3-3-2
1. INTRODUCTION
The successful application of GPS is
dependent on understanding its coordinate
system, achievable accuracy and
limitations. All GPS modes of operation
are not the same. Accuracy ranging from
hundred meters to a few millimeters can be
achieved depending upon the data
collection and processing techniques,
hardware, software, satellite geometry and
atmospheric condition.
In order to optimise the survey time, it is
necessary to know the accuracy achievable
in different modes of operation. It is also
necessary to know the procedures in order
to achieve higher accuracy. A GPS can be
used for level survey provided that the
accuracy achievable is good enough for the
desired application. In this research a
procedural was developed to achieve
centimeter level accuracy in height
component, which could be useful for level
survey.
2. OBJECTIVE
The main objective of this research is to
improve the height accuracy observed in
real time kinematic (RTK) mode.
3. RESEARCH STRUCTURE
The structure of this research is shown in
Figure 1. The structure mainly consists of
four components. The first one is to
develop the system itself, since this is the
first time a base station was installed in
Thailand (and hence at AIT) using mobile
phone for real time differential correction.
The next component includes the accuracy
Research Structure
Figure 1
analysis in both the static and kinematic
modes. In static mode, the accuracy was
analyzed for planimetrie and height
components where as for the kinematic
mode, only the height accuracy was
anlaysed. The height accuracy achieved in
kinematic mode was compared with the
level survey. An overhead road crossing at
a baselength of three kilometer was chosen
for real time kinematic survey. The road is
about 750 meters long, elevated up to eight
meters (approximately) at the center of the
road and has 31 piers. The error at each
pier location was calculated and analysed
to see whether there was any effect of
antenna velocity (vehicle speed) on
accuracy. Next, the analysis was done to
see whether the errors could be minimised.
The RMS error, the standard deviation of
the error itself and the scatter plot between
the errors at the calibration points were
analysed. Based on these analysis and the
two calibration points, an error correction