6.2 GNSS Scenarios and Assistance Data for Assisted GNSS Minimum Performance tests

37.571-53GPPPart 5: Test scenarios and assistance dataRelease 16TSUser Equipment (UE) conformance specification for UE positioning

Tools: ARFCN - Frequency Conversion for 5G NR/LTE/UMTS/GSM

6.2.1 General

This subclause defines the GNSS scenarios and assistance data IEs which shall be available for use as specified in all UTRA, E-UTRA and NR A-GNSS Minimum Performance test cases defined in TS 37.571-1 [6] subclauses 6, 7 and 13.

Subclauses 6.2.2 and 6.2.3 list the assistance data IEs required for minimum performance testing of UE-based mode, and subclauses 6.2.4 and 6.2.5 list the assistance data available for minimum performance testing of UE-assisted mode. Subclause 6.2.7 lists the values of the assistance data IE fields for all minimum performance testing.

In all cases the Assistance Data is given in the two necessary formats, RRC format for TS 37.571-1 [6] subclause 6 and LPP format for TS 37.571-1 [6] subclauses 7 and 13. Other information is also given separately for TS 37.571-1 [6] subclauses 6, 7 and 13 where it differs between the subclauses.

The A-GNSS minimum performance requirements are defined by assuming that all relevant and valid assistance data is received by the UE 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/Modernized GPS, as Code Number for Galileo, as the satellite Slot Number for GLONASS and as the Ranging Code Number for BDS.

As an alternative, the contents of clause 6.2 in version 16.5.0 of this current specification may be used until September 2023.

6.2.1.1 Satellite constellations and assistance data for A-GNSS minimum performance testing

For all Assisted GNSS minimum performance tests defined in TS 37.571-1 [6] subclause 6 and for all Assisted GNSS minimum performance Sub-Test Case Numbers except Number 1 defined in TS 37.571-1 [6] subclauses 7 and 13, the satellite constellation shall consist of 24 satellites for GLONASS; 27 satellites for GPS/Modernized GPS and Galileo; 5 GEO, 3 IGSO and 27 MEO Satellites for BDS; 4 satellites for QZSS; and 2 satellites for SBAS. Almanac assistance data shall be available for all these satellites. At least 7 of the satellites per GPS/Modernized GPS, Galileo, GLONASS or BDS constellation shall be visible to the UE (that is, above 15 degrees elevation with respect to the UE). 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 UE. 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.

For Assisted GNSS minimum performance Sub-Test Case Number 1 defined in TS 37.571-1 [6] subclauses 7 and 13, the satellite constellations for minimum performance testing shall consist of 24 satellites. Almanac assistance data shall be available for all these 24 satellites. At least 9 of the satellites shall be visible to the UE (that is above 5 degrees elevation with respect to the UE). Other assistance data shall be available for 9 of these visible satellites. In each test, signals are generated for only a sub-set of these satellites for which other assistance data is available. The number of satellites in this sub-set is specified in the test. The satellites in this sub-set shall all be above 15 degrees elevation with respect to the UE. The HDOP for the test shall be calculated using this sub-set of satellites. The selection of satellites for this sub-set shall be selected consistent with achieving the required HDOP for the test.

6.2.1.2 GNSS Scenarios for A-GNSS minimum performance testing

This subclause defines the GNSS scenarios that shall be used for all Assisted GNSS minimum performance tests defined in TS 37.571-1 [6] subclauses 6, 7 and 13.

The GNSS scenarios achieve the required HDOP for the Test Cases and they also satisfy the requirement that for each test instance the reference location shall change sufficiently such that the UE 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 UE. Each sub-test case is identified by a Sub-Test Case Number as defined below. For each GNSS scenario the parameters that vary with the sub-test are given for each sub-test.

Table 6.2.1.2-1: Sub-Test Case Number Definition for TS 37.571-1 subclause 6

Sub-Test Case Number	Supported GNSS
1	UE supporting A-GLONASS only
2	UE supporting A-Galileo only
3	UE supporting A-GPS and Modernized GPS only
4	UE supporting A-GPS and A-GLONASS only
8	UE supporting A-GPS and A-Galileo only
9	UE supporting A-BDS only
10	UE supporting A-GPS and A-BDS only

Table 6.2.1.2-2: Sub-Test Case Number Definition for TS 37.571-1 subclauses 7 and 13

Sub-Test Case Number	Supported GNSS
1	UE supporting A-GPS L1 C/A only
2	UE supporting A-GLONASS only
3	UE supporting A-Galileo only
4	UE supporting A-GPS and Modernized GPS only
5	UE supporting A-GPS and A-GLONASS only (Note)
8	UE supporting A-GPS and A-Galileo only (Note)
9	UE supporting A-BDS only
10	UE supporting A-GPS and A-BDS only (Note)
11	UE supporting A-GPS and A-GLONASS and A-BDS only (Note)
12	UE supporting A-GPS and A-Galileo and A-GLONASS only (Note)
13	UE supporting A-GPS and A-Galileo and A-BDS only (Note)
Note: "GPS" here means GPS L1 C/A, Modernized GPS, or both, dependent on UE capabilities.

6.2.1.2.1 GNSS Scenario #1

The following GNSS scenario #1 shall be used during the TTFF tests defined in TS 37.571-1 [6] subclauses 6, 7 and 13 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.

Rinex navigation data files: the required file(s) in the GNSS orbital data perf zip file specified in Annex B are given below.

Table 6.2.1.2.1-1: Rinex navigation data files for TS 37.571-1 subclause 6

Sub-Test Case Number	Rinex navigation datafile(s)
1	Perf GNSS GLONASS 2020_9_17 Rinex.txt
2	Perf GNSS Galileo 2020_9_17 Rinex.txt
3	Perf GNSS GPS 2020_9_17 Rinex.txt
4	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS GLONASS 2020_9_17 Rinex.txt
8	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS Galileo 2020_9_17 Rinex.txt
9	Perf GNSS BDS 2020_9_17 Rinex.txt
10	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS BDS 2020_9_17 Rinex.txt

Table 6.2.1.2.1-2: Rinex navigation data files for TS 37.571-1 subclauses 7 and 13

Sub-Test Case Number	Rinex navigation datafile(s)
1	Perf GNSS GPS 2020_9_17 Rinex.txt
2	Perf GNSS GLONASS 2020_9_17 Rinex.txt
3	Perf GNSS Galileo 2020_9_17 Rinex.txt
4	Perf GNSS GPS 2020_9_17 Rinex.txt
5	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS GLONASS 2020_9_17 Rinex.txt
8	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS Galileo 2020_9_17 Rinex.txt
9	Perf GNSS BDS 2020_9_17 Rinex.txt
10	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS BDS 2020_9_17 Rinex.txt
11	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS GLONASS 2020_9_17 Rinex.txt and Perf GNSS BDS 2020_9_17 Rinex.txt
12	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS Galileo 2020_9_17 Rinex.txt and Perf GNSS GLONASS 2020_9_17 Rinex.txt
13	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS Galileo 2020_9_17 Rinex.txt and Perf GNSS BDS 2020_9_17 Rinex.txt

UE location: the UE location is calculated as a random offset from the reference location using the method described in subclause 6.2.1.2.6. The reference location is: latitude: 35 degrees 44 minutes 39.432 seconds north, longitude: 139 degrees 40 minutes 48.633 seconds east, (Tokyo Japan), height: = 300m.

Nominal start time: 17^th September 2020 23:40:00 (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 below.

Table 6.2.1.2.1-3: Visible satellites for TS 37.571-1 subclause 6

Sub-Test Case Number	SV IDs of Visible satellites
1	3, 4, 5, 10, 16, 18, 19, 20 (GLONASS)
2	3, 5, 13, 15, 21, 27, 30 (Galileo)
3	3, 4, 6, 9, 11, 17, 19, 22, 28 (GPS)
4	GPS: 3, 4, 6, 9, 11, 17, 19, 22, 28. GLONASS: 3, 4, 5, 10, 16, 18, 19, 20.
8	GPS: 3, 4, 6, 9, 11, 17, 19, 22, 28. Galileo: 3, 5, 13, 15, 21, 27, 30.
9	21, 23, 28, 33, 34, 37, 38, 40, 42, 43, 59, 60 (BDS)
10	GPS: 3, 4, 6, 9, 11, 17, 19, 22, 28. BDS: 21, 23, 28, 33, 34, 37, 38, 40, 42, 43, 59, 60.

