507 lines
21 KiB
TeX
507 lines
21 KiB
TeX
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\abstract{ This chapter defines what is meant by the terms
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components, derived~components, functional~groups, component fault modes and `unitary~state' component fault modes.
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%The application of Bayes theorem in current methodologies, and
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%the suitability of the `null hypothesis' or `P' value statistical approach
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%are discussed.
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Data types and their relationships are described using UML.
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Mathematical constraints and definitions are made using set theory.
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}
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\section{Introduction}
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This chapter describes the data types and concepts for the Failure Mode Modular De-composition (FMMD) method.
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When analysing a safety critical system using
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this technique, we need clearly defined failure modes for
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all the components that are used to model the system.
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These failure modes have a constraint such that
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the component failure modes must be mutually exclusive.
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When this constraint is complied with we can use the FMMD process to
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build hierarchical bottom-up models of failure mode behaviour.
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%This and the definition of a component are
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%described in this chapter.
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%When building a system from components,
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%we should be able to find all known failure modes for each component.
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%For most common electrical and mechanical components, the failure modes
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%for a given type of part can be obtained from standard literature\cite{mil1991}
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%\cite{mech}. %The failure modes for a given component $K$ form a set $F$.
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%%
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%% Paragraph component and its relationship to its failure modes
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%%
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\section{ Defining the term `Component' }
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\begin{figure}[h]
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\centering
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\includegraphics[width=300pt,bb=0 0 437 141,keepaspectratio=true]{component_failure_modes_definition/component.jpg}
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% component.jpg: 437x141 pixel, 72dpi, 15.42x4.97 cm, bb=0 0 437 141
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\caption{A Component and its Failure Modes}
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\label{fig:component}
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\end{figure}
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Let us first define a component. This is anything we use to build a
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product or system with. This could be something quite complicated
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like an integrated microcontroller, or quite simple like the humble resistor.
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We can define a
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component by its name, a manufacturers part number and perhaps
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a vendors reference number.
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What these components all have in common is that they can fail, and fail in
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a number of well defined ways. For common components
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there is established literature for the failure modes for the system designer consider (often with accompanying statistical
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failure rates)\cite{mil1991}. For instance, a simple resistor is generally considered
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to fail in two ways, it can go open circuit or it can short.
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Thus we can associate a set of faults to this component $ResistorFaultModes=\{OPEN, SHORT\}$.
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The UML diagram in figure
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\ref{fig:component} shows a component as a data
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structure with its associated failure modes.
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From this diagram we see that each component must have at least one failure mode.
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Also to clearly show that the failure modes are unique events associated with one component,
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each failure mode is referenced back to only one component.
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This modelling constraint is due to the fact that even generic components with the same
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failure mode types, may have different statistical MTTF properties within the same
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circuitry\footnote{For example, consider resistors one of high resistance and one low.
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The generic failure modes for a resistor will be the same for both.
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The lower resistance part will draw more current and therefore have a statistically higher chance of failure.}.
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%% sharing failure modes arrrgghh so irrelevant
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%% wrong as well perhaps, as each component will have environmental constraints
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%% that determine its statistical behaviour. A 1 Meg ohm resistor
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%% is less stressed than a 100 ohm in the same circuit etc
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% Perhaps talk here about the failure modes being shared, but by being referenced
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% by the component ?
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A product naturally consists of many components and these are traditionally
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kept in a `parts list'. For safety critical product this is usually a formal document
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and is used by quality inspectors to ensure the correct parts are being fitted.
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For our UML diagram the parts list is simply a collection of components
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as shown in figure \ref{fig:componentpl}.
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\begin{figure}[h]
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\centering
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\includegraphics[width=400pt,bb=0 0 712 68,keepaspectratio=true]{component_failure_modes_definition/componentpl.jpg}
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% componentpl.jpg: 712x68 pixel, 72dpi, 25.12x2.40 cm, bb=0 0 712 68
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\caption{Parts List of Components}
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\label{fig:componentpl}
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\end{figure}
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Components in the parts list (bought in parts) will be termed `base~comonents'.
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Components derived from base~components may not require
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parts~numbers\footnote{It is common practise for sub assemblies, PCB's, mechanical parts,
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software modules and some collections of components to have part numbers}, and will
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not require a vendor reference, but must be named.
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%%
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%% Paragraph using failure modes to build from bottom up
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%%
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\section{Fault Mode Analysis, top down or bottom up?}
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Traditional static fault analysis methods work from the top down.
