6 GNSS information
3GPP51.010-7Mobile Station (MS) conformance specificationPart 7: Location Services (LCS) test scenarios and assistance dataRelease 12TS
6.1 GNSS Scenarios and Assistance Data for Assisted GNSS signalling tests
6.1.1 General
This subclause defines the GNSS scenario and the associated assistance data that shall be used for all Assisted GNSS signalling tests defined in TS 51.010-1 [4] subclauses 70.12 to 70.15.
The satellite simulator (SS) shall generate all the MS supported GNSS satellite signals defined in subclause 6.1.2 and shall provide assistance data dependent on the MS capabilities defined in subclause 6.1.3.
Where assistance data is required on a per-satellite basis, or where the values of the data also varies with time it is specified in comma-separated-variable files in the GNSS_data.zip file defined in Annex B. These files specify the values to be used for each satellite, indexed by satellite SV ID, and, where applicable, the values to be used indexed by both time and satellite SV ID.
Assistance data that is marked as "time varying" and the GNSS TOW and GANSS TOD fields are only specified and used in 0.96 or 1 second increments. Interpolation between these values shall not be used.
The accuracy of the GNSS TOW and GANSS TOD and assistance data that is marked as "time varying" in the provided assistance data shall be within +/- 2 s relative to the GNSS time in the system simulator.
Assistance data Information Elements and fields that are not specified shall not be used.
The A-GNSS signalling test cases may include several sub-test cases dependent on the GNSS supported by the MS. Each sub-test case is identified by a Sub-Test Case Number as defined in Table 6.1.1.1. The detailed assistance data content defined in subclause 6.1.3 depends on the particular sub-test case.
The term SV ID used in this subclause is defined as the satellite PRN for GPS and Galileo, as the satellite Slot Number for GLONASS and as the Ranging Code Number for BDS.
Most data for Galileo is for further study [FFS].
Table 6.1.1.1: Sub-Test Case Number Definition
Sub-Test Case Number |
Supported GNSS |
1 |
MS supporting A-GLONASS only |
2 |
MS supporting A-Galileo only |
3 |
MS supporting A-GPS and Modernized GPS only |
4 |
MS supporting A-GPS and A-GLONASS only |
5 |
Reserved |
6 |
Reserved |
7 |
Reserved |
8 |
Reserved |
9 |
MS supporting A-BDS only |
10 |
MS supporting A-GPS and A-BDS only |
6.1.2 GNSS Scenario
The following GNSS scenario shall be used. The assistance data specified in the following subclauses is consistent with this GNSS scenario:
– Yuma Almanac data: the required file(s) in the GNSS_data_sig.zip file specified in Annex B are given below.
Table 6.1.2.1: Yuma Almanac data files for TS 51.010-1 subclause 70.12 to 70.15
Sub-Test Case Number |
Yuma file(s) |
1 |
Sig_GNSS_1-1_Yuma.txt |
2 |
Sig_GNSS_1-2_Yuma.txt |
3 |
Sig_GNSS_1-3_Yuma.txt |
4 |
Sig_GNSS_1-1_Yuma.txt and Sig_GNSS_1-3_Yuma.txt |
5 |
[FFS] |
6 |
[FFS] |
7 |
[FFS] |
8 |
[FFS] |
9 |
Sig_GNSS_1-9_Yuma.txt |
10 |
Sig_GNSS_1-3_Yuma.txt and Sig_GNSS_1-9_Yuma.txt |
– MS location and Reference location: static at latitude: 35 degrees 44 minutes 39.432 seconds north, longitude: 139 degrees 40 minutes 48.633 seconds east, (Tokyo Japan 2012), height: 300m
– Start time: 1st January 2012 00:31:00 (GPS time)
– Visible satellites simulated are given below
Table 6.1.2.2: Satellites to be simulated for TS 51.010-1 subclause 70.12 to 70.15
Sub-Test Case Number |
SV IDs of Satellites to be simulated |
1 |
3, 4, 9, 10, 18, 20 |
2 |
[FFS] |
3 |
1, 11, 17, 20, 23, 28 (Note) |
4 |
GPS: 1, 17, 20, 28. GLONASS: 3, 10, 18, 20 |
5 |
[FFS] |
6 |
[FFS] |
7 |
[FFS] |
8 |
[FFS] |
9 |
1, 2, 7, 18, 21, 27 |
10 |
GPS: 1, 17, 20, 28. BDS: 1, 7, 18, 21 |
NOTE: For this sub-test the satellite simulator shall generate all the GPS signals supported by the MS for all the simulated satellites. |
– Ionospheric model: see values in subclause 6.1.3
– The levels of the simulated satellites shall all be at -125dBm +/- 6dB
6.1.3 Default Assistance Data Elements to be provided by the SS
The assistance data listed in subclause 6.1.3 are the assistance data elements to be pushed by the SS in some of the tests defined in TS 51.010-1 [4] subclause 70.12 to 70.15. After the reception of an RRLP MEASURE POSITION REQUEST message, the MS may request additional assistance data. In this case the SS shall provide the requested assistance data only if it is available as defined in subclause 6.1.4.
Table 6.1.3.1: GNSS assistance data to be provided to the MS
GNSS Assistance Data IE to be provided to the MS |
Mode used in test case |
|
MS-based |
MS-assisted |
|
GPS Reference Time |
Yes for sub-tests 3, 4, 10 |
Yes for sub-tests 3, 4, 10 |
GPS Reference Time Extension (Rel-10 onwards) |
Yes for sub-tests 3, 4, 10 |
Yes for sub-tests 3, 4, 10 |
GPS Reference Location |
Yes for sub-tests 3, 4, 10 |
No |
GPS Navigation Model |
Yes for sub-tests 3, 4, 10 |
No |
GPS Ionospheric Model |
Yes for sub-tests 3, 4, 10 |
No |
GPS UTC Model |
Yes for sub-test 4 |
Yes for sub-test 4 |
GPS Acquisition Assistance |
No |
Yes for sub-tests 3, 4, 10 |
GPS Acquisition Assistance Extension (Rel-10 onwards) |
No |
Yes for sub-tests 3, 4, 10 |
GANSS Reference Time |
Yes for sub-tests 1, 2, 9 |
Yes for sub-tests 1, 2, 9 |
GANSS Reference Location |
Yes for sub-tests 1, 2, 9 |
No |
GANSS Ionospheric Model |
Yes for sub-test 2 |
No |
GANSS Additional Ionospheric Model |
Yes for sub-test 1, 9, 10 |
No |
GANSS Time Model |
Yes for sub-test 4, 10 |
No |
GANSS Time Model Extension (Rel-10 onwards) |
Yes for sub-test 4, 10 |
No |
GANSS Navigation Model |
Yes for sub-tests 1, 2, 4, 9, 10 |
No |
GANSS Reference Measurement Information |
No |
Yes for sub-tests 1, 2, 4, 9, 10 |
GANSS Reference Measurement Extension (Rel-10 onwards) |
No |
Yes for sub-tests 1, 2, 4, 9, 10 |
GANSS Auxiliary Information |
Yes for sub-tests 1, 3, 4. Note. |
Yes for sub-tests 1, 3, 4. Note. |
Note: Also if MS supports multiple signals per GNSS |
6.1.4 Assistance Data values
Satellite SV IDs to be used
For assistance data IEs which contain the field SatID or SVID/PRNID, and where the values for these fields are not given below, then the following values shall be used.
Table 6.1.4.1: Satellite SV IDs to be used for SatID or SVID/PRNID
Sub-Test Case Number |
SV IDs of Satellites to be used |
1 |
3, 4, 9, 10, 18, 20 |
2 |
[FFS] |
3 |
1, 11, 17, 20, 23, 28 |
4 |
GPS: 1, 17, 20, 28. GLONASS: 3, 10, 18, 20 |
5 |
[FFS] |
6 |
[FFS] |
7 |
[FFS] |
8 |
[FFS] |
9 |
1, 2, 7, 18, 21, 27 |
10 |
GPS: 1, 17, 20, 28. BDS: 1, 7, 18, 21 |
Assistance Data GPS Reference Time
Table 6.1.4.2: GPS Reference Time (Fields occurring once per message)
Information Element |
Units |
Value/remark |
GPS Week |
weeks |
1669 |
GPS TOW |
sec |
1860 Start time. Add integer number of 0.96 seconds as required. (Note) |
Note: GPS TOW This is the value of GPS TOW in seconds when the GNSS scenario is started in the GNSS simulator. The value of GPS TOW to be used in the Reference Time IE shall be calculated at the time the IE is required by adding the elapsed time since the time the scenario was started in the GNSS simulator to this value, rounded up to the next 0.96 second interval. This "current GPS TOW" is then also used to determine the value of any other Information Elements marked as "Time varying" in subclause 6.1.4. |
Assistance Data GPS Reference Time Extension
Table 6.1.4.2a: GPS Reference Time Extension (Fields occurring once per message)
Information Element |
Units |
Value/remark |
Release |
GPS Week Cycle Number |
1024 weeks |
1 |
Rel-10 onwards |
Assistance Data GPS Reference Location
Table 6.1.4.3: GPS Reference Location
Information Element |
Units |
Value/remark |
---|---|---|
Latitude sign |
0 |
|
Degrees Of Latitude |
degrees |
35.744287 |
Degrees Of Longitude |
degrees |
139.680176 |
Altitude Direction |
0 |
|
Altitude |
m |
300 |
Uncertainty semi-major |
m |
3000 |
Uncertainty semi-minor |
m |
3000 |
Orientation of major axis |
degrees |
0 |
Uncertainty Altitude |
m |
500 |
Confidence |
% |
68 |
Assistance Data GPS Navigation Model
Table 6.1.4.4: Satellite Information
Information Element |
Units |
Value/remark |
Num_Sats_Total |
6 |
Table 6.1.4.5: GPS Navigation Model (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
SatID |
See Table 6.1.4.1 |
|
Satellite Status |
0 (see note) |
|
NOTE: For consistency Satellite Status is also given in file: Sig_GPS_Navigation_model.csv |
Table 6.1.4.6: GPS Ephemeris and Clock correction Information Elements (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
C/A or P on L2 |
See file: Sig_GPS_Navigation_model.csv |
|
URA Index |
See file: Sig_GPS_Navigation_model.csv |
|
SV Health |
See file: Sig_GPS_Navigation_model.csv |
|
IODC |
See file: Sig_GPS_Navigation_model.csv |
|
L2 P Data Flag |
See file: Sig_GPS_Navigation_model.csv |
|
SF 1 Reserved |
See file: Sig_GPS_Navigation_model.csv |
|
SF 2 Reserved |
See file: Sig_GPS_Navigation_model.csv |
|
SF 3 Reserved |
See file: Sig_GPS_Navigation_model.csv |
|
SF 4 Reserved |
See file: Sig_GPS_Navigation_model.csv |
|
TGD |
sec |
See file: Sig_GPS_Navigation_model.csv |
toc |
sec |
See file: Sig_GPS_Navigation_model.csv |
af2 |
sec/sec2 |
See file: Sig_GPS_Navigation_model.csv |
af1 |
sec/sec |
See file: Sig_GPS_Navigation_model.csv |
af0 |
sec |
See file: Sig_GPS_Navigation_model.csv |
Crs |
meters |
See file: Sig_GPS_Navigation_model.csv |
n |
semi-circles/sec |
See file: Sig_GPS_Navigation_model.csv |
M0 |
semi-circles |
See file: Sig_GPS_Navigation_model.csv |
Cuc |
radians |
See file: Sig_GPS_Navigation_model.csv |
e |
See file: Sig_GPS_Navigation_model.csv |
|
Cus |
radians |
See file: Sig_GPS_Navigation_model.csv |
(A)1/2 |
meters1/2 |
See file: Sig_GPS_Navigation_model.csv |
toe |
sec |
See file: Sig_GPS_Navigation_model.csv |
Fit Interval Flag |
See file: Sig_GPS_Navigation_model.csv |
|
AODO |
sec |
See file: Sig_GPS_Navigation_model.csv |
Cic |
radians |
See file: Sig_GPS_Navigation_model.csv |
OMEGA0 |
semi-circles |
See file: Sig_GPS_Navigation_model.csv |
Cis |
radians |
See file: Sig_GPS_Navigation_model.csv |
i0 |
semi-circles |
See file: Sig_GPS_Navigation_model.csv |
Crc |
meters |
See file: Sig_GPS_Navigation_model.csv |
|
semi-circles |
See file: Sig_GPS_Navigation_model.csv |
OMEGAdot |
semi-circles/sec |
See file: Sig_GPS_Navigation_model.csv |
Idot |
semi-circles/sec |
See file: Sig_GPS_Navigation_model.csv |
Assistance Data GPS Ionospheric Model
Table 6.1.4.7: GPS Ionospheric Model
Information Element |
Units |
Value/remark |
0 |
seconds |
4.6566129 10E-9 |
1 |
sec/semi-circle |
1.4901161 10E-8 |
2 |
sec/(semi-circle)2 |
-5.96046 10E-8 |
3 |
sec/(semi-circle)3 |
-5.96046 10E-8 |
0 |
seconds |
79872 |
1 |
sec/semi-circle |
65536 |
2 |
sec/(semi-circle)2 |
-65536 |
3 |
sec/(semi-circle)3 |
-393216 |
Assistance Data GPS UTC Model
Table 6.1.4.8: GPS UTC Model
Information Element |
Units |
Value/remark |
A1 |
sec/sec |
0 |
A0 |
seconds |
0 |
tot |
seconds |
249856 |
WNt |
weeks |
133 |
tLS |
seconds |
15 |
WNLSF |
weeks |
158 |
DN |
days |
7 |
tLSF |
seconds |
16 |
Assistance Data GPS Almanac
Table 6.1.4.9: GPS Almanac (Fields occurring once per message)
Information Element |
Units |
Value/remark |
Num_Sats_Total |
31 |
|
WNa |
weeks |
1669 |
Table 6.1.4.10: GPS Almanac (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
SatID |
PRNs: 1, 2, 3…21, 22, 23, 25, 26, 27…30, 31, 32 |
|
e |
dimensionless |
See file: Sig_GPS_Almanac.csv |
toa |
sec |
See file: Sig_GPS_Almanac.csv |
i |
semi-circles |
See file: Sig_GPS_Almanac.csv |
OMEGADOT |
semi-circles/sec |
See file: Sig_GPS_Almanac.csv |
SV Health |
See file: Sig_GPS_Almanac.csv |
|
A1/2 |
meters1/2 |
See file: Sig_GPS_Almanac.csv |
OMEGA0 |
semi-circles |
See file: Sig_GPS_Almanac.csv |
|
semi-circles |
See file: Sig_GPS_Almanac.csv |
M0 |
semi-circles |
See file: Sig_GPS_Almanac.csv |
af0 |
seconds |
See file: Sig_GPS_Almanac.csv |
af1 |
sec/sec |
See file: Sig_GPS_Almanac.csv |
Assistance Data GPS Almanac Extension
Table 6.1.4.10a: GPS Almanac Extension (Fields occurring once per message)
Information Element |
Units |
Value/remark |
Release |
Complete Almanac Provided |
1 (TRUE) |
Rel-10 onwards |
Assistance Data GPS Acquisition Assistance
Table 6.1.4.11: GPS Acquisition Assistance – Information Elements appearing once per message
Information Element |
Units |
Value/remark |
Number of Satellites |
6 |
|
GPS TOW |
1860 s Start time. Add integer number of 0.96 seconds as required. (Note) |
|
Note: GPS TOW |
Table 6.1.4.12: GPS Acquisition Assistance – Information Elements appearing once per satellite
Information Element |
Units |
Value/remark |
SVID/PRNID |
See Table 6.1.4.1 |
|
Doppler (0th order term) |
Hz |
Time varying. See file: Sig_GPS_Acquisition_assist.csv (Note) |
Doppler (1st order term) |
Hz/sec |
Time varying. See file: Sig_GPS_Acquisition_assist.csv (Note) |
Doppler Uncertainty |
Hz |
Time varying. See file: Sig_GPS_Acquisition_assist.csv (Note) |
Code Phase |
chips |
Time varying. See file: Sig_GPS_Acquisition_assist.csv (Note) |
Integer Code Phase |
Time varying. See file: Sig_GPS_Acquisition_assist.csv (Note) |
|
GPS Bit number |
Time varying. See file: Sig_GPS_Acquisition_assist.csv (Note) |
|
Code Phase Search Window |
chips |
Time varying. See file: Sig_GPS_Acquisition_assist.csv (Note) |
Azimuth |
deg |
Time varying. See file: Sig_GPS_Acquisition_assist.csv (Note) |
Elevation |
deg |
Time varying. See file: Sig_GPS_Acquisition_assist.csv (Note) |
Note: This field is "Time varying" and its value depends on the "current GPS TOW". The value of this field to be used shall be determined by taking the "current GPS TOW" value and selecting the field value in the Sig_GPS_Acquisition_assist.csv file corresponding to the value of "current GPS TOW ". |
Assistance Data GPS Acquisition Assistance Extension
Table 6.1.4.12a: GPS Acquisition Assistance Extension – Information Elements appearing once per message
Information Element |
Units |
Value/remark |
Release |
N_SAT |
6 |
Rel-10 onwards |
Table 6.1.4.12b: GPS Acquisition Assistance Extension – Information Elements appearing once per satellite
Information Element |
Units |
Value/remark |
Release |
SatID |
See Table 6.1.4.1 |
Rel-10 onwards |
|
Azimuth LSB |
degrees |
Time varying. Calculated from Azimuth, see file: Sig_GPS_Acquisition_assist.csv (Note) |
Rel-10 onwards |
Elevation LSB |
degrees |
Time varying. Calculated from Elevation, see file: Sig_GPS_Acquisition_assist.csv (Note) |
Rel-10 onwards |