Table 6.2.1.2.1-4: Visible satellites for TS 37.571-1 subclauses 7 and 13

Sub-Test Case Number	SV IDs of Visible satellites
1	3, 4, 6, 9, 11, 17, 19, 22, 28 (GPS)
2	3, 4, 5, 10, 16, 18, 19, 20 (GLONASS)
3	3, 5, 13, 15, 21, 27, 30 (Galileo)
4	3, 4, 6, 9, 11, 17, 19, 22, 28 (GPS)
5	GPS: 3, 4, 6, 9, 11, 17, 19, 22, 28. GLONASS: 3, 4, 5, 10, 16, 18, 19, 20.
8	GPS: 3, 4, 6, 9, 11, 17, 19, 22, 28. Galileo: 3, 5, 13, 15, 21, 27, 30.
9	21, 23, 28, 33, 34, 37, 38, 40, 42, 43, 59, 60 (BDS)
10	GPS: 3, 4, 6, 9, 11, 17, 19, 22, 28. BDS: 21, 23, 28, 33, 34, 37, 38, 40, 42, 43, 59, 60.
11	GPS: 3, 4, 6, 9, 11, 17, 19, 22, 28. GLONASS: 3, 4, 5, 10, 16, 18, 19, 20. BDS: 21, 23, 28, 33, 34, 37, 38, 40, 42, 43, 59, 60.
12	GPS: 3, 4, 6, 9, 11, 17, 19, 22, 28. Galileo: 3, 5, 13, 15, 21, 27, 30. GLONASS: 3, 4, 5, 10, 16, 18, 19, 20.
13	GPS: 3, 4, 6, 9, 11, 17, 19, 22, 28. Galileo: 3, 5, 13, 15, 21, 27, 30. BDS: 21, 23, 28, 33, 34, 37, 38, 40, 42, 43, 59, 60.

For BDS, the satellite types are given in Table 6.2.1.2.1-4A

Table 6.2.1.2.1-4A: BDS satellite types

Satellite type	SV IDs of Satellites
GEO	59, 60
IGSO	38, 40
MEO	21, 23, 28, 33, 34, 37, 42, 43

The satellites to be simulated in each sub-test case have been selected in order to achieve the required HDOP. They are defined below.

Table 6.2.1.2.1-5: Satellites to be simulated for TS 37.571-1 subclause 6

Sub-Test Case Number	SV IDs of Satellites to be simulated
1	3, 4, 5, 10, 18, 19 (GLONASS)
2	3, 5, 13, 15, 21, 27 (Galileo)
3	3, 4, 6, 17, 19, 22 (GPS)
4	GPS: 3, 4, 28. GLONASS: 5, 18, 19.
8	GPS: 3, 4, 28. Galileo: 3, 5, 21.
9	28, 40, 42, 43, 59, 60 (BDS)
10	GPS: 3, 4, 28. BDS: 38, 59, 60.
Note: The satellite simulator shall generate all the GPS, Galileo and BDS signals supported by the UE for all the simulated satellites.

Table 6.2.1.2.1-6: Satellites to be simulated for TS 37.571-1 subclauses 7 and 13

Sub-Test Case Number	SV IDs of Satellites to be simulated (Note 1)
1	Test case dependant. See Table 6.2.1.2.1-7
2	3, 4, 5, 10, 18, 19 (GLONASS)
3	3, 5, 13, 15, 21, 27 (Galileo)
4	3, 4, 6, 17, 19, 22 (GPS)
5	GPS: 3, 4, 28. GLONASS: 5, 18, 19.
8	GPS: 3, 4, 28. Galileo: 3, 5, 21.
9	28, 40, 42, 43, 59, 60 (BDS)
10	GPS: 3, 4, 28. BDS: 38, 59, 60.
11	GPS: 3, 4, 28. GLONASS: 5, 18, 19. BDS: 38, 59, 60. (Note 2)
12	GPS: 3, 4, 28. Galileo: 3, 5, 21. GLONASS: 5, 18, 19. (Note 2)
13	GPS: 3, 4, 28. Galileo: 3, 5, 21. BDS: 38, 59, 60. (Note 2)
Note 1: The satellite simulator shall generate all the GPS, Galileo and BDS signals supported by the UE for all the simulated satellites. Note 2: Only one of the following satellites shall be selected (by the device manufacturer): GPS SV ID 3, GLONASS SV ID 5, BDS SV ID 60 or Galileo SV ID 3

Table 6.2.1.2.1-7: Satellites to be simulated for TS 37.571-1 subclauses 7 and 13, sub-test 1

Test case	SV IDs of Satellites to be simulated
Sensitivity Coarse Time Assistance	3, 4, 6, 11, 17, 19, 22, 28
Sensitivity Fine Time Assistance	3, 4, 6, 11, 17,19, 22, 28
Nominal Accuracy	3, 4, 6, 11, 17, 19, 22, 28
Dynamic Range	3, 4, 6, 17, 19, 22
Multi-Path scenario	3, 4, 6, 17, 22

Ionospheric model: see values in subclause 6.2.7.

Tropospheric model: STANAG with SRI equal to 324.8, as defined in STANAG 4294 [17].

6.2.1.2.2 GNSS Scenario #2

The following GNSS scenario #2 shall be used during the TTFF tests defined in TS 37.571-1 [6] subclauses 6, 7 and 13 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.

Rinex navigation data files: the required file(s) in the GNSS orbital data perf zip file specified in Annex B are below.

Table 6.2.1.2.2-1: Rinex navigation data files for TS 37.571-1 subclause 6

Sub-Test Case Number	Rinex navigation datafile(s)
1	Perf GNSS 2-1 AGL.txt
2	Perf GNSS 2-2 Yuma.txt
3	Perf GNSS GPS 2020_9_17 Rinex.txt
4	Perf GNSS 2-3 Yuma.txt and Perf GNSS GLONASS 2020_9_17 Rinex.txt
8	Perf GNSS 2-3 Yuma.txt and Perf GNSS Galileo 2020_9_17 Rinex.txt
9	Perf GNSS 2-9 Yuma.txt
10	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS 2-9 Yuma.txt

Table 6.2.1.2.2-2: Yuma / AGL Almanac data files for TS 37.571-1 subclauses 7 and 13

Sub-Test Case Number	Yuma / AGL file(s)
1	Perf GNSS GPS 2020_9_17 Rinex.txt
2	Perf GNSS GLONASS 2020_9_17 Rinex.txt
3	Perf GNSS 2-2 Yuma.txt
4	Perf GNSS GPS 2020_9_17 Rinex.txt
5	Perf GNSS 2-3 Yuma.txt and Perf GNSS 2-1 AGL.txt
8	Perf GNSS 2-3 Yuma.txt and Perf GNSS Galileo 2020_9_17 Rinex.txt
9	Perf GNSS BDS 2020_9_17 Rinex.txt
10	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS BDS 2020_9_17 Rinex.txt
11	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS GLONASS 2020_9_17 Rinex.txt and Perf GNSS BDS 2020_9_17 Rinex.txt
12	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS Galileo 2020_9_17 Rinex.txt and Perf GNSS GLONASS 2020_9_17 Rinex.txt
13	Perf GNSS GPS 2020_9_17 Rinex.txt and Perf GNSS Galileo 2020_9_17 Rinex.txt and Perf GNSS BDS 2020_9_17 Rinex.txt

UE location: the UE location is calculated as a random offset from the reference location using the method described in subclause 6.2.1.2.6. The reference location is: latitude: 37 degrees 24 minutes 53.391 seconds north, longitude: 122 degrees 1 minutes 3.722 seconds west, (Sunnyvale, USA), height: = 50m.

Nominal start time: 17^th September 2020 23:40:00 (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 below.

