mission requirements. The advantage of the differential method is that an
overdetermined position solution (additional range measurements) is not required
as in RAIM to maintain positioning integrity. If the number of available satellite
corrections exceeds the number of tracking channels in the user receiver, these
position error estimates can also be used to select the set of satellites that provide
the most accurate position solution. Normally, the "all in view" position solution is
most accurate, and the correction UDRE values are near the same magnitude. If
one or more corrections have a relatively large UDRE, a subset of the satellites
may provide a more accurate solution.
The standard maritime DGPS design, being implemented by several countries
throughout the world, includes a differential user receiver located at a nearby
surveyed site to serve as an integrity monitor. The integrity monitor receives and
applies the corrections and develops a differential position solution in the same
manner as any other user receiver. This position solution is then compared with
the known antenna location. If the difference exceeds the allowed differentially
corrected position error, the transmission of all corrections is terminated. A
message is also sent to the users warning them to stop using all previously
transmitted corrections. Although this method protects well against large sudden
errors, rigorous integrity is only provided for a user that determines a position using
the same set of satellite corrections as the integrity monitor (typically the full set).
Receivers that use only a subset of the satellites and transmitted corrections will
have a higher DOP value for position determination and may have a significantly
greater position error than the integrity monitor.
A more effective integrity method is to check the integrity of each individual
correction in the range domain, rather than the position domain, providing integrity
for users of any correction subset. This method also uses multiple receivers in the
reference station (a minimum of two), but each receiver generates an independent
set of corrections. The receivers also use different antennas, sited a sufficient
distance apart that multipath effects are likely to be independent as well. The two
sets of corrections are directly compared prior to transmission. The difference
between each pair of corrections is a direct measurement of most of the
components of the actual instantaneous differential range error seen by the user
receiver. If a pair of corrections disagree by more than a predetermined amount,
for example, 3 X UDRE (that is, 3 sigma UDRE), correction transmissions are
interrupted for that satellite. In this way, the user does not receive or use any
corrections until the integrity is checked, and the user can have confidence that the
broadcast UDRE is a true measure of the expected range error. The reference
station also has the ability to continue broadcasting the corrections that remain
valid. This technique is particularly useful for applications that must meet short
integrity warning times, must provide a highly confident estimate of UDRE, must
minimize service interruptions, or that have slow correction transmission rates.
Additional enhancements to this technique can include the use of dissimilar
receivers to prevent common mode errors within the reference station, the use of
more than two receivers to "vote out" anomalous measurements, or the calculation
of an "average" correction between the reference station receivers.
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