Graphical symptom abstraction first draft after split
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*.bbl
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*.blg
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*paper.tex
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*_paper.tex
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*.txt
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@ -2,18 +2,25 @@
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#
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# Make the propositional logic diagram a paper
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#
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SOURCE = symptom_abstraction.tex
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all:
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pdflatex symptom_abstraction.tex
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okular symptom_abstraction.pdf
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# abstract.tex algorithm.tex fmmd.tex introduction.tex paper.tex process.tex sys_abs.tex topbot.tex
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#paper: paper.tex logic_diagram_paper.tex
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# latex paper.tex
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# dvipdf paper
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# okular paper.pdf
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paper: paper.tex symptom_abstraction_paper.tex $(SOURCE)
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#cat introduction.tex | sed s/chapter/paper/ > introduction.tex
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#latex paper.tex
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#dvipdf paper pdflatex cannot use eps ffs
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pdflatex paper.tex
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mv paper.pdf symptom_ex_process_paper.pdf
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okular symptom_ex_process_paper.pdf
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# Remove the need for referncing graphics in subdirectories
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#
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#logic_diagram_paper.tex: logic_diagram.tex
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# cat logic_diagram.tex | sed 's/logic_diagram\///' > logic_diagram_paper.tex
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symptom_abstraction_paper.tex: symptom_abstraction_paper.tex paper.tex $(SOURCE)
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cat symptom_abstraction.tex | sed 's/symptom_abstraction\///' > symptom_abstraction_paper.tex
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bib: $(SOURCE)
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bibtex paper
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symptom_abstraction/paper.tex
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35
symptom_abstraction/paper.tex
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\documentclass[a4paper,10pt]{article}
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\usepackage{graphicx}
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\usepackage{fancyhdr}
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\usepackage{tikz}
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\usepackage{amsfonts,amsmath,amsthm}
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\usepackage{algorithm}
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\usepackage{algorithmic}
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\usepackage{ifthen}
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\newboolean{paper}
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\setboolean{paper}{true} % boolvar=true or false
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%\input{../style}
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%\newtheorem{definition}{Definition:}
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\begin{document}
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\pagestyle{fancy}
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%\outerhead{{\small\bf Symptom Extraction Process}}
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%\innerfoot{{\small\bf R.P. Clark } }
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% numbers at outer edges
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\pagenumbering{arabic} % Arabic page numbers hereafter
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\author{R.P.Clark}
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\title{Symptom Extraction Process}
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\maketitle
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\input{symptom_abstraction_paper}
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\bibliographystyle{plain}
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\bibliography{../vmgbibliography,../mybib}
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\today
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\end{document}
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\ifthenelse {\boolean{paper}}
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{
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\begin{abstract}
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In modular systems design, it is often very useful to
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know the failure modes of the sub-systems used.
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This paper outlines a technique for determining the failure modes of a sub-system given
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its component parts.
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%, and the failure modes of those parts.
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The technique uses a graphical notation, based on Euler\cite{eulerviz} and Constraint
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diagrams\cite{constraint} to model failure modes and failure mode common symptom collection.
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The technique is designed for making building blocks for a hierarchical fault model.
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Once the failure modes have been determined for a sub-system,
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that sub-system may be treated as a `component' or `black box' and used
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in conjunction with other such analysed sub-systems, to model
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higher level sub-systems. In this way a hierarchy to represent the fault behaviour
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of a system can be built.
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%FMMD hierarchy
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The hierarchy is built from the bottom up.
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Starting with component failure modes at the bottom.
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Because the process is bottom-up, syntax checking and tracking can ensure that
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no component failure mode can be overlooked.
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Once a hierarchy is in place it can be converted into a fault data model.
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From the fault data model, automatic generation
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of FTA\cite{nasafta} (Fault Tree Analysis) and mimimal cuts sets\cite{nucfta} are possible.
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Also statistical reliability\cite{en61508} and MTTF (Mean Time to Failure) calculations can be produced
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automatically, where component failure mode statistics are available\cite{mil1991}.
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This paper focuses on the process of building the blocks that are used in the hierarchy.
