DESIGN AND SIMULATION OF A REAL-TIME MAPPING SATELLITE FOR
THE KINGDOM OF SAUDI ARABIA
Abdulaziz I. Alobaida and Kurt Novak
Military Institute of Surveying and Geographical Studies
P.O. Box 89088, Riyadh 11682
Saudi Arabia
Tel.: ( ).; Fax: ( )
ABSTRACT
The goal of this interdisciplinary research is to design a mapping
and remote sensing satellite system (to be named SULTAN) for the
Kingdom of Saudi Arabia (KSA) and its neighbouring regions and to
prove its mapping feasibility by a simulation Study. It will be
equipped with state-of-the-art remote sensing, positioning, and
attitude determination technology that is either currently
available or will be available in the near future. The satellite
System should provide the users with spatial data capable of
producing maps and map substitutes of scale 1/25,000 without the
need for ground control.
Two options are suggested and analyzed -- a system of one satellite
or of two satellites. In the case of a one-satellite system, a
threefold stereoscopic line scanner sensor will be investigated.
The second mapping system consists of two satellites, both equipped
in the above similar manner. The orbits of both satellites are
similarly inclined and separated by about 2.6 degrees in the right
ascension of their ascending nodes. These orbits were specifically
chosen such that an area on the equator of the Earth would be
covered by the vertically looking sensors of the first satellite
and about 30 degrees, off the nadir, titled sensors on the second
satellite. With this configuration, a specific scene can be
covered by six images, three from each satellite.
The orbits of the system will be. as low as possible, sun-
synchronous, possibly minimum-drift orbits, nearly circular and
polar. The positions of the satellites will be determined by on-
board GPS receivers, while the sensors attitude will be determined
by one or more stellar sensors.
The general form of the collinearity equation is used in which a
linear and higher order functions interpolate between orientation
images to relate image coordinates, sensor parameters, and ground
coordinates.
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