Note: This field is "Time varying" and its value depends on the "current GPS TOW" as described in subclause 5.1.3. The value of this field to be used shall be determined by taking the "current GPS TOW" value and selecting the field value in the Sig_GPS_Acquisition_assist.csv file corresponding to the value of "current GPS TOW". |
Assistance Data GANSS Reference Time
Table 6.1.4.13: Assistance Data GANSS Reference Time: sub-test 1
Information Element |
Units |
Value/remark |
---|---|---|
GANSS Day |
5844 |
|
GANSS TOD |
seconds |
12645 s Start time. Add integer number of 1 seconds as required. (Note) |
GANSS TOD Uncertainty |
125 (2.127 seconds) |
|
GANSS Time ID |
2 (GLONASS) |
|
Note: GANSS TOD This is the value of GANSS TOD when the GNSS scenario is started in the GNSS simulator. The value of GANSS TOD to be used in the Reference Time IE shall be calculated at the time the IE is required by adding the elapsed time since the time the scenario was started in the GNSS simulator to this value, rounded up to the next 1 second interval. This "current GANSS TOD" is then also used to determine the value of any other Information Elements marked as "Time varying" in subclause 6.1.4 |
Table 6.1.4.14: Assistance Data GANSS Reference Time: sub-test 2
Information Element |
Units |
Value/remark |
---|---|---|
GANSS Day |
FFS |
|
GANSS TOD |
seconds |
FFS Start time. Add integer number of 1 seconds as required. (Note) |
GANSS TOD Uncertainty |
125 (2.127 seconds) |
|
GANSS Time ID |
Not present (Galileo) |
|
Note: GANSS TOD This is the value of GANSS TOD when the GNSS scenario is started in the GNSS simulator. The value of GANSS TOD to be used in the Reference Time IE shall be calculated at the time the IE is required by adding the elapsed time since the time the scenario was started in the GNSS simulator to this value, rounded up to the next 1 second interval. This "current GANSS TOD" is then also used to determine the value of any other Information Elements marked as "Time varying" in subclause 6.1.4 |
Table 6.1.4.14a: Assistance Data GANSS reference time: sub-test 9
Information Element |
Units |
Value/remark |
Release |
---|---|---|---|
GANSS Day |
2191 |
||
GANSS Day Cycle Number |
0 |
||
GANSS TOD |
Seconds |
1846. Start time. Add integer number of 1 seconds as required. (Note) |
|
GANSS TOD Uncertainty |
125 (2.127 seconds) |
||
GANSS Time ID |
3 (BDS) |
||
Note: GANSS TOD This is the value of GANSS TOD when the GNSS scenario is started in the GNSS simulator. The value of GANSS TOD to be used in the Reference Time IE shall be calculated at the time the IE is required by adding the elapsed time since the time the scenario was started in the GNSS simulator to this value, rounded up to the next 1 second interval. This "current GANSS TOD" is then also used to determine the value of any other Information Elements marked as "Time varying" in subclause 6.1.4 |
Assistance Data GANSS Reference Location
Table 6.1.4.15: Assistance Data GANSS Reference Location
Information Element |
Units |
Value/remark |
---|---|---|
Latitude sign |
0 |
|
Degrees Of Latitude |
degrees |
35.744287 |
Degrees Of Longitude |
degrees |
139.680176 |
Altitude Direction |
0 |
|
Altitude |
m |
300 |
Uncertainty semi-major |
m |
3000 |
Uncertainty semi-minor |
m |
3000 |
Orientation of major axis |
degrees |
0 |
Uncertainty Altitude |
m |
500 |
Confidence |
% |
68 |
Assistance Data GANSS Ionospheric Model
Table 6.1.4.16: GANSS Ionospheric Model
Information Element |
Units |
Value/remark |
ai0 |
Solar Flux Units |
FFS |
ai1 |
Solar Flux Units/degree |
FFS |
ai2 |
Solar Flux Units/degree2 |
FFS |
Storm Flag 1 |
0 |
|
Storm Flag 2 |
0 |
|
Storm Flag 3 |
0 |
|
Storm Flag 4 |
0 |
|
Storm Flag 5 |
0 |
Assistance Data GANSS Additional Ionospheric Model
Table 6.1.4.16a: GANSS Additional Ionospheric Model (GLONASS)
Information Element |
Units |
Value/remark |
Data Id |
00 |
|
0 |
Seconds |
4.6566129 10E-9 |
1 |
sec/semi-circle |
1.4901161 10E-8 |
2 |
sec/(semi-circle)2 |
-5.96046 10E-8 |
3 |
sec/(semi-circle)3 |
-5.96046 10E-8 |
0 |
Seconds |
79872 |
1 |
sec/semi-circle |
65536 |
2 |
sec/(semi-circle)2 |
-65536 |
3 |
sec/(semi-circle)3 |
-393216 |
Table 6.1.4.16ab: GANSS additional ionospheric model (BDS)
Information Element |
Units |
Value/remark |
Data Id |
01 |
|
0 |
Seconds |
4.6566129 10E-9 |
1 |
sec/semi-circle |
1.4901161 10E-8 |
2 |
sec/(semi-circle)2 |
-5.96046 10E-8 |
3 |
sec/(semi-circle)3 |
-5.96046 10E-8 |
0 |
Seconds |
79872 |
1 |
sec/semi-circle |
65536 |
2 |
sec/(semi-circle)2 |
-65536 |
3 |
sec/(semi-circle)3 |
-393216 |
Assistance Data GANSS ID
Table 6.1.4.16b: GANSS ID: sub-test 1, 4
Information Element |
Units |
Value/remark |
---|---|---|
GANSS ID |
3 (GLONASS) |
Table 6.1.4.16c: GANSS ID: sub-test 2
Information Element |
Units |
Value/remark |
---|---|---|
GANSS ID |
Not present (Galileo) |
Table 6.1.4.16d: GANSS ID: sub-test 3
Information Element |
Units |
Value/remark |
---|---|---|
GANSS ID |
1 (Modernized GPS) |
Table 6.1.4.16e: GANSS ID: sub-test 9, 10
Information Element |
Units |
Value/remark |
---|---|---|
GANSS ID |
4 (BDS) |
Assistance Data GANSS Time Model
Table 6.1.4.17: GANSS time Model
Information Element |
Units |
Value/remark |
GANSS Time Model Reference Time |
1860 s |
|
TA0 |
Seconds |
0 |
GNSS_TO_ID |
0 (GPS) |
|
Assistance Data GANSS Time Model Extension
Table 6.1.4.17a: GANSS Time Model Extension (GLONASS)
Information Element |
Units |
Value/remark |
Release |
GNSS_TOD_ID |
0 (GPS) |
Rel-10 onwards |
|
Delta T |
Seconds |
15 |
Rel-10 onwards |
Table 6.1.4.17b: GANSS Time Model Extension (BDS)
Information Element |
Units |
Value/remark |
Release |
GNSS_TOD_ID |
0 (GPS) |
||
Delta T |
Seconds |
13 |
Assistance Data GANSS Navigation Model
Table 6.1.4.18: Void
Table 6.1.4.19: GANSS Navigation Model: sub-test 1, 4
Information Element |
Units |
Value/remark |
---|---|---|
Num_Sat |
6 |
|
Non-Broadcast Indication |
0 |
Table 6.1.4.20: Satellite Information (Fields occurring once per satellite): sub-test 1, 4
Information Element |
Units |
Value/remark |
SatID |
See Table 6.1.4.1 |
|
SV Health |
01111 (Note) |
|
IOD |
225 (Note) |
|
Note: For consistency SV Health and IOD are also given in file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
Table 6.1.4.21: GANSS Clock Model (Fields occurring once per satellite): sub-test 1, 4
Information Element |
Units |
Value/remark |
GLONASS Satellite Clock Model |
||
n(tb) |
seconds |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
n(tb) |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
|
n |
seconds |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
Table 6.1.4.22: GANSS Orbit Model (Fields occurring once per satellite): sub-test 1, 4
Information Element |
Units |
Value/remark |
---|---|---|
GLONASS Earth-Centered, Earth-fixed Parameters |
||
En |
days |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
P1 |
minutes |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
P2 |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
|
M |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
|
kilometers |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
|
kilometers/sec |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
|
kilometers/sec2 |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
|
kilometers |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
|
kilometers/sec |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
|
kilometers/sec2 |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
|
kilometers |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
|
kilometers/sec |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
|
kilometers/sec2 |
See file: Sig_GANSS_Navigation_Model_subtest1_4.csv |
Table 6.1.4.23: Void
Table 6.1.4.24: GANSS Navigation Model: sub-test 2
Information Element |
Units |
Value/remark |
---|---|---|
Num_Sat |
6 |
|
Non-Broadcast Indication |
0 |
Table 6.1.4.25: Satellite Information (Fields occurring once per satellite): sub-test 2
Information Element |
Units |
Value/remark |
SatID |
See Table 6.1.4.1 |
|
SV Health |
0 (Note) |
|
IOD |
[FFS] (Note) |
|
Note: For consistency SV Health and IOD are also given in file: See file: Sig_GANSS_Navigation_Model_subtest2.csv. |
Table 6.1.4.26: GANSS Clock Model (Fields occurring once per satellite): sub-test 2
Information Element |
Units |
Value/remark |
Satellite clock model (Galileo) |
||
toc |
seconds |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
af2 |
sec/sec2 |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
af1 |
sec/sec |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
af0 |
sec |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
TGD (BGD) |
sec |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
Model ID |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
Table 6.1.4.27: GANSS Orbit Model (Fields occurring once per satellite): sub-test 2
Information Element |
Units |
Value/remark |
---|---|---|
Keplerian Parameters |
||
toe |
seconds |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
|
semi-circles |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
n |
semi-circles/sec |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
M0 |
semi-circles |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
OMEGAdot |
semi-circles/sec |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
e |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
|
Idot |
semi-circles/sec |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
sqrtA |
meters1/2 |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
i0 |
semi-circles |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
OMEGA0 |
semi-circles |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
Crs |
meters |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
Cis |
radians |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
Cus |
radians |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
Crc |
meters |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
Cic |
radians |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
Cuc |
radians |
See file: Sig_GANSS_Navigation_Model_subtest2.csv |
Table 6.1.4.27a: GANSS Navigation Model: sub-test 9, 10
Information Element |
Units |
Value/remark |
---|---|---|
Num_Sat |
6 |
|
Non-Broadcast Indication |
0 |
Table 6.1.4.27b: Satellite Information (Fields occurring once per satellite): sub-test 9, 10
Information Element |
Units |
Value/remark |
SatID |
See Table 6.1.4.1 |
|
SV Health |
0 (Note) |
|
IOD |
0 (Note) |
|
Note: For consistency SV Health and IOD are also given in file: See file: Sig_GANSS_Navigation_Model_subtest9_10.csv. |
Table 6.1.4.27c: GANSS Clock Model (Fields occurring once per satellite): sub-test 9, 10
Information Element |
Units |
Value/remark |
BDS Satellite clock model |
||
AODC |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
|
toc |
seconds |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
a0 |
sec |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
a1 |
sec/sec |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
a2 |
sec/sec2 |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
TGD |
sec |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
Table 6.1.4.27d: GANSS Orbit Model (Fields occurring once per satellite): sub-test 9, 10
Information Element |
Units |
Value/remark |
---|---|---|
Keplerian Parameters |
||
AODE |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
|
URA Index |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
|
toe |
seconds |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
A1/2 |
meters1/2 |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
e |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
|
|
semi-circles |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
n |
semi-circles/sec |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
M0 |
semi-circles |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
OMEGA0 |
semi-circles |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
OMEGAdot |
semi-circles/sec |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
i0 |
semi-circles |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
Idot |
semi-circles/sec |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
Cuc |
radians |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
Cus |
radians |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
Crc |
meters |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
Crs |
meters |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
Cic |
radians |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
Cis |
radians |
See file: Sig_GANSS_Navigation_Model_subtest9_10.csv |
Assistance Data GANSS Reference Measurement Information
Table 6.1.4.28: Void
Table 6.1.4.29: GANSS reference measurement information: sub-test 1, 4 (Fields occurring once per message)
Information Element |
Units |
Value/remark |
GANSS Signal ID |
0 (G1) |
Table 6.1.4.30: GANSS Reference Measurement Information: sub-test 1, 4 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
---|---|---|
SVID |
See Table 6.1.4.1 |
|
Doppler (0th order term) |
m/s |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest1_4.csv (Note) |
Doppler (1st order term) |
m/s/s |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest1_4.csv (Note) |
Doppler Uncertainty |
m/s |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest1_4.csv (Note) |
Code Phase |
ms |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest1_4.csv (Note) |
Integer Code Phase |
ms |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest1_4.csv (Note) |
Code Phase Search Window |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest1_4.csv (Note) |
|
Azimuth |
deg |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest1_4.csv (Note) |
Elevation |
deg |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest1_4.csv (Note) |
Note: For sub-test 1: this field is "Time varying" and its value depends on the "current GANSS TOD". The value of this field to be used shall be determined by taking the "current GANSS TOD" value and selecting the field value in the Sig_GANSS_reference_measurement_information_subtest1_4.csv file corresponding to the value of "current GANSS TOD". For sub-test 4: this field is "Time varying" and its value depends on the "current GPS TOW". The value of this field to be used shall be determined by taking the "current GPS TOW" value and selecting the field value in the Sig_GANSS_reference_measurement_information_subtest1_4.csv file corresponding to the value of "current GPS TOW". |
Table 6.1.4.31: Void
Table 6.1.4.32: GANSS Reference Measurement Information: sub-test 2 (Fields occurring once per message)
Information Element |
Units |
Value/remark |
GANSS Signal ID |
0 (E1) |
