International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, Vol XXXV, Part B4. Istanbul 2004
This means that corresponding points are searched in areas only
where points have been found before due to good texture (Tang,
Heipke, 1996).
To further refine the result Multi Image Least Squares
Matching (MILSM) is carried out following the approach of
Krupnik (1994). In this method the tie points are matched in all
images simultaneously. Because it is the most accurate
matching technique available it is possible to further refine the
result of the feature based matching. In our implementation we
can decide whether to apply MILSM or not for each pyramid
level. To save computing time it is advisable to carry out
MILSM only on the last level, which represents the original
resolution. In this approach the affine transformation
parameters between areas defined around the matching location
called image patches are determined in an arbitrary number of
images. In order to avoid a datum defect, one image patch has
to be fixed serving as reference for the other patches. The least
squares adjustment can be described by
eo . A :
= ==2dp + dG - (gf Po ) — G,)
op e el !
where v denotes the residuals, G the theoretical grey values
computed as mean value from all image patches at (r, c), g(p)
the grey values of the image patches, p the affine
transformation parameters between the image patches, dG the
unknown differences to the initial value for the theoretical grey
values, dp the unknown corrections for the parameters and the
subscript 0 stands for initial values of the unknowns. One such
equation can be set up for every pixel of the reference patch
transformed into every available image. The discretisation of
equation (5) leads to the following linear system:
v= —g;(r,c)dâ, ip! (r.c)dà5
-g,(r.c)dà; - g; (r.c)dà;
-g. (r,c)da; = g. (r. c) da; (6)
«dG(r,c) -g' (r.c) G, (r.c)
yz dG (r.c) -g'(r.c)* G,(r.c)
where i denotes the number of the image patch, r the row— and
c the column coordinates of the image patch. The used symbols
are described in the following:
grey value of image patch i (i ^ 7, ..., n) atr, c
( x > .
g'(r,c) grey value of fixed reference image patch 0 at r, c
g. grey value gradient of image patch i w.r.t. r
eg“ grey value gradient of image patch i w.r.t. c
G,(r,c) initial value of theoretical grey value at r,c
daj,,da, ^ unknown shift parameters between image patch i
and reference image patch 0
da;,...,da, unknown rotation and shear parameters between
image patch i and reference image patch 0
dG(r,c) unknown change of theoretical grey value at r, c
It is also possible to choose whether to use all six unknown
parameters daj,...,da; for the MILSM or only the two shift
parameters da, , da; .
Finally, model points are derived via forward intersection of the
image coordinates of the tie points. They serve as an
approximation for the reduction of the search space on the next
lower pyramid level instead of the MOLA points. The MOLA
DTM is used only on the first pyramid level. The application
flow of the matching is shown in Figure 3.
input
observed ; ;
; interior
exterior ; :
: orientation
orientation
area of interest
= whole image
level =
start level
feature extraction
in area of interest
Y
pairwise feature based
matching in all combinations
Ÿ
| tuple generation using RANSAC |
forward intersection
geometric consistency check
back projection of all
3D-points from forward Least Squares Matching
intersection (optional)
MOLA DTM
(optional)
images and
image pyramids
Y
area of interest =
related image chips
X
forward intersection
level = level <= intermediate
level - 1 level
4 yes no
level = original
level
no yes coordinates
of tie points,
Figure 3: Application flow of the matching.
3. RESULTS
In this section, first the used HRSC imagery will be described.
In the second part the results of the matching will be presented
and discussed on the basis of the orbits 18, 22 and 68.
3.1 Data
For the evaluation of the matched tie points, imagery of the
orbits 18, 22 and 68 have been chosen which have been
received in the early phase of the Mars Express mission.
Besides the HRSC imagery, the observations of the exterior
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