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1. The F-12 series aircraft approach to design for control system reliability

Author

Schenk, F. L and Mcmaster, J. R

Subjects
Aircraft Design, Testing And Performance
Abstract

The 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.

Published
1976

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