Table 6.1.4.33: GANSS Reference Measurement Information: sub-test 2 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
---|---|---|
SVID |
See Table 6.1.4.1 |
|
Doppler (0th order term) |
m/s |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest2.csv (Note) |
Doppler (1st order term) |
m/s/s |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest2.csv (Note) |
Doppler Uncertainty |
m/s |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest2.csv (Note) |
Code Phase |
ms |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest2.csv (Note) |
Integer Code Phase |
ms |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest2.csv (Note) |
Code Phase Search Window |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest2.csv (Note) |
|
Azimuth |
deg |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest2.csv (Note) |
Elevation |
deg |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest2.csv (Note) |
Note: This field is "Time varying" and its value depends on the "current GANSS TOD". The value of this field to be used shall be determined by taking the "current GANSS TOD" value and selecting the field value in the Sig_GANSS_reference_measurement_information_subtest2.csv file corresponding to the value of "current GANSS TOD". |
Table 6.1.4.33aa: GANSS reference measurement information: sub-test 9, 10 (Fields occurring once per message)
Information Element |
Units |
Value/remark |
GANSS Signal ID |
0 (B1I) |
Table 6.1.4.33ab: GANSS Reference Measurement Information: sub-test 9, 10 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
---|---|---|
SVID |
See Table 6.1.4.1 |
|
Doppler (0th order term) |
m/s |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest9_10.csv (Note) |
Doppler (1st order term) |
m/s/s |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest9_10.csv (Note) |
Doppler Uncertainty |
m/s |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest9_10.csv (Note) |
Code Phase |
ms |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest9_10.csv (Note) |
Integer Code Phase |
ms |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest9_10.csv (Note) |
Code Phase Search Window |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest9_10.csv (Note) |
|
Azimuth |
deg |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest9_10.csv (Note) |
Elevation |
deg |
Time varying. See file: Sig_GANSS_reference_measurement_information_subtest9_10.csv (Note) |
Note: This field is “Time varying” and its value depends on the “current GANSS TOD”. The value of this field to be used shall be determined by taking the “current GANSS TOD” value and selecting the field value in the Sig GANSS reference measurement information subtest9_10.csv file corresponding to the value of “current GANSS TOD”. |
Assistance Data GANSS Reference Measurement Extension
Table 6.1.4.33a: GANSS Reference Measurement Extension: sub-test 1, 4 (Fields occurring once per message)
Information Element |
Units |
Value/remark |
Release |
Num_Sat |
6 |
Rel-10 onwards |
Table 6.1.4.33b: GANSS Reference Measurement Extension: sub-test 1, 4 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
Release |
SV_ID |
See Table 6.1.4.1 |
Rel-10 onwards |
|
Azimuth LSB |
degrees |
Time varying. Calculated from Azimuth, see file: Sig_GANSS_reference_measurement_information_subtest1_4.csv (Note) |
Rel-10 onwards |
Elevation LSB |
degrees |
Time varying. Calculated from Elevation, see file: Sig_GANSS_reference_measurement_information_subtest1_4.csv (Note) |
Rel-10 onwards |
Note: For sub-test 1: this field is "Time varying" and its value depends on the "current GANSS TOD". The value of this field to be used shall be determined by taking the "current GANSS TOD" value and selecting the field value in the Sig_GANSS_reference_measurement_information_subtest1_4.csv file corresponding to the value of "current GANSS TOD". For sub-test 4: this field is "Time varying" and its value depends on the "current GPS TOW". The value of this field to be used shall be determined by taking the "current GPS TOW" value and selecting the field value in the Sig_GANSS_reference_measurement_information_subtest1_4.csv file corresponding to the value of "current GPS TOW". |
Table 6.1.4.33c: GANSS Reference Measurement Extension: sub-test 2 (Fields occurring once per message)
Information Element |
Units |
Value/remark |
Release |
Num_Sat |
6 |
Rel-10 onwards |
Table 6.1.4.33d: GANSS Reference Measurement Extension: sub-test 2 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
Release |
SV_ID |
See Table 6.1.4.1 |
Rel-10 onwards |
|
Azimuth LSB |
degrees |
Time varying. Calculated from Azimuth, see file: Sig_GANSS_reference_measurement_information_subtest2.csv (Note) |
Rel-10 onwards |
Elevation LSB |
degrees |
Time varying. Calculated from Elevation, see file: Sig_GANSS_reference_measurement_information_subtest2.csv (Note) |
Rel-10 onwards |
Note: This field is "Time varying" and its value depends on the "current GANSS TOD". The value of this field to be used shall be determined by taking the "current GANSS TOD" value and selecting the field value in the Sig_GANSS_reference_measurement_information_subtest2.csv file corresponding to the value of "current GANSS TOD". |
Table 6.1.4.33e: GANSS Reference Measurement Extension: sub-test 9, 10 (Fields occurring once per message)
Information Element |
Units |
Value/remark |
Release |
Num_Sat |
6 |
Table 6.1.4.33f: GANSS Reference Measurement Extension: sub-test 6, 9 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
Release |
SV_ID |
See Table 6.1.4.1 |
||
Azimuth LSB |
degrees |
Time varying. Calculated from Azimuth, see file: Sig_GANSS_reference_measurement_information_subtest9_10.csv (Note) |
|
Elevation LSB |
degrees |
Time varying. Calculated from Elevation, see file: Sig_GANSS_reference_measurement_information_subtest9_10.csv (Note) |
|
Note: This field is “Time varying” and its value depends on the “current GANSS TOD”. The value of this field to be used shall be determined by taking the “current GANSS TOD” value and selecting the field value in the Sig GANSS reference measurement information subtest9_10.csv file corresponding to the value of “current GANSS TOD”. |
Assistance Data GANSS almanac
Table 6.1.4.34: Void
Table 6.1.4.35: GANSS almanac: sub-test 1, 4 (Fields occurring once per message)
Information Element |
Units |
Value/remark |
Num Sats Total |
24 |
|
Week Number |
Any value |
Table 6.1.4.35a: Void
Table 6.1.4.35b: GANSS almanac: sub-test 1, 4 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
GLONASS Keplerian Parameters |
||
NA |
days |
See file: Sig_GANSS_Almanac_subtest1_4.csv |
nA |
Slot Numbers: 1, 2, 3 …. 22, 23, 24 |
|
HnA |
See file: Sig_GANSS_Almanac_subtest1_4.csv |
|
nA |
semi-circles |
See file: Sig_GANSS_Almanac_subtest1_4.csv |
tnA |
seconds |
See file: Sig_GANSS_Almanac_subtest1_4.csv |
inA |
semi-circles |
See file: Sig_GANSS_Almanac_subtest1_4.csv |
TnA |
sec/orbit period |
See file: Sig_GANSS_Almanac_subtest1_4.csv |
T_DOTnA |
sec/orbit period2 |
See file: Sig_GANSS_Almanac_subtest1_4.csv |
nA |
See file: Sig_GANSS_Almanac_subtest1_4.csv |
|
nA |
semi-circles |
See file: Sig_GANSS_Almanac_subtest1_4.csv |
nA |
seconds |
See file: Sig_GANSS_Almanac_subtest1_4.csv |
CnA |
See file: Sig_GANSS_Almanac_subtest1_4.csv |
|
MnA |
See file: Sig_GANSS_Almanac_subtest1_4.csv |
Table 6.1.4.36: Void
Table 6.1.4.37: GANSS almanac: sub-test 2 (Fields occurring once per message)
Information Element |
Units |
Value/remark |
Num Sats Total |
24 |
|
Week Number |
FFS |
Table 6.1.4.38: GANSS almanac: sub-test 2 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
Keplerian parameters |
||
SVID |
SV IDs: [FFS] |
|
E |
See file: Sig_GANSS_Almanac_subtest2.csv |
|
i |
semi-circles |
See file: Sig_GANSS_Almanac_subtest2.csv |
OMEGADOT |
semi-circles/sec |
See file: Sig_GANSS_Almanac_subtest2.csv |
SV Status INAV |
See file: Sig_GANSS_Almanac_subtest2.csv |
|
delta A1/2 |
meters1/2 |
See file: Sig_GANSS_Almanac_subtest2.csv |
OMEGA0 |
semi-circles |
See file: Sig_GANSS_Almanac_subtest2.csv |
|
semi-circles |
See file: Sig_GANSS_Almanac_subtest2.csv |
M0 |
semi-circles |
See file: Sig_GANSS_Almanac_subtest2.csv |
af0 |
Seconds |
See file: Sig_GANSS_Almanac_subtest2.csv |
af1 |
sec/sec |
See file: Sig_GANSS_Almanac_subtest2.csv |
Table 6.1.4.38aa: GANSS almanac: sub-test 9, 10 (Fields occurring once per message)
Information Element |
Units |
Value/remark |
Num Sats Total |
30 |
|
Week Number |
313 |
Table 6.1.4.38ab: GANSS almanac: sub-test 9, 10 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
Keplerian parameters |
||
SV_ID |
SV IDs: 1, 2, 3, …, 30 |
|
toa |
seconds |
See file: Sig_GANSS_Almanac_subtest9_10.csv |
A1/2i |
meters1/2 |
See file: Sig_GANSS_Almanac_subtest9_10.csv |
e |
See file: Sig_GANSS_Almanac_subtest9_10.csv |
|
|
semi-circles |
See file: Sig_GANSS_Almanac_subtest9_10.csv |
M0 |
semi-circles |
See file: Sig_GANSS_Almanac_subtest9_10.csv |
0 |
semi-circles |
See file: Sig_GANSS_Almanac_subtest9_10.csv |
_dot |
semi-circles/sec |
See file: Sig_GANSS_Almanac_subtest9_10.csv |
i |
semi-circles |
See file: Sig_GANSS_Almanac_subtest9_10.csv |
a0 |
Seconds |
See file: Sig_GANSS_Almanac_subtest9_10.csv |
a1 |
sec/sec |
See file: Sig_GANSS_Almanac_subtest9_10.csv |
Hea |
See file: Sig_GANSS_Almanac_subtest9_10.csv |
Assistance Data GANSS Almanac Model Extension
Table 6.1.4.38a: GANSS Almanac Model Extension: sub-test 1, 4 (Fields occurring once per message)
Information Element |
Units |
Value/remark |
Release |
Complete Almanac Provided |
1 (TRUE) |
Rel-10 onwards |
Table 6.1.4.38b: GANSS Almanac Model Extension: sub-test 2 (Fields occurring once per message)
Information Element |
Units |
Value/remark |
Release |
Complete Almanac Provided |
1 (TRUE) |
Rel-10 onwards |
Table 6.1.4.38c: GANSS Almanac Model Extension: sub-test 9, 10 (Fields occurring once per message)
Information Element |
Units |
Value/remark |
Release |
Complete Almanac Provided |
1 (TRUE) |
Assistance Data GANSS Auxiliary Information
Table 6.1.4.39: Void
Table 6.1.4.40: GANSS Auxiliary Information: sub-test 1, 4 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
SVID |
Slot Numbers: See Table 6.1.4.1 |
|
Signals Available |
G1 |
|
Channel Number |
5, 6, -2, -7, -3, 2 |
Table 6.1.4.41: Void
Table 6.1.4.42: GANSS Auxiliary Information: sub-test 3 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
SVID |
PRNs: See Table 6.1.4.1 |
|
Signals Available |
L1C and others as supported by the MS |
6.2 GNSS Scenarios and Assistance Data for Assisted GNSS Minimum Performance tests
6.2.1 General
6.2.1.0 Introduction
This subclause defines the GNSS scenarios and assistance data IEs which shall be available for use as specified in all A-GNSS Minimum Performance test cases defined in TS 51.010-1 [4] subclause 70.16.
The information elements are given with reference to TS 44.031 [5], where the details are defined.
Subclauses 6.2.2 and 6.2.3 list the assistance data IEs required for performance testing of MS-based mode, and subclauses 6.2.4 and 6.2.5 list the assistance data available for performance testing of MS-assisted mode. Subclause 6.2.6 lists the values of the assistance data IE fields for all performance testing.
The A-GNSS minimum performance requirements are defined by assuming that all relevant and valid assistance data is received by the MS in order to perform GNSS measurements and/or position calculation. This subclause does not include nor consider delays occurring in the various signalling interfaces of the network.
The term SV ID used in this subclause is defined as the satellite PRN for GPS and Galileo, as the satellite Slot Number for GLONASS and as the Ranging Code Number for BDS.
Most data for Galileo is for further study [FFS].
6.2.1.1 Satellite constellations and assistance data for A-GNSS performance testing
The satellite constellation shall consist of 24 satellites for GLONASS; 27 satellites for GPS, Modernized GPS and Galileo; 3 satellites for QZSS; 2 satellites for SBAS; and 35 satellites for BDS. Almanac assistance data shall be available for all these satellites (30 satellites for BDS). At least 7 of the satellites per GPS, Modernized GPS, Galileo, GLONASS or BDS constellation shall be visible to the MS (that is, above 15 degrees elevation with respect to the MS). At least 1 of the satellites for QZSS shall be within 15 degrees of zenith; and at least 1 of the satellites for SBAS shall be visible to the MS. All other satellite specific assistance data shall be available for all visible satellites. In each test, signals are generated for only 6 satellites (or 7 if SBAS is included). The HDOP for the test shall be calculated using these satellites. The simulated satellites for GPS, Modernized GPS, Galileo, GLONASS and BDS shall be selected from the visible satellites for each constellation, consistent with achieving the required HDOP for the test.
6.2.1.2 GNSS Scenarios for A-GNSS performance testing
6.2.1.2.0 Introduction
This subclause defines the GNSS scenarios that shall be used for all Assisted GNSS performance tests defined in TS 51.010-1 [4] subclause 70.16.
The GNSS scenarios achieve the required HDOP for the Test Cases as defined in the Requirements specification TS 45.005 [8]. They also satisfy the requirement that for each test instance the reference location shall change sufficiently such that the MS shall have to use the new assistance data.
The viable running time during which the scenario maintains the required HDOP or HDOPs is given. Once this time has been reached the scenario shall be restarted from its nominal start time.
The test cases include sub-test cases dependent on the GNSS supported by the MS. Each sub-test case is identified by a Sub-Test Case Number as defined in Table 6.2.1.2.0.1. For each GNSS scenario the parameters that vary with the sub-test are given for each sub-test.
Table 6.2.1.2.0.1: Sub-Test Case Number Definition
Sub-Test Case Number |
Supported GNSS |
1 |
MS supporting A-GLONASS only |
2 |
MS supporting A-Galileo only |
3 |
MS supporting A-GPS and Modernized GPS only |
4 |
MS supporting A-GPS and A-GLONASS only |
5 |
Reserved |
6 |
Reserved |
7 |
Reserved |
8 |
Reserved |
9 |
MS supporting A-BDS only |
10 |
MS supporting A-GPS and A-BDS only |
6.2.1.2.1 GNSS Scenario #1
The following GNSS scenario #1 shall be used during the TTFF tests defined in TS 51.010-1 [4] subclause 70.16 with the exception of the Nominal Accuracy test. The assistance data specified in the following subclauses for GNSS scenario #1 is consistent with this GNSS scenario.
Yuma Almanac data: the required file(s) in the GNSS_data_perf.zip file defined in Annex B are given in Table 6.2.1.2.1.1.