Table 6.2.1.2.2-3: Visible satellites for TS 37.571-1 subclause 6

Sub-Test Case Number	SV IDs of Visible satellites
1	2, 3, 11, 12, 13, 17, 18, 19 (GLONASS)
2	3, 4, 5, 9, 15, 31, 36 (Galileo)
3	1, 3, 4, 10, 11, 21, 22, 25, 31, 32 (GPS)
4	GPS: 1, 3, 4, 10, 11, 21, 22, 25, 31, 32. GLONASS: 2, 3, 11, 12, 13, 17, 18, 19
8	GPS: 1, 3, 4, 10, 11, 21, 22, 25, 31, 32. Galileo: 3, 4, 5, 9, 15, 31, 36.
9	21, 22, 26, 34, 36, 42, 43, 44, 45 (BDS)
10	GPS: 1, 3, 4, 10, 11, 21, 22, 25, 31, 32. BDS: 21, 22, 26, 34, 36, 42, 43, 44, 45

Table 6.2.1.2.2-4: Visible satellites for TS 37.571-1 subclauses 7 and 13

Sub-Test Case Number	SV IDs of Visible satellites
1	1, 3, 4, 11, 21, 22, 25, 31, 32 (GPS)
2	2, 3, 11, 12, 13, 17, 18, 19 (GLONASS)
3	3, 4, 5, 9, 15, 31, 36 (Galileo)
4	1, 3, 4, 10, 11, 21, 22, 25, 31, 32 (GPS)
5	GPS: 1, 3, 4, 10, 11, 21, 22, 25, 31, 32. GLONASS: 2, 3, 11, 12, 13, 17, 18, 19
8	GPS: 1, 3, 4, 10, 11, 21, 22, 25, 31, 32. Galileo: 3, 4, 5, 9, 15, 31, 36.
9	21, 22, 26, 34, 36, 42, 43, 44, 45 (BDS)
10	GPS: 1, 3, 4, 10, 11, 21, 22, 25, 31, 32. BDS: 21, 22, 26, 34, 36, 42, 43, 44, 45
11	GPS: 1, 3, 4, 10, 11, 21, 22, 25, 31, 32. GLONASS: 2, 3, 11, 12, 13, 17, 18, 19. BDS: 21, 22, 26, 34, 36, 42, 43, 44, 45.
12	GPS: 1, 3, 4, 10, 11, 21, 22, 25, 31, 32. Galileo: 1, 3, 4, 5, 9, 15, 31. GLONASS: 2, 3, 11, 12, 13, 17, 18, 19.
13	GPS: 1, 3, 4, 10, 11, 21, 22, 25, 31, 32. Galileo: 3, 4, 5, 9, 15, 31, 36. BDS: 21, 22, 26, 34, 36, 42, 43, 44, 45.

For BDS, the satellite types are given in Table 6.2.1.2.2-4A

Table 6.2.1.2.2-4A: BDS satellite types

Satellite type	SV IDs of Satellites
GEO
IGSO
MEO	21, 22, 26, 34, 36, 42, 43, 44, 45

The satellites to be simulated in each sub-test case have been selected in order to achieve the required HDOP. They are defined below.

Table 6.2.1.2.2-5: Satellites to be simulated for TS 37.571-1 subclause 6

Sub-Test Case Number	SV IDs of Satellites to be simulated
1	2, 3, 12, 13, 17, 18 (GLONASS)
2	4, 5, 9, 15, 31, 36 (Galileo)
3	1, 3, 4, 11, 21, 22, 31, 32 (GPS)
4	GPS: 21, 22, 32. GLONASS: 2, 13, 18
8	GPS: 21, 22, 32. Galileo: 4, 5, 9.
9	21, 34, 42, 43, 44, 45 (BDS)
10	GPS: 21, 22, 32. BDS: 21, 44, 45.
Note: The satellite simulator shall generate all the GPS, Galileo and BDS signals supported by the UE for all the simulated satellites.

Table 6.2.1.2.2-6: Satellites to be simulated for TS 37.571-1 subclauses 7 and 13

Sub-Test Case Number	SV IDs of Satellites to be simulated (Note 1)
1	Test case dependant. See Table 6.2.1.2.2-7
2	2, 3, 12, 13, 17, 18 (GLONASS)
3	4, 5, 9, 15, 31, 36 (Galileo)
4	1, 3, 4, 11, 21, 22, 31, 32 (GPS)
5	GPS: 21, 22, 32. GLONASS: 2, 13, 18
8	GPS: 21, 22, 32. Galileo: 4, 5, 9.
9	21, 34, 42, 43, 44, 45 (BDS)
10	GPS: 21, 22, 32. BDS: 21, 44, 45.
11	GPS: 21, 22, 32. GLONASS: 2, 13, 18. BDS: 21, 44, 45. (Note 2)
12	GPS: 21, 22, 32. Galileo: 4, 5, 9. GLONASS: 2, 13, 18. (Note 2)
13	GPS: 21, 22, 32. Galileo: 4, 5, 9. BDS: 21, 44, 45. (Note 2)
Note 1: The satellite simulator shall generate all the GPS, Galileo and BDS signals supported by the UE for all the simulated satellites. Note 2: Only one of the following satellites shall be selected (by the device manufacturer): GPS SV ID 22, GLONASS SV ID 2, BDS SV ID 44 or Galileo SV ID 9.

Table 6.2.1.2.2-7: Satellites to be simulated for TS 37.571-1 subclauses 7 and 13, sub-test 1

Test case	SV IDs of Satellites to be simulated
Sensitivity Coarse Time Assistance	1, 3, 4, 11, 21, 22, 31, 32
Sensitivity Fine Time Assistance	1, 3, 4, 11, 21, 22, 31, 32
Nominal Accuracy	1, 3, 4, 11, 21, 22, 31, 32
Dynamic Range	1, 3, 4, 11, 21, 31
Multi-Path scenario	1, 3, 11, 21, 31

Ionospheric model: see values in subclause 6.2.7.

Tropospheric model: STANAG with SRI equal to 324.8, as defined in STANAG 4294 [17].

6.2.1.2.3 GNSS Scenario #3

The following GNSS scenario #3 shall be used during the Nominal Accuracy test defined in TS 37.571-1 [6] subclauses 6, 7 and 13. 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 UE and also whether QZSS is supported. The scenario to be used is defined below. 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 6.2.1.2.3-1: Scenarios used for Scenario #3

SBAS supported	Scenarios used
SBAS supported	UE supports QZSS	UE 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

Almanac data: Sig GNSS NAVIC 2020_9_17 Almanac.txt

Ephemeris data: Ephemeris data: Sig GNSS GPS 2020_9_17 Rinex.rnx, Sig GNSS GLONASS 2020_9_17 Rinex.rnx, Sig GNSS GALILEO 2020_9_17 Rinex.rnx, Sig GNSS BDS 2020_9_17 Rinex.rnx, Sig GNSS NAVIC 2020_9_17 Rinex.rnx

UE location: the UE location is calculated as a random offset from the reference location using the method described in subclause 6.2.1.2.6. The reference location is: latitude: 10 degrees 44 minutes 0 seconds north, longitude: 79 degrees 40 minutes 0 seconds east, (Sigar India), height:= 300m.

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:

Navic: PRN: 2, 3, 5, 6, 9.

GPS: PRN: 2, 19, 28

Galileo: tbd

Glonass: tbd

Beidou: tbd

6.2.1.2.3.3 QZSS Scenario #1

Almanac data: Sig GNSS QZSS 2020_9_17 Almanac.txt.

Ephemeris data: Sig GNSS QZSS 2020_9_17 Rinex.rnx.

UE 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, 194, 195, 199.

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.

UE 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.

UE 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

UE location: as for related GNSS scenario.

Satellite used for simulation: PRN 129.

6.2.1.2.3.7 GAGAN Scenario

Satellite positions: (PRN 127)55.0 degrees east, height: 35786037.417m, (PRN 128)83 degrees east, height: 35786037.417m, (PRN 132)93.5 degrees east, height: 35786037.417m

UE location: as for related GNSS scenario.

Satellite used for simulation: PRN 128.

6.2.1.2.4 GNSS Scenario #4

The following GNSS scenario #4 shall be used during the Nominal Accuracy test defined in TS 37.571-1 [6] subclauses 6, 7 and 13. The assistance data specified in the following subclauses for GNSS scenario #4 is consistent with this GNSS scenario.

Table 6.2.1.2.4-1: Scenarios used for Scenario #4

SBAS supported	Scenarios used
SBAS supported	UE supports QZSS	UE 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

Almanac data: Sig GNSS NAVIC 2020_9_17 Almanac.txt

UE location: the UE location is calculated as a random offset from the reference location using the method described in subclause 6.2.1.2.6. The reference location is: latitude: 3 degrees 56 minutes 31.668 seconds north, longitude: 73 degrees 29 minutes 26.0376 seconds east, (Maledives), height: 50m.

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:

Navic: PRN: 2, 3, 5, 6, 9

GPS: PRN: 2, 19, 28

Galileo: tbd

Glonass: tbd

Beidou: tbd

6.2.1.2.4.3 GNSS Scenario #4C

[FFS]

6.2.1.2.4.4 GNSS Scenario #4D

Almanac data: FFS.

