
To transform satellite altimeter range measurements into accurate sea-surface elevation measurements, a variety of models, algorithms, and corrections needs to be adopted and applied. These include the determination of the satellite position within a consistent geodetic reference frame, the correction for various media and environmental effects, and the removal of tidal and (possibly) atmospheric loading effects. Most of the adopted PATHFINDER corrections and algorithms are consistent across satellite missions, but some are specific to an individual mission. Below is the list of these many parameters. Whenever there is a satellite selection, the parameter is satellite-specific.
Satellite Ephemerides
TOPEX/POSEIDON
ERS
GEOSAT
Reference frame and reference ellipsoid
Solid-Earth Body Tide
Ocean Tide
Load Tide
Pole Tide
Cross-Track Geoid Correction
Atmospheric Loading (Inverted Barometer) -- Optional
Dry Troposphere
Wet Troposphere
TOPEX/POSEIDON
ERS
GEOSAT
Ionosphere
TOPEX
POSEIDON
ERS
GEOSAT
Sea State Bias
TOPEX
POSEIDON
ERS2
ERS1
GEOSAT
Calibration Issues
TOPEX
POSEIDON
ERS-1&2
GEOSAT

These pages last modified on 22 August 2002.
Algorithm pages are maintained by
Richard Ray
ray@nemo.gsfc.nasa.gov and
Brian Beckley.
brianb@nemo.gsfc.nasa.gov