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This paper applies the symptom extraction technique
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using Propositional Logic diagrams, to identify
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symptom groups in functional~groups under
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analysis.
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\end{abstract}
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}
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{}
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{
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\section{introduction}
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This chapter applies the symptom extraction technique
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using Propositional Logic diagrams, to identify
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symptom groups in functional~groups under
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analysis.
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}
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%\clearpage
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\section{Introduction}
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Fault finding is intinctively performed from the top-down.
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A faulty piece of equipment is examined and will have a
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symptom or specific fault. The area or sub-system within the
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equipemnt will next be looked into. Secific measurements
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and checks will be made, and finally a component or a low level sub-system
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will be found to be faulty.
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The technique here works the other way. It works from the bottom up.
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Starting with a collection of compoents that form
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a simple functional group, the effect of all component error modes are
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examined, as to their effect on the functional group.
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The effects on the functional group can then be collected as common symptoms,
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and now we may treat the functional group as a component. It has a known set of failure modes.
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By working from the bottom up, we can trace all possible sources
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that could cause a particular mode of equipment failure.
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This means that we can obtainm statistical estimates based on the known reliabilities
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of the components.
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It also means that every component failure mode must at the very least be considered.
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\subsection{Static Analysis}
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In the field of safety critical engineering; to comply with
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European Law a product must be certified under the approriate `EN' standard.
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Typically environmental stress, EMC, electrical stressing, endurance tests,
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software~inspections and project~management quality reviews are applied\cite{sccs}.
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Static testing is also applied. This is theoretical analysis of the design of the product from the safety
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perspective.
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Three main techniques are currenly used,
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Statistical failure models, FMEA (Failure mode Effects Analysis) and FTA (Fault Tree Analysis).
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The technique outlined here aims to provide a mathematical frame work
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to assist in the production of these three results of static analysis.
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{
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The aims are
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\begin{itemize}
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\item To automate the process where possible
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\item To apply a documented trail for each analysis phase (determination of functional groups, and analysis of component failure modes on those groups)
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\item To use a modular approach so that analysed sub-systems can be re-used
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\item Automatically ensure no failure mode is unhandled
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\item To produce a data model from which FTA, FMEA and statistical failure models may be obtained automatically
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\end{itemize}
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}
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\subsection{Systems, functional groups, sub-systems and failure modes}
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It is helpful here to define some terms, `system', `functional~group', `component', `base~component' and `sub-system'.
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A System, is really any coherent entity that would be sold as a safety critical product.
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A sub-system is a system that is part of some larger system.
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For instance a stereo amplifier separate is a sub-system. The
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whole Sound System, consists perhaps of the following `sub-systems':
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CD-player, tuner, amplifier~separate, loudspeakers and ipod~interface.
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%Thinking like this is a top~down analysis approach
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%and is the way in which FTA\cite{nucfta} analyses a System
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%and breaks it down.
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A sub-system will be composed of component parts, which
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may themselves be sub-systems. However each `component part'
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will have a fault/failure behaviour and it should
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always be possible to obtain a set of failure modes
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for each `component'.
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If we look at the sound system again as an
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example; the CD~player could fail in serveral distinct ways, no matter
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what has happened to it or has gone wrong inside it.
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Using the reasoning that working from the bottom up forces the consideration of all possible
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component failures (which can be missed in a top~down approach)
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we are presented with a problem. Which initial collections of base components should we choose ?
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For instance in the CD~player example; to start at the bottom; we are presented with
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a massive list of base~components, resistors, motors, user~switches, laser~diodes all sorts !
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Clearly, working from the bottom~up we need to pick small
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collections of components that work together in some way.
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These are termed `functional~groups'. For instance the circuitry that powers the laser diode
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to illuminate the CD might contain a handful of components, and as such would make a good candidate
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to be one of the base level functional~groups.
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In choosing the lowest level (base component) sub-systems we would look
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for the smallest `functional~groups' of components within a system. A functional~group is a set of components that interact
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to perform a specific function.
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When we have analysed the fault behaviour of a functional group, we can treat it as a `black box'.
