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Galileo OS SIS ICD.indd - GSA - Europa

Galileo OS SIS ICD.indd - GSA - Europa

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leap seconds. Since the next leap second was inserted at 01.01.2006, this implies that<br />

as of 01.01.2006 GST is ahead of UTC by fourteen (14) leap seconds.<br />

The epoch denoted in the navigation messages by TOW and WN will be measured<br />

relative to the leading edge of the fi rst chip of the fi rst code sequence of the fi rst page<br />

symbol. The transmission timing of the navigation message provided through the TOW<br />

is synchronised to each satellite’s version of <strong>Galileo</strong> System Time (GST).<br />

5.1.3. Clock Correction Parameters<br />

The clock correction parameters are transmitted according to the values stated in Table<br />

64.<br />

Parameter Defi nition Bits Scale<br />

factor<br />

Unit<br />

t0c Clock correction data reference Time of Week 14 60 s<br />

a f0 SV clock bias correction coeffi cient 31* 2 -34 s<br />

a f1 SV clock drift correction coeffi cient 21* 2 -46 s/s<br />

a f2 SV clock drift rate correction coeffi cient 6* 2 -59 s/s 2<br />

Total Clock Correction Size 72<br />

Table 64. <strong>Galileo</strong> Clock Correction Parameters<br />

* Parameters so indicated are two’s complement, with the sign bit (+ or -) occupying the MSB.<br />

Each <strong>Galileo</strong> satellite broadcasts its own clock correction data for all signals through<br />

the relevant signal, according to Table 65.<br />

Message<br />

Type<br />

Clock Model<br />

X=(f1,f2)<br />

Satellite Time<br />

Correction Model<br />

Parameters<br />

F/Nav (E1,E5a) af0 (E1,E5a)<br />

af1 (E1,E5a)<br />

af2 (E1,E5a)<br />

t0C (E1,E5a)<br />

I/NAV (E1,E5b) af0 (E1,E5b)<br />

af1 (E1,E5b)<br />

af2 (E1,E5b)<br />

t0C (E1,E5b)<br />

5.1.4. Satellite Time Correction Algorithm<br />

Table 65. <strong>Galileo</strong> Clock Correction Data<br />

© European Union 2010<br />

Document subject to terms of use and disclaimers p. ii-iii<br />

OD <strong>SIS</strong> <strong>ICD</strong>, Issue 1, February 2010<br />

Services<br />

Dual-Frequency (E1,E5a)<br />

Single-frequency E5a<br />

Dual-Frequency (E1,E5b)<br />

Single-frequency E5b<br />

Single-frequency E1<br />

Each satellite transmits time correction data. The predicted offset of the physical<br />

satellite signal TOT relative to the satellite signal TOT in GST can be computed for the<br />

dual frequency signal combination using the following formula:<br />

where<br />

TOT c(X) = TOT m(X) - Δt SV(X) Eq. 12<br />

● (X)=(f 1,f 2) is the dual frequency combination f 1 and f 2 used for the clock model<br />

● TOT C(X) is the corrected satellite TOT in GST for the signal combination X<br />

47

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