NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Proceedings of the 20th International Symposium on Space Flight DynamicsTopics include: Measuring Image Navigation and Registration Performance at the 3-Sigma Level Using Platinum Quality Landmarks; Flight Dynamics Performances of the MetOp A Satellite during the First Months of Operations; Visual Navigation - SARE Mission; Determining a Method of Enabling and Disabling the Integral Torque in the SDO Science and Inertial Mode Controllers; Guaranteeing Pointing Performance of the SDO Sun-Pointing Controllers in Light of Nonlinear Effects; SDO Delta H Mode Design and Analysis; Observing Mode Attitude Controller for the Lunar Reconnaissance Orbiter; Broken-Plane Maneuver Applications for Earth to Mars Trajectories; ExoMars Mission Analysis and Design - Launch, Cruise and Arrival Analyses; Mars Reconnaissance Orbiter Aerobraking Daily Operations and Collision Avoidance; Mars Reconnaissance Orbiter Interplanetary Cruise Navigation; Motion Parameters Determination of the SC and Phobos in the Project Phobos-Grunt; GRAS NRT Precise Orbit Determination: Operational Experience; Orbit Determination of LEO Satellites for a Single Pass through a Radar: Comparison of Methods; Orbit Determination System for Low Earth Orbit Satellites; Precise Orbit Determination for ALOS; Anti-Collision Function Design and Performances of the CNES Formation Flying Experiment on the PRISMA Mission; CNES Approaching Guidance Experiment within FFIORD; Maneuver Recovery Analysis for the Magnetospheric Multiscale Mission; SIMBOL-X: A Formation Flying Mission on HEO for Exploring the Universe; Spaceborne Autonomous and Ground Based Relative Orbit Control for the TerraSAR-X/TanDEM-X Formation; First In-Orbit Experience of TerraSAR-X Flight Dynamics Operations; Automated Target Planning for FUSE Using the SOVA Algorithm; Space Technology 5 Post-Launch Ground Attitude Estimation Experience; Standardizing Navigation Data: A Status Update; and A Study into the Method of Precise Orbit Determination of a HEO Orbiter by GPS and Accelerometer.
Document ID
20080012629
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Proceedings
Authors
Woodard, Mark (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Stengle, Tom
Date Acquired
August 24, 2013
Publication Date
September 24, 2007
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/CP-2007-214158
Meeting Information
Meeting: 20th International Symposium on Space Flight Dynamics
Location: Annapolis, MD
Country: United States
Start Date: September 24, 2007
End Date: September 28, 2007
Sponsors: NASA Goddard Space Flight Center
Distribution Limits
Public
Copyright
Public Use Permitted.

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle20080012649WorkModeling and Flight Data Analysis of Spacecraft Dynamics with a Large Solar Array Paddle20080012727WorkDetection of Orbital Debris Collision Risks for the Automated Transfer Vehicle20080012648WorkJitter Test Program and On-Orbit Mitigation Strategies for Solar Dynamic Observatory20080012641WorkEstablishing a Near Term Lunar Farside Gravity Model via Inexpensive Add-on Navigation Payload20080012717WorkSpaceborne Autonomous and Ground Based Relative Orbit Control for the TerraSAR-X/TanDEM-X Formation20080012695WorkEffects on Spacecraft Radiometric Data at Superior Solar Conjunction20080012658WorkSTEREO Mission Design20080012647WorkControl of Formation-Flying Multi-Element Space Interferometers with Direct Interferometer-Output Feedback20080012657WorkCoronas-F Orbit Monitoring and Re-Entry Prediction20080012709WorkComparing Consider-Covariance Analysis with Sigma-Point Consider Filter and Linear-Theory Consider Filter Formulations20080012666WorkPrecise Orbit Determination for ALOS20080012683WorkStationkeeping for the Lunar Reconnaissance Orbiter (LRO)20080012704WorkGame Theoretic Approach