An ultrareliable integrated digital computer for helicoptersThe US Army Fault-Tolerant Architecture (AFTA) has been defined to meet real-time fault-tolerant processing requirements of future Army applications. AFTA is the enabling technology that will allow the Army to configure existing processors and other hardware to provide high throughput and ultrahigh reliability necessary for terrain-following/terrain-avoidance (TF/TA) and nap-of-the-earth (NOE) flight control and other advanced Army applications. A brief description of AFTA's relevant attributes and theory of operation is given. The systems engineering models which permit the configuration on an AFTA to meet mission requirements as they evolve are presented, along with an example of their use to engineer an AFTA configuration. The resulting AFTA configuration, its predicted throughput, reliability, availability, weight, power, volume, and life-cycle cost impact, and the effects of possible engineering tradeoffs are presented.
Document ID
19920066649
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Harper, Richard E. (Charles Stark Draper Laboratory, Inc. Cambridge, MA, United States)
Grant, Gayle (U.S. Army, Avionics Research and Development Activity, Fort Monmouth NJ, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Aircraft Instrumentation
Meeting Information
Meeting: IEEE/AIAA Digital Avionics Systems Conference