Full text: Mapping surface structure and topography by airborne and spaceborne lasers

information within a surface (and a laser surface in particular) 
and the intensity values in imagery allows the concepts from 
image matching methods to be used in developing a suitable 
algorithm for surface matching (Kilian ef al., 1996). 
The mathematical formulation is derived by dividing the 
transformation into two steps, i.e., horizontal and vertical. The 
latter also includes leveling parameters. A similar approach is 
taken in the absolute orientation procedure in traditional 
photogrammetry (Kraus, 1993). Let a target surface be 
represented by 7 irregular distributed points with coordinates 
(x,y,z), and a source surface be represented by ; irregular 
distributed points with coordinates (x",y",z"). These two 
surfaces represent the same real surface, but they may have been 
captured by different methods, which might introduce some 
systematic errors between the two data sets. The problem is to 
determine the transformation parameters required for 
transforming the source surface into the coordinate system of the 
target surface. 
The horizontal transformation between the two surfaces may be 
described by two horizontal shifts, a rotation parameter and a 
scale factor. [Each point from the target surface may be 
transformed to the source surface by these parameters. The 
coordinates in the source surface are calculated by 
x" cos& sink y x") (AX 
y" —sink cosK | y'J ( AY 
where AX,AY are the horizontal shift parameters, xis the 
horizontal rotation and m is the scale factor. 
Once a horizontal transformation has been performed, the 
elevation shift AZ and leveling slopes a,b are introduced, to 
relate the two surfaces by 
z(xLy")eexrby rz" "y "HAZ. (2) 
The differences between the two surfaces in the case described 
here are assumed relatively small. In particular, small leveling 
angles are assumed. Based on this assumption, Equation 2 is 
rewritten as 
z(x^y?)sdgx doy zx" v"rdz, (3) 
where dp,d@ are the small leveling angles. 
The planar coordinates (x",y") from Equation 1 may be 
substituted into the right hand side of Equation 3 and in this way, 
the relationship between the height differences and the planar 
orientation parameters is established. Assuming further that the 
horizontal rotation is also small, and that the scale factor is close 
to 1, provides the following expression: 
z(x^y)2dgx'* doy dZ + 
C ENS : 
+=} s : + ). 
y’| |-dkK dm|| y’| | AY 
   
   
   
   
   
   
   
    
    
     
   
    
    
  
  
  
    
    
    
  
     
   
  
   
   
   
    
  
  
   
   
   
    
  
  
   
     
   
   
    
    
    
    
   
    
International Archives of Photogrammetry and Remote Sensing, Vol. 32, Part 3W14, La Jolla, CA, 9-11 Nov. 1999 
As can be clearly observed, this mathematical model is not linear, 
and therefore must be linearized in order to be solved in a 
standard least-squares method. Applying a Taylor series to the 
equation above, a linear observation equation for each point of 
the source surface is given by 
  
  
  
: ] dant dz 02 497, da dz 
y dx. gy ox 3$ dx dy 
[dp do AZ dk dm AX Nad 
It can be observed that the elevation differences between the two 
surfaces are considered as observations, while gradients are 
required for forming the design matrix. 
The gradients are calculated by reconstructing a small surface 
patch around a point in the target surface, using a planar or 
bilinear surface generation approach, avoiding the need to 
interpolate neither of the surfaces to a regular grid. The decision 
concerning which surface to use is based on an analysis of the 
surface residuals. If large residuals are obtained by 
reconstructing the small surface, a higher order surface is sought. 
Using the described approach, it is clear that in some 
circumstances not all the seven parameters can be accurately 
determined, due to high correlation among them. The number of 
parameters that can be determined depends mainly on surface 
geometry. In the case of matching two horizontal planes for 
instance, only a difference in height may be determined. The 
decision about which parameters to set is based on an analysis of 
the variance-covariance matrix and the surface spectrum. A 
discussion about such analysis is left for another paper. 
It should be noted that the proposed algorithm is suitable for 
surfaces with relatively moderate slopes. Areas with steep slopes 
should be eliminated from the calculations as laser measurements 
in these areas may be affected by large errors. 
3 EXPERIMENTAL RESULTS 
Experiments were conducted by applying the matching algorithm 
to both synthetic and real data. Using a synthetic data set, where 
the 3D transformation between the two surfaces is known, allows 
the elimination of any implementation flaws. Using real data 
indicates the capability of the algorithm to actually determine the 
transformation parameters between a laser surface and a surface 
generated by photogrammetric means. 
3.1 Experiments with synthetic data 
The synthetic data used for the experiments consists of a surface 
with a known parametric function, as shown in Figure 1. A large 
number of randomly distributed points on this surface were 
calculated to represent a target surface. These points are 
represented in Figure 1 as a triangular network. To simulate the 
affect of errors on the data, random noise was added to the 
elevations of these points. Another smaller set of 30 randomly 
distributed points was created in the same manner, which 
constitutes the source surface. These points were shifted and 
rotated by selected parameters, and therefore it was possible to 
   
International 
check the quality of th 
matching algorithm. TI 
the target surface by calc 
A stable solution for all 
within 3-4 iterations 
determined values of th 
for simulating the tran 
elevation differences be 
surface and the target su 
added initially to the tar; 
In another test with th 
errors in some points of 
efforts were made to re 
found that outliers in or 
not affect the ability of 
parameters. 
  
Figur: 
3.2 Experiments with 1 
Further testing was ur 
aerial imagery covering 
These data contain poin 
Mapper (ATM)  lase 
photography from NGS 
altimeter developed by | 
clevation changes in po 
systems. The instrument 
capability. 
Figure 2 shows part of 
area. For this testing 
measured manually on 
Several combinations o 
surface. The results of 
these sets. The first se 
second set contains two 
Each planar segment 
which was determined 1 
segment, the appropriat:
	        
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