Full text: Proceedings, XXth congress (Part 1)

ORIENTATION OF SATELLITE AND AIRBORNE IMAGERY FROM MULTI-LINE 
PUSHBROOM SENSORS WITH A RIGOROUS SENSOR MODEL 
Daniela Poli 
Institute of Geodesy and Photogrammetry, ETH Zurich, 8093 Zurich, Switzerland- daniela@geod.baug.ethz.ch 
Commission I, WG 1/5 
KEY WORDS: Pushbroom, Sensors, Modelling, Orientation, Self, Calibration 
ABSTRACT: 
Today CCD linear array scanners are widely used on satellite, airborne and helicopter platforms to provide images with along track 
stereo viewing. For the orientation of this kind of imagery, models based on the rigorous description of the acquisition geometry, on 
rational polynomial functions or on affine transformations are used. An overview is presented. Among these approaches, the model 
developed at the Institute of Geodesy and Photogrammetry (IGP), ETH Zurich, belongs to the class of rigorous models and is 
applicable to a wide class of pushbroom sensors carried on satellite, airplane and helicopter. The model can be used with single-lens 
and multi-lens sensors with synchronous and asynchronous stereo acquisition. The sensor position and attitude are modelled with 2M 
order piecewise polynomials depending on time. Additional pseudo-observations allow the reduction of the polynomial order from 2 
eX 
i 
to | if the trajectory allows it. In case of sensors carried on aircraft, the observations from GPS and INS instruments are integrated in 
the piecewise polynomials and are corrected from constant shifts ans misalignments between the GPS and INS local systems and the 
camera one and systematic errors contained in the observations. A self-calibration is also included for the corrections of radial and 
decentering lens distortions, principal point(s) displacement, focal length(s) variation and CCD line(s) rotation in the focal plane. 
Using a minimum of 6 Ground Control Points (GCPs) and, additionally, Tie Points (TPs), the external orientation and seclf- 
calibration parameters, together with the TPs ground coordinates, are estimated in a least-square adjustment. 
In order to demonstrate the model flexibility and potentials, different imagery from pushbroom sensors (TLS, EROS-AI, SPOT- 
5/HRS, ASTER, MOMS-02, MISR) have been oriented. In this paper a summary of the results obtained are presented and discussed. 
1. INTRODUCTION 
CCD linear array sensors, also called linear scanners, are widely 
used for the acquisition of images at different ground resolution 
for photogrammetric mapping and remote sensing applications. 
They scan the ground surface with an array of CCD elements in 
pushbroom mode. The image is formed by a side-to-side 
scanning movement as the platform travels along its path. 
CCD linear array sensors for remote sensing and 
photogrammetric applications are usually mounted on aerial and 
satellite platforms. Aerial platforms are primarily stable wing 
aircraft, but also helicopters are used. Acquisition from airborne 
sensors are often used to collect very detailed images and 
facilitate the collection of data over virtually any portion of the 
Earth's surface at any time. In space, the acquisition of images is 
sometimes conducted from the space shuttle or, more 
commonly, from satellites for Earth Observation (EO). Because 
of their orbits, satellites permit repetitive coverage of the Earth's 
surface on a continuing basis. Cost is often a significant factor 
in choosing among the various platform options. 
The images provided by linear CCD array sensors have very 
high potentials for photogrammetric mapping at high and low 
scales. 
The triangulation and photogrammetric point determination of 
pushbroom systems are rather different compared to standard 
approaches, which are usually applied for full frame imagery, 
(Haala et al., 2000). Additionally, the use of linear imaging 
sensors is more difficult with respect to photogrammetric data 
processing and requires an increased computational effort 
during the subsequent processing chain including matching, 
DTM and orthoimage generation. 
This work relates to the analysis of the orientation of CCD 
linear scanners. Different models can be found in literature. The 
rigorous ones are based on the photogrammetry collinearity 
equations, which are modified in order to include any external 
and internal orientation modelling. Other approaches are based 
on rational polynomial functions, affine models and direct 
linear transformations. An overview is given in the next section. 
At the Institute of Geodesy and Photogrammetry (IGP), ETH 
Zurich, a rigorous sensor model for the georeferencing of 
imagery acquired by multi-line CCD array sensors, carried on 
airborne or satellite, has been implemented. The model fulfils 
the requirement of being as flexible as possible and being 
adaptable to a wide class of linear array sensors. In fact 
pushbroom scanners show different geometric characteristics 
(optical systems, number of CCD lines, scanning mode and 
stereoscopy) and for each data set specific information are 
available (ephemeris, GPS/INS observations, calibration, other 
internal parameters). Therefore the model needs to be dependent 
on a certain number of parameters that change for each sensor. 
The results obtained with different satellite sensors will be 
presented. 
2. OVERVIEW OF EXISTING MODELS 
For the georeferencing of imagery acquired by pushbroom 
sensors many different geometric models of varying complexity, 
rigor and accuracy have been developed, as described in 
(Fritsch et al., 2000, Hattori et al., 2000 and Dowman et al., 
2003). The main approaches include rigorous models, rational 
  
   
  
  
  
  
  
  
  
  
  
   
  
  
   
  
  
   
  
  
   
   
  
   
   
  
  
  
   
   
   
   
   
   
  
  
  
   
  
  
    
   
   
     
   
  
      
    
  
    
    
    
     
      
  
    
   
   
   
   
   
   
  
   
   
   
   
   
    
Internati 
polynom 
affine prc 
The rigo 
the sensc 
which ar: 
pushbroc 
specific s 
used for 
spacebor 
In case c 
followed 
called 
photogra 
sensor e 
derived 1 
variation 
quadratic 
added: tl 
point co 
paramete 
formulati 
model). 
supplenx 
is availat 
unknown 
orientatic 
(Baltsavi 
Landsat 
advantag 
pushbroc 
paramete 
extended 
The prin 
geometri 
imagery 
method i 
al, 1992 
the so-c: 
images tl 
using La 
orientatic 
All unki 
adjustme 
determin 
points wl 
In the g 
model of 
spacebor 
on MOM 
1995), H 
model is 
imagery, 
spacebor 
paramete 
points, w 
100th re 
paramete 
Lagrange 
orientatic 
e.g. acq 
equation: 
attitude « 
block-im 
depender 
additiona 
each ext
	        
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.