Full text: Technical Commission VII (B7)

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International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, Volume XXXIX-B7, 2012 
XXII ISPRS Congress, 25 August — 01 September 2012, Melbourne, Australia 
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Digital Elevation Model ; $- 
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Figure 4. (a) Digital Orthophoto and Digital Elevation Model for Proposed Algorithm; (b) Digital Orthophoto and Digital 
Elevation Model for Google Earth Coordinates 
  
  
Linear Graph X Coordinate 
  
Linear Graph Y Coordinate 
Linear Graph Z Coordinate 
  
  
  
  
  
  
   
    
       
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
(Onboard GPS) (Onboard GPS) (Onboard GPS) 
seu VIG GES RT 1 362600 s 38 
R220.999 a 162400 = 2 
621000 = = y = 0.809x + 2.786 
A 162200 j 2. T 
620600 a A R°-0887 af. 
= ge 5 s a oto 
Ë 620600 ; 9 161800 9 pn 1 
à à 3 Roe 
2 © 5 ® 4 
3 620400 § 161600 $ x e # 
- i Mean AE :5.733 : 161400 Mean AE : 8.064 uo : 
520200 ertet SHE RN Min AE : 0.497 Mir AE : 0.355 : Mean AE : 0.526 
à ber pot NE ES 161200 Max AE : 20.375 NE eei 
ser # : 161000 mum 
619800 160800 0 
519800 620000 620200 620400 620600 520800 62:000 621200 ! 180500 161000 381500 162000 1625C0 1863000 0 5 10 15 20 25 
Actual Actual Actual 
(a) 
Linear Graph X Coordinate Linear Graph Y Coordinate Linear Graph Z Coordinate 
(GE GCP) (GE GCP) (GE GCP) 
621200 162600 20 
v7 1004x - 3004. V=0.391x+ 1368. of y=0.811x 1 2.773 s. 
R^» 0.999 Pa 162400 s nins. 1-052 4 X 
621000 R? = 0.999 as a 
i 162200 : 15 a t * 
SEE P ud 162000 ^ = "y 
Y 620600 #7 Tomo 6 H nF 
i a’ à A à 10 E 
2 QU ir = = => à 
i adios 2 161600 # 2 à 2 
Mean AE : 8.023 481400. beet retro un reer. Mean AE : 8.009 Mean AE : 0.617 
520200 m P MinAE:0.052. — 0 7 a i oe qe des -i Min AE : 0.007 
s Min AE : 0.095 161200 d i Max AE : 16.605 5 in AE : 0. 
T ert eds J AE : 36.25 # ide: | Max AE : 3.507 
620000 / Max AE : 36.25 161007 p ie " 
619800 160800 0 
619800 620000 620200 620400 620600 620800 621000 621200 186500 161000 161500 162000 162500 163000 o 5 10 15 20 25 
Actuaf Actual Actual 
Figure 5. (a) Linear graph X, Y, Z coordinates for GPS onboard; (b) Linear graph X, Y, Z coordinate for Google Earth (GE) coordinates. 
Figure 5 shows that most of points fit in the line 1:1 (red line 
on the graph) for X coordinate and it can be concluded that x 
coordinates for GPS onboard are precise while x coordinates for 
Google Earth (GE) control points are less precise because some of 
the points are located higher and lower than line 1:1. Most of 
points are located exactly in line 1:1 for Y coordinate, thus it can 
be concluded that y coordinates for GPS onboard and GE control 
points are precise and reliable. The situation is different for Z 
coordinate because some of points are randomly located above 
and below line 1:1. However, there is a slight difference between 
GPS onboard and GE control points in which the result of GPS 
onboard showed better precision compared to GE control points. 
In contrast, proposed algorithm gives better precision compared to 
GE control points. However, the detail of points located on line 
1:1 can be viewed if the linear graph is shown in a larger scale 
image size. 
5. DISCUSSION 
497 
In this study, the accuracy of photogrammetric product was 
assessed based on root mean square error, mean absolute error 
and linear fit equation and determination of correlation coefficient 
for each result. The general formula of linear fit equation is 
illustrated in Equation 8. 
y=a+bx (8) 
Where a,b = coefficient data 
As mention in section 3 and section 4, there are two cases in this 
study. The first case is by using GPS onboard as control point and 
integration with proposed algorithm in image registration and the 
second case is image processing by using control points acquired 
from Google Earth coordinates. Both results are divided into X, Y 
and Z coordinate. Therefore, the result of each coordinates can be 
assessed individually. The error distribution of each coordinate 
for GPS onboard and Google Earth coordinate can be viewed 
graphically in Figure 6. Figure 6 shows the results of 
 
	        
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