to Post-Docked Satellite Control20080012659WorkOptimal Electrodynamic Tether Phasing Maneuvers20080012660WorkTime-Varying Expression of the Formation Flying along Circular Trajectories20080012684WorkAnalysis of Capture Trajectories to the Vicinity of Libration Points20080012719WorkGPS-Based Reduced Dynamic Orbit Determination Using Accelerometer Data20080012681WorkBoeing Low-Thrust Geosynchronous Transfer Mission Experience20080012653WorkSpace Technology 5 Post-Launch Ground Attitude Estimation Experience20080012691WorkTrajectory Design and Orbit Determination for the Lunar CRater Observation and Sensing Satellite (LCROSS)20080012645WorkCNES Approaching Guidance Experiment within FFIORD20080012689WorkHill Problem Analytical Theory to the Order Four. Application to the Computation of Frozen Orbits around Planetary Satellites20080012672WorkA Study into the Method of Precise Orbit Determination of a HEO Orbiter by GPS and Accelerometer20080012711WorkImpacts of Center of Mass Shifts on Messenger Spacecraft Operations20080012720WorkGuaranteeing Pointing Performance of the SDO Sun-Pointing Controllers in Light of Nonlinear Effects20080012696WorkEvolution of the Debris Cloud Generated by the Fengyun-1C Fragmentation Event20080012694WorkAnalysis of Envisat Orbit Maintenance Strategies to Improve/Increase Envisat ASAR Interferometry Opportunities20080012635WorkSolar Cycle #24 and the Solar Dynamo20080012655WorkMeasuring Image Navigation and Registration Performance at the 3-Sigma Level Using Platinum Quality Landmarks20080012663WorkGRAS NRT Precise Orbit Determination: Operational Experience20080012643WorkA General Approach to the Geostationary Transfer Orbit Mission Recovery20080012703WorkMotion Parameters Determination of the SC and Phobos in the Project Phobos-Grunt20080012634WorkImplementation of Satellite Formation Flight Algorithms Using SPHERES Aboard the International Space Station20080012682WorkLow-Thrust Control of a Lunar Mapping Orbit20080012640WorkTopology of the Relative Motion: Circular and Eccentric Reference Orbit Cases20080012630WorkRosetta Navigation at its Mars Swing-By20080012702WorkMars Reconnaissance Orbiter Interplanetary Cruise Navigation20080012723WorkGaining Confidence in Navigating Rosetta at Mars Swing-By20080012667WorkLong Term Mean Local Time of the Ascending Node Prediction20080012662WorkSDO Delta H Mode Design and Analysis20080012679WorkSIMBOL-X: A Formation Flying Mission on HEO for Exploring the Universe20080012726WorkMulti-Objective Online Initialization of Spacecraft Formations20080012677WorkDeep Space Transportation System Using the Sun-Earth L2 Point20080012637WorkGalileo Station Keeping Strategy20080012714WorkEstimation of Cometary Rotation Parameters Based on Camera Images20080012728WorkOrbit Determination and Navigation of the Solar Terrestrial Relations Observatory (STEREO)20080012687WorkSolar Dynamics Observatory High Gain Antenna Handover Planning20080012631WorkGuidance Algorithms for Non-Drifting Trajectory Generation and Control in RendezVous Missions into Elliptical Orbits20080012729WorkFirst In-Orbit Experience of TerraSAR-X Flight Dynamics Operations20080012664WorkZero-Propellant Maneuver[TM] Flight Results for 180 deg ISS Rotation20080012638WorkMission Analysis for the Don Quijote Phase-A Study20080012688WorkAnalysis Method for Non-Nominal First Acquisition20080012705WorkStandardizing Navigation Data: A Status Update20080012710WorkContingency Support Simulation for the Tracking and Data Relay Satellite System (TDRSS)20080012674WorkSemianalytical Propagation of Satellite Orbits about an Arbitrary Central Body20080012652WorkAutomated Target Planning for FUSE Using the SOVA Algorithm20080012724WorkFuel-Optimal Trajectories in a Planet-Moon Environment Using Multiple Gravity Assists20080012686WorkDesign and Analysis of a Formation Flying System for the