Publication Date:
2017-10-02
Description:
Highly reliable fault-tolerant computer systems are discussed for use in flight-critical avionic and control systems of future commercial transport aircraft. Such aircraft are envisioned to have integrated systems, to be terminally configured, and to be equipped with fly-by-wire flight control systems, all of which require highly reliable, fault-tolerant computers. Two candidate computer architectures are identified as having the potential of satisfying the commercial transport aircraft requirements.
Keywords:
COMPUTER SYSTEMS
Type:
AGARD Integrity in Electron. Flight Control Systems; 17 p
Format:
text
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