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AIRBUS state of the art and practices on FDI and FTC in flight control system

机译:空中客车飞控系统中FDI和FTC的最新技术和实践

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This paper deals with industrial practices and strategies for Fault Tolerant Control (FTC) and Fault Detection and Isolation (FDI) in civil aircraft by focusing mainly on a typical Airbus Electrical Flight Control System (EFCS). This system is designed to meet very stringent requirements in terms of safety, availability and reliability that characterized the system dependability. Fault tolerance is designed into the system by the use of stringent processes and rules, which are summarized in the paper. The strategy for monitoring (fault detection) of the system components, as a part of the design for fault tolerance, is also described in this paper. Real application examples and implementation methodology are outlined. Finally, future trends and challenges are presented. This paper is a full version of the invited plenary talk presented by the author on the 1st July 2009 at the 7th IFAC Symposium Safeprocess '09, Barcelona.
机译:本文主要针对典型的空中客车电气飞行控制系统(EFCS),探讨民用飞机的容错控制(FTC)和故障检测与隔离(FDI)的工业实践和策略。该系统旨在满足表征系统可靠性的安全性,可用性和可靠性方面的严格要求。通过使用严格的过程和规则将容错设计到系统中,本文对此进行了总结。本文还介绍了监视(故障检测)系统组件的策略,作为容错设计的一部分。概述了实际的应用示例和实现方法。最后,提出了未来的趋势和挑战。本文是作者在2009年7月1日于巴塞罗那举行的第七届IFAC研讨会Safeprocess '09上提出的邀请全体演讲的完整版。

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