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They identify faults that can occur in a system, and then work down
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to see how they could be caused. Some apply statistical tequniques to
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determine the likelihood of component failures
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causing specific system level errors. For example, Bayes theorem \ref{bayes}, the relation between a conditional probability and its inverse,
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can be applied to specific failure modes in components and the probability of them causing given system level errors.
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Another top down technique is to apply cost benifit analysis
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to determine which faults are the highest priority to fix\cite{FMEA}.
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The aim of FMMD analysis is to produce complete failure
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models of safety critical systems from the bottom-up,
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starting, where possible with known base~component failure~modes.
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An advantage of working from the bottom up is that we can ensure that
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all component failure modes must be considered. A top down approach
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could miss individual failure modes of components.
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In order to analyse from the bottom-up, we need to take
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small groups of components from the parts~list that naturally
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work together to perform a simple function.
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The components to include in a functional group are chosen by a human, the analyst.
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%We can represent the `Functional~Group' as a class.
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When we have a
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`Functional~Group' we can look at the components it contains,
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and from this determine the failure modes of all the components that belong to it.
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%
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% and determine a failure mode model for that group.
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The `Functional~Group' as used by the analyst is a collection of component failures modes.
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Each of these failure modes, and optionally combinations of them, are
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analsyed for their effect on the failure mode behaviour of the `Functional~Group'.
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%
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From this we can determine a new set of failure modes, the failure modes of the
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`Functional~Group'.
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%
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Or in other words we can determine how the `Functional~Group' can fail.
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We can now consider the functional group as a sort of super component
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with a known set of failure modes.
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\subsection{From functional group to newly derived component}
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The process for taking a functional~group, considering
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all the failure modes of all the components in the group,
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and analysing it is called `symptom abstraction' and
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is dealt with in detail in chapter \ref{symptom_abstraction}.
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In terms of our UML model the symptom abstraction process takes a functional~group,
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and creates a new derived component from it.
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%To do this it first creates
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%a new set of failure modes, representing the fault behaviour
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%of the functional group. This is a human process and to do this the analyst
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%must consider all the failure modes of the components in the functional
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%group.
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The newly created derived~component requires a set of failure modes of its own.
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These failure modes are the failure mode behaviour of the functional group that it was derived from.
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Because these new failure modes were determined from a derived component we can call
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these `derived~failure~modes'.
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%It then creates a new derived~component object, and associates it to this new set of derived~failure~modes.
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We thus have a `new' component, or system building block, but with a known and traceable
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fault behaviour.
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The UML representation shows a `functional group' having a one to one relationship with a derived~component.
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We can represent this using an UML diagram in figure \ref{fig:cfg}.
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Using the symbol $\bowtie$ to indicate the analysis process that takes a
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functional group and converts it into a new component.
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$$ \bowtie ( FG ) \mapsto DerivedComponent $$
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\begin{figure}[h]
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\centering
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\includegraphics[width=400pt,bb=0 0 712 286,keepaspectratio=true]{component_failure_modes_definition/cfg.jpg}
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% cfg.jpg: 712x286 pixel, 72dpi, 25.12x10.09 cm, bb=0 0 712 286
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\caption{UML Meta model for FMMD hierarchy}
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\label{fig:cfg}
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\end{figure}
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\subsection{Keeping track of the derived \\ components position in the hierarchy}
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The UML meta model in figure \ref{fig:cfg}, shows the relationships
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between the classes and sub-classes.
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In use we will build a hierarchy of
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objects, with derived~components forming functional~groups, and creating
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derived components higher up in the structure.
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The level variable in each Component,
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indicates the position in the hierarchy. Base or parts~list components
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have a `level' of 0.
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% I do not know how to make this simpler
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Derived~components take a level based on the highest level
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component used to build the functional group it was derived from plus 1.
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So a derived component built from base level or parts list components
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would have a level of 1.
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%\clearpage
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% \section{Set Theory Description}
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%
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% $$ System \stackrel{has}{\longrightarrow} PartsList $$
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%
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% $$ PartsList \stackrel{has}{\longrightarrow} Components $$
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%
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% $$ Component \stackrel{has}{\longrightarrow} FailureModes $$
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%
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% $$ FunctionalGroup \stackrel{has}{\longrightarrow} Components $$
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%
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% Using the symbol $\bowtie$ to indicate an analysis process that takes a
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% functional group and converts it into a new component.
