Conversion Of Osculating Orbital Elements To Mean Orbital Elements
Attitude Determination Improvements for GOES
Experiences in Interagency and International Interfaces for Mission Support
An Evaluation of Attitude-Independent Magnetometer-Bias Determination Methods
Flight Dynamics Mission Support And Quality Assurance Process
Pulsed Plasma Thrusters for Small Spacecraft Attitude Control
Modular Software for Spacecraft Navigation Using the Global Positioning System (GPS)
Autonomous Navigation with Ground Station One-Way Forward-Link Doppler Data
South Atlantic Anomaly Entry and Exit As Measured by the X-Ray Timing Explorer
Attitude Accuracy Study for the Earth Observing System (EOS) AM-1 Spacecraft
Optimized TRIAD Algorithm for Attitude Determination
An Automated Real-Time Spacecraft Navigation System
ATTDES - An Expert System for Satellite Attitude Determination and Control, II
Geostationary Operational Environmental Satellite (GOES) Gyro Temperature Model
REQEST - A Recursive QUEST Algorithm for Sequential Attitude Determination