Missions • Tuesday, 19 August 2008 • 1400 hrs
Relating Satellite Coverage to Orbital Geometry
ASC-11: Satellite Constellations • Tuesday, 19 August 2008 • 0900 hrs
Pareto-Hypervolumes for the Reconfiguration of Satellite Constellations
ASC-11: Satellite Constellations • Tuesday, 19 August 2008 • 0900 hrs
Responsive Imaging Constellations for Support of Geographically Dispersed Theaters
ASC-11: Satellite Constellations • Tuesday, 19 August 2008 • 0900 hrs
Integration of Flight Dynamics Systems (FDS) with Integrated Trending and Plotting System (ITPS)
ASC-11: Satellite Constellations • Tuesday, 19 August 2008 • 0900 hrs
Summary Comments on the Atmosphere Density Tracking Study Stage 1 and Stage 2 Reports
ASC-27: Sensor Concepts and Utilization • Thursday, 21 August 2008 • 0900 hrs
Spacecraft Attitude Determination from Imagery
ASC-27: Sensor Concepts and Utilization • Thursday, 21 August 2008 • 0900 hrs
Covariance-Based Uncorrelated Track Association
ASC-27: Sensor Concepts and Utilization • Thursday, 21 August 2008 • 0900 hrs
Architecting the Very-Large-Aperture Flux-Pinned Space Telescope: A Scalable, Modular Optical Array with High Agility and Passively Stable Orbital Dynamics
ASC-27: Sensor Concepts and Utilization • Thursday, 21 August 2008 • 0900 hrs
Control of Spacecraft Occulter Arrays in Multi-Body Regimes
ASC-27: Sensor Concepts and Utilization • Thursday, 21 August 2008 • 0900 hrs
Prospects and Challenges of Particulate Solar Sail Propulsion
ASC-23: Solar Sail Trajectories and Applications • Wednesday, 20 August 2008 • 1400 hrs
Solar Sail Technology for Nanosatellites
ASC-23: Solar Sail Trajectories and Applications • Wednesday, 20 August 2008 • 1400 hrs
Solar Sails and Lunar South Pole Coverage
ASC-23: Solar Sail Trajectories and Applications • Wednesday, 20 August 2008 • 1400 hrs
Solar Reflector Gravity Tractor for Asteroid Collision Avoidance
ASC-23: Solar Sail Trajectories and Applications • Wednesday, 20 August 2008 • 1400 hrs
Periodic and Quasi-Periodic Motions of a Solar Sail on the Sun-Earth System
ASC-23: Solar Sail Trajectories and Applications • Wednesday, 20 August 2008 • 1400 hrs
SGP4 Orbit Determination
ASC-16: Space Surveillance and Conjunction Assessment • Tuesday, 19 August 2008 • 1400 hrs
Improvement of the TLE Accuracy Model Based on a Gaussian Mixture Depending on the Propagation Duration
ASC-16: Space Surveillance and Conjunction Assessment • Tuesday, 19 August 2008 • 1400 hrs
Space Catalogue Accuracy Modeling Simplifications
ASC-16: Space Surveillance and Conjunction Assessment • Tuesday, 19 August 2008 • 1400 hrs
Using Probability of Collision as a Metric for Space Surveillance Force Mix Analysis
ASC-16: Space Surveillance and Conjunction Assessment • Tuesday, 19 August 2008 • 1400 hrs
Short Term Consequences of Orbital Debris Events (An Orbital Debris Toolset)
ASC-16: Space Surveillance and Conjunction Assessment • Tuesday, 19 August 2008 • 1400 hrs
Autonomous Quality Space Imagery for LEO/GEO Space Operations
ASC-16: Space Surveillance and Conjunction Assessment • Tuesday, 19 August 2008 • 1400 hrs
Comparison of the Extended and Unscented Kalman Filters for Angles Based Relative Navigation
ASC-24: Spacecraft Guidance, Navigation, and Control • Wednesday, 20 August 2008 • 1400 hrs
An Evaluation and Comparison of Autonomous Orbit Transfer Controllers for the NASA Magnetospheric MultiScale Satellite
ASC-24: Spacecraft Guidance, Navigation, and Control • Wednesday, 20 August 2008 • 1400 hrs
Verification of Pointing Constraints for the Dawn Spacecraft
ASC-24: Spacecraft Guidance, Navigation, and Control • Wednesday, 20 August 2008 • 1400 hrs
Autonomous and Precise Navigation of the Proba-2 Spacecraft
ASC-24: Spacecraft Guidance, Navigation, and Control • Wednesday, 20 August 2008 • 1400 hrs
Autonomous GNC Algorithms for Rendezvous Missions to Near-Earth-Objects
ASC-24: Spacecraft Guidance, Navigation, and Control • Wednesday, 20 August 2008 • 1400 hrs
Response Characteristics of Orbit-Mean Satellite Drag to Varying Geomagnetic Conditions
ASC-19: Special Session: Atmospheric Density Analysis • Wednesday, 20 August 2008 • 0900 hrs
Thermospheric Density Modeling During Magnetic Storms
