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Conceptual nonorthogonal gyro configuration for guidance and navigationNonorthogonal sensor configuration using six single-degree-of-freedom inertial reference gyroscopes and a complete data processing and self-contained failure detection-and-isolation mechanism provides redundant capabilities to guidance and navigation systems. This system has been formulated in a strap-down configuration to attain maximum redundancy.
Document ID
19670000433
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Gilmore, J. P.
Date Acquired
August 3, 2013
Publication Date
November 1, 1967
Subject Category
Electronic Components And Circuits
Report/Patent Number
MSC-11363
Report Number: MSC-11363
Accession Number
67B10433
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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