Ephemeris data: Sig GNSS GPS 2020_9_17 Rinex.rnx, Sig GNSS GLONASS 2020_9_17 Rinex.rnx, Sig GNSS GALILEO 2020_9_17 Rinex.rnx, Sig GNSS BDS 2020_9_17 Rinex.rnx

UE location: the UE location is calculated as a random offset from the reference location using the method described in subclause 6.2.1.2.6. The reference location is: latitude: 34 degrees 59 minutes 20.1818 seconds north, longitude: 135 degrees 45 minutes 34.884 seconds east, (Kyoto, Japan), height: = 50m.

Nominal start time: as for GNSS scenario #1.

Visible satellites: as for GNSS scenario #1.

Simulated satellites: as for GNSS scenario #1.

6.2.1.2.4.5 QZSS Scenario #2

Almanac data: Sig GNSS QZSS 2020_9_17 Almanac.txt.

Ephemeris data: Sig GNSS QZSS 2020_9_17 Rinex.rnx

UE 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 193, 194, 195, 199

6.2.1.2.4.6 WAAS Scenario

Satellite positions: (PRN 135)133.0 degrees west, height: 35786037.417m, (PRN 138)107.3 degrees west, height: 35786037.417m.

UE location: as for related GNSS scenario.

Satellite used for simulation: PRN 138.

6.2.1.2.4.7 EGNOS Scenario

Satellite positions: (PRN 120)15.5 degrees west, height: 35786037.417m, (PRN 124) 21.5 degrees west, height: 35786037.417m.

UE location: as for related GNSS scenario.

Satellite used for simulation: PRN 124.

6.2.1.2.4.8 MSAS Scenario

Satellite positions: (PRN 129)140.0 degrees east, height: 35786037.417m, (PRN 137)145 degrees east, height: 35786037.417m.

UE location: as for related GNSS scenario.

Satellite used for simulation: PRN 137.

6.2.1.2.4.9 GAGAN Scenario

Satellite positions: (PRN 127)55.0 degrees east, height: 35786037.417m, (PRN 128)83 degrees east, height: 35786037.417m, (PRN 132)93.5 degrees east, height: 35786037.417m

UE location: as for related GNSS scenario.

Satellite used for simulation: PRN 128.

6.2.1.2.5 GNSS Scenario #5

The following GNSS scenario #5 shall be used during the Moving Scenario and Periodic Update test cases defined in TS 37.571-1 [6] subclauses 6, 7 and 13. The assistance data specified in the following subclauses for GNSS scenario #5 is consistent with this GNSS scenario.

GNSS scenario #5 is as GNSS scenario #2 except as detailed below.

Table 6.2.1.2.5-1: Void

Table 6.2.1.2.5-2: Void

UE location: the UE location is given as a trajectory as shown in Figure 6.6.1 and Figure 7.1 of TS 37.571-1 [6]. The reference location is at the centre of the trajectory and is as GNSS scenario #2.

Start location: at the point between l₁₁ and l₁₂ in Figure 6.6.1 and Figure 7.1 of TS 37.571-1 [6], going in a clock-wise direction.

Table 6.2.1.2.5-3: Void

Table 6.2.1.2.5-4: Void

Table 6.2.1.2.5-5: Void

Table 6.2.1.2.5-6: Satellites to be simulated for TS 37.571-1 subclauses 7 and 13

Sub-Test Case Number	SV IDs of Satellites to be simulated
1	1, 3, 11, 21, 31
2	As Table 6.2.1.2.2-6
3	As Table 6.2.1.2.2-6
4	As Table 6.2.1.2.2-6
5	As Table 6.2.1.2.2-6
8	As Table 6.2.1.2.2-6
9	As Table 6.2.1.2.2-6
10	As Table 6.2.1.2.2-6
11	As Table 6.2.1.2.2-6
12	As Table 6.2.1.2.2-6
13	As Table 6.2.1.2.2-6
Note: The satellite simulator shall generate all the GPS, Galileo and BDS signals supported by the UE for all the simulated satellites.

6.2.1.2.6 UE Location for TTFF test cases

This subclause defines the method for generating the random UE locations that are required to be used for the TTFF tests defined in TS 37.571-1 [6] subclauses 6, 7 and 13.

For every Test Instance in each TTFF test case, the UE location shall be randomly selected to be within 3 km of the Reference Location. The Altitude of the UE shall be randomly selected between 0 m to 500 m above WGS‑84 reference ellipsoid. These values shall have uniform random distributions.

The UE location is calculated as an offset from the Reference Location.

6.2.1.2.6.1 UE Location Offset

The UE 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 TS 23.032.

6.2.1.2.6.2 UE Altitude

The UE 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 UE based testing for TS 37.571-1 subclause 6

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 6.2.7.

The information elements are given with reference to TS 25.331 [34], where the details are defined.

a) GPS Reference Time IE

Fields of the IE	Release
GPS Week
GPS Week Cycle Number	Rel-10 onwards
GPS TOW msec
UE Positioning GPS ReferenceTime Uncertainty
GPS TOW Assist
SatID
TLM Message
TLM Reserved
Alert
Anti-Spoof

b) GANSS Reference Time IE

Fields of the IE	Release
GANSS Day
GANSS Day Cycle Number	Rel-10 onwards
GANSS TOD
GANSS TOD Uncertainty
GANSS Time ID

c) GANSS Time Model IE This information element is only required for multiGNSS tests.

Fields of the IE	Release
GANSS Time Model Reference Time
T_A0
GNSS_TOD_ID For each GNSS included in the test.
Delta_T	Rel-10 onwards

d) GPS Reference UE Position IE

Fields of the IE

Ellipsoid point with Altitude and uncertainty ellipsoid

e) GANSS Reference UE Position IE

Fields of the IE

Ellipsoid point with Altitude and uncertainty ellipsoid

f) GPS Navigation Model IE

Fields of the IE

All satellite information

g) GANSS Navigation Model IE

Fields of the IE

All satellite information

GANSS	Clock and Orbit Model Choice
Galileo	Model-1

h) GANSS Additional Navigation Model IE

Fields of the IE

All satellite information

GANSS	Clock and Orbit Model Choice
Modernized GPS	Model-3
GLONASS	Model-4
QZSS QZS-L1 C/A	Model-2
QZSS QZS-L1C/L2C/L5	Model-3
SBAS	Model-5
BDS	Model-6

i) GPS Ionospheric Model IE

Fields of the IE

All

j) GANSS Ionospheric Model IE

Fields of the IE

All

k) GANSS Additional Ionospheric Model IE

Fields of the IE

All

l) GPS UTC Model IE

Fields of the IE

All

m) GANSS Auxiliary Information IE

Fields of the IE

GANSS Auxiliary Information

6.2.3 Information elements required for UE based Sensitivity Fine Time Assistance test case for TS 37.571-1 subclause 6

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 6.2.7.

a) GPS Reference Time IE

Fields of the IE	Release
GPS Week
GPS Week Cycle Number	Rel-10 onwards
GPS TOW msec
UTRAN GPS reference time
UTRAN GPS timing of cell frames
CHOICE mode
FDD: Primary CPICH Info
TDD: cell parameters id
SFN
UE Positioning GPS ReferenceTime Uncertainty
TUTRAN-GPS drift rate
GPS TOW Assist
SatID
TLM Message
TLM Reserved
Alert
Anti spoof

b) GANSS Reference Time IE

Fields of the IE	Release
GANSS Day
GANSS Day Cycle Number	Rel-10 onwards
GANSS TOD
GANSS TOD Uncertainty
GANSS Time ID
UTRAN GANSS reference time
UTRAN GANSS timing of cell frames
CHOICE mode
FDD: Primary CPICH Info
TDD: cell parameters id
SFN
TUTRAN-GANSS drift rate

6.2.4 Information elements available for normal UE assisted testing for TS 37.571-1 subclause 6

a) GPS Reference Time IE

Fields of the IE	Release
GPS Week
GPS Week Cycle Number	Rel-10 onwards
GPS TOW msec
UE Positioning GPS ReferenceTime Uncertainty
GPS TOW Assist
SatID
TLM Message
TLM Reserved
Alert
Anti-Spoof

b) GANSS Reference Time IE

Fields of the IE	Release
GANSS Day
GANSS Day Cycle Number	Rel-10 onwards
GANSS TOD
GANSS TOD Uncertainty
GANSS Time ID

c) GANSS Time Model IE This information element is only required for multiGNSS tests.

