The Magnetometer Navigation (MAGNAV) algorithm is currently running as a flight experiment as part of the Wide Field Infrared Explorer (WIRE) Post-Science Engineering Testbed. Initialization of MAGNAV occurred on September 4, 2003. MAGNAV is designed to autonomously estimate the spacecraft orbit, attitude, and rate using magnetometer and sun sensor data. Since the Earth's magnetic field is a function of time and position, and since time is known quite precisely, the differences between the computed magnetic field and measured magnetic field components, as measured by the magnetometer throughout the entire spacecraft orbit, are a function of the spacecraft trajectory and attitude errors. Therefore, these errors are used to estimate both trajectory and attitude.
Results of the Magnetometer Navigation (MAGNAV) Inflight Experiment
2004
28 pages
Report
Keine Angabe
Englisch
Spacecraft Trajectories & Flight Mechanics , Unmanned Spacecraft , Navigation & Guidance System Components , Magnetometers , Navigation systems , Space flight , Algorithms , Spacecraft configurations , Spacecraft trajectory , Magnetic fields , Orbits , Attitude control , Vectors , Kalman filters , Sensors
AIAA-2004-4749 Results of the Magnetometer Navigation (MAGNAV) Inflight Experiment
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