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.
Type:
Grant
Filed:
May 8, 1990
Date of Patent:
December 31, 1991
Assignee:
HTS
Inventors:
W. Daniel Gorton, James Burr, Timothy Morris, David C. Tigwell, Michael Cavanaugh