Method and apparatus for tracking satellites in inclined orbits
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United States of America Patent
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-
Dec 31, 1991
Grant Date -
N/A
app pub date -
May 8, 1990
filing date -
May 8, 1990
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
A computerized antenna mount system for continuously tracking a satellite in geosynchronous orbit that has an inclined orbit with respect to the equator. An antenna mount that automatically adjusts the declination angle of a ground station satellite antenna as a function of time after iteratively compiling the declination angle history from one complete orbit of a satellite. Different satellite orbits may be so compiled with selection of each satellite and its corresponding orbit information from memory.
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