repeated in various locations within laser scanning strips,
internal deviations of laser data become visible.
2. MATERIAL
The test site in the Espoonlahti was flown with TopoSys Falcon
in May 2003 from the altitude of 400 m resulting in more than
10 measurements per m? (Figure 1). The data was pre-processed
by TopoSys. Five of the strips (numbers 2, 3, 4, 5 and 6) were
overlapping almost completely. The flight direction was almost
from southeast to northwest for the strips 2, 4 and 6. Two strips,
3 and 5, were flown to opposite direction.
Figure 1. TopoSys Falcon laser scanner provides dense point
sampling at the flight direction. However, there is a
gap between scanning strings causing uncertainty in
local planimetric registration in across-track
directions.
Figure 2. Thirty-nine small orientation sites cover an area of
1500 m x 100 m. Each site is visible from five
different laser strips. Aerial image courtesy to FM-
Kartta Ltd.
International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, Vol XXXV, Part B3. Istanbul 2004
Thirty-nine circular test sites, with radius from 12 to 15 meters,
were selected from the overlapping area of five laser strips. The
sites were chosen in the way that some buildings or part of the
buildings could be seen in each site. The buildings were
expected to be the most robust features for relative orientation
between the laser point clouds. Only the first pulse was used
from the laser scanning data.
The whole test area and small test sites can be seen in Figure 2.
The buildings in the test areas had both saddle roofs and flat
roofs. The size of the building varied from small one-storied
building to high apartment houses. The orientation of many
buildings in the test sites was unfortunately either parallel or
perpendicular to the flight direction, which caused some
problems when the across-track direction was inspected.
3. METHODS
The interactive orientation method (Rónnholm et al, 2003) was
used to find the direct relative orientation between two laser
point clouds. The interactive orientation method was originally
designed to be a tool for solving direct orientation between an
image and 3D reference data, like in the case of Figure 3. The
reference data for orientations can be 3-D control points,
vectors, objects or even laser point clouds, for example.
The interactive orientation method is based on visual
interpretation of superimposed 3-D data in the image. The
superimposing is done using the collinearity equations
zo UT A. rU EZ TZ x
7 (XX Yr (PY =-Yo V+ rm (ZZ) 7 a)
ee ar X= Todt tm fa ;
Rh KFZ =Z 1
where c = camera constant
x, y = 2-D image coordinates
X, Yo, Zo ^ coordinates of projection center
X, Y, Z = 3-D ground point
Xo, Yo = principle point
Kilos 7 elements of 3-D rotation matrix
After superimposing laser point cloud with some initial
orientation parameter values an operator is able to see, whether
the data is fitting correctly or not. If not, the image orientation is
not correct. The image orientation parameters contain three
independent shifts and rotations. With tools presented in
Rónnholm et al. (2003), these six parameters can be
interactively modified. After every correction, the laser point
cloud is superimposed again in the image, with the new
orientation parameters. The method leads to an iterative
process, until the orientations cannot be improved any more.
One disadvantage of the interactive method is that there is no
automation involved. On the other hand, this is as well an
advance, because human intelligence can understand and handle
quite complex data sets. For example, there is no need to filter
laser point clouds before orientations, because an operator can
interpret and fit the entity, even if some details do not seem to
correspond to each other. However, sometimes even small
details, if identifiable from both data sets, can be used as a tie
features. Actually, more important than filtering, is to improve
visual interpretability of laser point clouds with color-coding.
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