AIRBUS A320/A330/A340 electrical flight controls - A family of fault-tolerant systems

作者: D. Briere , P. Traverse

DOI: 10.1109/FTCS.1993.627364

关键词: Software designCondition monitoringRedundancy (engineering)Reliability engineeringControl channelControl systemComputer scienceFault toleranceFlight control surfacesDependability

摘要: The digital electrical flight control system of the Airbus A320/A330/A340 is discussed. A320 was first civil aircraft equipped with such a system. It certified and entered into service in quarter 1988. A330 A340 have identical systems, closely related to These systems are built very stringent dependability requirements both terms safety (the must not output erroneous signals) availability. basic building blocks fail-safe monitoring computers. channel performs function allocated computer (control surface for example). ensures that operates correctly. A high level redundancy Special attention has been paid possible external aggressions. tolerate hardware software design faults. described together significant differences between A330/A340, experience.

参考文章(3)
Pascal Traverse, Dependability of Digital Computers on Board Airplanes Springer, Vienna. pp. 133- 152 ,(1991) , 10.1007/978-3-7091-9123-1_6
C. FAVRE, Fly-by-wire for commercial aircraft: the Airbus experience International Journal of Control. ,vol. 59, pp. 139- 157 ,(1994) , 10.1080/00207179408923072
Beaudry, Performance-Related Reliability Measures for Computing Systems IEEE Transactions on Computers. ,vol. 27, pp. 540- 547 ,(1978) , 10.1109/TC.1978.1675145