Full text: CMRT09

CMRT09: Object Extraction for 3D City Models, Road Databases and Traffic Monitoring - Concepts, Algorithms, and Evaluation 
188 
Preparatory work regarding the existing database is required in 
order to exploit the on-line segmentation results in a pilot 
assistance system. A set of planar surfaces characterizing the 
urban terrain is needed for the later comparison (e.g. facades, 
rooftops). In our experiments, even this information originated 
from previously collected ALS data, which were recorded under 
optimal DGPS conditions, but it might as well be derived from 
any other existing city model. 
Within our approach, we assume that INS navigation is 
continuously available and that we have an initial guess of the 
sensor position (e.g. from non-differential GPS). If we have to 
navigate through GPS dropouts, the positioning accuracy will 
degrade because of INS drift effects, but we can assume that the 
measured ALS data are still roughly aligned to the stored 
information. In addition to their position in 3D space, features 
like size and normal direction are assigned to all segmented 
planar patches, thus it is comparatively easy to find 
corresponding objects in the database. We use this information 
to achieve precise alignment between the measured ALS data 
and the existing city model, which finally enables us to correct 
the presumed sensor position. 
1.3 Related work 
In recent years, airborne laser scanning systems have been 
explored by various scientists from different points of view. The 
complexity of ALS data acquisition leads to a number of 
potential error sources. Schenk (2001) and Filin (2003) address 
this problem and categorize different influences that should be 
considered. In addition to varying exactness of the navigational 
information sources, several systematic effects can lead to 
reduced point positioning accuracy. Exemplary limiting factors 
are scanning precision and range resolution of the specific laser 
scanning device. Other negative effects can be introduced by 
inaccurate synchronization of the system components. 
Considerable discrepancies are caused by mounting errors or 
disregarded lever arms (displacements between laser scanner, 
INS, and GPS antenna). Skaloud and Lichti (2006) approached 
this problem with a rigorous method to estimate the system 
calibration parameters such that 3D points representing a plane 
are conditioned to show best possible planarity. In order to use 
ALS within the scope of aircraft navigation, we presuppose that 
the sensor system has been calibrated beforehand. 
Some procedures described in this paper are concerned with the 
segmentation of point clouds into planar surfaces. Many 
different methods regarding this topic can be found in literature. 
Some authors are interested in detecting even more kinds of 
objects like spheres, cylinders, or cones. Rabbani et al. (2007) 
describe two methods for registration of point clouds, in which 
they fit models to the data by analyzing least squares quality 
measures. Vosselman et al. (2004) use a 3D Hough transform to 
recognize structures in point clouds. Filin & Pfeifer (2006) 
propose a segmentation method that is based on cluster analysis 
in a feature space. Among all available approaches, the 
RANSAC algorithm (Fischler & Bolles, 1981) has several 
advantages to utilize in the shape extraction problem (Schnabel 
et al., 2006). We apply a RANSAC-based robust estimation 
technique to fit straight line segments to the scan line data. 
Moreover, an extension of this method is used to identify 
locally planar patches in the model data. The amount of outliers 
lets us distinguish between buildings and irregularly shaped 
objects like trees. Fundamental ideas on fast segmentation of 
range data into planar regions based on scan line analysis have 
been published by Jiang and Bunke (1994). Their algorithm 
divides each row of a range image into straight line segments 
which are combined in a region growing process. Despite the 
fact that we are considering continuously recorded scan lines 
instead of range images, we basically follow this approach 
during the on-line data analysis. 
Several existing concepts of terrain-based navigation for aerial 
vehicles can be found, e.g. image based navigation (IBN), 
terrain-following radar (TFR), or terrain contour matching 
(TERCOM). Other than these methods, laser scanning is a 
comparatively new technique. Toth et al. (2008) propose the use 
of LiDAR for terrain navigation, as it provides distinct 3D 
measurements that can easily be used for exact comparison to 
previously recorded data. In their concept, the iterative-closest- 
point algorithm (Besl & McKay, 1992) is chosen for surface 
matching. Instead of an 1CP approach, we identify matching 
planar objects with regard to several geometric features (i.e. 
position, size, normal direction). Similar methods have 
demonstrated high performance for markerless TLS registration 
(Brenner et al., 2008). The problem of determining the 
transformation parameters is transferred to a system of linear 
equations that can be solved immediately. 
2. EXPERIMENTAL SETUP 
Data used for this study were collected during a field campaign 
in 2008, using the sensor equipment that is briefly described in 
this section. 
2.1 Sensor carrier 
The sensors described below have been attached to a helicopter 
of type BellUH-lD (Figure 1). Laser scanner and IMU are 
mounted on a common sensor platform at the side of the 
helicopter, which can be tilted to allow different perspectives, 
i.e. nadir or oblique view. In an operational system, the pilot 
must be able to react to upcoming dangers, e.g. during degraded 
visibility conditions. Therefore, an obliquely forward-looking 
sensor configuration was used in our experiments. The lever 
arms of the components in the system are known, and the 
correct bore-sight angles have been determined. Calibration of 
these parameters is not topic of this paper, suitable methods can 
be found in (Skaloud & Lichti, 2006). 
2.2 Laser Scanner 
The RIEGL LMS-Q560 laser scanner makes use of the time-of- 
flight distance measurement principle with a pulse repetition 
rate of 100 kHz. Opto-mechanical beam scanning provides 
single scan lines, where each measured distance can be 
georeferenced according to position and orientation of the
	        
Waiting...

Note to user

Dear user,

In response to current developments in the web technology used by the Goobi viewer, the software no longer supports your browser.

Please use one of the following browsers to display this page correctly.

Thank you.