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616<br />

Wire and Wireless Communication Applications Chap. 8<br />

where the true azimuth, as measured clockwise from the north, is given by either A or 360° -A, as<br />

appropriate, since a calculator gives a value between 0 and 180° for cos -1 (x). Using these formulas<br />

for the Washington, D.C., TVRO site, † we get l = 134 - 77 = 57° and<br />

b = cos -1 [ cos(38.8) cos(57)] = 64.9°<br />

(8–51)<br />

The slant range is<br />

d = 3(26,205) 2 + (3963) 2 - 2(3963)(26,205) cos 64.9)<br />

= 24,784 miles<br />

(8–52)<br />

The elevation angle of the TVRO antenna is<br />

E = tan -1 1<br />

c<br />

tan (64.9)<br />

The azimuth angle of the TVRO antenna is<br />

-<br />

3963<br />

(26,205) sin (64.9) d = 16.88<br />

(8–53)<br />

A = cos -1 -tan (38.8)<br />

c<br />

tan (64.9) d = 247.9°<br />

(8–54)<br />

Thus, the look angles of the TVRO antenna at Washington, D.C., to the satellite are E = 16.8°<br />

and A = 247.9°.<br />

A block diagram describing the receiving system is shown in Fig. 8–26. Using (8–43), the<br />

CNR at the detector input of the receiver is<br />

a C N b dB<br />

= (P EIRP ) dBw - (L FS ) dB + a G AR<br />

- k<br />

T dB - B dB<br />

syst<br />

bdB<br />

(8–55)<br />

The corresponding path loss for d = 24,784 mi at a frequency of 4 GHz is<br />

(L FS ) dB = 20 log a 4pd b = 196.5 dB<br />

l<br />

5 meter<br />

antenna<br />

Transmission<br />

feedline<br />

G a =0.98<br />

LNA<br />

G a =50 dB<br />

T e =120 K<br />

FM<br />

receiver<br />

T e =2610 K<br />

B IF =30 MHz<br />

Composite<br />

video out<br />

m c (t)<br />

Figure 8–26<br />

TVRO terminal.<br />

† Here for convenience and for ease in interpretation of answers, the calculator is set to evaluate all trigonometric<br />

functions in degrees (not radians).

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