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Electronic integrator for gyro rate output voltagesCircuit which integrates spacecraft gyro output voltages to provide analog position signals has been developed. Accurate integration is provided by all solid state system which uses no choppers and takes advantage of commercially available flight qualified components.
Document ID
19720000554
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Crawford, R. A.
Hand, P. J.
Horiuchi, H. H.
Date Acquired
August 6, 2013
Publication Date
September 1, 1972
Subject Category
Electronic Components And Circuits
Report/Patent Number
NPO-11499
Report Number: NPO-11499
Accession Number
72B10555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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