During the last decade, an increasing number of primary and secondary
fly-by-wire systems have been developed for civil aircraft. These syst
ems have reduced the gap in form and implementation technology which h
ad developed between civil and military electronic flight control syst
ems. However, there remain significant differences. These differences
include systems architecture, redundancy management, external interfac
es, software methods and, to a lesser extent, hardware. This paper des
cribes some of those differences and why they exist. In particular, th
e impact of performance, reliability, availability and safety requirem
ents is considered together with the effect of industry traditions and
standards.