Fields of the IE	Release
GANSS Time Model Reference Time
T_A0
GNSS_TOD_ID For each GNSS included in the test.
Delta_T	Rel-10 onwards

d) GPS Reference UE Position IE

Fields of the IE

Ellipsoid point with Altitude and uncertainty ellipsoid

e) GANSS Reference UE Position IE

Fields of the IE

Ellipsoid point with Altitude and uncertainty ellipsoid

f) GPS Almanac IE

Fields of the IE	Release
Almanac Reference Week
Complete Almanac Provided	Rel-10 onwards
All Satellite information

g) GANSS Almanac IE

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 C/A	Model-2
QZSS QZS-L1C/L2C/L5	Model-3,4
SBAS	Model-6
BDS	Model-7

h) GPS Navigation Model IE

Fields of the IE

All satellite information

i) GANSS Navigation Model IE

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 C/A	Model-2
QZSS QZS-L1C/L2C/L5	Model-3
SBAS	Model-5
BDS	Model-6

j) GPS Acquisition Assistance IE

Fields of the IE	Release
GPS TOW msec
UE Positioning GPS ReferenceTime Uncertainty
Satellite information
SatID
Doppler (0th order term)
Extra Doppler
Doppler (1st order term)
Doppler Uncertainty
Code Phase
Integer Code Phase
GPS Bit number
Code Phase Search Window
Azimuth and Elevation
Azimuth
Elevation
Azimuth LSB	Rel-10 onwards
Elevation LSB	Rel-10 onwards

k) GANSS Reference Measurement Information IE

Fields of the IE	Release
Satellite information
SatID
Doppler (0th order term)
Extra Doppler
Doppler (1st order term)
Doppler Uncertainty
Code Phase
Integer Code Phase
Code Phase Search Window
Azimuth and Elevation
Azimuth
Elevation
Azimuth LSB	Rel-10 onwards
Elevation LSB	Rel-10 onwards

l) GANSS Auxiliary Information IE

Fields of the IE

GANSS Auxiliary Information

m) GPS UTC Model IE

Fields of the IE

GPS UTC Model

6.2.5 Information elements available for UE assisted Sensitivity Fine Time Assistance test case for TS 37.571-1 subclause 6

The A-GPS and A-GANSS 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 6.2.7.

a) GPS Reference Time IE

Fields of the IE	Release
GPS Week
GPS Week Cycle Number	Rel-10 onwards
GPS TOW msec
UTRAN GPS reference time
UTRAN GPS timing of cell frames
CHOICE mode
FDD: Primary CPICH Info
TDD: cell parameters id
SFN
UE Positioning GPS ReferenceTime Uncertainty
TUTRAN-GPS drift rate
GPS TOW Assist
SatID
TLM Message
TLM Reserved

b) GANSS Reference Time IE

Fields of the IE	Release
GANSS Day
GANSS Day Cycle Number	Rel-10 onwards
GANSS TOD
GANSS TOD Uncertainty
GANSS Time ID
UTRAN GANSS timing of cell frames
CHOICE mode
FDD: Primary CPICH Info
TDD: cell parameters id
SFN
TUTRAN-GANSS drift rate

c) GPS Acquisition Assistance IE

Fields of the IE	Release
GPS TOW msec
UTRAN GPS reference time
UTRAN GPS timing of cell frames
CHOICE mode
FDD: Primary CPICH Info
TDD: cell parameters id
SFN
UE Positioning GPS ReferenceTime Uncertainty
Satellite information
SatID
Doppler (0th order term)
Extra Doppler
Doppler (1st order term)
Doppler Uncertainty
Code Phase
Integer Code Phase
GPS Bit number
Code Phase Search Window
Azimuth and Elevation
Azimuth
Elevation
Azimuth LSB	Rel-10 onwards
Elevation LSB	Rel-10 onwards

6.2.6 Information elements available for A-GNSS test cases in TS 37.571-1 subclauses 7 and 13

The following A-GNSS assistance data elements shall be provided to the UE in the tests. The assistance data provided depends on the mode being used in the test case, the assistance data supported by the UE and the GNSSs supported by the UE. Assistance data IEs not supported by the UE shall not be sent. Assistance data IEs supported by the UE but not listed below shall not be sent. The values of the fields are specified in subclause 6.2.7.

The information elements are given with reference to TS 37.355 [8], where the details are defined.

Table 6.2.6-1: Assistance Data to be provided to the UE for A-GNSS test cases in TS 37.571-1 subclauses 7 and 13

Assistance Data IE supported by the UE	Mode used in test case
Assistance Data IE supported by the UE	UE-based	UE-assisted, GNSS-AcquisitionAssistance supported by the UE	UE-assisted, GNSS-AcquisitionAssistance not supported by the UE
GNSS-Reference Time	Yes	Yes	Yes
GNSS-ReferenceLocation	Yes	No	Yes
GNSS-IonosphericModel	Yes	No	No
GNSS-TimeModelList	Yes for sub-tests 5, 8, 10, 11, 12 and 13	No	Yes for sub-tests 5, 8, 10, 11, 12 and 13
GNSS-NavigationModel	Yes	No	Yes
GNSS-AcquisitionAssistance	No	Yes	No
GNSS-Almanac	No	No	Yes
GNSS-UTC-Model	Yes for sub-tests 5, 11 and 12	Yes for sub-tests 5, 11 and 12	Yes for sub-tests 5, 11 and 12
GNSS-AuxiliaryInformation	Yes for sub-tests 2, 5, 11 and 12 (for GLONASS). Yes for sub-test 4 (for multiple GPS signals). Yes for sub-tests 9, 10, 11 and 13 if the UE supports BDS B1C.Yes for sub-tests 5, 8, 10, 11, 12 and, 13 if the UE supports multiple GPS signals	Yes for sub-tests 2, 5, 11 and 12 (for GLONASS). Yes for sub-test 4 (for multiple GPS signals). Yes for sub-tests 9, 10, 11 and 13 if the UE supports BDS B1C. Yes for sub-tests 5, 8, 10, 11, 12 and 13 if the UE supports multiple GPS signals	Yes for sub-tests 2, 4, 5, 11 and 12 (for GLONASS). Yes for sub-test 4 (for multiple GPS signals). Yes for sub-tests 9, 10, 11 and 13 if the UE supports BDS B1C. Yes for sub-tests 5, 8, 10, 11, 12 and 13 if the UE supports multiple GPS signals

a) GNSS- Reference Time IE

GNSS- Reference Time IE

Information Element	All tests except Sensitivity Fine Time Assistance	Sensitivity Fine Time Assistance test
GNSS-ReferenceTime
gnss-SystemTime
gnss-TimeID	Yes	Yes
gnss-DayNumber	Yes	Yes
gnss-TimeOfDay	Yes	Yes
gnss-TimeOfDayFrac-msec	Yes	Yes
notificationOfLeapSecond	Yes if gnss-TimeID = ‘glonass’	Yes if gnss-TimeID = ‘glonass’
gps-TOW-Assist	Yes if gnss-TimeID = ‘gps’	Yes if gnss-TimeID = ‘gps’
referenceTimeUnc	Yes	No
gnss-ReferenceTimeForOneCell	No	Yes
networkTime		Yes
secondsFromFrameStructureStart		Yes
fractionalSecondsFromFrameStructureStart		Yes
frameDrift		Yes
cellID		Yes
physCellId		Yes if TS 37.571-1 subclause 7, or subclause 13 Test Configuration A
cellGlobalIdEUTRA		Yes if TS 37.571-1 subclause 7, or subclause 13 Test Configuration A
earfcn/earfcn-v9a0		Yes if TS 37.571-1 subclause 7, or subclause 13 Test Configuration A
nrPhysCellId-r15		Yes if TS 37.571-1 subclause 13 Test Configuration B
nrCellGlobalID-r15		Yes if TS 37.571-1 subclause 13 Test Configuration B
nrARFCN-r15		Yes if TS 37.571-1 subclause 13 Test Configuration B
referenceTimeUnc		Yes

b) GNSS-ReferenceLocation IE

GNSS-ReferenceLocation IE

Name of the IE	Fields of the IE
GNSS-ReferenceLocation	threeDlocation

c) GNSS-IonosphericModel IE

GNSS-IonosphericModel IE

Name of the IE		Fields of the IE
GNSS-IonosphericModel		KlobucharModelParameter⁽³⁾
		KlobucharModel2Parameter⁽²⁾
		NeQuickModelParameter⁽¹⁾
Note 1: Only required if GNSSs supported include Galileo. Note 2: Only required if GNSSs supported include BDS B1C. Note 3: In the case of BDS, only required if BDS B1I supported.

d) GNSS-TimeModelList IE This information element is only required for multiGNSS tests.

