Experience of One UK Electronic Equipment Supplier With Bite on Engine/Flight Control Systems Over the Past Ten Years — Part 2
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 October 1986
Abstract
The ECU safety system is such that all internal and external fault monitoring circuit outputs are consolidated and passed through a short time‐constant filter to eliminate transient effects. Once this signal appears a 500mS time‐out is started. At the end of this period a lane changeover is initiated together with a cockpit fault warning. If the fault condition is removed during the time‐out period, it is reset.
Citation
de Gaye, R. (1986), "Experience of One UK Electronic Equipment Supplier With Bite on Engine/Flight Control Systems Over the Past Ten Years — Part 2", Aircraft Engineering and Aerospace Technology, Vol. 58 No. 10, pp. 10-14. https://doi.org/10.1108/eb036345
Publisher
:MCB UP Ltd
Copyright © 1986, MCB UP Limited