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Probabilistic Performance Analysis of Fault Diagnosis Schemes

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Chapter 6<br />

Applications<br />

6.1 Introduction<br />

In this chapter, we explore various applications <strong>of</strong> the performance analysis framework<br />

developed in the preceding chapters. To begin, we examine, from a high level, the various<br />

usages <strong>of</strong> the performance metrics. Then, we demonstrate how the performance metrics<br />

are computed for two aerospace examples. The first example is a simplified air-data sensor<br />

system consisting <strong>of</strong> a pitot-static probe and a flight path angle measurement. The second<br />

example is a linearized model <strong>of</strong> a vertical take-<strong>of</strong>f and landing (vtol) fixed-wing aircraft. For<br />

the first example, we consider the effects <strong>of</strong> uncertain signals, and for the second example,<br />

we consider the effects <strong>of</strong> additive model uncertainty.<br />

6.2 Types <strong>of</strong> Studies<br />

Although there are many ways to interpret the performance metrics, the following types <strong>of</strong><br />

studies stand out as natural applications <strong>of</strong> our performance analysis framework:<br />

1. Selecting a fault detection scheme: Given a fixed system G θ , the performance metrics<br />

can be used to select the best fault diagnosis scheme from a finite set <strong>of</strong> schemes<br />

{<br />

V<br />

(i ) = (F (i ) ,δ (i ) ) : i = 1,2,...,m } .<br />

This type <strong>of</strong> application is most useful when the fault diagnosis schemes are designed<br />

using disparate methodologies with incomparable design criteria.<br />

2. Trade studies: Given a collection <strong>of</strong> systems<br />

{<br />

G<br />

(i )<br />

θ<br />

: i = 1,2,...,m}<br />

and a collection <strong>of</strong> fault diagnosis schemes<br />

{<br />

V<br />

(i ) = (F (i ) ,δ (i ) ) : i = 1,2,...,m } ,<br />

100

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