Closed loop roll control for momentum biased satellites
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United States of America Patent
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-
Oct 28, 1980
Grant Date -
N/A
app pub date -
Jul 23, 1979
filing date -
Jul 23, 1979
priority date (Note) -
Expired
status (Latency Note)
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Abstract
An attitude control and stabilization system for momentum biased satellites utilizing a pair of counterrotating flywheels mounted parallel to its yaw axis. The speed of one of the wheels of the pair is controlled by sensing and correcting the roll axis errors of the satellite.
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