Table 6.2.1.2.1.1: Yuma Almanac data files
Sub-Test Case Number |
Yuma file(s) |
1 |
Perf_GNSS_1-1_Yuma.txt |
2 |
Perf_GNSS_1-2_Yuma.txt |
3 |
Perf_GNSS_1-3_Yuma.txt |
4 |
Perf_GNSS_1-1_Yuma.txt and Perf_GNSS_1-3_Yuma.txt |
5 |
[FFS] |
6 |
[FFS] |
7 |
[FFS] |
8 |
[FFS] |
9 |
Perf_GNSS_1-9_Yuma.txt |
10 |
Perf_GNSS_1-3_Yuma.txt and Perf_GNSS_1-9_Yuma.txt |
MS location: the MS location is calculated as a random offset from the reference location using the method described in subclause 6.2.1.2.5. The reference location is: latitude: 35 degrees 44 minutes 39.432 seconds north, longitude: 139 degrees 40 minutes 48.633 seconds east, (Tokyo Japan 2012), height: = 300m.
Nominal start time: 1st January 2012 00:31:00 (GPS time).
Viable running time to maintain specified HDOP values: 19 minutes.
Visible satellites available for simulation and for which Assistance Data (other than Almanac) shall be generated are given in Table 6.2.1.2.1.2
Table 6.2.1.2.1.2: Visible satellites
Sub-Test Case Number |
SV IDs of Visible satellites |
1 |
3, 4, 5, 9, 10, 18, 19, 20 |
2 |
[FFS] |
3 |
1, 4, 11, 17, 19, 20, 23, 28, 32 |
4 |
GPS: 1, 4, 11, 17, 19, 20, 23, 28, 32. GLONASS: 3, 4, 5, 9, 10, 18, 19, 20 |
5 |
[FFS] |
6 |
[FFS] |
7 |
[FFS] |
8 |
[FFS] |
9 |
1, 2, 3, 4, 6, 7, 17, 18, 21, 22, 23, 26, 27, 28 |
10 |
GPS: 1, 4, 11, 17, 19, 20, 23, 28, 32. BDS: 1, 2, 3, 4, 6, 7, 17, 18, 21, 22, 23, 26, 27, 28 |
The satellites to be simulated in each test case have been selected in order to achieve the required HDOP. They are defined in Table 6.2.1.2.1.3.
Table 6.2.1.2.1.3: Satellites to be simulated
Sub-Test Case Number |
SV IDs of Satellites to be simulated |
1 |
3, 4, 9, 10, 18, 20 |
2 |
[FFS] |
3 |
1, 11, 17, 19, 23, 28 (Note) |
4 |
GPS: 20, 28, 32. GLONASS: 5, 10, 20 |
5 |
[FFS] |
6 |
[FFS] |
7 |
[FFS] |
8 |
[FFS] |
9 |
1, 2, 7, 18, 21, 27 |
10 |
GPS: 20, 28, 32. BDS: 1, 7, 21 |
NOTE: For this sub-test the satellite simulator shall generate all the GPS signals supported by the MS for all the simulated satellites. |
Ionospheric model: see values in subclause 6.2.6.6.
Tropospheric model: STANAG with SRI equal to 324.8, as defined in STANAG 4294 [6].
6.2.1.2.2 GNSS Scenario #2
The following GNSS scenario #2 shall be used during the TTFF tests defined in TS 51.010-1 [4] subclause 70.16 with the exception of the Nominal Accuracy test. The assistance data specified in the following subclauses for GNSS scenario #2 is consistent with this GNSS scenario.
Yuma Almanac data: the required file(s) in the GNSS_data_perf.zip file defined in Annex B are given in Table 6.2.1.2.2.1.
Table 6.2.1.2.2.1: Yuma Almanac data files
Sub-Test Case Number |
Yuma file(s) |
1 |
Perf_GNSS_2-1_Yuma.txt |
2 |
Perf_GNSS_2-2_Yuma.txt |
3 |
Perf_GNSS_2-3_Yuma.txt |
4 |
Perf_GNSS_2-1_Yuma.txt and Perf_GNSS_2-3_Yuma.txt |
5 |
[FFS] |
6 |
[FFS] |
7 |
[FFS] |
8 |
[FFS] |
9 |
Perf_GNSS_2-9_Yuma.txt |
10 |
Perf_GNSS_2-3_Yuma.txt and Perf_GNSS_2-9_Yuma.txt |
MS location: the MS location is calculated as a random offset from the reference location using the method described in subclause 6.2.1.2.5. The reference location is: latitude: 37 degrees 24 minutes 53.391 seconds north, longitude: 122 degrees 1 minute 3.722 seconds west, (Sunnyvale, USA), height: = 50m.
Nominal start time: 1st June 2012, 00:01:00 (GPS time).
Viable running time to maintain specified HDOP values: 19 minutes.
Visible satellites available for simulation and for which Assistance Data (other than Almanac) shall be generated are given in Table 6.2.1.2.2.2
Table 6.2.1.2.2.2: Visible satellites
Sub-Test Case Number |
SV IDs of Visible satellites |
1 |
1, 8, 9, 10, 16, 19, 20, 21 |
2 |
[FFS] |
3 |
1, 7, 8, 11, 15, 17, 26, 27, 28 |
4 |
GPS: 1, 7, 8, 11, 15, 17, 26, 27, 28. GLONASS: 1, 8, 9, 10, 16, 19, 20, 21 |
5 |
[FFS] |
6 |
[FFS] |
7 |
[FFS] |
8 |
[FFS] |
9 |
4, 15, 16, 17, 18, 25, 26, 27 |
10 |
GPS: 1, 7, 8, 11, 15, 17, 26, 27, 28. BDS: 4, 15, 16, 17, 18, 25, 26, 27 |
The satellites to be simulated in each test case have been selected in order to achieve the required HDOP. They are defined in Table 6.2.1.2.2.3.
Table 6.2.1.2.2.3: Satellites to be simulated
Sub-Test Case Number |
SV IDs of Satellites to be simulated |
1 |
1, 8, 9, 10, 19, 20 |
2 |
[FFS] |
3 |
1, 7, 8, 17, 27, 28 (Note) |
4 |
GPS: 1, 8, 26. GLONASS: 8, 10, 20 |
5 |
[FFS] |
6 |
[FFS] |
7 |
[FFS] |
8 |
[FFS] |
9 |
15, 16, 17, 25, 26, 27 |
10 |
GPS: 1, 8, 26. BDS: 15, 25, 27 |
NOTE: For this sub-test the satellite simulator shall generate all the GPS signals supported by the MS for all the simulated satellites. |
Ionospheric model: see values in subclause 6.2.6.6.
Tropospheric model: STANAG with SRI equal to 324.8, as defined in STANAG 4294 [6].
6.2.1.2.3 GNSS Scenario #3
6.2.1.2.3.0 Introduction
The following GNSS scenario #3 shall be used during the Nominal Accuracy test defined in TS 51.010-1 [4] subclause 70.16. The assistance data specified in the following subclauses for GNSS scenario #3 is consistent with this GNSS scenario.
The scenario used varies dependent on the SBAS supported by the MS and also whether QZSS is supported. The scenario to be used is defined in Table 6.2.1.2.3.0.1. Where more than one SBAS is supported use the scenario for MSAS if MSAS and QZSS are supported, otherwise use the scenario for the first supported SBAS in the list.
Table 6.2.1.2.3.0.1: Scenarios used for Scenario #3
SBAS supported |
Scenarios used |
|
MS supports QZSS |
MS does not support QZSS |
|
None |
GNSS Scenario #1 with QZSS Scenario #1 |
GNSS Scenario #1 |
WAAS |
[FFS] |
GNSS Scenario #2 with WAAS |
EGNOS |
[FFS] |
GNSS Scenario #3A with EGNOS |
MSAS |
GNSS Scenario #1 with QZSS Scenario #1 and MSAS |
GNSS Scenario #1 with MSAS |
GAGAN |
[FFS] |
GNSS Scenario #3B with GAGAN |
6.2.1.2.3.1 GNSS Scenario #3A
[FFS]
6.2.1.2.3.2 GNSS Scenario #3B
[FFS]
6.2.1.2.3.3 QZSS Scenario #1
Yuma Almanac data: see file Perf_QZSS_1_Yuma.txt in the GNSS_data_perf.zip file defined in Annex B.
MS location: as for GNSS scenario #1.
Nominal start time: as for GNSS scenario #1.
Viable running time to maintain specified requirements: as for GNSS scenario #1.
Satellite meeting specified requirements to be used for simulation and for which Assistance Data (other than Almanac) shall be generated: PRN 193.
6.2.1.2.3.4 WAAS Scenario
Satellite positions: (PRN 135)133.0 degrees west, height: 35786037.417m, (PRN 138)107.3 degrees west, height: 35786037.417m.
MS location: as for related GNSS scenario.
Satellite used for simulation: PRN 135.
6.2.1.2.3.5 EGNOS Scenario
Satellite positions: (PRN 120)15.5 degrees west, height: 35786037.417m, (PRN 124) 21.5 degrees west, height: 35786037.417m.
MS location: as for related GNSS scenario.
Satellite used for simulation: PRN 120.
6.2.1.2.3.6 MSAS Scenario
Satellite positions: (PRN 129)140.0 degrees east, height: 35786037.417m, (PRN 137)145 degrees east, height: 35786037.417m
MS location: as for related GNSS scenario.
Satellite used for simulation: PRN 129.
6.2.1.2.3.7 GAGAN Scenario
[FFS]
6.2.1.2.4 GNSS Scenario #4
6.2.1.2.4.0 Introduction
The following GNSS scenario #4 shall be used during the Nominal Accuracy test defined in TS 51.010-1 [4] subclause 70.16. The assistance data specified in the following subclauses for GNSS scenario #4 is consistent with this GNSS scenario.
The scenario used varies dependent on the SBAS supported by the MS and also whether QZSS is supported. The scenario to be used is defined in Table 6.2.1.2.4. 0.1. Where more than one SBAS is supported use the scenario for MSAS if MSAS and QZSS are supported, otherwise use the scenario for the first supported SBAS in the list.
Table 6.2.1.2.4.0.1: Scenarios used for Scenario #4
SBAS supported |
Scenarios used |
|
MS supports QZSS |
MS does not support QZSS |
|
None |
GNSS Scenario #4D with QZSS Scenario #2 |
GNSS Scenario #2 |
WAAS |
[FFS] |
GNSS Scenario #4C with WAAS |
EGNOS |
[FFS] |
GNSS Scenario #4A with EGNOS |
MSAS |
GNSS Scenario #4D with QZSS Scenario #2 and MSAS |
GNSS Scenario #4D with MSAS |
GAGAN |
[FFS] |
GNSS Scenario #4B with GAGAN |
6.2.1.2.4.1 GNSS Scenario #4A
[FFS]
6.2.1.2.4.2 GNSS Scenario #4B
[FFS]
6.2.1.2.4.3 GNSS Scenario #4C
[FFS]
6.2.1.2.4.4 GNSS Scenario #4D
[FFS]
6.2.1.2.4.5 QZSS Scenario #2
Yuma Almanac data: see file Perf_QZSS_2_Yuma.txt in the GNSS_data_perf.zip file defined in Annex B.
MS location: as for GNSS scenario #4D.
Nominal start time: as for GNSS scenario #4D.
Viable running time to maintain specified requirements: as for GNSS scenario #4D.
Satellite meeting specified requirements to be used for simulation and for which Assistance Data (other than Almanac) shall be generated: PRN [FFS].
6.2.1.2.3.6 WAAS Scenario
Satellite positions: (PRN 135)133.0 degrees west, height: 35786037.417m, (PRN 138)107.3 degrees west, height: 35786037.417m.
MS location: as for related GNSS scenario.
Satellite used for simulation: PRN 138.
6.2.1.2.3.7 EGNOS Scenario
Satellite positions: (PRN 120)15.5 degrees west, height: 35786037.417m, (PRN 124) 21.5 degrees west, height: 35786037.417m.
MS location: as for related GNSS scenario.
Satellite used for simulation: PRN 124.
6.2.1.2.3.8 MSAS Scenario
Satellite positions: (PRN 129)140.0 degrees east, height: 35786037.417m, (PRN 137)145 degrees east, height: 35786037.417m.
MS location: as for related GNSS scenario.
Satellite used for simulation: PRN 137.
6.2.1.2.3.9 GAGAN Scenario
[FFS]
6.2.1.2.5 MS Location for TTFF test cases
6.2.1.2.5.0 Introduction
This subclause defines the method for generating the random MS locations that are required to be used for the TTFF tests defined in TS 51.010-1 [4] subclause 70.16.
For every Test Instance in each TTFF test case, the MS location shall be randomly selected to be within 3 km of the Reference Location. The Altitude of the MS shall be randomly selected between 0 m to 500 m above WGS‑84 reference ellipsoid. These values shall have uniform random distributions.
The MS location is calculated as an offset from the Reference Location.
6.2.1.2.5.1 MS Location Offset
The MS location offset shall be calculated by selecting the next pair of random numbers, representing a pair of latitude and longitude offsets in degrees, from a standard uniform random number generator, with the following properties:
The ranges of the latitude and longitude offsets values shall be such that when translated onto the surface of the earth they shall lie within a 3km radius circle, centred on the Reference location specified for the GNSS scenario under consideration. For the purposes of this calculation make the following assumptions:
a) Over the 3km radius circle at the Reference location the earth is flat and the meridians and parallels form a rectangular grid
b) The earth is spherical with a radius of 6371141m (equal to the WGS 84 value at 35 degrees latitude)
The resolution used for the latitude and longitude offsets values shall be 90/2E23 for the latitude offset values and 360/2E24 for the longitude offset values, representing the coding resolution in degrees specified in 3GPP TS 23.032 [7].
6.2.1.2.5.2 MS Altitude
The MS altitude value shall be calculated by selecting the next random number from a standard uniform random number generator, in the range 0 to 500, representing meters. The resolution used for the random number shall be 1, representing 1 meter.
6.2.2 Information elements required for normal MS based testing
The following A-GPS and A-GANSS assistance data IEs and fields shall be present for each test as appropriate for the GNSS(s) used during the test. Fields not specified shall not be present. The values of the fields are specified in subclause 6.2.6.
a) GPS Reference Time IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
GPS Week |
GPS TOW |
GPS TOW Assist |
SatID |
TLM Message |
Anti-Spoof |
Alert |
TLM Reserved |
aa) GPS Reference Time Extension IE. This information element is defined in subclause A.4.2.4c of TS 44.031 [5].
Fields of the IE |
Release |
GPS Week Cycle Number |
Rel-10 onwards |
b) GANSS Reference Time IE. This information element is defined in subclause A.4.2.6.1 of TS 44.031 [5].
Fields of the IE |
GANSS Day |
GANSS TOD |
GANSS TOD Uncertainty |
GANSS Time ID |
c) GANSS Time Model IE. This information element is only required for multi system tests, and is defined in subclause A.4.2.6.2 of TS 44.031 [5].
Fields of the IE |
GNSS_TOD_ID For each GNSS included in the test. |
ca) GANSS Time Model Extension IE. This information element is only required for multi system tests, and is defined in subclause A.4.2.6.2 of TS 44.031 [5].
Fields of the IE |
Release |
GNSS_TOD_ID For each GNSS included in the test. |
Rel-10 onwards |
Delta T |
Rel-10 onwards |
d) GPS Reference Location IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
Ellipsoid point with Altitude and uncertainty ellipsoid |
e) GANSS Reference Location IE. This information element is defined in subclause A.4.2.6.1 of TS 44.031 [5].
Fields of the IE |
Ellipsoid point with Altitude and uncertainty ellipsoid |
f) GPS Navigation Model IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
All satellite information |
g) GANSS Navigation Model IE. This information element is defined in subclause A.4.2.6.2 of TS 44.031 [5].