ASC-19: Special Session: Atmospheric Density Analysis • Wednesday, 20 August 2008 • 0900 hrs
Analysis of High Latitude Localized Neutral Density Variations
ASC-19: Special Session: Atmospheric Density Analysis • Wednesday, 20 August 2008 • 0900 hrs
Latitudinal and Diurnal Variations of Neutral Density for Quiet Geomagnetic Conditions
ASC-19: Special Session: Atmospheric Density Analysis • Wednesday, 20 August 2008 • 0900 hrs
Thermospheric Densities from Analysis of 6-Year GRACE Accelerometer Data
ASC-19: Special Session: Atmospheric Density Analysis • Wednesday, 20 August 2008 • 0900 hrs
Results from the Atmospheric Neutral Density Experiment Risk Reduction Mission
ASC-19: Special Session: Atmospheric Density Analysis • Wednesday, 20 August 2008 • 0900 hrs
Calibrating Precision Orbit Derived Total Density
ASC-19: Special Session: Atmospheric Density Analysis • Wednesday, 20 August 2008 • 0900 hrs
A New Empirical Thermospheric Density Model JB2008 Using New Solar and Geomagnetic Indices
ASC-7: Special Session: Atmospheric Density Modeling • Monday, 18 August 2008 • 1400 hrs
A Blending Technique in Thermospheric Density Modeling
ASC-7: Special Session: Atmospheric Density Modeling • Monday, 18 August 2008 • 1400 hrs
A Critical Assessment of Satellite Drag and Atmospheric Density Modeling
ASC-7: Special Session: Atmospheric Density Modeling • Monday, 18 August 2008 • 1400 hrs
Sensitivity of Orbit Predictions to Density Variability
ASC-7: Special Session: Atmospheric Density Modeling • Monday, 18 August 2008 • 1400 hrs
A Formulation of the Clohessy-Wiltshire Equations to Include Dynamic Atmospheric Drag
ASC-7: Special Session: Atmospheric Density Modeling • Monday, 18 August 2008 • 1400 hrs
Satellite Fragmentation Modeling with IMPACT
ASC-3: Special Session: Chinese Anti-Satellite Test • Monday, 18 August 2008 • 0900 hrs
Fengyun-1C Orbital Debris Cloud Short-Term Risk Analysis
ASC-3: Special Session: Chinese Anti-Satellite Test • Monday, 18 August 2008 • 0900 hrs
Debris Cloud Visualization
ASC-3: Special Session: Chinese Anti-Satellite Test • Monday, 18 August 2008 • 0900 hrs
Debris Risk Assessment Process
ASC-3: Special Session: Chinese Anti-Satellite Test • Monday, 18 August 2008 • 0900 hrs
Navigation Challenges of the Mars Phoenix Lander Mission
ASC-28: Special Session: Mars Phoenix Lander • Thursday, 21 August 2008 • 0900 hrs
Orbit Determination for the 2007 Mars Phoenix Lander
ASC-28: Special Session: Mars Phoenix Lander • Thursday, 21 August 2008 • 0900 hrs
Propulsive Maneuver Design for the 2007 Mars Phoenix Lander Mission
ASC-28: Special Session: Mars Phoenix Lander • Thursday, 21 August 2008 • 0900 hrs
NASA Phoenix 2007 Mars Lander Thruster Calibration Estimator: Design and Validation
ASC-28: Special Session: Mars Phoenix Lander • Thursday, 21 August 2008 • 0900 hrs
Overview of the Phoenix Entry, Descent and Landing System Architecture
ASC-28: Special Session: Mars Phoenix Lander • Thursday, 21 August 2008 • 0900 hrs
Aerodynamics for the Mars Phoenix Entry Capsule
ASC-28: Special Session: Mars Phoenix Lander • Thursday, 21 August 2008 • 0900 hrs
Analysis of effectiveness of Phoenix Entry Reaction Control System
ASC-28: Special Session: Mars Phoenix Lander • Thursday, 21 August 2008 • 0900 hrs
Global Low-Thrust Trajectory Optimization Through Hybridization of a Genetic Algorithm and a Direct Method
ASC-12: Techniques for Low-Thrust Trajectory Optimization I • Tuesday, 19 August 2008 • 0900 hrs
A Hybrid Differential Dynamic Programming Algorithm for Robust Low-Thrust Optimization
ASC-12: Techniques for Low-Thrust Trajectory Optimization I • Tuesday, 19 August 2008 • 0900 hrs
Shape-Based Approximation Method for Low-Thrust Trajectory Optimization
ASC-12: Techniques for Low-Thrust Trajectory Optimization I • Tuesday, 19 August 2008 • 0900 hrs
Trajectory Optimization Using the Reduced Eccentric Anomaly Low-Thrust Coefficients
ASC-12: Techniques for Low-Thrust Trajectory Optimization I • Tuesday, 19 August 2008 • 0900 hrs
Preliminary Findings Concerning Applications of Non-Linear Constrained Optimization Methods on Low-Thrust Orbit Transfers
ASC-12: Techniques for Low-Thrust Trajectory Optimization I • Tuesday, 19 August 2008 • 0900 hrs