GNSS-TimeModelList IE

Name of the IE	Fields of the IE
GNSS-TimeModelList
	gnss-TO-ID For each GNSS included in the test.
	deltaT

e) GNSS-NavigationModel IE

GNSS-NavigationModel IE

Name of the IE	Fields of the IE
GNSS-NavigationModel

GNSS Clock and Orbit Model Choices

GNSS		Clock and Orbit Model Choice
GPS L1 C/A		Model-2
Modernized GPS		Model-3
GLONASS		Model-4
QZSS QZS-L1 C/A		Model-2
QZSS QZS-L1C/L2C/L5		Model-3
SBAS		Model-5
Galileo		Model-1
BDS B1I		Model-6
BDS B1C		Model-7

f) GNSS-AcquisitionAssistance IE

GNSS-AcquisitionAssistance IE

Name of the IE	Fields of the IE
GNSS-AcquisitionAssistance

g) GNSS-Almanac IE

GNSS-Almanac IE

Name of the IE	Fields of the IE
GNSS-Almanac

GNSS Almanac Choices

GNSS		Almanac Model Choice
GPS L1 C/A		Model-2
Modernized GPS		Model-3,4
GLONASS		Model-5
QZSS QZS-L1 C/A		Model-2
QZSS QZS-L1C/L2C/L5		Model-3,4
SBAS		Model-6
Galileo		Model-1
BDS B1I		Model-7
BDS B1C		Model-3, 4

h) GNSS-UTC-Model IE

GNSS-UTC-Model IE

Name of the IE	Fields of the IE
GNSS-UTC-Model

GNSS UTC Model Choices

GNSS		UTC Model Choice
GPS L1 C/A		Model-1
Modernized GPS		Model-2
GLONASS		Model-3
QZSS QZS-L1 C/A		Model-1
QZSS QZS-L1C/L2C/L5		Model-2
SBAS		Model-4
Galileo		Model-1
BDS B1I		Model-5
BDS B1C		Model-2

i) GNSS-AuxiliaryInformation IE

GNSS-AuxiliaryInformation IE

Name of the IE	Fields of the IE
GNSS-AuxiliaryInformation

6.2.7 Contents of Information elements for A-GNSS Minimum performance testing

6.2.7.1 General

This subclause defines the assistance data values that shall be used for all Assisted GNSS minimum performance tests defined in TS 37.571-1 [6] subclauses 6, 7 and 13. It is given for GNSS scenarios #1, #2, #3, #4 and #5 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.

Assistance data that is marked as “time varying” is created and used in 80ms increments.

Assistance data Information Elements and fields that are not specified shall not be used.

6.2.7.2 IE Random Offset Values

This subclause defines the methods for generating the random offsets that are required to be applied to some assistance data IEs for certain tests defined in TS 37.571-1 [6] subclauses 6, 7 and 13.

6.2.7.2.1 GNSS TOW

For every Test Instance in each TTFF test case, the IE GPS TOW msec or GANSS TOD or gnss-TimeofDay plus gnss-TimeofDayFrac-msec 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.

6.2.7.2.2 GNSS/cellular time offset

In addition, for every Fine Time Assistance Test Instance the IE UTRAN GPS timing of cell frames or the UTRAN GANSS timing of cell frames or fractionalSecondsFromFrameStructureStart 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:

For UTRAN GPS timing of cell frames the range shall be the number of UMTS chips 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. For UTRAN GANSS timing of cell frames or fractionalSecondsFromFrameStructureStart the range shall be the range specified for the GNSS Fine Time assistance error range in the Test Requirements, Test parameters table for the test under consideration.

For UTRAN GPS timing of cell frames the resolution used for the random number shall be 1, representing 1 UMTS bit. For UTRAN GANSS timing of cell frames or fractionalSecondsFromFrameStructureStart the resolution used for the random number shall be 1us.

6.2.7.3 Contents of Information elements for A-GNSS Minimum performance testing in TS 37.571-1 subclause 6

6.2.7.3.1 Assistance Data Reference Time

Contents of UE positioning GPS reference time (sub-tests 3, 4, 8 and 10)

Reference Time (Fields occurring once per message)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GPS Week	Weeks	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
GPS Week Cycle Number (Rel-10 onwards)		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
GPS TOW msec	msec	Start time derived from data in clause 6.2.1.2. Add number of ms as required. (Note 1)	Start time derived from data in clause 6.2.1.2. Add number of ms as required. (Note 1)	Start time derived from data in clause 6.2.1.2. Add number of ms as required. (Note 1)
UTRAN GPS reference time		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
UTRAN GPS timing of cell frames		Note 2	Note 2	–
CHOICE mode		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	–
FDD: Primary CPICH Info		100	100	–
TDD: cell parameters id		0	0
SFN		Note 2	Note 2	–
UE Positioning GPS ReferenceTime Uncertainty		For Sensitivity Fine Time Assistance test case: ‘51’ (10.2uS). Otherwise: ‘125’ (2.127s)	For Sensitivity Fine Time Assistance test case: ‘51’ (10.2uS). Otherwise: ‘125’ (2.127s)	‘125’ (2.127s)
TUTRAN-GPS drift rate		0. Present for Sensitivity Fine Time Assistance test case. Absent otherwise	0. Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
Note 1: GPS TOW msec This is the value in ms of GPS TOW msec when the GPS scenario is initially started in the GNSS simulator. For all TTFF test cases, each time a GPS 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. The actual value of GPS TOW msec to be used in the Reference Time IE (before the addition of the random offset, if applicable) 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. The accuracy shall be such that the Maximum Test System Uncertainty for Coarse Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. For all TTFF test cases a random offset is then added to the value of GPS TOW msec as described in subclause 6.2.7.2. Note 2: UTRAN GPS timing of cell frames and SFN. The values of UTRAN GPS timing of cell frames (before the addition of the random offset) and SFN shall be calculated at the time the IE is required. The accuracy of the relationship between the two fields shall be such that the Maximum Test System Uncertainty for Fine Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. A random offset is then added to the value of UTRAN GPS timing of cell frames as described in subclause 6.2.7.2.

Satellite Information

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Number of satellites	–	9	10	10

Reference Time – GPS TOW Assist (Fields occurring once per satellite)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SatID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

Reference Time – GPS TOW Assist (Fields occurring once per satellite)

Information Element	Units	Value/remark GNSS All
TLM Message	Bit string	Derived from data in clause 6.2.1.2
TLM Reserved	Bit string	Derived from data in clause 6.2.1.2
Alert	Boolean	0
Anti-Spoof	Boolean	1

Contents of UE positioning GANSS reference time (sub-tests 1, 2, and 9)

GANSS reference time: sub-test 1

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GANSS Day	days	Derived from data in clause 6.2.1.25844	Derived from data in clause 6.2.1.25996	Derived from data in clause 6.2.1.25996
GANSS Day Cycle Number (Rel-10 onwards)		Derived from data in clause 6.2.1.20	Derived from data in clause 6.2.1.20	Derived from data in clause 6.2.1.20
GANSS TOD	seconds	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (Note 1)
GANSS TOD Uncertainty		125 (2.127 seconds)	125 (2.127 seconds)	125 (2.127 seconds)
GANSS Time ID		2 (GLONASS)	2 (GLONASS)	2 (GLONASS)
UTRAN GANSS reference time		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
UTRAN GANSS timing of cell frames		Note 2	Note 2	–
CHOICE mode		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	–
FDD: Primary CPICH Info		100	100	–
TDD: cell parameters id		0	0
SFN		Note 2	Note 2	–
TUTRAN-GANSS drift rate		0. Present for Sensitivity Fine Time Assistance test case. Absent otherwise	0. Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
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 GNSS 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. The actual value of GANSS TOD to be used in the Reference Time IE (before the addition of the random offset, if applicable) 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. The accuracy shall be such that the Maximum Test System Uncertainty for Coarse Time Assistance, specified in Table C.1.2 of TS 37.571-1[6], shall be met. For all TTFF test cases a random offset is then added to the value of GANSS TOD as described in subclause 6.2.7.2. Note 2: UTRAN GANSS timing of cell frames and SFN. The values of UTRAN GANSS timing of cell frames (before the addition of the random offset) and SFN shall be calculated at the time the IE is required. The accuracy of the relationship between the two fields shall be such that the Maximum Test System Uncertainty for Fine Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. A random offset is then added to the value of UTRAN GPS timing of cell frames as described in subclause 6.2.7.2.

