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Performance evaluation system for inertial navigation equipmentTesting system studies inertial characteristics of gyroscopic devices. System consisting of instrument support package, dynamic test table, torque control electronics, and real-time computer evaluates performance of prototype gyroscopic strapdown units in inertial-grade attitude-reference systems. System is applicable to commercial aircraft.
Document ID
19710000086
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mc Kern, R. A. (MIT)
Date Acquired
August 6, 2013
Publication Date
April 1, 1971
Subject Category
Electronic Systems
Report/Patent Number
MSC-13542
Report Number: MSC-13542
Accession Number
71B10087
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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