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The F-12 series aircraft approach to design for control system reliabilityThe F-12 series aircraft control system design philosophy is reviewed as it pertains to functional reliability. The basic control system, i.e., cables, mixer, feel system, trim devices, and hydraulic systems are described and discussed. In addition, the implementation of the redundant stability augmentation system in the F-12 aircraft is described. Finally, the functional reliability record that has been achieved is presented.
Document ID
19760024078
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schenk, F. L. (Lockheed-California Co. San Diego, CA, United States)
Mcmaster, J. R. (Lockheed-California Co. San Diego, CA, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1976
Publication Information
Publication: NASA. Dryden Flight Res. Center Advanced Control Technol. and its Potential for Future Transport Aircraft
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N31166
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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