Processing Approach
•20 km along track filter
•Crossover analysis for internal accuracy
•Upward continue gravity anomalies
•Comparison of observations & gravity anomalies at 7.6 km to establish external accuracy
•Remove EGM reference field at elevation
•Downward continue to surface and restore reference field
•Compare to gravity anomalies at the surface
FMS/IMU provides data for removing most along-track aircraft noise
20-km filter removes remaining signal
Anticipate 2 mgal accuracy
EGM will either be EGM96 or GGM01C
Gravity anomalies will either be gridded surface data (taking into account elevations) or Faye Anomalies