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We can now call our functional~group a sub-system. The goal here is to know how will behave under fault conditions !
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%Imagine buying one such `sub~system' from a very honest vendor.
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%One of those sir, yes but be warned it may fail in these distinct ways, here
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%in the honest data sheet the set of failure modes is listed!
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This type of thinking is starting to become more commonplace in product literature, with the emergence
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of reliability safety standards such as IOC1508\cite{sccs},EN61508\cite{en61508}.
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FIT (Failure in Time - expected number of failures per billion hours of operation) values
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are published for some micro-controllers. A micro~controller
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is a complex sub-system in its self and could be considered a `black~box' with a given reliability.
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\footnote{Microchip sources give an FIT of 4 for their PIC18 series micro~controllers\cite{microchip}, The DOD
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1991 reliability manual\cite{mil1991} applies a FIT of 100 for this generic type of component}
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As electrical components have detailed datasheets a useful extension of this would
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be failure modes of the component, with environmental factors and MTTF statistics.
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Currently this sort of information is generally only available for generic component types\cite{mil1991}.
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%At higher levels of analysis, functional~groups are pre-analysed sub-systems that interact to
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%erform a given function.
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\vspace{0.3cm}
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%\begin{table}[p]
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@ -208,7 +81,9 @@ in a region enclosed by the contours representing the failure modes it investiga
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The effect on the sub-system of each test case is analysed.
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%It is then represented on the diagram by an asterisk on the contour representing the failure mode.
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The `test~case~results' are archived.
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The `test~case~results' are archived.
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That is to say the results from each test case are now associated with the
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asterisk point.
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When all test cases have been analysed, we switch our attention to a higher abstraction level.
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% We treat the sub-system as a black box, or as a component part itsself.
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% We can now look at the test case results from the perspective of a `user'
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@ -268,7 +143,7 @@ is represented as a contour. These contours represent the failure modes of the s
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\section{A general Sub-System example}
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Consider a functional group $FG$ with component parts $A$,$B$ and $C$.
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Consider a functional group $FG$ with component parts $C_1$,$C_2$ and $C_3$.
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Each part has a set of related fault modes (i.e. ways in which it can fail to operate correctly).
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Let us define the following failure modes for each component part, defining a function $FM()$ where $K$
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is a component part and $F$ is its set of failure modes\footnote{Base component failure modes are defined, often with
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@ -281,9 +156,9 @@ $$
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\\
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For our example above
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\\
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$$ FM(A) = \{ a_1, a_2, a_3 \} $$
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$$ FM(B) = \{ b_1, b_2 \} $$
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$$ FM(C) = \{ c_1, c_2 \} $$
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$$ FM(C_1) = \{ a_1, a_2, a_3 \} $$
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$$ FM(C_2) = \{ b_1, b_2 \} $$
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$$ FM(C_3) = \{ c_1, c_2 \} $$
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We can now represent the sub-system as a set of component faulure modes $FG_{cfm}$,
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thus
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@ -371,7 +246,7 @@ This is performed on the diagram by linking the test cases with lines to form `s
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For the sake of example let us consider the fault symptoms $SP1 = \{fs_2, fs_4, fs_5\}$ to be an identical
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failure mode at the {\em sub-system} level. These can then be joined to form a spider. Likewise
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let $SP2 = \{fs_1, fs_3, fs_7\}$ be an identical failure mode at the {\em sub-system} level.
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Let $\{fs_6\}$ be a distinct failure mode at {\em sub-system} level.
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Let $SP3 = \{fs_6\}$ be a distinct failure mode at {\em sub-system} level.
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The diagram can now be drawn as in figure \ref{fig:gensubsys3}.
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@ -399,7 +274,7 @@ The result of this will be, a set of failure modes for the sub-system, as thoug
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or a {\em component} to be used in higher level designs.
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We have now in $SP1$, $SP2$ and $fs_6$ the three ways in which this sub-system can fail.
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We have now in $SP1$, $SP2$ and $SP_3$ the three ways in which this sub-system can fail.
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In other words we have derived failure modes for this sub-system.
