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Figure 4. Diagram showing key areas and dimensions
As can be seen from Figure 4, each of the areas concerned is
circular in nature and the centre point and radius of each was of
prime concern. The vertical axis of the hopper is defined by the
upper and lower circles designated 1 and 2 in Figure 4, whilst
the origin of the design system is defined as an offset below the
centre of circle 2. The flange, designated as circle 3 in Figure 4,
defines the horizontal orientation of the design system and is
specified to be at a design distance and angle from the origin.
Clearly, each circle would have to be targeted appropriately to
allow the computation of the plane of best fit and circle of best
fit, then the centre and radius. The measurement task here was
the coordinate determination of approximately 50 target points.
The location of these targets is shown in Figure 5. Additional
targets shown on the sides of the hopper are necessary for
photogrammetric measurement only, in order to strengthen the
self-calibrating network.
Plan view of target array
Figure 5. Target locations in principle planes
THEODOLITE TRIANGULATION
Initially the use of an on-line triangulation system, comprising
of three total stations and PC based software was considered.
The advantage of the online system is that it provides
coordinates with a quality measure for every intersection
measurement as it is taken, and measurements can be repeated
immediately as required. The online capability of theodolite
triangulation initially proved to be very enticing.
Based on an object diameter of 6 metres and a minimum
instrument set back of 5 metres, it was calculated that
approximately ten instrument stations would be required to
adequately cover the object. This ideal configuration and a
configuration which accounts for the proximity of the wall and
other obstructions along one side of the object are shown in
Figure 6.
Figure 6. Ten station coverage with and without obstructions
Points adjacent to the obstructions will no doubt suffer a
degradation of accuracy due to fewer, sharper intersection
angles. The number of instrument stations can be reduced by
increasing the minimum set back to effectively improve the
angular coverage. This improvement will of course be at the
expense of target coordinate precision due to the increase in
target range. The level of coordinate precision degradation can
of course be estimated through network simulations. Naturally
enough, even a six or seven station network would be
complicated by the need to “leap-frog” instruments around the
object. The establishment of a three head triangulation system
requires 1-2 hours depending on the determination of control.
Once established, approximately 30 minutes is required to shift
and reintegrate a new instrument station into the system. Based
on the following parameters it is possible to estimate the time
taken to complete the measurement phase using theodolite
triangulation :
Three instrument initial establishment 1.5 hr
Seven station re-establishments (30 minutes each) 3 hr
Target measurement (50 targets @ approx. 2min. each) 1.5hr
Total measurement time 6 hr
These figures do not take into account object targeting which is
a requirement regardless of the measurement method selected.
The height of the object poses other issues which must be
addressed. The hopper stands to a height of 2.5 metres and for
easy work access was supported on a tooling jig, giving an
additional 1 metre of height. Sighting to points on the top of
the hopper would therefore require the purchase or manufacture
of an offset rod which could be placed flush against the edge of
the top circle surface. The number of measurements for offsets
is doubled or tripled, as offset rods have multiple targets which
provide the information necessary to locate the point of interest,
International Archives of Photogrammetry and Remote Sensing. Vol. XXXI, Part B5. Vienna 1996
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