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Technical Provisions for Mode S Services and Extended Squitter

Technical Provisions for Mode S Services and Extended Squitter

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DRAFT - Working Paper ASP TSGWP11-01 <strong>for</strong> review by the TSG during the meeting in June 2011 in Paris<br />

CD-22 <strong>Technical</strong> <strong>Provisions</strong> <strong>for</strong> <strong>Mode</strong> S <strong>Services</strong> <strong>and</strong> <strong>Extended</strong> <strong>Squitter</strong><br />

well in excess of any operationally useful coverage since an aircraft at 600 km (325 NM) will only be visible to a surface<br />

receiver if the aircraft is at an altitude greater than 21 000 m (70 000 ft).<br />

The elements of this coding technique are illustrated in Figure CD-4. For ease of explanation, the figure shows four<br />

contiguous area cells on a flat earth. The basic encoding provides unambiguous position within the dotted box centered<br />

on the receiver, i.e. a minimum of 333 km (180 NM). Beyond this range, ambiguous position reporting can result. For<br />

example, an aircraft shown at A would have an ambiguous image at B. However, in this case the in<strong>for</strong>mation provided<br />

by the sector antenna eliminates the ambiguity. This technique will work out to a range shown as the aircraft labeled C.<br />

At this range, the image of C (shown as D) is at a range where it could be received through the sidelobes of the sector<br />

antenna.<br />

360 NM<br />

360 NM<br />

360 NM<br />

x x<br />

B D<br />

360 NM<br />

Draft<br />

Figure CD-4. Maximum range considerations <strong>for</strong> CPR encoding<br />

DRAFT - Working Paper ASP TSGWP11-01 <strong>for</strong> review by the TSG during the meeting in June 2011 in Paris<br />

x<br />

A<br />

C x

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