DEMONSTRATION OF THE APPLICATION OF MAJORITY LOGIC FOR INCREASED RELIABILITY IN AUTOMATIC FLIGHT CONTROL SYSTEMS.
Rept. for 15 May 61-30 Sep 62,
GENERAL ELECTRIC CO SCHENECTADY N Y
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The design and performance are described of a flight control system demonstrator. The demon strator illustrates the enhancement in re liability available through the application of redundancy. It consists of a single axis vehicle simulation controlled by a digital, triply redundant, self-adaptive flight controller with suitable displays. Also included is a reli ability analysis of the demonstration system and a handbook form accumulation of information to aid in the effective application of active redundancy. Author