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%
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% $$ \bowtie ( FG ) \mapsto DerivedComponent $$
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%
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\section{Unitary State Component Failure Mode sets}
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\paragraph{Design Descision/Constraint}
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An important factor in defining a set of failure modes is that they
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should be as clearly defined as possible.
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It should not be possible for instance for
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a component to have two or more failure modes active at once.
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Having a set of failure modes where $N$ modes could be active simultaneously
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would mean having to consider an additional $2^N-1$ failure mode scenarios.
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Should a component be analysed and simultaneous failure mode cases exit,
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the combinations could be represented by new failure modes, or
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the component should be considered from a fresh perspective,
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perhaps considering it as several smaller components
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within one package.
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\begin{definition}
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A set of failure modes where only one fault mode
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can be active at a time is termed a `unitary~state' failure mode set.
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%This is termed the $U$ set thoughout this study.
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This corresponds to the `mutually exclusive' definition in
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probability theory\cite{probandstat}.
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\end{definition}
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Let the set of all possible tomponents to be $\mathcal{C}$
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and let the set of all possible failure modes be $\mathcal{F}$.
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We can define a function $FM$
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\begin{equation}
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FM : \mathcal{C} \mapsto \mathcal{F}
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\end{equation}
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defined by
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$$ FM ( C ) = F $$
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i.e. take a given component $C$ and return its set of failure modes $F$.
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\begin{definition}
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We can define a set $\mathcal{U}$ which is a set of sets of failure modes, where
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the component failure modes in each of its members are unitary~state.
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Thus if the failure modes of $F$ are unitary~state, we can say $F \in \mathcal{U}$.
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\end{definition}
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\section{Component failure modes:\\ Unitary State example}
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An example of a component with an obvious set of ``unitary~state'' failure modes is the electrical resistor.
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Electrical resistors can fail by going OPEN or SHORTED.
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For a given resistor R we can apply the
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the function $FM$ to find its set of failure modes thus $ FM(R) = \{R_{SHORTED},R_{OPEN}\} $.
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A resistor cannot fail with both conditions open and short active at the same time ! The conditions
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OPEN and SHORT are thus mutually exclusive.
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Because of this the failure mode set $F=FM(R)$ is `unitary~state'.
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Thus because both fault modes cannot be active at the same time, the intersection of $ R_{SHORTED} $ and $ R_{OPEN} $ cannot exist.
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$$ R_{SHORTED} \cap R_{OPEN} = \emptyset $$
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therefore
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$$ FM(R) \in \mathcal{U} $$
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We can make this a general case by taking a set $F$ (where $f_1, f_2 \in F$) representing a collection
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of component failure modes.
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We can define a boolean function {\ensuremath{\mathcal{ACTIVE}}} that returns
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whether a fault mode is active (true) or dormant (false).
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We can say that if any pair of fault modes is active at the same time, then the failure mode set is not
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unitary state:
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we state this formally
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\begin{equation}
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\forall f_1,f_2 \in F \dot ( f_1 \neq f_2 \wedge \mathcal{ACTIVE}({f_1}) \wedge \mathcal{ACTIVE}({f_2}) ) \implies F \not\in \mathcal{U}
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\end{equation}
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%
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% \begin{equation}
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% c1 \cap c2 \neq \emptyset | c1 \neq c2 \wedge c1,c2 \in C \wedge C \not\in U
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% \end{equation}
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That is to say that it is impossible that any pair of failure modes can be active at the same time
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for the failure mode set $F$ to exist in the family of sets $\mathcal{U}$.
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Note where there are more than two failure~modes,
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by banning any pairs from being active at the same time,
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we have banned larger combinations as well.
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\section{Handling Simultaneous Component Faults}
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For some integrity levels of static analysis there is a need to consider not only single
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failure modes in isolation, but cases where more then one failure mode may occur
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simultaneously.
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It is an implied requirement of EN298 for instance to consider double simultaneous faults.
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To generalise, we may need to consider $N$ simultaneous
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failure modes when analysing a functional group. This involves finding
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all combinations of failures modes of size $N$ and less.
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The Powerset concept from Set theory is useful to model this.
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The powerset, when applied to a set S is the set of all subsets of S, including the empty set
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\footnote{The empty set ( $\emptyset$ ) is a special case for FMMD analysis, it simply means there
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is no fault active in the functional~group under analysis}
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and S itself.
