Propagation Effects Handbook for Satellite Systems - DESCANSO ...
Propagation Effects Handbook for Satellite Systems - DESCANSO ...
Propagation Effects Handbook for Satellite Systems - DESCANSO ...
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Step 4 The specific attenuation coefficients are determined by<br />
interpolation from Table 6.3-3, with a polarizaiton tilt angle of<br />
45° (circular polarization);<br />
Step 5 The<br />
Eq. (6.3-15<br />
K= o.o163, a = 1.2175<br />
attenuation exceeded <strong>for</strong> 0.01% of an average year, from<br />
~ is;<br />
Ao.ol = (0.0163) (42)1.217S(7.53) (0.771 )<br />
= 8.96 dB<br />
Step 6 The attenuation exceeded <strong>for</strong> other percentages is then<br />
determined from Eq. (3.6-16);<br />
% Attenuation (dB)<br />
1.0 1.08<br />
0.5 1.56<br />
0.3 2.02<br />
001 3(42<br />
0.05 4.67<br />
0.03 5.80<br />
0.01 8.96<br />
0.005 11.48<br />
0.003 13.65<br />
0.001<br />
19.16<br />
Figure 6.3-8 shows a plot of the resulting attenuation prediction<br />
distribution, compared with three years of measured distributions<br />
obtained with the CTS satellite (Ippolito 1979). The CCIR<br />
prediction is seen to over-predict slightly <strong>for</strong> higher percentage<br />
values, and to vastly under-predict <strong>for</strong> percentages below about<br />
0.01%0<br />
6-36