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Solid-state controllerAttitude controllers are used to guide roll, pitch, and yaw of vehicle in flight. Controllers enclose multitude of switches, gears, cams, and other hardware needed to transmit pilot's commands to attitude control systems. New design, using magnetic coupled transducers, eliminates many mechanical parts, improving reliability and reducing maintenance.
Document ID
19730000466
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Bailey, C. L.
Date Acquired
August 7, 2013
Publication Date
March 1, 1974
Subject Category
Mechanics
Report/Patent Number
MSC-12394
Report Number: MSC-12394
Accession Number
73B10466
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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