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

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Optical Methods <strong>for</strong> Assessing Fade Margins 10-5<br />

10.4 Clear, Shadowed <strong>and</strong> Blocked <strong>Propagation</strong> States<br />

Fading <strong>for</strong> mobile satellite communications can be modeled by assuming that distinct<br />

signal level statistics pertain to three major propagation states, i.e., when the line-<strong>of</strong>-sight<br />

is clear with multipath contributions, shadowing by foliage, <strong>and</strong> blocked by buildings.<br />

Karasawa et al. [1994] fitted L-B<strong>and</strong> satellite fade data obtained in urban Japan at 32°<br />

elevation to a cumulative probability distribution consisting <strong>of</strong> a weighted linear<br />

combination <strong>of</strong> fading density functions developed by Rice, Loo, <strong>and</strong> Rayleigh. This<br />

linear combination is expressed by<br />

fν ( v) = C f Rice( v) + S f Loo( v) + B f Rayleigh(<br />

v)<br />

, (10-2)<br />

where C, S, B are probabilities <strong>of</strong> clear, shadowed, <strong>and</strong> blocked states, <strong>and</strong> fv denotes the<br />

probability density function (PDF) <strong>for</strong> the signal envelope. The Ricean density<br />

distribution is given by<br />

2 [ ] ( )<br />

f ( v) = 2Kv exp − K( v + 1) I 2Kv<br />

, (10-3)<br />

Rice o<br />

Loo’s density function [Loo, 1985] is given by<br />

f Loo<br />

( 20log(<br />

z)<br />

− m)<br />

2<br />

2 Kv 1<br />

2 2<br />

( v)<br />

8.<br />

686 exp<br />

K(<br />

v z ) I0<br />

( 2Kvz<br />

)dz<br />

2<br />

z<br />

0<br />

2<br />

⎥ ⎥ ∞ ⎡<br />

⎤<br />

= ∫ ⎢−<br />

− +<br />

, (10-4)<br />

π σ ⎢⎣<br />

σ<br />

⎦<br />

<strong>and</strong> the Rayleigh density function is given by<br />

2<br />

f Rayleigh( v) = 2Kv<br />

exp( −Kv<br />

) , (10-5)<br />

where ν is the received voltage relative to the clear path voltage, K is the ratio <strong>of</strong> the<br />

direct power received to the multipath power, I 0( ν ) is the modified Bessel function with<br />

argumentν , m is the mean <strong>of</strong> log(ν ) , <strong>and</strong> σ is the st<strong>and</strong>ard deviation <strong>of</strong> log(ν ) . It<br />

should be noted that (10-2) does not account <strong>for</strong> any specular reflection or any building<br />

diffracted power <strong>for</strong> blocked conditions.<br />

Satellite beacon <strong>and</strong> photogrammetrically measured values <strong>of</strong> K <strong>for</strong> the three fade<br />

states are tabulated in Table 10-3. Employing earth-satellite measurements at 1.5 GHz<br />

<strong>and</strong> 32° elevation <strong>for</strong> urban Tokyo, Karasawa et al. [1994] estimated values <strong>of</strong> C, S, B <strong>of</strong><br />

0.55, 0.1, 0.35, respectively. The “path-state mixture vector” <strong>for</strong> this case is defined as<br />

M =< 055 . , 01 . , 0. 35 > . (10-6)<br />

For the fit using (10-6), the RMS fade prediction error over the 5% to 95% interval is 1.3<br />

dB (3 rd column, last row in Table 10-3). The measured ( Δ ) <strong>and</strong> modeled (short dashed)<br />

cumulative fade distributions (CDF) <strong>of</strong> Karasawa et al. [1994] are plotted in Figure 10-4.<br />

Shown to the right <strong>of</strong> the distribution are error curves defined as the difference between<br />

the measured <strong>and</strong> modeled dB values. A peak error <strong>of</strong> approximately 3 dB occurs at a

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