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@ -447,7 +322,7 @@ In other words we have derived failure modes for this sub-system.
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This sub-system may now therfore, be represented as three separate failure modes.
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We may now treat this sub-system as we would a component with a known set of failure modes.
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The failure modes of the Sub-system $SS$ are now the set $SS_{fm} = \{ SP1, Sp2, fs_6 \}$.
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The failure modes of the Sub-system $SS$ are now the set $SS_{fm} = \{ SP1, SP2, SP_3 \}$.
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Defining the function `$\bowtie$' to represent the {\em symptom abstraction} process, we may now
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write
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@ -491,222 +366,7 @@ with known failure modes.
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\clearpage
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\section{A Formal Algorithmic Description of `Symptom Abstraction'}
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The algorithm for {\em symptom abstraction} is described in
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this section
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%describes the symptom abstraction process
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using set theory.
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The {\em symptom abstraction process} (given the symbol `$\bowtie$') takes a functional group $FG$
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and converts it to a sub-system $SS$.
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The sub-system $SS$ is a collection
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of failure~modes of the sub-system.
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The sub-system $SS$ may now be treated
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as a component with a known set of failure modes.
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Thus $SS$ can be used as a system building block at a higher
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level of fault abstraction.
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The algorithm has been broken down into five stages, each following on from the other.
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\begin{algorithm}[h+]
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~\label{alg:sympabs1}
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\caption{Determine failure modes: $FG \mapsto FG_{cfm}$} \label{alg:sympabs11}
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\begin{algorithmic}[1]
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%\REQUIRE Obtain a list of components for the System $S$ under investigation.
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%ENSURE Decomposition of $S$ into atomic components where each component $c$ has a know set of $fm$ failure modes.
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%\STATE Determine functional groups $fg_n \subset S$ of components, where n is an index number and the number of functional groups found.
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\STATE { Let $FG$ be a set of components } \COMMENT{ The functional group should be chosen to be minimally sized collections of components that perform a specific function}
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\STATE { Let $c$ represent a component}
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\STATE { Let $CFM$ represent a set of failure modes }
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\STATE { $FM(c) \mapsto CFM $} \COMMENT {Let the function $FM$ take a component and return a set of all its failure modes}
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%\ENSURE { $ \forall c | c \in FG \wedge FM(c) \neq \emptyset $}
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%\ENSURE { $ c | c \in FG \wedge FM(c) \neq \emptyset $}
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\ENSURE{ Each component $c \in FG $ has a known set of failure modes i.e. $FM(c) \neq \emptyset$ }
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%\REQUIRE{ Ensure that all components belong to at least one functional group $\bigcup_{i=1...n} fg_i = S $ }
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%symptom_abstraction
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% okular
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\STATE {let $FG_{cfm}$ be a set of failure modes}
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\STATE {Collect all failure modes from the components into the set $FM_{cfm}$}
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%\FORALL { $c \in FG $ }
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%\STATE { $ FM(c) \in FG_{cfm} $ } \COMMENT {Collect all failure modes from the components into the set $FM_{cfm}$}
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%\ENDFOR
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%\hline
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Algorthim \ref{alg:sympabs11} has taken a functional group $FG$ and returned a set of failure~modes $FG_{cfm}$.
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The next task is to formulate `test cases'. These are the collections of failure~modes that will be used
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in the analysis stages.
