adjustment. Depending on the application area and the
desired image scale the required positioning accuracy
may vary significantly. The Figures 1 and 2 summarize
the respective required accuracies for the two application
areas.
350
300
E 250 |
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Figure 1 Required Accuracy for Navigation and
Automatic Camera Control
The above figure is based on the assumption that 3%
overlap error is tolerated in a conventional survey flight.
Similarly, a ,rule of thumb“ can be used for the
estimation of the required accuracy for the combined
block adjustment.
A zog nu tis
REQ 0 B
Typically the measurements of a block adjustment can
be carried out with a oo of roughly 10 um. The
corresponding required accuracy (Aago) of the camera
perspective centers is related to this value via the scale.
Due to the intersection geometry and the averaging
effects in a block adjustment a detoriation factor of 1.5 to
3 may be applied (see also Ackermann [1992])
08
2 0.5 Wee toques NOR LN AN ES cS afi
S
= tt
0.1 NR S A cat AN eue petto sn boa mn Kae
0 ! ! t f
1000 2500 5000 10000 20000 50000
Scale []
Figure 2 Required Position Accuracy for the Camera
Perspective Centers in a Combined Block Adjustment
As it can be seen from the above figures the accuracy
requirements may vary between a few centimeters to
hundreds of meters depending on the required scale and
application. It is obvious that the techniques and the
hardware requirements to achieve the quoted positioning
accuracies are also extremely different. Similar to the
International Archives of Photogrammetry and Remote Sensing. Vol. XXXI, Part B3. Vienna 1996
difference in required accuracy, also the operational
circumstances for the two major photogrammetric
applications are different. While absolute, real-time
positioning with medium accuracy is required for
navigation and camera control, highly accurate post-
processed positions are required for the GPS based
aerial triangulation. Table 1 summarizes the operational
circumstances and the solutions which are provided by
GPS for the specific application areas.
Operational navigation + GPS based
Circumstances | automatic aerial
camera control ,triangulation
Required 10-300 m 0.01-1m
Accuracy
Movement highly dynamic highly dynamic
Time of position Real Time Post-Processing
Differential only limited, with yes
positioning radio link
Baseline-Length 10-500 km 10-500 km
Receiver Update min. 1 Hz min. 1 Hz
Rate
Ambiguity not required required in large
Resolution scale
applications
Observation Code only, Phase only,
Type Carrier smoothed | Carrier smoothed
code code
Table 1 Operational Circumstances for the major
photogrammetric application areas
After giving this short introduction to the specific needs
of photogrammetric GPS applications, the remainder of
this paper will concentrate on GPS-hardware and
algorithmic aspects, which are of special importance for
photogrammetry.
3. HARDWARE AND SOFTWARE ASPECTS
Today many GPS receivers are already built for specific
applications, like GIS data collection, precise static (or
static like) geodetic surveying, high dynamic or low
dynamic navigation, or even leisure time applications,
but there is no receiver on the market which has been
specifically designed for photogrammetric applications.
From the photogrammetrists point of view, to choose a
receiver and the corresponding processing software is
rather difficult. Especially the highly dynamic
environment and the stringent accuracy requirements
over extremely long baselines are not standard
capabilities which can easily be solved with today's GPS
technology. To find the appropriate receivers and
software, which can provide such high precision results
even under these stringent conditions is rather difficult,
as also the terms in the data sheets and the quoted
performance parameters are often misunderstood or
misleading. (A good overview over today's receiver
technology can be found for example in van Dierendonck
[1994]).
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