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98 Smart Technologies <strong>for</strong> Safety Engineering<br />

R 7<br />

3<br />

C 2<br />

R9<br />

C 1<br />

R2<br />

R4<br />

R1<br />

1<br />

R6<br />

2 7<br />

R8<br />

R3<br />

R5<br />

5<br />

4 R10 6<br />

J<br />

R11<br />

R 12<br />

Figure 3.54 Numerical example of an electrical circuit<br />

equations (98) or (99). In the DC case, the following results are obtained:<br />

In the AC case,<br />

D u =<br />

<br />

L u2 =<br />

u L 6<br />

<br />

L u2 =<br />

u L 6<br />

<br />

−0.1<br />

; D<br />

0.4<br />

u =<br />

<br />

450 75<br />

75 450<br />

<br />

−0.12019 + 0.06525i<br />

−0.17981 − 0.06525i<br />

<br />

293.3097 − 64.7071i<br />

<br />

231.6903 + 64.7071i<br />

231.6903 + 64.7071i 293.3097 − 64.7071i<br />

The columns of influence matrices are calculated as voltage responses to unit distortions, imposed<br />

consecutively in elements R2 and R6. The values of distortions, modeling the introduced<br />

modifications, are calculated from Equation (105):<br />

DC :<br />

AC :<br />

<br />

0 ε2 ε0 <br />

−3<br />

0.0956 × 10<br />

=<br />

6 0.4910 × 10−3 <br />

<br />

0 −3<br />

ε2 (0.2226 + 0.0656i) × 10<br />

=<br />

(0.2338 − 0.0531i) × 10−3 <br />

ε 0 6<br />

An arbitrary response of the modified circuit can now be quickly calculated as a superposition<br />

of the linear and residual responses.

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