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\end{algorithmic}
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\end{algorithm}
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\begin{algorithm}[h+]
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~\label{alg:sympabs2}
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\caption{Determine Test Cases: $FM_{cfm} \mapsto TC $} \label{alg:sympabs22}
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\begin{algorithmic}[1]
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\REQUIRE {Determine the test cases to be applied}
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\STATE { All test cases are now chosen by the investigating engineer(s). Typically all single
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component failures are investigated
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with some specially selected combination faults}
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\STATE { Let $TC$ be a set of test cases }
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\STATE { Let $tc_j$ be set of component failure modes where $j$ is an index of $J$}
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\COMMENT { Each set $tc_j$ is a `test case' }
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\STATE { $ \forall j \in J | tc_j \in TC $ }
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%\STATE { $ \bigcup_{j=1...N} tc_j = \bigcup TC $ }
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%\COMMENT { All $tc_j$ test cases sets belong to $TC$ }
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%\REQUIRE { $ TC \subset \bigcup (FM_{cfm}) $ }
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%\COMMENT { $TC$ is the set of all test_cases
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% Let TC be a subset of the powerset of the failure modes $ FG_{cfm} $,
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%i.e. only failure modes present in $ FG_{cfm} $ are present in sets belonging to $ TC $}
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\COMMENT { Ensure the test cases are complete and unique }
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\FORALL { $tc_j \in TC$ }
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%\ENSURE {$ tc_j \in \bigcap FG_{cfm} $}
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\ENSURE {$ tc_j \in \mathcal{P} FG_{cfm} $}
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\COMMENT { require that the test case is a member of the powerset of $FM_{cfm}$ }
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\ENSURE { $ \forall \; j2 \; \in J ( \forall \; j1 \; \in J | tc_{j1} \neq tc_{j2} \; \wedge \; j1 \neq j2 ) $}
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\COMMENT { Test cases must be unique }
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\ENDFOR
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\STATE { let $f$ represet a component failure mode }
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\REQUIRE { That all failure modes are represented in at least one test case }
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\ENSURE { $ \forall f | (f \in FM_{cfm}) \wedge (f \in \bigcup TC) $ }
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\COMMENT { This corresponds to checking that at least each failure mode is considered at least once in the analysis; some european standards
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imply checking all double fault combinations\cite{en298} }
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%\hline
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Algorithm \ref{alg:sympabs22} has taken the set of failure modes $FM_{cfm}$ and returned a set of test cases $TC$.
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The next stages is to analyse the effect of each test case on the functional group.
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\end{algorithmic}
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\end{algorithm}
|
||||
|
||||
\begin{algorithm}[h+]
|
||||
~\label{alg:sympabs3}
|
||||
\caption{Analyse Test Cases: $ TC \mapsto R $} \label{alg:sympabs33}
|
||||
\begin{algorithmic}[1]
|
||||
\STATE { let r be a `test case result'}
|
||||
\STATE { Let the function $Analyse : tc \mapsto r $ } \COMMENT { This analysis is a human activity, examining the failure~modes in the test case and determining how the functional~group will fail under those conditions}
|
||||
\STATE { $ R $ is a set of test case results $r_j \in R$ where the index $j$ corresponds to $tc_j \in TC$}
|
||||
\FORALL { $tc_j \in TC$ }
|
||||
\STATE { $ rc_j = Analyse(tc_j) $} \COMMENT {this is Fault Mode Effects Analysis (FMEA) applied in the context of the functional group}
|
||||
\STATE { $ rc_j \in R $ }
|
||||
\ENDFOR
|
||||
|
||||
%\hline
|
||||
Algorithm \ref{alg:sympabs33} has built the set $R$, the sub-system/functional group results for each test case.
|
||||
\end{algorithmic}
|
||||
\end{algorithm}
|
||||
|
||||
|
||||
|
||||
|
||||
\begin{algorithm}[h+]
|
||||
~\label{alg:sympabs4}
|
||||
|
||||
\caption{Find Common Symptoms: $ R \mapsto SP $} \label{alg:sympabs44}
|
||||
|
||||
\begin{algorithmic}[1]
|
||||
|
||||
|
||||
%\REQUIRE {All failure modes for the components in $fm_i = FM(fg_i)$}
|
||||
\STATE {Let $sp_l$ be a set of `test cases results' where $l$ is an index set $L$}
|
||||
\STATE {Let $SP$ be a set whose members are sets $sp_l$}
|
||||
\COMMENT{ $SP$ is the set of `fault symptoms' for the sub-system}
|
||||
%
|
||||
%\COMMENT{This corresponds to a fault symptom of the functional group $FG$}
|
||||
%\COMMENT{where double failure modes are required the cardinality constrained powerset of two must be applied to each failure mode}
|
||||
|
||||
\FORALL { $ r_j \in R$ }
|
||||
\STATE { $sp_l \in \mathcal{P} R \wedge sp_l \in SP$ }
|
||||
\STATE { $sp_l \in \bigcap R \wedge sp_l \in SP$ } \COMMENT{ Collect common symptoms.
