Title :
An ultrareliable integrated digital computer for helicopters
Author :
Harper, Richard E. ; Grant, Gayle
Author_Institution :
Charles Stark Draper Lab., Cambridge, MA, USA
Abstract :
The 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 the high throughput and ultrahigh reliability necessary for terrain-following/terrain-avoidance and nap-of-the-earth 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
Keywords :
aerospace computer control; aircraft control; fault tolerant computing; helicopters; military equipment; real-time systems; AFTA; TF/TA flight control; US Army Fault-Tolerant Architecture; helicopters; nap-of-the-earth flight control; real-time fault-tolerant processing; systems engineering models; terrain-following/terrain avoidance flight control; ultrareliable integrated digital computer; Aerospace engineering; Application software; Computer architecture; Fault tolerance; Hardware; Helicopters; Military computing; Power engineering and energy; Reliability engineering; Throughput;
Conference_Titel :
Digital Avionics Systems Conference, 1991. Proceedings., IEEE/AIAA 10th
Conference_Location :
Los Angeles, CA
DOI :
10.1109/DASC.1991.177156