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Solid-state turn coordinator displayA solid state turn coordinator display which employs light emitting diodes (LED's) as the display medium was developed to demonstrate the feasibility of such displays for aircraft applications. The input to the display is supplied by a fluidic inertial rate sensor used in an aircraft wing leveler system. The display is composed of the LED radial display face and the electronics necessary to address and drive the individual lines of LED's. Three levels of brightness are provided to compensate for the different amounts of ambient light present in the cockpit.
Document ID
19760025098
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Meredith, B. D.
(NASA Langley Research Center Hampton, VA, United States)
Crouch, R. K.
(NASA Langley Research Center Hampton, VA, United States)
Kelly, W. L., IV
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1975
Subject Category
Aircraft Instrumentation
Report/Patent Number
NASA-TM-X-72782
Report Number: NASA-TM-X-72782
Accession Number
76N32186
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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