Fields of the IE |
All satellite information |
GANSS |
Clock and Orbit Model Choice |
Galileo |
Model-1 |
Modernized GPS |
Model-3 |
GLONASS |
Model-4 |
QZSS QZS-L1 |
Model-2 |
QZSS QZS-L1C/L2C/L5 |
Model-3 |
SBAS |
Model-5 |
BDS |
Model-6 |
h) GPS Ionospheric Model IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
All |
i) GANSS Ionospheric Model IE. This information element is defined in subclause A.4.2.6.1 of TS 44.031 [5].
Fields of the IE |
All |
j) GANSS Additional Ionospheric Model IE. This information element is defined in subclause A.4.2.6.1 of TS 44.031 [5].
Fields of the IE |
All |
k) GPS UTC Model IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
All |
l) Void
m) GANSS Auxiliary Information IE. This information element is defined in subclause A.4.2.6.2 of TS 44.031 [5].
Fields of the IE |
GANSS Auxiliary Information |
6.2.3 Information elements required for MS based Sensitivity Fine Time Assistance test case
The A-GPS and A-GANSS assistance data IEs and fields that shall be present for the Sensitivity Fine Time Assistance test case shall be those specified in subclause 6.2.2 with the following exception. Fields not specified shall not be present. The values of the fields are specified in subclause 6.2.6.
a) GPS Reference Time IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
GPS Week |
GPS TOW |
BCCH Carrier |
BSIC |
FNm |
TN |
BN |
GPS TOW Assist |
SatID |
TLM Message |
Anti-Spoof |
Alert |
TLM Reserved |
b) GANSS Reference Time IE. This information element is defined in subclause A.4.2.6.1 of TS 44.031 [5].
Fields of the IE |
GANSS Day |
GANSS TOD |
GANSS TOD Uncertainty |
GANSS Time ID |
BCCH Carrier |
BSIC |
FNm |
TN |
BN |
6.2.4 Information elements available for normal MS assisted testing
The following A-GPS and A-GANSS assistance data IEs and fields shall be available for use in each test as appropriate for the GNSS(s) used during the test. Fields not specified shall not be present. The values of the fields are specified in subclause 6.2.6.
a) GPS Reference Time IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
GPS Week |
GPS TOW |
GPS TOW Assist |
SatID |
TLM Message |
Anti-Spoof |
Alert |
TLM Reserved |
aa) GPS Reference Time Extension IE. This information element is defined in subclause A.4.2.4c of TS 44.031 [5].
Fields of the IE |
Release |
GPS Week Cycle Number |
Rel-10 onwards |
b) GANSS Reference Time IE. This information element is defined in subclause A.4.2.6.1 of TS 44.031 [5].
Fields of the IE |
GANSS Day |
GANSS TOD |
GANSS TOD Uncertainty |
GANSS Time ID |
c) GANSS Time Model IE. This information element is only required for multi system tests, and is defined in subclause A.4.2.6.2 of TS 44.031 [5].
Fields of the IE |
GNSS_TOD_ID For each GNSS included in the test. |
ca) GANSS Time Model Extension IE. This information element is only required for multi system tests, and is defined in subclause A.4.2.6.2 of TS 44.031 [5].
Fields of the IE |
Release |
GNSS_TOD_ID For each GNSS included in the test. |
Rel-10 onwards |
Delta T |
Rel-10 onwards |
d) GPS Reference Location IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
Ellipsoid point with Altitude and uncertainty ellipsoid |
e) GANSS Reference Location IE. This information element is defined in subclause A.4.2.6.1 of TS 44.031 [5].
Fields of the IE |
Ellipsoid point with Altitude and uncertainty ellipsoid |
f) GPS Almanac IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
Almanac Reference Week |
All Satellite information |
fa) GPS Almanac Extension IE. This information element is defined in subclause A.4.2.4c of TS 44.031 [5].
Fields of the IE |
Release |
Complete Almanac Provided |
Rel-10 onwards |
g) GANSS Almanac Model IE. This information element is defined in subclause A.4.2.6.2 of TS 44.031 [5].
Fields of the IE |
GANSS Almanac Model |
GANSS |
Almanac Model Choice |
Galileo |
Model-1 |
Modernized GPS |
Model-3,4 |
GLONASS |
Model-5 |
QZSS QZS-L1 |
Model-2 |
QZSS QZS-L1C/L2C/L5 |
Model-3,4 |
SBAS |
Model-6 |
BDS |
Model-7 |
ga) GANSS Almanac Model Extension IE. This information element is defined in subclause A.4.2.6.2 of TS 44.031 [5].
Fields of the IE |
Release |
Complete Almanac Provided |
Rel-10 onwards |
h) GPS Navigation Model IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
All satellite information |
i) GANSS Navigation Model IE. This information element is defined in subclause A.4.2.6.2 of TS 44.031 [5].
Fields of the IE |
All satellite information |
GANSS |
Clock and Orbit Model Choice |
Galileo |
Model-1 |
Modernized GPS |
Model-3 |
GLONASS |
Model-4 |
QZSS QZS-L1 |
Model-2 |
QZSS QZS-L1C/L2C/L5 |
Model-3 |
SBAS |
Model-5 |
BDS |
Model-6 |
j) GPS Acquisition Assistance IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
GPS TOW |
Satellite information |
SVID/PRNID |
Doppler (0th order term) |
Doppler (1st order term) |
Doppler Uncertainty |
Code Phase |
Integer Code Phase |
GPS Bit number |
Code Phase Search Window |
Azimuth |
Elevation |
ja) GPS Acquisition Assistance Extension IE. This information element is defined in subclause A.4.2.4c of TS 44.031 [5].
Fields of the IE |
Release |
N_SAT |
Rel-10 onwards |
SatID |
Rel-10 onwards |
Azimuth LSB |
Rel-10 onwards |
Elevation LSB |
Rel-10 onwards |
k) GANSS Reference Measurement Information IE. This information element is defined in subclause A.4.2.6.2 of TS 44.031 [5].
Fields of the IE |
SV_ID |
Doppler (0th order term) |
Doppler (1st order term) |
Doppler Uncertainty |
Code Phase |
Integer Code Phase |
Code Phase Search Window |
Azimuth |
Elevation |
ka) GANSS Reference Measurement Extension IE. This information element is defined in subclause A.4.2.6.2 of TS 44.031 [5].
Fields of the IE |
Release |
Num_Sat |
Rel-10 onwards |
SV_ID |
Rel-10 onwards |
Azimuth LSB |
Rel-10 onwards |
Elevation LSB |
Rel-10 onwards |
l) GANSS Auxiliary Information IE. This information element is defined in subclause A.4.2.6.2 of TS 44.031 [5].
Fields of the IE |
GANSS Auxiliary Information |
m) GPS UTC Model IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
All |
6.2.5 Information elements available for MS assisted Sensitivity Fine Time Assistance test case
The A-GNSS assistance data IEs and fields that shall be available for use for the Sensitivity Fine Time Assistance test case shall be those specified in subclause 6.2.4 with the following exceptions. Fields not specified shall not be present. The values of the fields are specified in subclause 6.2.6.
a) GPS Reference Time IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
GPS Week |
GPS TOW |
BCCH Carrier |
BSIC |
FNm |
TN |
BN |
GPS TOW Assist |
SatID |
TLM Message |
Anti-Spoof |
Alert |
TLM Reserved |
b) GANSS Reference Time IE. This information element is defined in subclause A.4.2.6.1 of TS 44.031 [5].
Fields of the IE |
GANSS Day |
GANSS TOD |
GANSS TOD Uncertainty |
GANSS Time ID |
BCCH Carrier |
BSIC |
FNm |
TN |
BN |
c) GPS Acquisition Assistance IE. This information element is defined in subclause A.4.2.4 of TS 44.031 [5].
Fields of the IE |
GPS TOW |
BCCH Carrier |
BSIC |
Frame # |
Timeslots # |
Bit # |
SVID/PRNID |
Doppler (0th order term) |
Doppler (1st order term) |
Doppler Uncertainty |
Code Phase |
Integer Code Phase |
GPS Bit number |
Code Phase Search Window |
Azimuth |
Elevation |
6.2.6 Contents of Information elements for Minimum performance testing
6.2.6.1 General
This subclause defines the assistance data values that shall be used for all Assisted GNSS performance tests defined in TS 51.010-1 [4] subclause 70.16. It is given for GNSS scenarios #1, #2, #3 and #4 and QZSS Scenarios #1 and #2, where it is different for each scenario; otherwise it is marked "All" where the same value is used for all scenarios.
Where assistance data is required on a per-satellite basis, or where the values of the data also varies with time it is specified in comma-separated-variable files in the GNSS_data_perf.zip file defined in Annex B. These files specify the values to be used for each satellite, indexed by satellite SV ID, and, where applicable, the values to be used indexed by both time and satellite SV ID.
Assistance data that is marked as "time varying" is specified and used in 80 ms increments. Interpolation between these values shall not be used.
Assistance data Information Elements and fields that are not specified shall not be used.
6.2.6.2 IE Random Offset Values
6.2.6.2.0 Introduction
This subclause defines the methods for generating the random offsets that are required to be applied to one or two assistance data IEs for certain tests defined in TS 51.010-1 [4] subclause 70.16.
6.2.6.2.1 GNSS TOW
For every Test Instance in each TTFF test case, the IE GPS TOW or GANSS TOD shall have a random offset, relative to GNSS system time, within the allowed error range of Coarse Time Assistance defined in the test case. This offset value shall have a uniform random distribution.
The offset value shall be calculated by selecting the next random number from a standard uniform random number generator, in the range specified for the GNSS Coarse Time assistance error range in the Test Requirements, Test parameters table for the test under consideration. The resolution used for the random number shall be 0.01, representing 10ms.
6.2.6.2.2 GNSS bit number (BN or Bit #)
In addition, for every Fine Time Assistance Test Instance the IE BN or Bit # shall have a random offset, relative to the true value of the relationship between the two time references, within the allowed error range of Fine Time Assistance defined in the test case. This offset value shall have a uniform random distribution.
The offset value shall be calculated by selecting the next random number from a standard uniform random number generator with the following properties:
The range shall be the number of GSM bits whose duration is less than the range specified for the GNSS Fine Time assistance error range in the Test Requirements, Test parameters table for the test under consideration.
The resolution used for the random number shall be 1, representing 1 GSM bit.
6.2.6.3 Satellite SV IDs to be used
For assistance data IEs which contain the field SatID or SVID/PRNID, and where the values for these fields are not given below, then the following values shall be used.
Table 6.2.6.3.1: Satellite SV IDs to be used for SatID or SVID/PRNID
Sub-Test Case Number |
GNSS #1 |
GNSS #2 |
GNSS #4C |
1 |
3, 4, 5, 9, 10, 18, 19, 20 |
1, 8, 9, 10, 16, 19, 20, 21 |
[FFS] |
2 |
[FFS] |
[FFS] |
[FFS] |
3 |
1, 4, 11, 17, 19, 20, 23, 28, 32 |
1, 7, 8, 11, 15, 17, 26, 27, 28 |
[FFS] |
4 |
GPS: 1, 4, 11, 17, 19, 20, 23, 28, 32. GLONASS: 3, 4, 5, 9, 10, 18, 19, 20 |
GPS: 1, 7, 8, 11, 15, 17, 26, 27, 28. GLONASS: 1, 8, 9, 10, 16, 19, 20, 21 |
[FFS] |
5 |
[FFS] |
[FFS] |
[FFS] |
6 |
[FFS] |
[FFS] |
[FFS] |
7 |
[FFS] |
[FFS] |
[FFS] |
8 |
[FFS] |
[FFS] |
[FFS] |
9 |
1, 2, 3, 4, 6, 7, 17, 18, 21, 22, 23, 26, 27, 28 |
4, 15, 16, 17, 18, 25, 26, 27 |
[FFS] |
10 |
GPS: 1, 4, 11, 17, 19, 20, 23, 28, 32. BDS: 1, 2, 3, 4, 6, 7, 17, 18, 21, 22, 23, 26, 27, 28 |
GPS: 1, 7, 8, 11, 15, 17, 26, 27, 28. BDS: 4, 15, 16, 17, 18, 25, 26, 27 |
[FFS] |
6.2.6.4 Assistance Data Contents
Assistance Data GPS Reference Time: sub-test 3, 4, 10
Table 6.2.6.4.1: GPS Reference Time (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
GPS Week |
Weeks |
1669 |
1690 |
[FFS] |
GPS TOW |
1860 s Start time. Add number of 80ms as required. (Note 1) |
432060 s Start time. Add number of 80ms as required. (Note 1) |
[FFS] |
|
BCCH Carrier |
ARFCN of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
ARFCN of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
– |
|
BSIC |
BSIC of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
BSIC of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
– |
|
FNm |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
– |
|
TN |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
– |
|
BN |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
– |
|
Note 1: GPS TOW Note 2: GSM Frame Number (FNm), Timeslot Number (TN) and Bit Number (BN) |
Table 6.2.6.4.2: Satellite Information
Parameter |
Units |
Value/remark GPS All |
Number of satellites |
9 |
Table 6.2.6.4.3: Reference Time – GPS TOW Assist (Fields occurring once per satellite)
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
SatID |
See Table 6.2.6.3.1 |
See Table 6.2.6.3.1 |
See Table 6.2.6.3.1 |
Table 6.2.6.4.4: Reference Time – GPS TOW Assist (Fields occurring once per satellite)
Parameter |
Units |
Value/remark GNSS All |
TLM Message |
Bit string |
10922 |
Anti-Spoof |
Bit string |
1 |
Alert |
0 |
|
TLM Reserved |
2 |
Assistance Data GPS Reference Time Extension: sub-test 3, 4, 10
Table 6.2.6.4.4a: GPS Reference Time Extension (Fields occurring once per message)
Parameter |
Units |
Value/remark GNSS All |
Release |
GPS Week Cycle Number |
1024 weeks |
1 |
Rel-10 onwards |
Assistance Data GPS Reference Location: sub-test 3, 4, 10
Table 6.2.6.4.5: GPS Reference Location
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
Latitude sign |
0 |
0 |
[FFS] |
|
Degrees of latitude |
degrees |
35.744287 |
37.414831 |
[FFS] |
Degrees of longitude |
degrees |
139.680176 |
-122.017701 |
[FFS] |
Altitude Direction |
0 |
0 |
[FFS] |
|
Altitude |
m |
300 |
50 |
[FFS] |
Uncertainty semi-major |
m |
3000 |
3000 |
[FFS] |
Uncertainty semi-minor |
m |
3000 |
3000 |
[FFS] |
Orientation of major axis |
degrees |
0 |
0 |
[FFS] |
Uncertainty altitude |
m |
500 |
500 |
[FFS] |
Confidence |
% |
68 |
68 |
[FFS] |
Assistance Data GPS Navigation Model: sub-test 3, 4, 10
Table 6.2.6.4.6: Satellite Information
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
Number of satellites |
9 |
9 |
[FFS] |
Table 6.2.6.4.7: Navigation Model (Fields occurring once per satellite)
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
SatID |
See Table 6.2.6.3.1 |
See Table 6.2.6.3.1 |
See Table 6.2.6.3.1 |
|
Satellite Status |
0 (Note) |
0 (Note) |
[FFS] |
|
Note: For consistency Satellite Status is also given in file: Perf_GPS_Navigation_model_XX.csv. |
Table 6.2.6.4.8: Ephemeris and Clock Correction parameters (Fields occurring once per satellite)
Parameter |
Units |
Value/remark GNSS All |
C/A or P on L2 |
See file: Perf_GPS_Navigation_model_XX.csv |
|
URA Index |
See file: Perf_GPS_Navigation_model_XX.csv |
|
SV Health |
See file: Perf_GPS_Navigation_model_XX.csv |
|
IODC |
See file: Perf_GPS_Navigation_model_XX.csv |
|
L2 P Data Flag |
See file: Perf_GPS_Navigation_model_XX.csv |
|
SF 1 Reserved |
See file: Perf_GPS_Navigation_model_XX.csv |
|