GANSS reference time: sub-test 2

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GANSS Day	days	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
GANSS Day Cycle Number (Rel-10 onwards)		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
GANSS TOD	seconds	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (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)
UTRAN GANSS reference time		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
UTRAN GANSS timing of cell frames		Note 2	Note 2	–
CHOICE mode		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	–
FDD: Primary CPICH Info		100	100	–
TDD: cell parameters id		0	0
SFN		Note 2	Note 2	–
TUTRAN-GANSS drift rate		0. Present for Sensitivity Fine Time Assistance test case. Absent otherwise	0. Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
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 GNSS 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. The actual value of GANSS TOD to be used in the Reference Time IE (before the addition of the random offset, if applicable) 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. The accuracy shall be such that the Maximum Test System Uncertainty for Coarse Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. For all TTFF test cases a random offset is then added to the value of GANSS TOD as described in subclause 6.2.7.2. Note 2: UTRAN GANSS timing of cell frames and SFN. The values of UTRAN GANSS timing of cell frames (before the addition of the random offset) and SFN shall be calculated at the time the IE is required. The accuracy of the relationship between the two fields shall be such that the Maximum Test System Uncertainty for Fine Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. A random offset is then added to the value of UTRAN GPS timing of cell frames as described in subclause 6.2.7.2.

GANSS reference time: sub-test 9

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GANSS Day	days	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
GANSS Day Cycle Number (Rel-10 onwards)		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
GANSS TOD	seconds	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (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)
UTRAN GANSS reference time		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
UTRAN GANSS timing of cell frames		Note 2	Note 2	–
CHOICE mode		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	–
FDD: Primary CPICH Info		100	100	–
TDD: cell parameters id		0	0
SFN		Note 2	Note 2	–
TUTRAN-GANSS drift rate		0. Present for Sensitivity Fine Time Assistance test case. Absent otherwise	0. Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
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 GNSS 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. The actual value of GANSS TOD to be used in the Reference Time IE (before the addition of the random offset, if applicable) 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. The accuracy shall be such that the Maximum Test System Uncertainty for Coarse Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. For all TTFF test cases a random offset is then added to the value of GANSS TOD as described in subclause 6.2.7.2. Note 2: UTRAN GANSS timing of cell frames and SFN. The values of UTRAN GANSS timing of cell frames (before the addition of the random offset) and SFN shall be calculated at the time the IE is required. The accuracy of the relationship between the two fields shall be such that the Maximum Test System Uncertainty for Fine Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. A random offset is then added to the value of UTRAN GPS timing of cell frames as described in subclause 6.2.7.2.

6.2.7.3.2 Assistance Data Time Model

Contents of UE positioning GANSS time model (sub-test 4)

GANSS time model

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GANSS Time Model Reference Time		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
T_A0	seconds	0	0	0
GNSS_TOD_ID		0 (GPS)	0 (GPS)	0 (GPS)
Delta_T (Rel-10 onwards)	seconds	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

Contents of UE positioning GANSS time model (sub-tests 8 and 10)

GANSS time model: sub-test 8

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GANSS Time Model Reference Time		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
T_A0	seconds	0	0	0
GNSS_TOD_ID		0 (GPS)	0 (GPS)	0 (GPS)
Delta_T (Rel-10 onwards)	seconds	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GANSS time model: sub-test 10

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GANSS Time Model Reference Time		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
T_A0	seconds	0	0	0
GNSS_TOD_ID		0 (GPS)	0 (GPS)	0 (GPS)
Delta_T (Rel-10 onwards)	seconds	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

6.2.7.3.3 Assistance Data Reference UE Position

Contents of UE positioning GPS reference UE position (sub-tests 3, 4, 8 and 10)

Derived from data in clause 6.2.1.2 and the following information:

Uncertainty of the semi-major axis: 3 km.

Uncertainty of the semi-minor axis: 3 km.

Orientation of the major axis: 0 degrees.

Uncertainty of the altitude information: 500 m.

Confidence factor: 68%.

Contents of UE positioning GANSS reference UE position (sub-tests 1, 2 and 9)

GANSS reference UE position

Derived from data in clause 6.2.1.2 and the following information:

Uncertainty of the semi-major axis: 3 km.

Uncertainty of the semi-minor axis: 3 km.

Orientation of the major axis: 0 degrees.

Uncertainty of the altitude information: 500 m.

Confidence factor: 68%.

6.2.7.3.4 Assistance Data Navigation Model

Contents of UE positioning GPS navigation model (sub-tests 3, 4, 8 and 10)

Satellite Information

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Number of satellites	–	9	10	10

GPS Navigation Model (Fields occurring once per satellite)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SatID	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
Satellite Status	Boolean	0	0	0

GPS Ephemeris and Clock Correction parameters (Fields occurring once per satellite)

Derived from data in clause 6.2.1.2

Contents of UE positioning GANSS navigation model (sub-tests 2 and 8)

GANSS navigation model

Information Element	Units	Value/remark GNSS All
Non-Broadcast Indication	–	Not present

Satellite Information

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Number of satellites	–	7	7	7

GANSS navigation model (Fields occurring once per satellite)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SatID	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
SV Health		0	0	0
IOD		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GANSS Clock Model (Fields occurring once per satellite)

Galileo Satellite clock model (“Model 1”)

Derived from data in clause 6.2.1.2

GANSS Orbit Model (Fields occurring once per satellite)

Galileo orbit model: Keplerian Parameters (“Model 1”)

Derived from data in clause 6.2.1.2

Contents of UE positioning GANSS additional navigation models (sub-tests 1 and 4)

GANSS additional navigation models

Information Element	Units	Value/remark GNSS All
Non-Broadcast Indication	–	Not present

Satellite Information

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Number of satellites	–	8	8	8

GANSS additional navigation models (Fields occurring once per satellite)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SatID	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
SV Health		000000	000000	000000
IOD		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GANSS additional clock models (Fields occurring once per satellite)

GLONASS Satellite Clock Model (“Model 4”)

Derived from data in clause 6.2.1.2

GANSS additional orbit models (Fields occurring once per satellite)

GLONASS Earth-Centered, Earth-fixed Parameters (“Model 4”)

Derived from data in clause 6.2.1.2

Contents of UE positioning GANSS additional navigation model (sub-tests 9 and 10)

GANSS additional navigation model

Information Element	Units	Value/remark GNSS All
Non-Broadcast Indication	–	Not present

Satellite Information

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Number of satellites	–	12	9	9

GANSS additional navigation model (Fields occurring once per satellite)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SatID	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
SV Health		0	0	0
IOD		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GANSS additional Clock Model (Fields occurring once per satellite)

BDS Satellite clock model (“Model 6”)

Derived from data in clause 6.2.1.2

GANSS additional Orbit Model (Fields occurring once per satellite)

BDS orbit model: BDS Keplerian Parameters (“Model 6”)

Derived from data in clause 6.2.1.2

6.2.7.3.5 Assistance Data Ionospheric Model

Contents of UE positioning GPS ionospheric model (sub-tests 3 and 4)

GPS ionospheric model

Derived from data in clause 6.2.1.2

Contents of UE positioning GANSS ionospheric model (sub-tests 2 and 8)

GANSS ionospheric model

Derived from data in clause 6.2.1.2

Contents of UE positioning GANSS additional ionospheric model (sub-tests 1, 9 and 10)

GANSS additional ionospheric model (QZSS)

Derived from data in clause 6.2.1.2 and the following information:

DataId: 00

GANSS additional ionospheric model (BDS)

Derived from data in clause 6.2.1.2 and the following information:

DataId: 01

6.2.7.3.6 Assistance Data Almanac

Contents of UE positioning GPS almanac (sub-tests 3, 4, 8 and 10)

GPS Almanac (Field occurring once per message)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
WN_a	Weeks	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
Complete Almanac Provided (Rel-10 onwards)		TRUE	TRUE	TRUE

Satellite Information

Information Element	Units	Value/remark GNSS All
Number of satellites	–	27

GPS Almanac (Fields occurring once per satellite)

FFS

Contents of UE positioning GANSS almanac (sub-tests 1, 2, 4, 8, 9, and 10)

GANSS almanac: sub-tests 1, 4 (Field occurring once per message)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Week Number	Weeks	N/A	N/A	N/A
Complete Almanac Provided (Rel-10 onwards)		TRUE	TRUE	TRUE

