Full text: XVIIth ISPRS Congress (Part B4)

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APPLICATION OF DIGITAL CAMERAS AND 
GPS FOR AERIAL PHOTOGRAMMETRIC 
MAPPING 
Kurt Novak 
Department of Geodetic Science and Surveying, Center for Mapping 
The Ohio State University 
Commission I 
ABSTRACT 
This paper describes the development and application of a fully digital, aerial image 
acquisition system which is integrated with GPS. A high resolution digital camera captures 
overlapping vertical images from an airplane. The exposure stations are tagged with the 
GPS time and the accurate position of the airplane. During post-processing images and 
navigation data are integrated. All information is stored in an image data-base related to a 
GIS. Kinematics GPS is applied to determine the exposure stations within ten centimeters. 
An aerial triangulation solves for additional camera parameters and is controlled by the GPS 
locations of the perspective centers. The major application of this new system will be the 
mapping of utility lines, roads, pipelines, and the generation of digital elevation models and 
orthophotos for engineering applications. 
Keywords: Aerotriangulation, Camera, Digital Systems, GPS, Integrated System 
1. INTRODUCTION 
The development of integrated mobile mapping systems 
is a major research focus at the Center for Mapping of the 
Ohio State University. The most famous so far is probably 
the GPS-Van, which is a vehicle-based mapping system that 
combines GPS, inertial sensors and a digital stereo-vision 
system for creating highway inventories (Novak, 1991; 
Bossler et al., 1991). The same sensors used in the GPS- 
Van can also be implemented in an airplane. Some hardware 
components are not absolutely necessary in the airplane, 
such as the inertial system or a second camera, as the 
parameters measured by these devices can be easily 
recovered by analytical triangulation techniques. 
The digital aerial mapping system described in this paper 
was named MapCam. It consists of a fully digital, high- 
resolution, frame CCD camera that can capture imagery at 
pre-defined times and store the data on a digital tape. A GPS 
receiver operating in kinematic mode allows to tag the 
images with the accurate position of the airplane; it is applied 
during post-processing to control aerial triangulation. All 
information captured during the flight is stored in a GIS; 
flight-lines and exposure stations define a geographic 
reference, and the images are stored relative to these 
locations as attributes. Any image can be displayed on the 
computer-screen by selecting its geographic location on a 
digital map. All photogrammetric operations, such as image 
coordinate measurement, aerial triangulation, DEM and 
feature extraction can be done on a post-processing 
workstation semi-automatically. The extracted information 
is directly available in the GIS. 
GPS controlled aerial triangulation is being applied 
operationally by various organizations (Lapine, 1990). The 
purpose of GPS is to eliminate ground control for aerial 
mapping; to our knowledge, however, all applications relate 
to metric, aerial, film cameras, so that the analysis of the 
imagery must be done by an operator on an analog or 
analytical stereo-plotter. 
Electronic cameras have been applied for remote sensing 
purposes in airplanes. In most cases low resolution, analog 
video cameras were used. Some special sensors have been 
developed for digital, aerial mapping, such as the MOMS 
(Ebner et al., 1991) camera. Both are based on pushbroom 
type CCD arrays, which provide in-flight stereo by a 
vertical, as well as a forward and an aft-looking scan. The 
high price of these systems, which are mostly at the 
prototype stage, and the complicated geometrical camera 
model prohibited their wide distribution to date. To our 
knowledge nobody experimented with high-resolution frame 
CCD cameras together with GPS in airplanes. 
In this paper various aspects of the development of 
MapCam are discussed. In the next chapter the hardware 
components are described. Then we explain the 
mathematical model which we applied to perform aerial 
triangulation and camera calibration. Some products, such 
as DEMs and digital orthophotos, are derived and displayed 
in a 3-dimensional perspective view. In the final chapter 
potential applications are shown to demonstrate the 
versatility of MapCam. 
2. HARDWARE COMPONENTS 
The MapCam system consists of three major 
components: a digital, high resolution CCD camera, a GPS 
receiver and a computer-control and storage unit. Our CCD 
camera is a Kodak Hawkeye M-3 (figure 1), which 
incorporates a solid state CCD sensor of 1280 (H) x 1024 
(V) pixels in the body of a regular Nikon F-3 camera. The 
exposure is controlled by the electronics of the Nikon 
camera. It applies a slit-type focal plane shutter. The CCD 
sensor transfers digital data to a frame buffer, which is 
installed in a separate box together with a portable harddisk 
that holds up to 120 images. The Hawkeye M-3 camera can 
be operated from a battery and can be easily carried around. 
In order to circumvent the limitations of the harddisk we 
connected the data-capture box to a digital tape drive 
(Exabyte) through a SCSI interface. We also included a 
data-compression board to reduce transfer rates and save 
storage space. One Exabyte tape holds up to 5 GBytes of 
uncompressed data which corresponds to 3,850 images. 
Currently data-transfer is limited to one image per second. 
We experimented with two different types of GPS 
systems: for metric mapping applications we used a pair of 
Trimble 4000 ST survey-quality receivers. They operate in 
kinematic mode, which means that one is positioned over a 
known base-station, the other is mounted on the fuselage of 
our top-wing airplane. They are both observing phases of 
the GPS carrier signal, and provide a clock for 
synchronizing all components of MapCam. With these type 
of receivers we can completely eliminate ground control for 
aero-triangulation, as the exposure stations can be 
determined to better than 10 cm. However, satellite lock 
must be maintained continuously once the airplane's GPS 
antenna was initialized over a known target on the runway. 
This means that the pilot must fly very wide turns without 
banking the airplane. 
 
	        
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