SF 2 Reserved |
See file: Perf_GPS_Navigation_model_XX.csv |
|
SF 3 Reserved |
See file: Perf_GPS_Navigation_model_XX.csv |
|
SF 4 Reserved |
See file: Perf_GPS_Navigation_model_XX.csv |
|
TGD |
sec |
See file: Perf_GPS_Navigation_model_XX.csv |
toc |
sec |
See file: Perf_GPS_Navigation_model_XX.csv |
af2 |
sec/sec2 |
See file: Perf_GPS_Navigation_model_XX.csv |
af1 |
sec/sec |
See file: Perf_GPS_Navigation_model_XX.csv |
af0 |
sec |
See file: Perf_GPS_Navigation_model_XX.csv |
Crs |
meters |
See file: Perf_GPS_Navigation_model_XX.csv |
n |
semi-circles/sec |
See file: Perf_GPS_Navigation_model_XX.csv |
M0 |
semi-circles |
See file: Perf_GPS_Navigation_model_XX.csv |
Cuc |
radians |
See file: Perf_GPS_Navigation_model_XX.csv |
e |
See file: Perf_GPS_Navigation_model_XX.csv |
|
Cus |
radians |
See file: Perf_GPS_Navigation_model_XX.csv |
(A)1/2 |
meters1/2 |
See file: Perf_GPS_Navigation_model_XX.csv |
toe |
sec |
See file: Perf_GPS_Navigation_model_XX.csv |
Fit Interval Flag |
See file: Perf_GPS_Navigation_model_XX.csv |
|
AODO |
sec |
See file: Perf_GPS_Navigation_model_XX.csv |
Cic |
radians |
See file: Perf_GPS_Navigation_model_XX.csv |
OMEGA0 |
semi-circles |
See file: Perf_GPS_Navigation_model_XX.csv |
Cis |
radians |
See file: Perf_GPS_Navigation_model_XX.csv |
i0 |
semi-circles |
See file: Perf_GPS_Navigation_model_XX.csv |
Crc |
meters |
See file: Perf_GPS_Navigation_model_XX.csv |
|
semi-circles |
See file: Perf_GPS_Navigation_model_XX.csv |
OMEGAdot |
semi-circles/sec |
See file: Perf_GPS_Navigation_model_XX.csv |
Idot |
semi-circles/sec |
See file: Perf_GPS_Navigation_model_XX.csv |
Assistance Data GPS Ionospheric Model: sub-test 3, 4, 10
Table 6.2.6.4.9: GPS Ionospheric Model
Information Element |
Units |
Value/remark GNSS All |
0 |
seconds |
4.6566129 10E-9 |
1 |
sec/semi-circle |
1.4901161 10E-8 |
2 |
sec/(semi-circle)2 |
-5.96046 10E-8 |
3 |
sec/(semi-circle)3 |
-5.96046 10E-8 |
0 |
seconds |
79872 |
1 |
sec/semi-circle |
65536 |
2 |
sec/(semi-circle)2 |
-65536 |
3 |
sec/(semi-circle)3 |
-393216 |
Assistance Data GPS UTC Model: sub-test 4
Table 6.2.6.4.10: GPS UTC Model
Information Element |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
A1 |
sec/sec |
0 |
0 |
FFS |
A0 |
seconds |
0 |
0 |
FFS |
tot |
seconds |
249856 |
77824 |
FFS |
WNt |
weeks |
133 |
155 |
FFS |
tLS |
seconds |
15 |
15 |
FFS |
WNLSF |
weeks |
158 |
158 |
FFS |
DN |
days |
7 |
7 |
FFS |
tLSF |
seconds |
16 |
16 |
FFS |
Assistance Data GPS Almanac: sub-test 3, 4, 10
Table 6.2.6.4.11: GPS Almanac (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS All |
Num_Sats_Total |
27 |
Table 6.2.6.4.11a: GPS Almanac (Field occurring once per message)
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
WNa |
weeks |
1669 |
1691 |
[FFS] |
Table 6.2.6.4.12: GPS Almanac (Fields occurring once per satellite)
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
SatID |
PRNs: 1, 2, 4, 5, 6, 7, 8, 9, 10, 11, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 25, 26, 27, 28, 29, 30, 32 |
PRNs: 1, 2, 3, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 25, 26, 27, 28, 30 |
[FFS] |
Table 6.2.6.4.13: GPS Almanac (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
e |
dimensionless |
See file: Perf_GPS_Almanac_XX.csv |
toa |
sec |
See file: Perf_GPS_Almanac_XX.csv |
i |
semi-circles |
See file: Perf_GPS_Almanac_XX.csv |
OMEGADOT |
semi-circles/sec |
See file: Perf_GPS_Almanac_XX.csv |
SV Health |
See file: Perf_GPS_Almanac_XX.csv |
|
A1/2 |
meters1/2 |
See file: Perf_GPS_Almanac_XX.csv |
OMEGA0 |
semi-circles |
See file: Perf_GPS_Almanac_XX.csv |
|
semi-circles |
See file: Perf_GPS_Almanac_XX.csv |
M0 |
semi-circles |
See file: Perf_GPS_Almanac_XX.csv |
af0 |
seconds |
See file: Perf_GPS_Almanac_XX.csv |
af1 |
sec/sec |
See file: Perf_GPS_Almanac_XX.csv |
Assistance Data GPS Almanac Extension: sub-test 3, 4, 10
Table 6.2.6.4.13a: GPS Almanac Extension (Fields occurring once per message)
Parameter |
Units |
Value/remark GNSS All |
Release |
Complete Almanac Provided |
1 (TRUE) |
Rel-10 onwards |
Assistance Data GPS Acquisition Assistance: sub-test 3, 4, 10
Table 6.2.6.4.14: GPS Acquisition Assistance (Fields occurring once per message)
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
GPS TOW |
1860 s Start time. Add number of 80ms as required. (Note 1) |
432060s Start time. Add number of 80ms as required. (Note 1) |
[FFS] |
|
BCCH Carrier |
ARFCN of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
ARFCN of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
Absent |
|
BSIC |
BSIC of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
BSIC of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
||
Frame # |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
||
Timeslots # |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
||
Bit # |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
||
Note 1: GPS TOW This is the value in ms of GPS TOW when the GNSS scenario is initially started in the GPS simulator. For all TTFF test cases, each time a GNSS scenario is used, the GPS start time shall be advanced by 120 seconds from the value last used so that, at the time the fix is made, it is at least 2 minutes later than the previous fix made with that scenario. Note 2: GSM Frame Number (Frame #), Timeslot Number (Timeslots #) and Bit Number (Bit #) |
Table 6.2.6.4.15: Satellite Information
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
Number of satellites |
9 |
9 |
[FFS] |
Table 6.2.6.4.16: GPS Acquisition Assistance (Fields occurring once per satellite)
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
SVID/PRNID |
See Table 6.2.6.3.1 |
See Table 6.2.6.3.1 |
See Table 6.2.6.3.1 |
Table 6.2.6.4.17: GPS Acquisition Assistance (Fields occurring once per satellite)
Parameter |
Units |
Value/remark GNSS All |
Doppler (0th order term) |
Hz |
Time varying. See file: Perf_GPS_Acquisition_assist_XX.csv (Note) |
Doppler (1st order term) |
Hz/sec |
Time varying. See file: Perf_GPS_Acquisition_assist_XX.csv (Note) |
Doppler Uncertainty |
Hz |
Time varying. See file: Perf_GPS_Acquisition_assist_XX.csv (Note) |
Code Phase |
chips |
Time varying. See file: Perf_GPS_Acquisition_assist_XX.csv (Note) |
Integer Code Phase |
Time varying. See file: Perf_GPS_Acquisition_assist_XX.csv (Note) |
|
GPS Bit number |
Time varying. See file: Perf_GPS_Acquisition_assist_XX.csv (Note) |
|
Code Phase Search Window |
chips |
Time varying. See file: Perf_GPS_Acquisition_assist_XX.csv (Note) |
Azimuth |
deg |
Time varying. See file: Perf_GPS_Acquisition_assist_XX.csv (Note) |
Elevation |
deg |
Time varying. See file: Perf_GPS_Acquisition_assist_XX.csv (Note) |
Note: Acquisition Assistance parameters This field is "Time varying" and its value depends on the "final GPS TOW" as described in subclause 6.2.6.8. The value of this field to be used shall be determined by taking the "final GPS TOW" value and selecting the nearest field value in the Perf_GPS_Acquisition_assist_XX.csv file corresponding to the value of "final current GPS TOW". |
Assistance Data GPS Acquisition Assistance Extension: sub-test 3, 4, 10
Table 6.2.6.4.17a: GPS Acquisition Assistance Extension (Fields occurring once per message)
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
Release |
N_SAT |
9 |
9 |
[FFS] |
Rel-10 onwards |
Table 6.2.6.4.17b: GPS Acquisition Assistance Extension (Fields occurring once per satellite)
Parameter |
Units |
Value/remark GNSS All |
Release |
SatID |
See Table 6.2.6.3.1 |
Rel-10 onwards |
|
Azimuth LSB |
degrees |
Time varying. Calculated from Azimuth, see file: Perf_GPS_Acquisition_assist_XX.csv (Note) |
Rel-10 onwards |
Elevation LSB |
degrees |
Time varying. Calculated from Elevation, see file: Perf_GPS_Acquisition_assist_XX.csv (Note) |
Rel-10 onwards |
Note: This field is "Time varying" and its value depends on the "current GPS TOW" as described in subclause 5.1.3. The value of this field to be used shall be determined by taking the "current GPS TOW" value and selecting the field value in the Perf_GPS_Acquisition_assist_XX.csv file corresponding to the value of "current GPS TOW". |
Assistance Data GANSS Reference Time: sub-test 1, 2, 9
Table 6.2.6.4.18: Assistance Data GANSS Reference Time: sub-test 1 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
GANSS Day |
5844 |
5996 |
[FFS] |
|
GANSS TOD |
seconds |
12645 s Start time. Add number of 1 seconds as required. (Note 1) |
10845 Start time. Add number of 1 seconds as required. (Note 1) |
[FFS] |
GANSS TOD Uncertainty |
125 (2.127 seconds) |
125 (2.127 seconds) |
125 (2.127 seconds) |
|
GANSS Time ID |
2 (GLONASS) |
2 (GLONASS) |
2 (GLONASS) |
|
BCCH Carrier |
ARFCN of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
ARFCN of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
||
BSIC |
BSIC of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
BSIC of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
||
FNm |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
||
TN |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
||
BN |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
||
Note 1: GANSS TOD This is the value in seconds of GANSS TOD when the GNSS scenario is initially started in the GNSS simulator. For all TTFF test cases, each time a GNSS scenario is used, the GANSS start time shall be advanced by 120 seconds from the value last used so that, at the time the fix is made, it is at least 2 minutes later than the previous fix made with that scenario. Note 2: GSM Frame Number (FNm), Timeslot Number (TN) and Bit Number (BN) |
Table 6.2.6.4.19: Assistance Data GANSS Reference Time: sub-test 2 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
GANSS Day |
FFS |
FFS |
FFS |
|
GANSS TOD |
seconds |
FFS Start time. Add number of 1 seconds as required. (Note 1) |
FFS Start time. Add number of 1 seconds as required. (Note 1) |
FFS Start time. Add number of 1 seconds as required. (Note 1) |
GANSS TOD Uncertainty |
125 (2.127 seconds) |
125 (2.127 seconds) |
125 (2.127 seconds) |
|
GANSS Time ID |
Not present (Galileo) |
Not present (Galileo) |
Not present (Galileo) |
|
BCCH Carrier |
ARFCN of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
ARFCN of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
||
BSIC |
BSIC of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
BSIC of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
||
FNm |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
||
TN |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
||
BN |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
||
Note 1: GANSS TOD This is the value in seconds of GANSS TOD when the GNSS scenario is initially started in the GNSS simulator. For all TTFF test cases, each time a GNSS scenario is used, the GANSS start time shall be advanced by 120 seconds from the value last used so that, at the time the fix is made, it is at least 2 minutes later than the previous fix made with that scenario. Note 2: GSM Frame Number (FNm), Timeslot Number (TN) and Bit Number (BN) |
Table 6.2.6.4.19a: Assistance Data GANSS Reference Time: sub-test 9 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #5 |
||
---|---|---|---|---|---|---|
GANSS Day |
days |
2191 |
2343 |
2343 |
||
GANSS Day Cycle Number |
0 |
0 |
0 |
|||
GANSS TOD |
seconds |
1846. Start time. (Note 1) |
432046. Start time. (Note 1) |
432046. Start time. (Note 1) |
||
GANSS TOD Uncertainty |
125 (2.127 seconds) |
125 (2.127 seconds) |
125 (2.127 seconds) |
|||
GANSS Time ID |
3 (BDS system time) |
3 (BDS system time) |
3 (BDS system time) |
|||
BCCH Carrier |
ARFCN of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
ARFCN of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
||||
BSIC |
BSIC of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
BSIC of serving BCCH Present for Sensitivity Fine Time Assistance test case. Absent otherwise. |
||||
FNm |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
||||
TN |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
||||
BN |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
Present for Sensitivity Fine Time Assistance test case. Absent otherwise. Note 2 |
||||
Note 1: GANSS TOD This is the value in seconds of GANSS TOD when the GNSS scenario is initially started in the GNSS simulator. For all TTFF test cases, each time a GNSS scenario is used, the GANSS start time shall be advanced by 120 seconds from the value last used so that, at the time the fix is made, it is at least 2 minutes later than the previous fix made with that scenario. Note 2: GSM Frame Number (FNm), Timeslot Number (TN) and Bit Number (BN) |
Assistance Data GANSS Reference Location: sub-test 1, 2, 9
Table 6.2.6.4.20: Assistance Data GANSS Reference Location
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
Latitude sign |
0 |
0 |
[FFS] |
|
Degrees of latitude |
degrees |
35.744287 |
37.414831 |
[FFS] |
Degrees of longitude |
degrees |
139.680176 |
-122.017701 |
[FFS] |
Altitude Direction |
0 |
0 |
[FFS] |
|
Altitude |
m |
300 |
50 |
[FFS] |
Uncertainty semi-major |
m |
3000 |
3000 |
[FFS] |
Uncertainty semi-minor |
m |
3000 |
3000 |
[FFS] |
Orientation of major axis |
degrees |
0 |
0 |
[FFS] |
Uncertainty altitude |
m |
500 |
500 |
[FFS] |
Confidence |
% |
68 |
68 |
[FFS] |
Assistance Data GANSS Ionospheric Model: sub-test 2
Table 6.2.6.4.21: GANSS Ionospheric Model
Information Element |
Units |
Value/remark GNSS All |
ai0 |
Solar Flux Units |
FFS |
ai1 |
Solar Flux Units/degree |
FFS |
ai2 |
Solar Flux Units/degree2 |
FFS |
Storm Flag 1 |
0 |
|
Storm Flag 2 |
0 |
|
Storm Flag 3 |
0 |
|
Storm Flag 4 |
0 |
|
Storm Flag 5 |
0 |
Assistance Data GANSS Additional Ionospheric Model: sub-test 1, 9
Table 6.2.6.4.21a: GANSS Additional Ionospheric Model: sub-test 1
Information Element |
Units |
Value/remark GNSS All |
Data Id |
00 |
|
0 |
Seconds |
4.6566129 10E-9 |
1 |
sec/semi-circle |
1.4901161 10E-8 |
2 |
sec/(semi-circle)2 |
-5.96046 10E-8 |
3 |
sec/(semi-circle)3 |
-5.96046 10E-8 |
0 |
Seconds |
79872 |
1 |
sec/semi-circle |
65536 |
2 |
sec/(semi-circle)2 |
-65536 |
3 |
sec/(semi-circle)3 |
-393216 |
Table 6.2.6.4.21ba: GANSS Additional Ionospheric Model: sub-test 9
Information Element |
Units |
Value/remark GNSS All |
Data Id |
01 |
|
0 |
Seconds |
4.6566129 10E-9 |
1 |
sec/semi-circle |
1.4901161 10E-8 |
2 |
sec/(semi-circle)2 |
-5.96046 10E-8 |
3 |
sec/(semi-circle)3 |
-5.96046 10E-8 |
0 |
Seconds |
79872 |
1 |
sec/semi-circle |
65536 |
2 |
sec/(semi-circle)2 |
-65536 |
3 |
sec/(semi-circle)3 |
-393216 |