|
||||
Analyse the sub-system's fault behaviour under the failure modes in $tc_j$ and determine the symptoms $sp_l$ that it
|
||||
causes in the functional group $FG$}
|
||||
%\ENSURE { $ \forall l2 \in L ( \forall l1 \in L | \exists a \in sp_{l1} \neq \exists b \in sp_{l2} \wedge l1 \neq l2 ) $}
|
||||
|
||||
\ENSURE {$ \forall a \in sp_l | \forall sp_i \in \bigcap_{i=1..L} SP ( sp_i = sp_l \implies a \in sp_i)$}
|
||||
|
||||
\COMMENT { Ensure that the elements in each $sp_l$ are not present in any other $sp_l$ set }
|
||||
|
||||
\ENDFOR
|
||||
|
||||
|
||||
|
||||
\STATE { The Set $SP$ can now be considered to be the set of fault modes for the sub-system that $FG$ represents}
|
||||
|
||||
%\hline
|
||||
Algorithm \ref{alg:sympabs44} raises the failure~mode abstraction level.
|
||||
The failures have now been considered not from the component level, but from the sub-system or
|
||||
functional group level.
|
||||
We now have a set $SP$ of the symptoms of failure.
|
||||
|
||||
\end{algorithmic}
|
||||
\end{algorithm}
|
||||
|
||||
\begin{algorithm}[h+]
|
||||
~\label{alg:sympabs5}
|
||||
|
||||
\caption{Treat the symptoms as failure modes of the Sub-System: $ SP \mapsto SS $} \label{alg:sympabs55}
|
||||
|
||||
\begin{algorithmic}[1]
|
||||
|
||||
\STATE { Let $SS$ be a set of faliure modes with failure modes $f$ indexed by $l$ }
|
||||
\FORALL { $sp_l \in SP$ }
|
||||
\STATE { $ f_l = ConvertToFaultMode(sp_l) $}
|
||||
\STATE { $ f_l \in SS $}
|
||||
\ENDFOR
|
||||
%\hline
|
||||
|
||||
Algorithm \ref{alg:sympabs55} is the final stage in the process. We now have a
|
||||
sub-system $SS$, which has its own set of failure~modes. This can now be treated
|
||||
as a component, and used to form functional~groups at a higher level of failure~mode~abstraction.
|
||||
\end{algorithmic}
|
||||
\end{algorithm}
|
||||
|
||||
|
||||
|
||||
\clearpage
|
||||
\section{To conclude}
|
||||
|
||||
The technique provides a methodology for bottom-up analysis of the fault behaviour of complex safety critical systems.
|
||||
|
||||
\subsection{Hierarchical Simplification}
|
||||
|
||||
Because symptom abstraction collects fault modes, the number of faults to handle decreases
|
||||
as the hierarchy progresses upwards.
|
||||
This is seen in real life Systems. At the highest levels the number of faults
|
||||
reduces. A Sound system might have, for instance only four faults at its highest or System level,
|
||||
\small
|
||||
$$ SoundSystemFaults = \{TUNER\_FAULT, CD\_FAULT, SOUND\_OUT\_FAULT, IPOD\_FAULT\}$$
|
||||
\normalsize
|
||||
The number of causes for any of these faults is very large !
|
||||
It does not matter which combination of causes caused the fault to the user.
|
||||
But as the hierarchy goes up in abstraction level the number of faults goes down.
|
||||
|
||||
\subsection{Tracable Fault Modes}
|
||||
|
||||
Because the fault modes are determined from the bottom-up, the causes
|
||||
for all high level faults naturally form trees.
|
||||
Minimal cut sets \cite{nasafta} can be determined from these, and by
|
||||
analysing the statistical likely hood of the component failures
|
||||
the MTTF and SIL\cite{en61508} levels can be automatically calculated.
|
||||
|
||||
|
Loading…
Reference in New Issue
Block a user