Handbook of Propagation Effects for Vehicular and ... - Courses
Handbook of Propagation Effects for Vehicular and ... - Courses
Handbook of Propagation Effects for Vehicular and ... - Courses
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6-12<br />
6.6 Satellite Diversity<br />
6.6.1 Background<br />
<strong>Propagation</strong> <strong>Effects</strong> <strong>for</strong> <strong>Vehicular</strong> <strong>and</strong> Personal Mobile Satellite Systems<br />
Akturan <strong>and</strong> Vogel [1997] <strong>and</strong> Vogel [1997] describe a method by which they derive<br />
single <strong>and</strong> joint probability distributions <strong>and</strong> diversity gains associated with<br />
communications employing multiple satellites. The method consists <strong>of</strong>: (1) video<br />
recording hemispherical images <strong>of</strong> the surrounding environment through a fisheye lens<br />
mounted atop a mobile vehicle or photographing still images <strong>of</strong> the surrounding<br />
environment through a fisheye lens held head-high, (2) per<strong>for</strong>ming image analysis <strong>of</strong><br />
sequences <strong>of</strong> the hemispherical scenes, (3) simulating a constellation <strong>of</strong> “potentially<br />
visible satellite” locations <strong>for</strong> the particular region <strong>of</strong> the world <strong>and</strong> different times <strong>of</strong> the<br />
day, (4) extracting “path-state” in<strong>for</strong>mation associated with the line-<strong>of</strong>-sight <strong>for</strong> each<br />
“potentially visible satellite” (e.g., clear, shadowed, or blocked) <strong>for</strong> different times <strong>of</strong> the<br />
day <strong>for</strong> each scene, (5) injecting the “path-state” in<strong>for</strong>mation into an appropriate density<br />
distribution model, <strong>and</strong> (6) computing single <strong>and</strong> joint cumulative distributions associated<br />
with different satellite-look scenarios. Details concerning the density function models <strong>for</strong><br />
the different path states are described in Chapter 10.<br />
6.6.2 Cumulative Distributions<br />
Figure 6-9 depicts a series <strong>of</strong> L-B<strong>and</strong> distributions (f ≈ 1.6 GHz) <strong>for</strong> different diversity<br />
scenarios to the satellite <strong>for</strong> urban Japan, assuming a simulated “Globalstar” constellation<br />
<strong>of</strong> 48 satellites [Schindall, 1995]. In deriving the distributions given in Figure 6-9, 236<br />
images were combined with approximately 1000 independent constellation snapshots<br />
encompassing a 24 hour period (<strong>for</strong> each image). Hence, an equivalence <strong>of</strong> 236,000 sets<br />
<strong>of</strong> path states went into the database, where approximately 50% <strong>of</strong> the time three<br />
satellites were potentially visible. The distribution labeled “Highest Satellite” represents<br />
the distribution associated with the satellite having the greatest elevation angle. This<br />
distribution was derived under the condition that the mobile antenna transmits to or<br />
receives radiation from a different satellite position every time a new satellite achieves<br />
the highest elevation angle, independent <strong>of</strong> azimuth. The highest elevation path may not<br />
necessarily have a “clear” path state. That is, depending upon the scene at the time, it<br />
may be representative <strong>of</strong> a “blocked” path state. The distribution labeled “Best Satellite”<br />
is also derived from multiple satellites where the antenna is pointed to the satellite giving<br />
the smallest fade.<br />
In calculating this distribution, a decision <strong>for</strong> “best satellite” was made<br />
approximately every 20 seconds be<strong>for</strong>e “h<strong>and</strong>-over” was potentially executed. The<br />
distribution labeled “2 Best Satellites” represents the joint distribution associated with the<br />
two satellites giving jointly the “smallest fades”. At any instant <strong>of</strong> time, different pairs <strong>of</strong><br />
satellites may fall under the “2 Best Satellite” category. The distributions labeled “3 Best<br />
Satellites” <strong>and</strong> “4 Best Satellites” are analogously defined. The above joint distributions<br />
were derived assuming “combining diversity” where the signals received are “added,” as<br />
opposed to “h<strong>and</strong>-<strong>of</strong>f” where the satellite with the “highest” signal is processed. It is<br />
apparent that each <strong>of</strong> the above distributions is calculated from many different satellites<br />
at variable elevation <strong>and</strong> azimuth angles. Using the “Highest Satellite” distribution as the