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Bilateral Scattering Stability and Gain 263<br />

power and input power are positive, corresponding to positive R L<br />

and positive<br />

R.n, respectively. Regions having positive or negative 'I are shown in Figure<br />

7.19 by superscripts. Note that the region outside the Smith chart in Figure<br />

7.19b represents power going into both input and output ports, since R L O. Figure 7.19c represents a backward amplifier within the small<br />

stability circle, because both R.n and R L are negative. The shaded areas<br />

represent loci where 'I is negative and R;n < 0 when R L<br />

>0; this does not occur<br />

in Figure 7.19c, f, where the device is unconditionally stable.<br />

The Smith chart origins usually represent 50+jO ohms; the system must be<br />

stable for 50-ohm terminations in order to be measurable. When the stability<br />

circle does not enclose the origin <strong>of</strong> the termination's Smith chart (r;), it<br />

defines a region <strong>of</strong> negative-real network terminal impedance (Z;n or Zq), as<br />

shown in Figure 7.19a-c. For example, Figure 7.19c shows that only certain<br />

negative-real load impedances could produce negative-real input impedances.<br />

Conversely, when the stability circle does enclose the origin <strong>of</strong> the termination's<br />

Smith chart (r;), it defines a region <strong>of</strong> positive-real network terminal<br />

impedance (Z;n or Zq), as shown in Figure 7.19d-f. For example, Figure 7.19f<br />

shows that any load with reflection magnitude just slightly greater than unity<br />

will Cause negative-real input impedance. It is interesting to note that conjugate-image<br />

matching is always possible for unconditionally stable networks,<br />

but this mayor may not be possible for conditionally stable networks.<br />

Example 7.9. Suppose that the device scattering parameters have been measured<br />

on a 50-ohm system and found to be<br />

S= [0.385 /-55°<br />

2.7 /78°<br />

0.045 /90° ]<br />

0.89 / - 26.5° .<br />

(7.106)<br />

Using (E.2), stability factor K=0.909, so that the stability circles are <strong>of</strong><br />

interest. Using (E.15)-(E.18), the output plane stability circle is centered at<br />

r,,= 1.178 /29.88°, with radius p'2=0.193; the input plane stability circle is<br />

centered at r,1 = 8.372 / - 57.6°, with radius P,I = 9.271. These circles are<br />

plotted in Figure 7.21, in the following section.<br />

7.4.3. Bilateral Gains and TennilllJtions. There are several useful gain expressions<br />

applicable to Figure 7.17 that are available from the renormalized<br />

scattering parameters in (7.92)-(7.95). Transducer gain G T has been defined in<br />

(7.96). Some simplification <strong>of</strong> the magnitude <strong>of</strong> (7.94) is available:<br />

IS'II'(1-lr,1 2 )(1 -lr,1 2 )<br />

2 •<br />

II-rIS" - r,S22+rlr,~1<br />

(7.107)<br />

Using (4.51), it is easy to show that the efficiency may be expressed as<br />

'I<br />

IS,,,'<br />

I-IS;,I' .<br />

(7.108)

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