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Technical Provisions for Mode S Services and Extended Squitter

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Appendix C C-51<br />

3. The decoded position latitude, Rlati, is then computed from the values of j, Dlati, <strong>and</strong> YZi using the<br />

equation:<br />

Rlat<br />

i<br />

⎛ YZi<br />

= Dlati<br />

⋅⎜<br />

j + 17<br />

⎝ 2<br />

⎞<br />

⎟<br />

⎠<br />

4. Dloni (the longitude zone size, in the E-W direction) is then computed from Rlati using the equation:<br />

⎧ 90°<br />

⎪<br />

,<br />

NL(<br />

Rlati<br />

) − i<br />

Dloni<br />

= ⎨<br />

⎪ 90°<br />

,<br />

⎪⎩<br />

when NL<br />

when NL<br />

( Rlat )<br />

i<br />

( Rlat )<br />

i<br />

− i > 0<br />

− i = 0<br />

Note.— When per<strong>for</strong>ming the NL function, the encoding process must ensure that the NL value<br />

is established in accordance with Note 5 of §C.2.6.2.d.<br />

5. The longitude zone coordinate m is then computed from the values of lons, Dloni, <strong>and</strong> XZi using the<br />

equation:<br />

( lon , Dlon )<br />

⎛ lon ⎞ ⎛<br />

⎞<br />

s 1 MOD s i XZ i<br />

m = floor ⎜<br />

⎟ + floor<br />

⎜ +<br />

−<br />

⎟ 17<br />

⎝ Dloni<br />

⎠ ⎝ 2 Dloni<br />

2 ⎠<br />

6. The decoded position longitude, Rloni, is then computed from the values of m, XZi, <strong>and</strong> Dloni using<br />

the equation:<br />

⎛ XZi<br />

⎞<br />

Rlon i = Dloni<br />

⋅⎜<br />

m + 17 ⎟<br />

⎝ 2 ⎠<br />

C.2.6.7 GLOBALLY UNAMBIGUOUS AIRBORNE POSITION DECODING<br />

The CPR algorithm shall utilize one airborne-encoded “even” <strong>for</strong>mat reception (denoted XZ0, YZ0), together<br />

with one airborne-encoded “odd” <strong>for</strong>mat reception (denoted XZ1, YZ1), to regenerate the global geographic<br />

position latitude, Rlat, <strong>and</strong> longitude, Rlon. The time between the “even” <strong>and</strong> “odd” <strong>for</strong>mat encoded position<br />

reports shall be not longer than 10 seconds <strong>for</strong> airborne <strong>for</strong>mats.<br />

Notes.—<br />

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

Draft<br />

1. This algorithm might be used to obtain globally unambiguous position reports <strong>for</strong> aircraft out of the<br />

range of ground sensors, whose position reports are coming via satellite data links. It might also be applied<br />

to ensure that local positions are being correctly decoded over long ranges from the receiving sensor.<br />

2. The time difference limit of 10 seconds between the even- <strong>and</strong> odd-<strong>for</strong>mat position reports <strong>for</strong><br />

airborne <strong>for</strong>mats is determined by the maximum permitted separation of 3 NM. Positions greater than 3 NM<br />

apart cannot be used to solve <strong>for</strong> a unique global position. An aircraft capable of a speed of 1850 km/h<br />

(1000 kt) will fly about 5.1 km (2.8 NM) in 10 seconds. There<strong>for</strong>e, the CPR algorithm will be able to<br />

unambiguously decode its position over a 10-second delay between position reports.<br />

Given a 17-bit airborne position encoded in the “even” <strong>for</strong>mat (XZ0, YZ0) <strong>and</strong> another encoded in the “odd”<br />

<strong>for</strong>mat (XZ1, YZ1), separated by no more than 10 seconds (= 3 NM), the CPR algorithm shall regenerate the<br />

geographic position from the encoded position reports by per<strong>for</strong>ming the following sequence of steps:<br />

a. Compute Dlat0 <strong>and</strong> Dlat1 from the equation:<br />

Dlat i<br />

360°<br />

=<br />

4⋅<br />

NZ − i<br />

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

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