A Graphical Method for Preliminary Design of Low-Thrust Gravity-Assist Trajectories
ASC-20: Techniques for Low-Thrust Trajectory Optimization II • Wednesday, 20 August 2008 • 0900 hrs
Geometric Interpretation of Adjoint Equations in Optimal Low Thrust Trajectories
ASC-20: Techniques for Low-Thrust Trajectory Optimization II • Wednesday, 20 August 2008 • 0900 hrs
Low-Thrust Transfers Using Primer Vector Theory and a Second-Order Penalty Method
ASC-20: Techniques for Low-Thrust Trajectory Optimization II • Wednesday, 20 August 2008 • 0900 hrs
High-Order Equality Constraint Tracking Algorithm for Nonlinear Optimization
ASC-20: Techniques for Low-Thrust Trajectory Optimization II • Wednesday, 20 August 2008 • 0900 hrs
High Speed Solution of Spacecraft Trajectory Problems Using Taylor Series Integration
ASC-20: Techniques for Low-Thrust Trajectory Optimization II • Wednesday, 20 August 2008 • 0900 hrs
Beyond Newton's Method: Generalized Higher-Order Approximation Methods
ASC-4: Techniques for Trajectory Optimization • Monday, 18 August 2008 • 0900 hrs
Guess-Free Trajectory Optimization
ASC-4: Techniques for Trajectory Optimization • Monday, 18 August 2008 • 0900 hrs
A Novel Coordinate Transformation for Obstacle Avoidance and Optimal Trajectory Planning
ASC-4: Techniques for Trajectory Optimization • Monday, 18 August 2008 • 0900 hrs
Path-Constrained Trajectory Optimization for Proximity Operations
ASC-4: Techniques for Trajectory Optimization • Monday, 18 August 2008 • 0900 hrs
Spacecraft Trajectory Optimization Based on Discrete Sets of Pseudo-Impulses
ASC-4: Techniques for Trajectory Optimization • Monday, 18 August 2008 • 0900 hrs
On Testing Global Optimization Algorithms for Space Trajectory Design
ASC-4: Techniques for Trajectory Optimization • Monday, 18 August 2008 • 0900 hrs
FIRE: A Fast, Accurate, and Smooth Planetary Body Ephemeris Interpolation System
ASC-4: Techniques for Trajectory Optimization • Monday, 18 August 2008 • 0900 hrs
Mechanics of a Very Long Tethered System
ASC-33: Tether Dynamics • Thursday, 21 August 2008 • 1400 hrs
On the Dynamics of a Tethered System Near the Collineal Libration Points
ASC-33: Tether Dynamics • Thursday, 21 August 2008 • 1400 hrs
Conditions for Tether Collapse after Payload Separation of a Reusable Spinning Tether
ASC-33: Tether Dynamics • Thursday, 21 August 2008 • 1400 hrs
Climber Motion Optimization for the Tethered Space Elevator
ASC-33: Tether Dynamics • Thursday, 21 August 2008 • 1400 hrs
Io Exploration with Electrodynamic Tethers
ASC-33: Tether Dynamics • Thursday, 21 August 2008 • 1400 hrs
First Mission Results of the YES2 Tethered SpaceMail Experiment
ASC-33: Tether Dynamics • Thursday, 21 August 2008 • 1400 hrs
Method to Maintain Artificial Gravity During Transfer Maneuvers for Tethered Spacecraft
ASC-33: Tether Dynamics • Thursday, 21 August 2008 • 1400 hrs
Improved Repetitive Control Filter Design for Both Learning Frequency Cutoff and Interpolation
ASC-8: Topics in Spacecraft Dynamics and Control • Monday, 18 August 2008 • 1400 hrs
Designing Iterative Learning Control Subject to Actuator Limitations Using QP Methods
ASC-8: Topics in Spacecraft Dynamics and Control • Monday, 18 August 2008 • 1400 hrs
Bellman Pseudospectral Method
ASC-8: Topics in Spacecraft Dynamics and Control • Monday, 18 August 2008 • 1400 hrs
An Initial Examination of Using Pseudospectral Methods for Timescale and Differential Geometric Analysis of Nonlinear Optimal Control Problems
ASC-8: Topics in Spacecraft Dynamics and Control • Monday, 18 August 2008 • 1400 hrs
Passive Vertical Stabilization of Two Tethered Nanosatellites with Engineered Damping
ASC-8: Topics in Spacecraft Dynamics and Control • Monday, 18 August 2008 • 1400 hrs
Time and Frequency Domain Evaluation of Settling Time in Repetitive Control
ASC-8: Topics in Spacecraft Dynamics and Control • Monday, 18 August 2008 • 1400 hrs
On the Ill-Conditioning in MPC when used to Address the Repetitive Control Problem
ASC-8: Topics in Spacecraft Dynamics and Control • Monday, 18 August 2008 • 1400 hrs
High-Order State and Parameter Transition Tensor Calculations
ASC-8: Topics in Spacecraft Dynamics and Control • Monday, 18 August 2008 • 1400 hrs