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ISPRS Commission III, Vol.34, Part 3A »Photogrammetric Computer Vision“, Graz, 2002
5.1 Results
The indirect georeferencing algorithm described in Equation 6
was tested in order to estimated the parameters modelling the
sensor external orientation and the ground coordinates of the
TPs. From the available 40 object points, a group of them was
used as GCPs and the remaining as TPs. The TPs ground
coordinates estimated by the triangulation were compared to
their correct values and used for the tests’ control. Various
combinations of GCPs and TPs were chosen in order to
evaluate the influence of the ground information. Table 1
provides a summary of the resulting absolute accuracy in the
different test configurations. 6, 10 and 20 GCPs were tested,
using 5 and 10 segments for the external orientation modelling.
An absolute accuracy in the range 4-13 cm for X, 3-12 cm for Y
and 8-19 cm for Z were achieved, corresponding to 0.6-2.1
pixels, 0.2-2 pixels and 1.3-3 pixels. Anyway the fact that the
image coordinates were estimated at 0.5 pixels accuracy could
have affected the results. The comparison between the results
from the different tests confirms that the triangulation accuracy
is influenced by the number and distribution of ground
information and improves with the number of GCPs. As far as
the modelling functions are concerned, the division of the
trajectory in a larger number of segments does not imply any
substantial improvements.
GCPs+ TPs
20+20 | 10+30 | 6+34
RMS, 150.070 170.082 | 0.131
5 segments RMS, | 0.028 | 0.088 | 0.090
RMS; | 0.086 | 0.172 | 0.146
RMSy | 0.041 | 0.050 | 0.057
10 segments | RMSy | 0.059 | 0.099 | 0.124
RMS; | 0.112. | 0.138 | 0.192
Table 1. RMS values (in meters) of the estimated
TPs coordinates.
6. CONCLUSIONS
A general sensor model for multi-line CCD array sensors with
along stereo viewing has been presented. The model combines
the classic photogrammetric collinearity equations with the
sensor external orientation modelling, resulting in an integrated
triangulation. The functions used to describe the external
orientation are based on piecewise polynomials. The model can
be applied on sensors carried on both airplane and satellites,
with optical systems consisting of one or more lenses. The
algorithm can also include and correct any external orientation
observations provided by GPS and INS instruments carried on
board.
The proposed model has been tested on a simulated sensor (1
lens, 3 CCD arrays) carried on airplane, with different GCPs
and TPs distributions. The results have been presented. An
accuracy in the range of 0.6-2.1 pixels in X, 0.2-2 pixels in Y
and 1.3-3 pixels in Z was achieved using 6, 10 and 20 GCPs
and dividing the trajectory in 5 and 10 segments.
In the next future, the model will be applied to a real dataset
from the Japanese TLS (Three-Line Sensor) by Starlabo,
Tokyo.
7. ACKNOWLEDGMENTS
This work is part of Cloudmap2 project, funded by the
European Commission under the Fifth Framework program for
Energy, Environment and Sustainable Development.
I would like to thank Mr. Zhang Li, from my department, for
his helpful suggestions.
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