NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
2001 Flight Mechanics SymposiumThis conference publication includes papers and abstracts presented at the Flight Mechanics Symposium held on June 19-21, 2001. Sponsored by the Guidance, Navigation and Control Center of Goddard Space Flight Center, this symposium featured technical papers on a wide range of issues related to attitude/orbit determination, prediction and control; attitude simulation; attitude sensor calibration; theoretical foundation of attitude computation; dynamics model improvements; autonomous navigation; constellation design and formation flying; estimation theory and computational techniques; Earth environment mission analysis and design; and, spacecraft re-entry mission design and operations.

Government, industry, and the academic community participated in the preparation and presentation of these papers.
Document ID
20010084958
Document Type
Conference Publication (CP)
Authors
John P Lynch (Goddard Space Flight Center Greenbelt, Maryland, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2001
Publication Information
Subject Category
Astrodynamics
Report/Patent Number
NONP-NASA-CD-2001126425
NAS 1.55:209986
Rept-2001-02668-0
NASA/CP-2001-209986
Meeting Information
Flight Mechanics Symposium(Greenbelt, MD)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Flight mechanics
Attitude determination
Mission analysis
Spacecraft dynamics
Orbit determination

Available Downloads

NameType 20010084958.pdf STI

Related Records

IDRelationTitle20010084968Analytic SubsidiaryA Preliminary Formation Flying Orbit Dynamics Analysis for Leonardo-BRDF20010084960Analytic SubsidiaryA Non-Linear Approach to Spacecraft Trajectory Control in the Vicinity of a Libration Point20010084983Analytic SubsidiaryMaximum Torque and Momentum Envelopes for Reaction Wheel Arrays20010084964Analytic SubsidiaryHigh Earth Orbit Design for Lunar-Assisted Medium Class Explorer Missions20010084990Analytic SubsidiaryThe Integration, Testing and Flight of the EO-1 GPS20010084984Analytic SubsidiaryA Fully Coupled Multi-Rigid-Body Fuel Slosh Dynamics Model Applied to the Triana Stack20010084989Analytic SubsidiaryPreliminary Results of NASA's First Autonomous Formation Flying Experiment: Earth Observing-1 (EO-1)20010084971Analytic SubsidiaryCalibration of Gyros with Temperature Dependent Scale Factors20010084959Analytic SubsidiarySolar Activity Forecasting for use in Orbit Prediction20010084991Analytic SubsidiaryTrajectory Design and Control for the Compton Gamma Ray Observatory Re-Entry20010084998Analytic SubsidiaryHubble Space Telescope Servicing Mission 3A Rendezvous Operations20010084995Analytic SubsidiaryImage Mission Attitude Support Experiences20010084966Analytic SubsidiaryEvaluation of Relative Navigation Algorithms for Formation-Flying Satellites20010084967Analytic SubsidiaryRelative Navigation for Formation Flying of Spacecraft20010084978Analytic SubsidiaryState-Dependent Pseudo-Linear Filter for Spacecraft Attitude and Rate Estimation20010084962Analytic SubsidiaryUnique Non-Keplerian Orbit Vantage Locations for Sun-Earth Connection and Earth Science Vision Roadmaps20010084999Analytic SubsidiaryOn-Orbit Performance of Autonomous Star Trackers20010084981Analytic SubsidiaryUsing Automation to Improve the Flight Software Testing Process20010084979Analytic SubsidiaryTriana Safehold: A New Gyroless, Sun-Pointing Attitude Controller20010084992Analytic SubsidiaryEntry Debris Field Estimation Methods and Application to Compton Gamma Ray Observatory Disposal20010084972Analytic SubsidiaryOn-Orbit Calibration of Redundant Spacecraft Gyros by Optimal Reduction to Three Axes20010084969Analytic SubsidiaryReducing Formation-Keeping Maneuver Costs for Formation Flying Satellites in Low-Earth Orbit20010084982Analytic SubsidiaryA Two-Wheel Observing Mode for the MAP Spacecraft20010084977Analytic SubsidiaryA Nonlinear Spacecraft Attitude Controller and Observer with an Unknown Constant Gyro Bias and Gyro Noise20010084976Analytic SubsidiaryIn-Space Calibration of a Gyro Quadruplet20010084987Analytic SubsidiaryPrecise Orbit Determination for GEOSAT Follow-On Using Satellite Laser Ranging Data and Intermission Altimeter Crossovers20010084974Analytic SubsidiaryValidating GOES Instrument Thermal Deformations20010084988Analytic SubsidiaryTracking and Data Relay Satellite (TDRS-3) Range Biases and Momentum Unload Modeling for Terra (EOS-AMI)20010084965Analytic SubsidiaryAlternate Forms of Relative Attitude Kinematics and Dynamics Equations