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'''Double Integrating Gyro'''
 
</dt><BR/>A single-degree-of-freedom [[Gyro|gyro]] having 
essentially no restraint of its spin axis about the output axis. In this gyro 
an [[Output|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 [[NASA SP-7|Dictionary of Technical Terms for Aerospace Use]]''
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