FM as function name to lower case
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@ -18,7 +18,20 @@ It is intended to be used to formally prove systems to meet EN and UL standards,
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EN298, EN61508, EN12067, EN230, UL1998.
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EN298, EN61508, EN12067, EN230, UL1998.
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\end{abstract}
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\end{abstract}
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}
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}
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{}
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{
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This chapter describes a process for analysing safety critical systems, to formally prove how safe the
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designs and built -in safety measures are. It provides
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the rigourous method for creating a fault effects model of a system from the bottom up using {\bc} level fault modes.
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Using symptom extraction, and taking {\fgs} of components, a fault behaviour
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hierarchy is built, forming a fault model tree.
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From the fault model trees,
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modular re-usable sections of safety critical systems,
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and accurate, statistical estimation for fault frequency can be derived automatically.
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It provides the means to trace the causes of dangerous detected and dangerous undetected faults.
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It is intended to be used to formally prove systems to meet EN and UL standards, including and not limited to
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EN298, EN61508, EN12067, EN230, UL1998.
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}
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\section{Introduction}
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\section{Introduction}
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@ -141,25 +154,25 @@ This analysis and symptom collection process is described in detail in the Sympt
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\subsubsection{An algebraic notation for identifying FMMD enitities}
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\subsubsection{An algebraic notation for identifying FMMD enitities}
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Each component $C$ is a set of failure modes for the component.
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Each component $C$ is a set of failure modes for the component.
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We can define a function $FM$ that returns the
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We can define a function $fm$ that returns the
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set of failure modes $F$ for the component $C$.
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set of failure modes $F$ for the component $C$.
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Let the set of all possible components be $\mathcal{C}$
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Let the set of all possible components be $\mathcal{C}$
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and let the set of all possible failure modes be $\mathcal{F}$.
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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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We can define a function $fm$
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\begin{equation}
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\begin{equation}
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FM : \mathcal{C} \mapsto \mathcal{P}\mathcal{F}
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fm : \mathcal{C} \mapsto \mathcal{P}\mathcal{F}
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\end{equation}
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\end{equation}
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defined by, where C is a component and F is a set of failure modes.
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defined by, where C is a component and F is a set of failure modes.
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$$ FM ( C ) = F $$
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$$ fm ( C ) = F $$
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%$$ \mathcal{FM}(C) \rightarrow S $$
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%$$ \mathcal{fm}(C) \rightarrow S $$
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%$$ {FM}(C) \rightarrow S $$
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%$$ {fm}(C) \rightarrow S $$
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We can indicate the abstraction level of a component by using a superscript.
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We can indicate the abstraction level of a component by using a superscript.
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Thus for the component $C$, where it is a `base component' we can assign it
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Thus for the component $C$, where it is a `base component' we can assign it
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@ -210,11 +223,11 @@ $$ \bowtie( FG^0_1 ) = C^1_1 $$
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to look at this analysis process in more detail.
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to look at this analysis process in more detail.
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By way of exqample applying ${FM}$ to obtain the failure modes $f_N$
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By way of exqample applying ${fm}$ to obtain the failure modes $f_N$
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$$ {FM}(C^0_1) = \{ f_1, f_2 \} $$
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$$ {fm}(C^0_1) = \{ f_1, f_2 \} $$
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$$ {FM}(C^0_2) = \{ f_3, f_4, f_5 \} $$
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$$ {fm}(C^0_2) = \{ f_3, f_4, f_5 \} $$
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The analyst now considers failure modes $f_{1..5}$ in the context of the {\fg}.
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The analyst now considers failure modes $f_{1..5}$ in the context of the {\fg}.
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@ -224,7 +237,7 @@ We can now create a {\dc} $C^1_1$ with this set of failure modes.
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Thus:
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Thus:
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$$ {FM}(C^1_1) = \{ s_6, s_7, s_8 \} $$
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$$ {fm}(C^1_1) = \{ s_6, s_7, s_8 \} $$
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We can represent this analysis process in a diagram see figure \ref{fig:onestage}
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We can represent this analysis process in a diagram see figure \ref{fig:onestage}
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