In order to improve accuracies to the sub-meter
level, the carrier phase observable is generally
required. One exception may be the use of narrow
correlator technology on baselines of up to 20 km
with the addition of chokering groundplanes to
minimize multipath. However, in most cases
differential carrier phase processing is
implemented which adds significant complexity to
the operation in terms of data acquisition and
especially data processing due to the issues of
carrier phase cycle slips and ambiguity resolution.
The benefit is that ultimate accuracies in the order
of a few cm can be achieved for static and
kinematic applications within 10 km from a
monitor station.
As previously mentioned, GPS data can be acquired
using a variety of techniques which are generally
dictated by the application as well as the required
accuracy. Table 3 summarizes the major techniques
that are used for the collection of GPS positioning
information as well as their general features.
For static applications there are generally three
techniques which are used, namely conventional
static, rapid static and semi-kinematic. The first
technique is the most robust and reliably gives
results at the 1-3 ppm level (i.e. 1-3 cm per 10 km of
monitor-remote separation). Its main
disadvantage is the low productivity caused by
the long observation span. In recent years rapid
static surveying has become feasible due to the
increased satellite constellation, P codeless
receivers as well as improved processing
algorithms. In general this technique can give cm-
level accuracies in minutes, but is limited to
baselines where integer ambiguities can be
resolved, i.e. generally less than about 15 km. If
rapid static surveying is implemented using a
receiver that does not output the carrier phase
(only the carrier-smoothed code), the accuracy is
limited to about 1-3 m. Semi-kinematic positioning
is an alternative to rapid static in that it does not
depend on P codeless technology. In this case the
carrier phase integer ambiguities are initialized
at a starting point and then the receiver is
transported to other points of interest. As long as
lock is maintained to at least four satellites during
these movements, cm-level accuracies can be
achieved. However, if less than four satellites are
tracked, the ambiguities must be re-initialized. It
is expected that the rapid static technique will
fully replace semi-kinematic positioning once the
cost of P codeless technology decreases further. For
more information on semi-kinematic surveying see
Cannon (1991).
Table 3: GPS Data Collection Techniques
Technique General Features
- carrier phase processing VIE
Conventional - highest achievable accuracy
Static - long observation span (30-60 min)
- low productivity
- carrier phase processing
Rapid - accuracy from cm to sub-metre
Static - Short observation span (5-15 min)
(also called - may need P codeless receivers
Fast Static) - high productivity
- generally for baselines « 15 km
- carrier phase processing
- accuracy at the cm-level
memi. - must maintain lock to 4 SVs
kinematic ders
- high productivity
- generally for baselines « 15 km
; - code or code-smoothed processing
Kinematic
- accuracy at the one to several m
(also called ee ; F
- easily implemented in real-time
Dynamic) hi ios
- high productivity
- carrier phase processing
Kinematic - static initialization required
with - accuracy at the several cm level
Static - generally for baselines < 50 km
Initialization - must maintain lock to 4 SVs
- high productivity
- carrier phase processing
- no static initialization required
On-the-fly - accuracy at the several cm level
Kinematic - generally for baselines < 50 km
(OTF) generally need P codeless units
high productivity
The need for real-time positioning is usually
driven by navigation or guidance requirements,
however knowledge of high quality results during
the observation span is also beneficial. Of the
techniques presented in Table 3, the kinematic
(dynamic) mode of operation is the easiest to
implement in real-time. This is due to the use of
the code observable which simplifies the
processing requirements as wells as data
transmission. Corrections from the monitor receiver
can be transmitted at a rate as low as 50 bps using
an internationally accepted standard format, i.e.
RTCM-SC104. Accuracies in the real-time mode of
operation are generally within those achieved in
post-mission, assuming no significant breaks in the
correction transmission. The U.S Coast Guard has
initiated differential GPS (DGPS) correction
transmission from its existing marine radiobeacons
and the current coverage includes part of the US
east coast as well as the Gulf of Mexico. Future
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