Assistance Data GANSS ID: sub-test 1, 2, 3, 4, 9, 10
Table 6.2.6.4.21b: GANSS ID: sub-test 1, 4
Information Element |
Units |
Value/remark GNSS All |
---|---|---|
GANSS ID |
3 (GLONASS) |
Table 6.2.6.4.21c: GANSS ID: sub-test 2
Information Element |
Units |
Value/remark GNSS All |
---|---|---|
GANSS ID |
Not present (Galileo) |
Table 6.2.6.4.21d: GANSS ID: sub-test 3
Information Element |
Units |
Value/remark GNSS All |
---|---|---|
GANSS ID |
1 (Modernized GPS) |
Table 6.2.6.4.21e: GANSS ID: sub-test 9, 10
Information Element |
Units |
Value/remark GNSS All |
---|---|---|
GANSS ID |
4 (BDS) |
Assistance Data GANSS Time Model: sub-test 4, 10
Table 6.2.6.4.22: Void
Table 6.2.6.4.23: GANSS time Model
Information Element |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
GANSS Time Model Reference Time |
1860 (s) |
432060 (s) |
[FFS] |
|
TA0 |
Seconds |
0 |
0 |
[FFS] |
GNSS_TO_ID |
0 (GPS) |
0 (GPS) |
0 (GPS) |
Assistance Data GANSS Time Model Extension: sub-test 4, 10
Table 6.2.6.4.23a: GANSS Time Model Extension: sub-test 4
Information Element |
Units |
Value/remark GNSS All |
Release |
GNSS_TOD_ID |
0 (GPS) |
Rel-10 onwards |
|
Delta T |
Seconds |
15 |
Rel-10 onwards |
Table 6.2.6.4.23aa: GANSS Time Model Extension: sub-test 10
Information Element |
Units |
Value/remark GNSS All |
Release |
GNSS_TOD_ID |
0 (GPS) |
||
Delta T |
Seconds |
13 |
Assistance Data GANSS Navigation Model: sub-test 1, 2, 4, 9, 10
Table 6.2.6.4.24: Void
Table 6.2.6.4.25: GANSS Navigation Model: sub-test 1, 4
Information Element |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
---|---|---|---|---|
Num_Sat |
8 |
8 |
[FFS] |
|
Non-Broadcast Indication |
0 |
0 |
[FFS] |
Table 6.2.6.4.26: Satellite Information (Fields occurring once per satellite): sub-test 1, 4
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
SatID |
See Table 6.2.6.3.1 |
See Table 6.2.6.3.1 |
See Table 6.2.6.3.1 |
|
SV Health |
01111 (Note) |
01111 (Note) |
01111 (Note) |
|
IOD |
225 (Note) |
195 (Note) |
[FFS] |
|
Note: For consistency SV Health and IOD are also given in file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv. |
Table 6.2.6.4.27: GANSS Clock Model (Fields occurring once per satellite): sub-test 1, 4
Information Element |
Units |
Value/remark GNSS All |
GLONASS Satellite Clock Model |
||
n(tb) |
seconds |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
n(tb) |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
|
n |
seconds |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
Table 6.2.6.4.28: GANSS Orbit Model (Fields occurring once per satellite): sub-test 1, 4
Information Element |
Units |
Value/remark GNSS All |
---|---|---|
GLONASS Earth-Centered, Earth-fixed Parameters |
||
En |
days |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
P1 |
minutes |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
P2 |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
|
M |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
|
kilometers |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
|
kilometers/sec |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
|
kilometers/sec2 |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
|
kilometers |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
|
kilometers/sec |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
|
kilometers/sec2 |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
|
kilometers |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
|
kilometers/sec |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
|
kilometers/sec2 |
See file: Perf_GANSS_Navigation_Model_subtest1_4_XX.csv |
Table 6.2.6.4.29: Void
Table 6.2.6.4.30: GANSS Navigation Model: sub-test 2
Information Element |
Units |
Value/remark GNSS All |
---|---|---|
Num_Sat |
6 |
|
Non-Broadcast Indication |
0 |
Table 6.2.6.4.31: Satellite Information (Fields occurring once per satellite): sub-test 2
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
SatID |
See Table 6.2.6.3.1 |
See Table 6.2.6.3.1 |
See Table 6.2.6.3.1 |
|
SV Health |
0 (Note) |
0 (Note) |
0 (Note) |
|
IOD |
[FFS] (Note) |
[FFS] (Note) |
[FFS] (Note) |
|
Note: For consistency SV Health and IOD are also given in file: See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv. |
Table 6.2.6.4.32: GANSS Clock Model (Fields occurring once per satellite): sub-test 2
Information Element |
Units |
Value/remark GNSS All |
(Galileo)Satellite clock model |
||
toc |
seconds |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
af2 |
sec/sec2 |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
af1 |
sec/sec |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
af0 |
sec |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
TGD(BGD) |
sec |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
Model ID |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
Table 6.2.6.4.33: GANSS Orbit Model (Fields occurring once per satellite): sub-test 2
Information Element |
Units |
Value/remark GNSS All |
---|---|---|
Keplerian Parameters |
||
toe |
seconds |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
|
semi-circles |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
n |
semi-circles/sec |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
M0 |
semi-circles |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
OMEGAdot |
semi-circles/sec |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
e |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
|
Idot |
semi-circles/sec |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
sqrtA |
meters1/2 |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
i0 |
semi-circles |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
OMEGA0 |
semi-circles |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
Crs |
meters |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
Cis |
radians |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
Cus |
radians |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
Crc |
meters |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
Cic |
radians |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
Cuc |
radians |
See file: Perf_GANSS_Navigation_Model_subtest2_XX.csv |
Table 6.2.6.4.33a: GANSS Navigation Model: sub-test 9, 10
Information Element |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
---|---|---|---|---|
Num_Sat |
14 |
8 |
[FFS] |
|
Non-Broadcast Indication |
0 |
0 |
[FFS] |
Table 6.2.6.4.33b: Satellite Information (Fields occurring once per satellite): sub-test 9, 10
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
SatID |
See Table 6.2.6.3.1 |
See Table 6.2.6.3.1 |
See Table 6.2.6.3.1 |
|
SV Health |
0 (Note) |
0 (Note) |
[FFS] |
|
IOD |
0 (Note) |
843 (Note) |
[FFS] |
|
Note: For consistency SV Health and IOD are also given in file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv. |
Table 6.2.6.4.33c: GANSS Clock Model (Fields occurring once per satellite): sub-test 9, 10
Information Element |
Units |
Value/remark GNSS All |
BDS Satellite Clock Model |
||
AODC |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv. |
|
toc |
seconds |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv. |
a0 |
sec |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv. |
a1 |
sec/sec |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv. |
a2 |
sec/sec2 |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv. |
TGD |
sec |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv. |
Table 6.2.6.4.33d: GANSS Orbit Model (Fields occurring once per satellite): sub-test 9, 10
Information Element |
Units |
Value/remark GNSS All |
---|---|---|
BDS Keplerian Parameters |
||
AODE |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
|
URA Index |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
|
toe |
seconds |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
A1/2 |
meters1/2 |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
e |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
|
|
semi-circles |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
n |
semi-circles/sec |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
M0 |
semi-circles |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
OMEGA0 |
semi-circles |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
OMEGAdot |
semi-circles/sec |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
i0 |
semi-circles |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
Idot |
semi-circles/sec |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
Cuc |
radians |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
Cus |
radians |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
Crc |
meters |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
Crs |
meters |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
Cic |
radians |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
Cis |
radians |
See file: Perf_GANSS_Navigation_Model_subtest9_10_XX.csv |
Assistance Data GANSS Reference Measurement Information: sub-test 1, 2, 4, 9, 10
Table 6.2.6.4.34: Void
Table 6.2.6.4.35: GANSS Reference Measurement Information: sub-test 1, 4 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS All |
GANSS Signal ID |
0 (G1) |
Table 6.2.6.4.36: GANSS Reference Measurement Information: sub-test 1, 4 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark GNSS All |
---|---|---|
SVID |
See Table 6.2.6.3.1 |
|
Doppler (0th order term) |
m/s |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv (Note) |
Doppler (1st order term) |
m/s/s |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv (Note) |
Doppler Uncertainty |
m/s |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv (Note) |
Code Phase |
ms |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv (Note) |
Integer Code Phase |
ms |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv (Note) |
Code Phase Search Window |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv (Note) |
|
Azimuth |
deg |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv (Note) |
Elevation |
deg |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv (Note) |
Note: For sub-test 1: this field is "Time varying" and its value depends on the "current GANSS TOD". The value of this field to be used shall be determined by taking the "current GANSS TOD" value and selecting the field value in the Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv file corresponding to the value of "current GANSS TOD". For sub-test 4: this field is "Time varying" and its value depends on the "current GPS TOW". The value of this field to be used shall be determined by taking the "current GPS TOW" value and selecting the field value in the Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv file corresponding to the value of "current GPS TOW". |
Table 6.2.6.4.37: Void
Table 6.2.6.4.38: GANSS Reference Measurement Information: sub-test 2 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS All |
GANSS Signal ID |
0 (E1) |
Table 6.2.6.4.39: GANSS Reference Measurement Information: sub-test 2 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark GNSS All |
---|---|---|
SVID |
See Table 6.2.6.3.1 |
|
Doppler (0th order term) |
m/s |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest2_XX.csv (Note) |
Doppler (1st order term) |
m/s/s |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest2_XX.csv (Note) |
Doppler Uncertainty |
m/s |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest2_XX.csv (Note) |
Code Phase |
ms |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest2_XX.csv (Note) |
Integer Code Phase |
ms |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest2_XX.csv (Note) |
Code Phase Search Window |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest2_XX.csv (Note) |
|
Azimuth |
deg |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest2_XX.csv (Note) |
Elevation |
deg |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest2_XX.csv (Note) |
Note: This field is "Time varying" and its value depends on the "current GANSS TOD". The value of this field to be used shall be determined by taking the "current GANSS TOD" value and selecting the field value in the Perf_GANSS_reference_measurement_information_subtest2_XX.csv file corresponding to the value of "current GANSS TOD". |
Table 6.2.6.4.39aa: GANSS Reference Measurement Information: sub-test 9, 10 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS All |
GANSS Signal ID |
0 (B1I) |
Table 6.2.6.4.39ab: GANSS Reference Measurement Information: sub-test 9, 10 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark GNSS All |
---|---|---|
SVID |
See Table 6.2.6.3.1 |
|
Doppler (0th order term) |
m/s |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv (Note) |
Doppler (1st order term) |
m/s/s |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv (Note) |
Doppler Uncertainty |
m/s |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv (Note) |
Code Phase |
ms |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv (Note) |
Integer Code Phase |
ms |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv (Note) |
Code Phase Search Window |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv (Note) |
|
Azimuth |
deg |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv (Note) |
Elevation |
deg |
Time varying. See file: Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv (Note) |
Note: For sub-test 9: this field is "Time varying" and its value depends on the "current GANSS TOD". The value of this field to be used shall be determined by taking the "current GANSS TOD" value and selecting the field value in the Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv file corresponding to the value of "current GANSS TOD". For sub-test 10: this field is "Time varying" and its value depends on the "current GPS TOW". The value of this field to be used shall be determined by taking the "current GPS TOW" value and selecting the field value in the Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv file corresponding to the value of "current GPS TOW". |
Assistance Data GANSS Reference Measurement Extension: sub-test 1, 2, 4, 9, 10
Table 6.2.6.4.39a: GANSS Reference Measurement Extension: sub-test 1, 4 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
Release |
Num_Sat |
8 |
8 |
[FFS] |
Rel-10 onwards |
Table 6.2.6.4.39b: GANSS Reference Measurement Extension: sub-test 1, 4 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark GNSS All |
Release |
SV_ID |
See Table 6.2.6.3.1 |
Rel-10 onwards |
|
Azimuth LSB |
degrees |
Time varying. Calculated from Azimuth, see file: Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv (Note) |
