Method for optimizing spacecraft yaw pointing to minimize geometric pointing error in antenna systems
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United States of America Patent
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Issued Date -
Mar 11, 2004
app pub date -
Aug 22, 2002
filing date -
Aug 22, 2002
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
Payload performance is optimized by determining yaw trajectory employing a method which develops a mathematical expression to define the payload in terms of `n` location(s) on the earth; determining the pointing error of the `n` location(s); combining the error so as to product a single performance parameter and minimizing the value of the performance parameter by appropriately varying yaw.
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