Cross-Scale Mission Concept20080012715WorkThe METOP-A Orbit Acquisition Strategy and its LEOP Operational Experience20080012718WorkAnalytical Approach Validation for the Spin-Stabilized Satellite Attitude20080012678WorkExoMars Mission Analysis and Design - Launch, Cruise and Arrival Analyses20080012722WorkTracking and Data Relay Satellite (TDRS) Orbit Estimation Using an Extended Kalman Filter20080012713WorkA Jitter-Mitigating High Gain Antenna Pointing Algorithm for the Solar Dynamics Observatory20080012661WorkOptimal Low-Thrust Limited-Power Transfers between Arbitrary Elliptic Coplanar Orbits20080012669WorkMission Design for NASA's Inner Heliospheric Sentinels and ESA's Solar Orbiter Missions20080012633WorkExpanding Hardware-in-the-Loop Formation Navigation and Control with Radio Frequency Crosslink Ranging20080012675WorkAnti-Collision Function Design and Performances of the CNES Formation Flying Experiment on the PRISMA Mission20080012730WorkAttitude Sensor and Gyro Calibration for Messenger20080012642WorkFlight Mechanics of the Entry, Descent and Landing of the ExoMars Mission20080012676WorkOrbit Determination of LEO Satellites for a Single Pass through a Radar: Comparison of Methods20080012700WorkTransfer to the Collinear Libration Point L3 in the Sun-Earth+Moon System20080012698WorkGPS-Based Precision Baseline Reconstruction for the TanDEM-X SAR-Formation20080012725WorkOrbit Mechanics about Small Asteroids20080012670WorkProximity Navigation of Highly Constrained Spacecraft20080012708WorkAutonomous On-Board Calibration of Attitude Sensors and Gyros20080012656WorkFlight Dynamics Performances of the MetOp A Satellite during the First Months of Operations20080012685WorkA Multibody Slosh Analysis for the Lunar Reconnaissance Orbiter20080012651WorkThe Determination of Titan Gravity Field from Doppler Tracking of the Cassini Spacecraft20080012650WorkOperational Experience with Autonomous Star Trackers on ESA Interplanetary Spacecraft20080012646WorkCluster: Mission Overview and End-of-Life Analysis20080012680WorkBroken-Plane Maneuver Applications for Earth to Mars Trajectories20080012692WorkOptimization of Return Trajectories for Orbital Transfer Vehicle between Earth and Moon20080012697WorkOrbit Determination System for Low Earth Orbit Satellites20080012699WorkA Contingency in the Rosetta Reaction Control System: Alternative Cruise Trajectory Strategies to Cope with Degraded Delta-V Resources20080012693WorkSmart-1 Moon Impact Operations20080012706WorkVisual Navigation - SARE Mission20080012639WorkOptimisation of the Future Routine Orbit for Mars Express20080012668WorkTwo-Stage Path Planning Approach for Designing Multiple Spacecraft Reconfiguration Maneuvers20080012644WorkContingency Operations during Failure of Inertial Attitude Acquisition Due to Star Tracker Blinding for Three-Axes-Stabilized Interplanetary Spacecraft20080012632WorkFormation Design Strategy for SCOPE High-Elliptic Formation Flying Mission20080012654WorkSTEREO Mission Design Implementation20080012636WorkFour-Formation In-Track Configuration Maintenance Strategy20080012673WorkAttitude Control Flight Experience: Coping with Solar Radiation and Ion Engines Leak Thrust in Hayabusa (MUSES-C)20080012665WorkManeuver Recovery Analysis for the Magnetospheric Multiscale Mission20080012701WorkOrbit Determination and Navigation of the Time History of Events and Macroscale Interactions during Substorms (THEMIS)20080012707WorkDetermining a Method of Enabling and Disabling the Integral Torque in the SDO Science and Inertial Mode Controllers20080012716WorkObserving Mode Attitude Controller for the Lunar Reconnaissance Orbiter20080012690WorkMars Reconnaissance Orbiter Aerobraking Daily Operations and Collision Avoidance20080012721WorkSELENE Translunar Trajectory Reconfiguration Plan Provided for the Case of Main Engine Anomaly
No Preview Available