Rel-10 onwards |
Elevation LSB |
degrees |
Time varying. Calculated from Elevation, see file: Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv (Note) |
Rel-10 onwards |
Note: For sub-test 1: this field is "Time varying" and its value depends on the "current GANSS TOD". The value of this field to be used shall be determined by taking the "current GANSS TOD" value and selecting the field value in the Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv file corresponding to the value of "current GANSS TOD". For sub-test 4: this field is "Time varying" and its value depends on the "current GPS TOW". The value of this field to be used shall be determined by taking the "current GPS TOW" value and selecting the field value in the Perf_GANSS_reference_measurement_information_subtest1_4_XX.csv file corresponding to the value of "current GPS TOW". |
Table 6.2.6.4.39c: GANSS Reference Measurement Extension: sub-test 2 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
Release |
Num_Sat |
[FFS] |
[FFS] |
[FFS] |
Rel-10 onwards |
Table 6.2.6.4.39d: GANSS Reference Measurement Extension: sub-test 2 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark GNSS All |
Release |
SV_ID |
See Table 6.2.6.3.1 |
Rel-10 onwards |
|
Azimuth LSB |
degrees |
Time varying. Calculated from Azimuth, see file: Perf_GANSS_reference_measurement_information_subtest2_XX.csv (Note) |
Rel-10 onwards |
Elevation LSB |
degrees |
Time varying. Calculated from Elevation, see file: Perf_GANSS_reference_measurement_information_subtest2_XX.csv (Note) |
Rel-10 onwards |
Note: This field is "Time varying" and its value depends on the "current GANSS TOD". The value of this field to be used shall be determined by taking the "current GANSS TOD" value and selecting the field value in the Perf_GANSS_reference_measurement_information_subtest2_XX.csv file corresponding to the value of "current GANSS TOD". |
Table 6.2.6.4.39e: GANSS Reference Measurement Extension: sub-test 9, 10 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
Release |
Num_Sat |
14 |
8 |
[FFS] |
Table 6.2.6.4.39f: GANSS Reference Measurement Extension: sub-test 9, 10 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark GNSS All |
Release |
SV_ID |
See Table 6.2.6.3.1 |
||
Azimuth LSB |
degrees |
Time varying. Calculated from Azimuth, see file: Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv (Note) |
|
Elevation LSB |
degrees |
Time varying. Calculated from Elevation, see file: Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv (Note) |
|
Note: For sub-test 9: this field is "Time varying" and its value depends on the "current GANSS TOD". The value of this field to be used shall be determined by taking the "current GANSS TOD" value and selecting the field value in the Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv file corresponding to the value of "current GANSS TOD". For sub-test 10: this field is "Time varying" and its value depends on the "current GPS TOW". The value of this field to be used shall be determined by taking the "current GPS TOW" value and selecting the field value in the Perf_GANSS_reference_measurement_information_subtest9_10_XX.csv file corresponding to the value of "current GPS TOW". |
Assistance Data GANSS Almanac Model: sub-test 1, 2, 4, 9, 10
Table 6.2.6.4.40: Void
Table 6.2.6.4.41: GANSS Almanac Model: sub-test 1, 4 (Fields occurring once per message)
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
Num Sats Total |
24 |
24 |
24 |
|
Week Number |
Any value |
Any value |
Any value |
Table 6.2.6.4.42: Void
Table 6.2.6.4.42a: GANSS Almanac Model: sub-test 1, 4 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark GNSS All |
GLONASS Keplerian Parameters |
||
NA |
days |
See file: Perf_GANSS_Almanac_subtest1_4_XX.csv |
nA |
Slot Numbers: 1, 2 , 3 …….22, 23, 24 |
|
HnA |
See file: Perf_GANSS_Almanac_subtest1_4_XX.csv |
|
nA |
semi-circles |
See file: Perf_GANSS_Almanac_subtest1_4_XX.csv |
tnA |
seconds |
See file: Perf_GANSS_Almanac_subtest1_4_XX.csv |
inA |
semi-circles |
See file: Perf_GANSS_Almanac_subtest1_4_XX.csv |
TnA |
sec/orbit period |
See file: Perf_GANSS_Almanac_subtest1_4_XX.csv |
T_DOTnA |
sec/orbit period2 |
See file: Perf_GANSS_Almanac_subtest1_4_XX.csv |
nA |
See file: Perf_GANSS_Almanac_subtest1_4_XX.csv |
|
nA |
semi-circles |
See file: Perf_GANSS_Almanac_subtest1_4_XX.csv |
nA |
seconds |
See file: Perf_GANSS_Almanac_subtest1_4_XX.csv |
CnA |
See file: Perf_GANSS_Almanac_subtest1_4_XX.csv |
|
MnA |
See file: Perf_GANSS_Almanac_subtest1_4_XX.csv |
Table 6.2.6.4.43: Void
Table 6.2.6.4.44: GANSS Almanac Model: sub-test 2 (Fields occurring once per message)
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
Num Sats Total |
24 |
24 |
24 |
|
Week Number |
FFS |
FFS |
FFS |
Table 6.2.6.4.45: GANSS Almanac Model: sub-test 2 (Fields occurring once per satellite)
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
Keplerian parameters |
||||
SVID |
SV IDs: [FFS] |
SV IDs: [FFS] |
SV IDs: [FFS] |
Table 6.2.6.4.46: GANSS Almanac Model: sub-test 2 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark GNSS All |
e |
See file: Perf_GANSS_Almanac_subtest2_XX.csv |
|
i |
semi-circles |
See file: Perf_GANSS_Almanac_subtest2_XX.csv |
OMEGADOT |
semi-circles/sec |
See file: Perf_GANSS_Almanac_subtest2_XX.csv |
SV Status INAV |
See file: Perf_GANSS_Almanac_subtest2_XX.csv |
|
delta A1/2 |
meters1/2 |
See file: Perf_GANSS_Almanac_subtest2_XX.csv |
OMEGA0 |
semi-circles |
See file: Perf_GANSS_Almanac_subtest2_XX.csv |
|
semi-circles |
See file: Perf_GANSS_Almanac_subtest2_XX.csv |
M0 |
semi-circles |
See file: Perf_GANSS_Almanac_subtest2_XX.csv |
af0 |
Seconds |
See file: Perf_GANSS_Almanac_subtest2_XX.csv |
af1 |
sec/sec |
See file: Perf_GANSS_Almanac_subtest2_XX.csv |
Table 6.2.6.4.46aa: GANSS Almanac Model: sub-test 9, 10 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
Num Sats Total |
30 |
30 |
[FFS] |
|
Week Number |
312 |
334 |
[FFS] |
|
Toa |
147000 |
147000 |
[FFS] |
|
IODa |
0 |
0 |
[FFS] |
Table 6.2.6.4.46ab: GANSS Almanac Model: sub-test 9, 10 (Fields occurring once per satellite)
Information Element |
Units |
Value/remark |
BDS Keplerian Parameters |
||
SV_ID |
SV IDs: 1, 2, 3, …, 30 |
|
toa |
seconds |
See file: Perf_GANSS_Almanac_subtest9_10_XX.csv |
A1/2 |
meters1/2 |
See file: Perf_GANSS_Almanac_subtest9_10_XX.csv |
e |
See file: Perf_GANSS_Almanac_subtest9_10_XX.csv |
|
|
semi-circles |
See file: Perf_GANSS_Almanac_subtest9_10_XX.csv |
M0 |
semi-circles |
See file: Perf_GANSS_Almanac_subtest9_10_XX.csv |
0 |
semi-circles |
See file: Perf_GANSS_Almanac_subtest9_10_XX.csv |
_dot |
semi-circles/sec |
See file: Perf_GANSS_Almanac_subtest9_10_XX.csv |
i |
semi-circles |
See file: Perf_GANSS_Almanac_subtest9_10_XX.csv |
a0 |
seconds |
See file: Perf_GANSS_Almanac_subtest9_10_XX.csv |
a1 |
sec/sec |
See file: Perf_GANSS_Almanac_subtest9_10_XX.csv |
Hea |
See file: Perf_GANSS_Almanac_subtest9_10_XX.csv |
Assistance Data GANSS Almanac Model Extension: sub-test 1, 2, 4, 9, 10
Table 6.2.6.4.46a: GANSS Almanac Model Extension: sub-test 1, 4 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS All |
Release |
Complete Almanac Provided |
1 (TRUE) |
Rel-10 onwards |
Table 6.2.6.4.46b: GANSS Almanac Model Extension: sub-test 2 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS All |
Release |
Complete Almanac Provided |
1 (TRUE) |
Rel-10 onwards |
Table 6.2.6.4.46c: GANSS Almanac Model Extension: sub-test 9, 10 (Fields occurring once per message)
Information Element |
Units |
Value/remark GNSS All |
Release |
Complete Almanac Provided |
1 (TRUE) |
Assistance Data GANSS Auxiliary Information: sub-test 1, 3, 4
Table 6.2.6.4.47: Void
Table 6.2.6.4.48: GANSS Auxiliary Information: sub-test 1, 4 (Fields occurring once per satellite)
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
SVID |
Slot Numbers: see Table 6.2.6.3.1 |
Slot Numbers: see Table 6.2.6.3.1 |
Slot Numbers: see Table 6.2.6.3.1 |
|
Signals Available |
G1 |
G1 |
G1 |
|
Channel Number |
5, 6, 1, -2, -7, -3, 3, 2 |
1, 6, -2, -7, -1, 3, 2, 4 |
[FFS] |
Table 6.2.6.4.49: Void
Table 6.2.6.4.50: GANSS Auxiliary Information: sub-test 3 (Fields occurring once per satellite)
Parameter |
Units |
Value/remark GNSS #1 |
Value/remark GNSS #2 |
Value/remark GNSS #4C |
SVID |
PRNs: see Table 6.2.6.3.1 |
PRNs: see Table 6.2.6.3.1 |
SV IDs: see Table 6.2.6.3.1 |
|
Signals Available |
L1C and others as supported by the MS |
L1C and others as supported by the MS |
L1C and others as supported by the MS |
Annex A (normative):
GPS data files
A.1 GPS data files for signalling tests
The GPS data files for use in GPS signalling tests are contained in archive GPS_Data_Sig_V5.zip which accompanies this document.
A.2 GPS data files for Minimum Performance tests
The GPS data files for use in GPS Minimum Performance tests are contained in archive GPS_Data_Perf_V4.zip which accompanies this document. The different scenarios are designated with suffixes XX in the zip file, where XX is 01, 02, 03 for scenarios #1, #2, #3.
Annex B (normative):
GNSS data files
B.1 GNSS data files for signalling tests
The GNSS data files for use in GNSS signalling tests are contained in archive GNSS_Data_Sig_V7.zip which accompanies the present document.
B.2 GNSS data files for Minimum Performance tests
The GNSS data files for use in GNSS Minimum Performance tests are contained in archive GNSS_Data_Perf_V8.zip which accompanies the present document. The different scenarios are designated with suffixes XX in the zip file, where XX is 01, 02, 03 etc. for scenarios #1, #2, #3 etc.
Annex C (informative):
Change history
Date |
TSG # |
TSG Doc |
CR |
Rev |
Subject/Comment |
Version Old |
Version New |
2010-02 |
– |
– |
– |
– |
First draft |
– |
0.0.1 |
2010-03 |
– |
– |
– |
– |
Scenario and Assistance Data text added from TS 51.010-1 |
0.0.1 |
0.0.2 |
2010-03 |
– |
– |
– |
– |
Version 1.0.0 for information |
0.0.2 |
1.0.0 |
2010-08 |
– |
– |
– |
– |
Additions of Assistance Data text and editorial corrections |
1.0.0 |
1.1.0 |
2010-08 |
– |
– |
– |
– |
Editorial corrections |
1.1.0 |
1.2.0 |
2010-08 |
– |
– |
– |
– |
Editorial corrections |
1.2.0 |
1.3.0 |
2010-08 |
GP-47 |
GP-101608 |
– |
– |
Version 2.0.0 for approval |
1.3.0 |
2.0.0 |
2010-08 |
– |
– |
– |
– |
Minor editorial corrections |
2.0.0 |
2.0.1 |
2010-09 |
– |
– |
– |
– |
Editorial corrections |
2.0.1 |
9.0.0 |
2010-12 |
GP-48 |
GP-101720 |
0001 |
– |
CR 51.010-7-0001 GPS Assistance Data corrections |
9.0.0 |
9.1.0 |
2011-03 |
GP-49 |
GP-110019 |
0002 |
– |
CR 51.010-7-0002 Corrections to term “PRN” |
9.1.0 |
9.2.0 |
2011-06 |
GP-50 |
GP-110558 |
0004 |
– |
CR 51.010-7-0004 Removal of incorrect data file |
9.2.0 |
9.3.0 |
2011-06 |
GP-50 |
GP-110837 |
0003 |
1 |
CR 51.010-7-0003 Addition of Assistance Data values for A-GNSS |
9.2.0 |
9.3.0 |
2012-06 |
GP-54 |
GP-120477 |
0006 |
– |
CR 51.010-7-0006 Corrections to GPS Almanac data file for signalling test cases |
9.3.0 |
9.4.0 |
2012-09 |
GP-55 |
GP-121040 |
0007 |
1 |
CR 51.010-7-0007 Addition of missing Assistance Data |
9.4.0 |
9.5.0 |
2012-12 |
GP-56 |
– |
– |
– |
Correction of version of GP-121040 in the history table |
9.5.0 |
9.5.1 |
2013-03 |
GP-57 |
GP-130075 |
0008 |
1 |
CR 51.010-7-0008 Corrections to GNSS assistance data |
9.5.1 |
9.6.0 |
2013-03 |
GP-57 |
GP-130076 |
0009 |
1 |
CR 51.010-7-0009 Changes to assistance data file names |
9.5.1 |
9.6.0 |
2013-03 |
GP-57 |
GP-130077 |
0010 |
1 |
CR 51.010-7-0010 Temporary removal of GLONASS aquisition assistance data files |
9.5.1 |
9.6.0 |
2013-03 |
GP-57 |
GP-130079 |
0012 |
1 |
CR 51.010-7-0012 Corrections to GPS Almanac assistance data files |
9.5.1 |
9.6.0 |
2013-03 |
GP-57 |
GP-130078 |
0011 |
1 |
CR 51.010-7-0011 Addition of Rel-10 IE fields |
9.6.0 |
10.0.0 |
2013-09 |
GP-59 |
GP-130756 |
0014 |
1 |
CR 51.010-7-0014 Additions and corrections to Assistance Data |
10.0.0 |
10.1.0 |
2014-03 |
GP-61 |
GP-140037 |
0015 |
– |
CR 51.010-7-0015 Correction to GPS Navigation Model value |
10.1.0 |
10.2.0 |
2014-03 |
GP-61 |
GP-140038 |
0016 |
– |
CR 51.010-7-0016 Correction to OmegaA0 values for scenario #1 |
10.1.0 |
10.2.0 |
2014-03 |
GP-61 |
GP-140041 |
0019 |
– |
CR 51.010-7-0019 Adjustment of SV IDs of Satellites to be simulated |
10.1.0 |
10.2.0 |
2014-03 |
GP-61 |
GP-140074 |
0020 |
– |
CR 51.010-7-0020 Deletion of FN1 |
10.1.0 |
10.2.0 |
2014-03 |
GP-61 |
GP-140087 |
0017 |
1 |
CR 51.010-7-0017 Correction to GPS Almanac value |
10.1.0 |
10.2.0 |
2014-03 |
GP-61 |
– |
– |
– |
Upgraded to Rel-11 with no change |
10.2.0 |
11.0.0 |
2014-03 |
GP-61 |
GP-140088 |
0018 |
1 |
CR 51.010-7-0018 Corrections to GLONASS GANSS Day values |
11.0.0 |
12.0.0 |
2014-06 |
GP-62 |
GP-140266 |
0022 |
– |
CR 51.010-7-0022 Clarification of Assistance Data usage with sub-tests |
12.0.0 |
12.1.0 |
2014-06 |
GP-62 |
GP-140267 |
0023 |
– |
CR 51.010-7-0023 Correction to T_lamda_n_A values for scenario #1 and signalling tests |
12.0.0 |
12.1.0 |
2014-12 |
GP-64 |
GP-140764 |
0024 |
– |
CR 51.010-7-0024 Introduction of BDS into A-GNSS Signalling tests |
12.1.0 |
12.2.0 |
2014-12 |
GP-64 |
GP-140766 |
0026 |
– |
CR 51.010-7-0026 Introduction of BDS into A-GNSS Signalling files |
12.1.0 |
12.2.0 |
2014-12 |
GP-64 |
GP-140792 |
0028 |
– |
CR 51.010-7-0028 Update of Foreword |
12.1.0 |
12.2.0 |
2015-03 |
GP-65 |
GP-150039 |
0029 |
– |
CR 51.010-7-0029 Introduction of BDS into A-GNSS Minimum Performance tests |
12.2.0 |
12.3.0 |
2015-03 |
GP-65 |
GP-150040 |
0030 |
– |
CR 51.010-7-0030 Introduction of BDS into A-GNSS Minimum Performance files |
12.2.0 |
12.3.0 |
2015-06 |
GP-66 |
GP-150335 |
0031 |
– |
CR 51.010-7-0031 Update of newly introduced BDS table numbering |
12.3.0 |
12.4.0 |
2015-06 |
GP-66 |
GP-150336 |
0032 |
– |
CR 51.010-7-0032 Removal of GPS UTC Model for sub-test 10 |
12.3.0 |
12.4.0 |
2015-06 |
GP-66 |
GP-150337 |
0033 |
– |
CR 51.010-7-0033 Corrections to BDS Clock Model and Navigation Model for SIG tests |
12.3.0 |
12.4.0 |
2015-06 |
GP-66 |
GP-150338 |
0034 |
– |
CR 51.010-7-0034 Corrections to BDS Clock Model and Navigation Model for Minimum Performance tests |
12.3.0 |
12.4.0 |
2015-09 |
GP-67 |
GP-150338 |
0035 |
– |
CR 51.010-7-0035 Corrections to the GANSS additional ionospheric model for A-BDS |
12.4.0 |
12.5.0 |
2015-09 |
GP-67 |
GP-150338 |
0036 |
– |
CR 51.010-7-0036 Corrections to the IOD in GANSS Navigation Model for A-BDS Scenario #2 |
12.4.0 |
12.5.0 |
2015-09 |
GP-67 |
GP-150338 |
0037 |
– |
CR 51.010-7-0037 Galileo and BDS updates and corrections |
12.4.0 |
12.5.0 |