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In order to consider combinations for the set S where the number of elements in each sub-set of S is $N$ or less, a concept of the `cardinality constrained powerset'
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is proposed and described in the next section.
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\pagebreak[4]
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\subsection{Cardinality Constrained Powerset }
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\label{ccp}
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A Cardinality Constrained powerset is one where sub-sets of a cardinality greater than a threshold
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are not included. This theshold is called the cardinality constraint.
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To indicate this the cardinality constraint $cc$, is subscripted to the powerset symbol thus $\mathcal{P}_{cc}$.
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Consider the set $S = \{a,b,c\}$.
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The powerset of S:
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$$ \mathcal{P} S = \{ \emptyset, \{a,b,c\}, \{a,b\},\{b,c\},\{c,a\},\{a\},\{b\},\{c\} \} $$
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$\mathcal{P}_{2} S $ means all subsets of S where the cardinality of the subsets is
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less than or equal to 2 or less.
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$$ \mathcal{P}_{2} S = \{ \{a,b\},\{b,c\},\{c,a\},\{a\},\{b\},\{c\} \} $$
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Note that $\mathcal{P}_{1} S $ for this example is:
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$$ \mathcal{P}_{1} S = \{ \{a\},\{b\},\{c\} \} $$
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\paragraph{Calculating the number of elements in a cardinality constrained powerset}
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A $k$ combination is a subset with $k$ elements.
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The number of $k$ combinations (each of size $k$) from a set $S$
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with $n$ elements (size $n$) is the binomial coefficient
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$$ C^n_k = {n \choose k} = \frac{n!}{k!(n-k)!}$$
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To find the number of elements in a cardinality constrained subset S with up to $cc$ elements
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in each combination sub-set,
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we need to sum the combinations,
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%subtracting $cc$ from the final result
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%(repeated empty set counts)
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from $1$ to $cc$ thus
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%
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% $$ {\sum}_{k = 1..cc} {\#S \choose k} = \frac{\#S!}{k!(\#S-k)!} $$
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%
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\begin{equation}
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|{\mathcal{P}_{cc}S}| = \sum^{k}_{1..cc} \frac{|{S}|!}{ k! ( |{S}| - k)!}
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\label{eqn:ccps}
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\end{equation}
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\subsection{Actual Number of combinations to check \\ with Unitary State Fault mode sets}
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Where all the fault modes in $S$ were to be independent,
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the cardinality constrained powerset
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calculation (in equation \ref {eqn:ccps}) would give the correct number of test case combinations to check.
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Because sets of failure modes in FMMD analysis are constrained to be unitary state,
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the actual number of test cases to check will usually
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be less than this.
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This is because combinations of faults within a components failure mode set,
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are impossible under the conditions of unitary state failure mode.
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To correct equation \ref{eqn:ccps} we must subtract the number of component `internal combinations'
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for each component in the functional group under analysis.
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Note we must sequentially subtract using combinations above 1 up to the cardinality constraint.
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For example, say
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the cardinality constraint was 3, we would need to subtract both
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$|{n \choose 2}|$ and $|{n \choose 3}|$.
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\subsubsection{Example: Two Component functional group \\ cardinality Constraint of 2}
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For example: were we to have a simple functional group with two components R and T, of which
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$$FM(R) = \{R_o, R_s\}$$ and $$FM(T) = \{T_o, T_s, T_h\}$$.
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This means that the functional~group $FG=\{R,T\}$ will have a component failure mode set
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of $FG_{cfg} = \{R_o, R_s, T_o, T_s, T_h\}$
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For a cardinality constrained powerset of 2, because there are 5 error modes ( $|{FG_{cfg}}|=5$),
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applying equation \ref{eqn:ccps} gives :-
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$$\frac{5!}{1!(5-1)!} + \frac{5!}{2!(5-2)!} = 15$$
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This is composed of ${5 \choose 1}$
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five single fault modes, and ${5 \choose 2}$ ten double fault modes.
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However we know that the faults are mutually exclusive within a component.
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We must then subtract the number of `internal' component fault combinations
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for each component in the functional~group.
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For component R there is only one internal component fault that cannot exist
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$R_o \wedge R_s$. As a combination ${2 \choose 2} = 1$. For the component $T$ which has
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three fault modes ${3 \choose 2} = 3$.
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Thus for $cc == 2$, under the conditions of unitary state failure modes in the components $R$ and $T$, we must subtract $(3+1)$.
