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Fault Detection and Diagnostics for Rooftop Air Conditioners

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106<br />

Harms’Result<br />

Harms plotted all four sets of data (see Figure A1-10) <strong>and</strong> fit the following model<br />

by minimizing the least squares error.<br />

( ) ⎡ρ<br />

( ) ⎤<br />

0.5<br />

m&<br />

= c T −c ⎣ P −P<br />

ref 1 super 2 f 5 6<br />

Harms determined c 1 = 0.51* 10, c2<br />

= 1. So,<br />

m&<br />

= 0 .51* 10( Tsh, operating<br />

−1)<br />

ρ(<br />

Pup<br />

− Pdown<br />

)<br />

where the upper boundary of ( T<br />

,<br />

−1)<br />

was set at 8 o C .<br />

sh operating<br />

Figure A1-10 <strong>and</strong> Table A1-2 show the results of the global linear assumption <strong>and</strong><br />

nonlinear parameter estimation approaches. To test how well the experimental data are<br />

fitted to a linear model, the model correlated by Harms was tested using the same data<br />

used <strong>for</strong> training. It is obvious that the nonlinear parameter estimation obtained better<br />

results than the global linear assumption which is comparable to the interpolation<br />

per<strong>for</strong>mance of Harms’ model. In addition, from the testing of Harms’model, it can be<br />

seen that linearization will inherently result in larger errors under many circumstances.<br />

⎦<br />

4.5<br />

4<br />

3.5<br />

A<br />

B<br />

C<br />

HT<br />

C d A [mm 2 ]<br />

3<br />

2.5<br />

2<br />

1.5<br />

1<br />

0.5<br />

0<br />

0 2 4 6 8 10 12 14 16<br />

T super [°C]<br />

Figure A1-10 The<br />

C d<br />

A value of the 5-ton Trane RTU TXV as a function of superheat<br />

106

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