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Journal of Control Science and Engineering
/
2008
/
Article
/
Tab 7
/
Research Article
Design and Analysis of Robust Fault Diagnosis Schemes for a Simulated Aircraft Model
Table 7
PM Monte Carlo analysis with
𝑝
=
1
0
and
𝑟
f
a
%.
Faulty sensor
𝑟
m
f
𝑟
t
d
𝑟
t
i
,
𝜏
m
d
𝜏
m
i
,
𝛿
𝑒
0
.
0
0
2
0
.
0
0
3
0
.
9
9
7
2
7
𝛿
𝑎
s
0
.
0
0
1
0
.
0
0
1
0
.
9
9
9
1
8
𝛿
𝑟
s
0
.
0
0
2
0
.
0
0
3
0
.
9
9
7
2
5
𝛿
t
h
s
0
.
0
0
3
0
.
0
0
2
0
.
9
9
8
3
5
𝜈
=
1
2
s