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The number of combinations to check is thus 11, $|\mathcal{P}_{2}(FG_{cfg})| = 11$, for this example and this can be verified
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by listing all the required combinations:
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$$ \mathcal{P}_{2}(FG_{cfg}) = \{
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\{R_o T_o\}, \{R_o T_s\}, \{R_o T_h\}, \{R_s T_o\}, \{R_s T_s\}, \{R_s T_h\}, \{R_o \}, \{R_s \}, \{T_o \}, \{T_s \}, \{T_h \}
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\}
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$$
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And by inspection
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$$
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\{
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\{R_o T_o\}, \{R_o T_s\}, \{R_o T_h\}, \{R_s T_o\}, \{R_s T_s\}, \{R_s T_h\}, \{R_o \}, \{R_s \}, \{T_o \}, \{T_s \}, \{T_h \}
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\}
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| = 11
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$$
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\subsubsection{Establishing Formulae for unitary state failure mode \\
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cardinality calculation}
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The cardinality constrained powerset in equation \ref{eqn:ccps}, can be corrected for
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unitary state failure modes.
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This is written as a general formula in equation \ref{eqn:correctedccps}.
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%\indent{
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where :
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\begin{itemize}
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\item Let $C$ be a set of components (indexed by $j \in J$)
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that are members of the functional group $FG$
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i.e. $ \forall j \in J | C_j \in FG $
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\item Let $|FM({C}_{j})|$
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indicate the number of mutually exclusive fault modes of each component
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\item Let $FG_{cfg}$ be the collection of all failure modes
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from all the components in the functional group.
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\item Let $SU$ be a set of failure modes from the functional group,
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where all contributing components $C_j$
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are guaranteed to be `unitary state' i.e. $(SU = FG_{cfg}) \wedge (\forall j \in J | FM(C_j) \in \mathcal{U}) $
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\end{itemize}
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%}
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\begin{equation}
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|{\mathcal{P}_{cc}SU}| = {\sum^{k}_{1..cc} \frac{|{SU}|!}{k!(|{SU}| - k)!}}
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- \sum^{p}_{2..cc}{{\sum^{j}_{j \in J} {|FM({C_{j})}| \choose p}}}
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\label{eqn:correctedccps}
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\end{equation}
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Expanding the combination in equation \ref{eqn:correctedccps}
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|
|
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\begin{equation}
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|{\mathcal{P}_{cc}SU}| = {\sum^{k}_{1..cc} \frac{|{SU}|!}{k!(|{SU}| - k)!}}
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- \sum^{p}_{2..cc}{{\sum^{j}_{j \in J} \frac{|FM({C_j})|!}{p!(|FM({C_j})| - p)!}} }
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\label{eqn:correctedccps2}
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\end{equation}
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Equation \ref{eqn:correctedccps2} is useful for an automated tool that
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would verify that a `N' simultaneous failures model had complete failure mode coverage.
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By knowing how many test cases should be covered, and checking the cardinality
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associated with the test cases, complete coverage would be confirmed.
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|
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\pagebreak[4]
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\section{Component Failure Modes and Statistical Sample Space}
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%\paragraph{NOT WRITTEN YET PLEASE IGNORE}
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A sample space is defined as the set of all possible outcomes.
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For a component in FMMD analysis, this set of all possible outcomes is its normal correct
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operating state and all its failure modes.
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When dealing with failure modes, we are not interested in
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the state where the component is working perfectly or `OK' (i.e. operating with no error).
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We are interested only in ways in which it can fail.
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By definition while all components in a system are `working perfectly'
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that system will not exhibit faulty behaviour.
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Thus the statistical sample space $\Omega$ for a component or derived~component $C$ is
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%$$ \Omega = {OK, failure\_mode_{1},failure\_mode_{2},failure\_mode_{3} ... failure\_mode_{N} $$
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$$ \Omega(C) = \{OK, failure\_mode_{1},failure\_mode_{2},failure\_mode_{3}, \ldots ,failure\_mode_{N}\} $$
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The failure mode set $F$ for a given component or derived~component $C$
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is therefore
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$$ F = \Omega(C) \backslash OK $$
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The $OK$ statistical case is the largest in probability, and is therefore
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|
of interest when analysing systems from a statistical perspective.
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This is of interest for the application of conditional probability calculations
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|
such as Bayes theorem.
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\vspace{40pt}
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