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Handbook of Propagation Effects for Vehicular and ... - Courses

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9-14<br />

<strong>Propagation</strong> <strong>Effects</strong> <strong>for</strong> <strong>Vehicular</strong> <strong>and</strong> Personal Mobile Satellite Systems<br />

where T ( 50%)<br />

is the mean value <strong>of</strong> the fade occurrence interval at the fade<br />

I<br />

exceedance percentage <strong>of</strong> 50% <strong>and</strong> m(P) is given by (9-31). The mean value <strong>of</strong> the fade<br />

duration at the fade exceedance P or T D (P)<br />

may be calculated by<br />

⎛ P ⎞<br />

D ( P)<br />

= T ( P)<br />

⎜1<br />

− ⎟ . (9-29)<br />

⎝ 100 ⎠<br />

T I<br />

The mean fade occurrence interval at P = 50% may be calculated using<br />

3<br />

TI ( 50%)<br />

= , (9-30)<br />

f<br />

−10<br />

where f-10 is called the “-10 dB spectral b<strong>and</strong>width.” This corresponds to the b<strong>and</strong>width<br />

over which the power density decays to –10 dB relative to the peak power density<br />

(characterized in Figure 9-11). The parameter m(P) in (9-28) is evaluated using the<br />

following equations.<br />

2<br />

m(<br />

P)<br />

= 2.<br />

33 − 0.<br />

847α<br />

− 0.<br />

144α<br />

− 0.<br />

0657α<br />

α =<br />

log( 100<br />

− P)<br />

<strong>for</strong><br />

70%<br />

≤ P ≤<br />

3<br />

99.<br />

9%<br />

(9-31)<br />

The b<strong>and</strong>width f-10 was derived from a theoretical fading model <strong>of</strong> Karasawa <strong>and</strong><br />

Shiokawa [1984b] <strong>and</strong> is plotted as a function <strong>of</strong> elevation angle in Figure 9-11 at<br />

1.5 GHz <strong>for</strong> two maritime conditions. The upper bound (denoted by f-10U) corresponds to<br />

a significant wave height <strong>of</strong> 5 m, ship velocity <strong>of</strong> 20 knots, with a roll <strong>of</strong> 30°. The lower<br />

bound (f-10L) corresponds to a significant wave height <strong>of</strong> 1 m, ship velocity <strong>of</strong> 0 knots,<br />

with 0° roll. Least square fits <strong>of</strong> the lower <strong>and</strong> upper curves in Figure 9-11 have the <strong>for</strong>m<br />

⎛θ<br />

o ⎞<br />

f−10<br />

U , L = a + bexp⎜<br />

⎟ . (9-32)<br />

⎝ c ⎠<br />

The values <strong>of</strong> a,b,c are tabulated in Table 9-3 <strong>for</strong> the upper bound f-10U <strong>and</strong> lower bound<br />

f-10L.

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