The following is from the University of Texas at Austin, considered a
reliable resource for GPS information. See
http://www.utexas.edu/depts/grg/gcraft/notes/gps/gps.html
GPS Error Sources
GPS errors are a combination of noise, bias, blunders.
Noise, Bias, and Blunders
Noise errors are the combined effect of PRN code noise (around 1
meter) and noise within the receiver noise (around 1 meter).
Bias errors result from Selective Availability and other factors
Selective Availability (SA)
SA is the intentional degradation of the SPS signals by a
time varying bias. SA is controlled by the DOD to limit
accuracy for non-U. S. military and
government users. The potential accuracy of the C/A code of
around 30
meters is reduced to 100 meters (two standard deviations).
The SA bias on each satellite signal is different, and so
the resulting position solution is a function of the
combined SA bias from each SV used
in the navigation solution. Because SA is a changing
bias with low frequency terms in excess of a few hours, position solutions
or individual SV pseudo-ranges cannot be effectively averaged over periods
shorter than a few hours. Differential corrections must be updated at a
rate less than the correlation time of SA (and other bias
errors).
Other Bias Error sources;
SV clock errors uncorrected by Control Segment can result in
one meter
errors.
Ephemeris data errors: 1 meter
Tropospheric delays: 1 meter. The troposphere is the lower
part (ground level to from 8 to 13 km) of
the atmosphere that experiences the changes
temperature, pressure, and humidity associated with weather changes.
Complex models of tropospheric delay require estimates or
measurements of these parameters.
Unmodeled ionosphere delays: 10 meters. The ionosphere is
the layer of the atmosphere from 50 to 500 km that consists
of ionized air. The transmitted model can only remove about
half of the possible 70 ns of delay leaving a ten meter
un-modeled residual.
Multipath: 0.5 meters. Multipath is caused by reflected
signals from surfaces near the receiver that
can either interfere with or be mistakenfor the signal that
follows the straight line path from the satellite. Multipath is
difficult to detect and sometime hard to avoid.
Blunders can result in errors of hundred of kilometers.
Control segment mistakes due to computer or human error can cause
errors
from one meter to hundreds of kilometers.
User mistakes, including incorrect geodetic datum selection, can
cause errors from 1 to hundreds of meters.
Receiver errors from software or hardware failures can cause
blunder errors of any size.
Noise and bias errors combine, resulting in typical ranging errors of
around
fifteen meters for each satellite used in the position solution.
IMHO, Loran-C is still the most reliable, cost effective, widely available
(continental US) technique for providing navigational redundancy.
Mel Kowal
MEI LEE
Swantown Marina, Olympia, WA