NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Flight Mechanics/Estimation Theory Symposium 1996This conference publication includes 34 papers and abstracts presented at the Flight Mechanics/ Estimation Theory Symposium on May 14-16, 1996. Sponsored by the Flight Dynamics Division of Goddard Space Flight Center, this symposium featured technical papers on a wide range of issues related to orbit-attitude prediction, determination, and control; attitude sensor calibration; attitude determination error analysis; attitude dynamics; and orbit decay and maneuver strategy. Government, industry, and the academic community participated in the preparation and presentation of these papers.
Document ID
19960035748
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Proceedings
Authors
Greatorex, Scott (NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1996
Subject Category
Astrodynamics
Report/Patent Number
NAS 1.55:3333
Rept-96B00071
NASA-CP-3333
Report Number: NAS 1.55:3333
Report Number: Rept-96B00071
Report Number: NASA-CP-3333
Accession Number
96N30487
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19960035761WorkAn Evaluation of Attitude-Independent Magnetometer-Bias Determination Methods19960035766WorkModular Software for Spacecraft Navigation Using the Global Positioning System (GPS)19960035757WorkSolar and Heliospheric Observatory (SOHO) Flight Dynamics Simulations Using MATLAB (R)19960035776WorkDownlink Probability Density Functions for EOS-McMurdo Sound19960035777WorkHeuristic Modeling for TRMM Lifetime Predictions19960035750WorkREQUEST: A Recursive QUEST Algorithm for Sequential Attitude Determination19960035762WorkAccuracy Studies of a Magnetometer-Only Attitude-and-Rate-Determination System19960035755WorkInvestigation of Models and Estimation Techniques for GPS Attitude Determination19960035760WorkAttitude Determination Improvements for GOES19960035778WorkAutonomous Navigation With Ground Station One-Way Forward-Link Doppler Data19960035770WorkThe Solar and Heliospheric Observatory (SOHO) Mission: An Overview of Flight Dynamics Support of the Early Mission Phase19960035749WorkA Simplified Pattern Match Algorithm for Star Identification19960035752WorkVariations on the Davenport Gyroscope Calibration Algorithm19960035765WorkBalancing Science Objectives and Operational Constraints: A Mission Planner's Challenge19960035759WorkAttitude and Trajectory Estimation Using Earth Magnetic Field Data19960035780WorkApplication of Tracking and Data Relay Satellite (TDRS) Differenced One-Way Doppler (DOWD) Tracking Data for Orbit Determination and Station Acquisition Support of User Spacecraft Without TDRS Compatible Transponders19960035764WorkATTDES: An Expert System for Satellite Attitude Determination and Control19960035775WorkConversion of Osculating Orbital Elements to Mean Orbital Elements19960035773WorkPulsed Plasma Thrusters for Small Spacecraft Attitude Control19960035754WorkAttitude Estimation Using Modified Rodrigues Parameters19960035779WorkReducing On-Board Computer Propagation Errors Due to Omitted Geopotential Terms by Judicious Selection of Uploaded State Vector19960035769WorkSouth Atlantic Anomaly Entry and Exit as Measured by the X-Ray Timing Explorer19960035758WorkAttitude Accuracy Study for the Earth Observing System (EOS) AM-1 Spacecraft19960035767WorkARTSN: An Automated Real-Time Spacecraft Navigation System19960035774WorkHomotopy Solutions of Kepler's Equations19960035751WorkOptimized TRIAD Algorithm for Attitude Determination19960035763WorkGeostationary Operational Environmental Satellite (GOES) Gyro Temperature Model19960035772WorkExperiences in Interagency and International Interfaces for Mission Support19960035771WorkFlight Dynamics Mission Support and Quality Assurance Process19960035756WorkAttitude Drift Analysis for the WIND and POLAR Missions19960035749WorkA Simplified Pattern Match Algorithm for Star Identification19960035750WorkREQUEST: A Recursive QUEST Algorithm for Sequential Attitude Determination19960035751WorkOptimized TRIAD Algorithm for Attitude Determination19960035752WorkVariations on the Davenport Gyroscope Calibration Algorithm19960035753WorkSatellite Angular Rate Estimation From Vector Measurements19960035754WorkAttitude Estimation Using Modified Rodrigues Parameters19960035755WorkInvestigation of Models and Estimation Techniques for GPS Attitude Determination19960035756WorkAttitude Drift Analysis for the WIND and POLAR Missions19960035757WorkSolar and Heliospheric Observatory (SOHO) Flight Dynamics Simulations Using MATLAB (R)19960035758WorkAttitude Accuracy Study for the Earth Observing System (EOS) AM-1 Spacecraft19960035759WorkAttitude and Trajectory Estimation Using Earth Magnetic Field Data19960035760WorkAttitude Determination Improvements for GOES19960035761WorkAn Evaluation of Attitude-Independent Magnetometer-Bias Determination Methods19960035762WorkAccuracy Studies of a Magnetometer-Only Attitude-and-Rate-Determination System19960035763WorkGeostationary Operational Environmental Satellite (GOES) Gyro Temperature Model19960035764WorkATTDES: An Expert System for Satellite Attitude Determination and Control19960035765WorkBalancing Science Objectives and Operational Constraints: A Mission Planner's Challenge19960035766WorkModular Software for Spacecraft Navigation Using the Global Positioning System (GPS)19960035767WorkARTSN: An Automated Real-Time Spacecraft Navigation System19960035768WorkExperience Gained From Launch and Early Orbit Support of the Rossi X-Ray Timing Explorer (RXTE)19960035769WorkSouth Atlantic Anomaly Entry and Exit as Measured by the X-Ray Timing Explorer19960035770WorkThe Solar and Heliospheric Observatory (SOHO) Mission: An Overview of Flight Dynamics Support of the Early Mission Phase19960035771WorkFlight Dynamics Mission Support and Quality Assurance Process19960035772WorkExperiences in Interagency and International Interfaces for Mission Support19960035773WorkPulsed Plasma Thrusters for Small Spacecraft Attitude Control19960035774WorkHomotopy Solutions of Kepler's Equations19960035775WorkConversion of Osculating Orbital Elements to Mean Orbital Elements19960035776WorkDownlink Probability Density Functions for EOS-McMurdo Sound19960035777WorkHeuristic Modeling for TRMM Lifetime Predictions19960035778WorkAutonomous Navigation With Ground Station One-Way Forward-Link Doppler Data19960035779WorkReducing On-Board Computer Propagation Errors Due to Omitted Geopotential Terms by Judicious Selection of Uploaded State Vector19960035780WorkApplication of Tracking and Data Relay Satellite (TDRS) Differenced One-Way Doppler (DOWD) Tracking Data for Orbit Determination and Station Acquisition Support of User Spacecraft Without TDRS Compatible Transponders19960035768WorkExperience Gained From Launch and Early Orbit Support of the Rossi X-Ray Timing Explorer (RXTE)19960035753WorkSatellite Angular Rate Estimation From Vector Measurements
No Preview Available