Difference between revisions of "Double Integrating Gyro"
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Double Integrating Gyro
</dt>
A single-degree-of-freedom gyro having
essentially no restraint of its spin axis about the output axis. In this gyro
an output
signal is produced by gimbal angular displacement, relative to the base, which
is proportional to the double integral of the angular rate of the base about
the input axis.
</dd>
References
This article is based on NASA's Dictionary of Technical Terms for Aerospace Use