ir line
course,
antical
plane
"mation
.4) is
n and,
ent of
2,1)
wn co-
es the
origi-
,S are
XN re-
Pelzer
dx are
2.2)
ose to
art of
of the
he un-
certainties from relative orientation and its
fictitious weights (2.3.1) take the form
1/9 = 2 02 ( y2 + 2 ) (3.2.3)
because of (3.1.2) and (3.1.3). It shows the fact
that, in the normal case, the weights decrease
strictly with y only. As weights do not influence
very much results of adjustments, relation (3.2.3)
could also be used for images which do not deviate
to much from normal position.
3.3 Propagation of errors concerning reconstruction
After relative orientation and transformation to
the normal case, the uncertainty of the model will
depend on the dispersion Su (3.3.2) of the image
coordinates xn. Since small variations of X read
( using the left image P')
dX = d\Nxn” + \ndxn°, (3.3.1)
as derived from (1.3.3) by differentiation, the
uncertainties result again from the expectation
SM = E{dXdXT}, i.e.
Su = E{AANZ}xn’Xn'T + AN[xn’E{d\ndxn’T}
*E(dAudxu' )xu'7] * AN2E{dxn’dxn’T}.
By means of the differential form
dxn"-dxn’ :
dÀAN 3 —————— = AN? (dxu "-dxu ! ) (3.3.2)
(XN "-xN ! )?
of equ. (1.3.2) the expectations are:
E{d\n2} = AN* (Ox"x"*tOx'x'-20x'x*),
E{d\ndxn’T} = ANZ | Ox'x"rOx'x' Ox"*y"t0Ox'y; D |
Ox*x"-0x?x?
E{d\ndxn ? }=)\n2 Ox"y'-Ox'y* ,
0
Ox'x* Ox t'y? 0
E{dxn’dxn’T}= Gx*y* Oy'y* 0
0 0 0
and regarding E{da’dx"T}=E{dx’da"T}=E{dx’dx"T}=0,
the co-variances of the correlation P’-P" may be
taken from Sn’"=E{dxn’dxn"}, i.e.
Sn’” = Ox'x" Ox’'y" = O0? Ba'Qa'"Ba'!,
Oy'x" QOy'y"
for the uncertainty of a stereoscopically recon-
structed model. It is seen that ANz1/(xu"-xu?) re-
presents the dominating factor and that the first
term of this relation will have the most important
influence at the limits of accuracy. Thus quality
control of stereophotogrammetric evaluation should
focus mainly on this expression in order to avoid
regions of insufficient precision.
4. NUMERICAL EXAMPEL
The following page contains a stereo pair (1,2)
taken by a Rolleimetric 6006 (c=51.18) in general
positions. These two images are to be correlated in
order to get their relative orientation. The coor-
dinates of the points of correlation are (in mm):
P’=1 P"z2
X y X y
-10.620 1.694 -1.851 2.316
8.308 0.808 14.936 1.613
-16.623 14.596 -7.583 13.604
17.472 13.804 22.767 17.806
.904 -1.314 | -15.519 -0.481
14.764 -2.293 1.799 -1,931
-21.802 6.968 | -18.058 6.299
-12.778 8.770 -4.346 8.746
0 0 0160500 TO —
|
-—
—
Result of computational correlation:
-0.00391 0.26581 0.01067
Z = | 0.28609 0.01536 -0.99664 |,
-0.00645 1.00000 -0.01313
det(Z) = -0.0001351 + 0 because of neglecting the
conditions of orthonormalization.
Provisional epipole in P’:
(x0’)= 192.457 (yo’)= 1.476
Approximate rotations of P’:
(0) = -16.546 (K’) = -0.488
Provisional epipole in P":
(x0")=-178.264 (yo’)= -0.569
Approximate rotations of P":
(9°) = 147.799 AK)
(52)
The rotations are given in grads.
Matrix of correlation from
(Z)=(1/c32)(R’)TB(R") =
—0.203
-0.868
-0.00404 0.26580 0.01111
= 0.28548 0.01706 -0.99454
-0.00696 1.00000 -0.01310
Error equations:
Nr. dé’ dK’ de ds" dk" 6p
m
1 4.81 -141.38 -2545.03 28.22 -829.52 0.0500 1.0
2 17.77 -1129.97 -2524.54 -0.18 11.25 . 0.0118 1.0
Q’"=| OT and Q12 from (2.3.2). 3 -36.4 132.58 -2731.04 314.63 -1147.66 -1.0271 1.1
Qiz 4 511.63 -1679.62 -2736.65 -106.82 351.20 -1.1611 1.1
5. -1.71 -73.60 -2359.54 -35.51 -1525.32 -0.0885 1.0
Finally, there results the somewhat long but useful 6 *71.63 71860.76 2274.17 -29.04 -566.33 -0.1081 0.9
formula 7 -45.25 348.39 -2479.64 224.47 -1731.91 -0.6591 1.0
8 7.05 -41.83 -2608.91 162.05 -963.52 -0.6622 1.0
OXX OXy Oxz XN’YN” -xu'c
Sm = Oyy Ovz - AN*(Ox"x"*Ox'x'-20x'x") yn’? =-yN’C |+
symm. 02z symmetric c?
2XN' (Ox'x"-Ox' x?) YN ' (Ox'x"-Ox'x* )*XN' (Ox"y'-Ox^ y?) -C(Ox'x"-Ox'x') Ox'x' Ox^y* 0
+AN3 2yN' (Ox"y'-Ox' y?) -C(Ox"y'-Ox'y*) +AN2 Oy'y’ 0
symmetric 0 symmetric 0
(3.3.3)