International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, Vol XXXV, Part B3. Istanbul 2004
T from the coordinate system of HISS to a world coordinate
system is calculated, where the origin of HISS is at the center of
GPS antenna. On the other hand, a transformation matrix La
from the coordinate system of LD-A and a transformation
matrix 7, from the coordinate system of line camera to the
coordinate system of HISS are calculated based on the exterior
calibration parameters. A laser point with a range distance of r
at the angle of a on scanning plan is geo-referenced to the
world coordinate system as follow,
(x.v.2]l) = Ty Ty, (=r sin æ,0,-r cos 1)” (1)
In the case of line image, focus length (/) of the line
camera as well as a formula defining the relationship between
the index of an image pixel (/) and its projection angle (o)
towards the projection axis is obtained from sensor's
specification.
® = 2xarcsin((h — 0)/2/ f) (2)
where o is the image center, which is obtained by doing
physical measurement using sample images. Using formula 2,
projection vector of the image pixel (h) is geo-referenced to the
world coordinate system as follows,
(x, p,2,0)" - T, T, (0,-cosæ,sin w,0" (3)
An example of line images, a view of geo-referenced laser
points, as well as a projection of laser points onto line images is
shown in Figure 4.
EEE
Tie Vee Zoom (Pm
Figure 4. An example of the geo-referenced laser points and line
images
Figure 5. A motivational example of erroneous geo-referencing
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Figure 6. A set of tie points on building corners
3. RECTIFICATION OF GPS/INS PARAMETERS
In the followings, we will first introduce the method for
rectifying GPS/INS parameters at each updates using a number
of ground truths. The method for obtaining the true value of
position and orientation parameters at a number of GPS/INS
updates is addressed subsequently.
3.1 Rectification using a number of ground truths
Let (9.50,,0,) denote the xyz coordinates of vehicle position,
(w,y,x) denote the roll, pitch and yaw angles of vehicle
orientation, transformation from HISS to the world coordinate
system can be formulated as follows.
T. = Shv-R, - R, +R, (4)
where
10. 0 o. cosk (= sink 0.0
0-10 0} sink cosx #00}
Shv = “| R=
00 4-9. 0 0 1 0
0520 0 | = 0 a |
cosy 0 —siny O0 | 0 0 0
0 l 0 0p 0 coso -sino 0
R,=| | R= ;
siny 0 cosy O0 0 sino cosw 0
0 0 0 I 0 — 9 0 I
In this research, four parameters at each GPS/INS update,
ie. o 20.20 of vehicle position andk of vehicle orientation,
x2 yt
are corrected, while pitch and roll angles remain as they are, as
the errors inside are not so obvious comparing to other
parameters. Let
p-Q,yz4) =R,RT,(-rsina,0,~rcosa,l) 6)
denote the calculations on the parameters that will not be
adjusted. Geo-referencing of a laser point p = (x, y,z,1)" can
be re-formularized as follows,
p=Shv-R_-p (6)
More specifically,
P, = p, *cosk— p, *sink+o,
(7)
P, = P, *sink + p, *cosk+o,
p.e pte,
Figure 5 shows a motivational example of erroneous geo-
referencing, where the denotation of 7; is simplified to 7,
g
representing the transformation matrix that is composed of the
position and orientation parameters at GPS/INS update #. 7°
denotes the true value of 7, 2, =T" T, is the vehicle's
relative motion (relative transformation) from GPS/INS update
#i to #. Suppose the true transformation matrixes at the
GPS/INS updates #s and #e are known, where D-T.T' eT.
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