NASA NTRS · 19720000554
Electronic integrator for gyro rate output voltages
Abstract
Circuit 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.
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Crawford, R. A., Hand, P. J., Horiuchi, H. H.. 1972-09-01. Electronic integrator for gyro rate output voltages. https://ntrs.nasa.gov/citations/19720000554
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