Satellite Information GLO-KP: sub-tests 1 and 4

Information Element	Units	Value/remark GNSS All
Number of satellites	–	24

GANSS almanac: sub-tests 1 and 4 (Fields occurring once per satellite)

GLONASS Keplerian Parameters (“Model 5”)

FFS

GANSS almanac: sub-tests 2 and 8 (Field occurring once per message)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Week Number	Weeks	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
Complete Almanac Provided (Rel-10 onwards)		TRUE	TRUE	TRUE

GANSS almanac: sub-tests 2 and 8 (Field occurring once per message)

Galileo Keplerian Parameters (“Model 1”)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
T_oa		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
IOD_a		0	0	0

Satellite Information KP: sub-tests 2 and 8

Information Element	Units	Value/remark GNSS All
Number of satellites	–	27

GANSS almanac: sub-tests 2 and 8 (Fields occurring once per satellite)

Galileo Keplerian Parameters (“Model 1”)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SV ID	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GANSS almanac: sub-tests 2 and 8 (Fields occurring once per satellite)

Galileo Keplerian Parameters (“Model 1”)

FFS

GANSS almanac: sub-tests 9 and 10 (Field occurring once per message)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Week Number	Weeks	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
Complete Almanac Provided (Rel-10 onwards)		TRUE	TRUE	TRUE

GANSS almanac: sub-tests 9 and 10 (Field occurring once per message)

BDS Keplerian Parameters (“Model 7”)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
T_oa		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
IOD_a		Not present	Not present	Not present

Satellite Information KP: sub-tests 9 and 10

Information Element	Units	Value/remark GNSS All
Number of satellites	–	35

GANSS almanac: sub-tests 9 and 10 (Fields occurring once per satellite)

BDS Keplerian Parameters (“Model 7”)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SV ID	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GANSS almanac: sub-tests 9 and 10 (Fields occurring once per satellite)

BDS Keplerian Parameters (“Model 7”)

FFS

6.2.7.3.7 Assistance Data UTC Model

Contents of UE positioning GPS UTC model (sub-test 4)

GPS UTC model

Derived from data in clause 6.2.1.2 and the following information:

A1: 0

A0: 0

6.2.7.3.8 Assistance Data Acquisition Assistance and Reference Measurement Information

Contents of UE positioning GPS acquisition assistance (sub-tests 3, 4, 8 and 10)

GPS Acquisition Assistance (Fields occurring once per message)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GPS TOW msec	msec	Start time derived from data in clause 6.2.1.2. Add number of ms as required. (Note 1)	Start time derived from data in clause 6.2.1.2. Add number of ms as required. (Note 1)	Start time derived from data in clause 6.2.1.2. Add number of ms as required. (Note 1)
UTRAN GPS reference time		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
UTRAN GPS timing of cell frames		Note 2	Note 2	–
CHOICE mode		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	–
FDD: Primary CPICH Info		100	100	–
TDD: cell parameters id		0	0
SFN		Note 2	Note 2	–
UE Positioning GPS ReferenceTime Uncertainty		For Sensitivity Fine Time Assistance test case: ‘51’ (10.2uS). Otherwise: ‘125’ (2.127s)	For Sensitivity Fine Time Assistance test case: ‘51’ (10.2uS). Otherwise: ‘125’ (2.127s)	‘125’ (2.127s)
Note 1: GPS TOW msec This is the value in ms of GPS TOW msec when the GPS scenario is initially started in the GNSS simulator. For all TTFF test cases, each time a GPS 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. The actual value of GPS TOW msec to be used in the Acquisition Assistance IE (before the addition of the random offset, if applicable) 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. The accuracy shall be such that the Maximum Test System Uncertainty for Coarse Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. For all TTFF test cases a random offset is then added to the value of GPS TOW msec as described in subclause 6.2.7.2. This “final GPS TOW msec” value is then also used to determine the value of the Acquisition Assistance Information Elements marked as “Time varying”. Note 2: UTRAN GPS timing of cell frames and SFN The values of UTRAN GPS timing of cell frames (before the addition of the random offset) and SFN shall be calculated at the time the IE is required. The accuracy of the relationship between the two fields shall be such that the Maximum Test System Uncertainty for Fine Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. A random offset is then added to the value of UTRAN GPS timing of cell frames as described in subclause 6.2.7.2

Satellite Information

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Number of satellites	–	9	10	10

GPS Acquisition Assistance (Fields occurring once per satellite)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SatID	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GPS Acquisition Assistance (Fields occurring once per satellite)

These fields are time varying (see clause 6.2.7.1) and are derived from data in clause 6.2.1.2 and the following information:

Doppler uncertainty: 40 m/s

Code Phase Search Window: derived for each satellite using a 3 km radius UE position uncertainty.

Contents of UE positioning GANSS reference measurement information (sub-tests 1, 2, 4, 8, 9, and 10)

GANSS reference measurement information: sub-tests 1 and 4 (Fields occurring once per message)

Information Element	Units	Value/remark GNSS All
GANSS Signal ID		Not present

Satellite Information: sub-tests 1 and 4

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Number of satellites	–	8	8	8

GANSS reference measurement information: sub-tests 1 and 4 (Fields occurring once per satellite)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SatID	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GANSS reference measurement information: sub-tests 1 and 4 (Fields occurring once per satellite)

These fields are time varying (see clause 6.2.7.1) and are derived from data in clause 6.2.1.2 and the following information:

Doppler uncertainty: 40 m/s

Code Phase Search Window: derived for each satellite using a 3 km radius UE position uncertainty

GANSS reference measurement information: sub-tests 2 and 8 (Fields occurring once per message)

Information Element	Units	Value/remark GNSS All
GANSS Signal ID		Not present

Satellite Information: sub-tests 2 and 8

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Number of satellites	–	7	7	7

GANSS reference measurement information: sub-tests 2 and 8 (Fields occurring once per satellite)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SatID	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GANSS reference measurement information: sub-tests 2 and 8 (Fields occurring once per satellite)

These fields are time varying (see clause 6.2.7.1) and are derived from data in clause 6.2.1.2 and the following information:

Doppler uncertainty: 40 m/s

Code Phase Search Window: derived for each satellite using a 3 km radius UE position uncertainty

GANSS reference measurement information: sub-tests 9 and 10 (Fields occurring once per message)

Information Element	Units	Value/remark GNSS All
GANSS Signal ID		Not present

Satellite Information: sub-tests 9 and 10

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Number of satellites	–	12	9	9

GANSS reference measurement information: sub-tests 9 and 10 (Fields occurring once per satellite)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SatID	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GANSS reference measurement information: sub-tests 9 and 10 (Fields occurring once per satellite)

These fields are time varying (see clause 6.2.7.1) and are derived from data in clause 6.2.1.2 and the following information:

Doppler uncertainty: 40 m/s

Code Phase Search Window: derived for each satellite using a 3 km radius UE position uncertainty

6.2.7.3.9 Assistance Data Auxiliary Information

Contents of UE positioning GANSS auxiliary information (sub-tests 1, 3, 4, 8 and 10)

GANSS auxiliary information: sub-tests 1 and 4 (Fields occurring once per message)

Information Element	Units	Value/remark GNSS All
GANSS-ID-3		Present (GLONASS)

Aux Info List: sub-tests 1 and 4

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Number of satellites	–	8	8	8

GANSS auxiliary information: sub-tests 1 and 4 (Fields occurring once per satellite)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SatID	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
Signals Available	–	10000000 (G1)	10000000 (G1)	10000000 (G1)
Channel number	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GANSS auxiliary information: sub-tests 3, 4, 8 and 10 (Fields occurring once per message)

Information Element	Units	Value/remark GNSS All
GANSS-ID-1		Sub-test 3: present (Modernized GPS), sub-tests 4, 8 and 10 if the UE supports multiple GPS signals: present (Modernized GPS)

Aux Info List: sub-tests 3 and 4, 8, 10

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
Number of satellites	–	9	10	10

GANSS auxiliary information: sub-tests 3 and 4, 8, 10 (Fields occurring once per satellite)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
SatID	–	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
Signals Available	–	As supported by the UE	As supported by the UE	As supported by the UE

6.2.7.3.10 Assistance Data GANSS ID

Contents of GANSS ID (sub-tests 1, 2, 3, 4, 8, 9 and 10)

GANSS ID: sub-tests 1 and 4

Information Element	Units	Value/remark GNSS All
GANSS ID		3 (GLONASS)

GANSS ID: sub-tests 2 and 8

Information Element	Units	Value/remark GNSS All
GANSS ID		Not present (Galileo)

GANSS ID: sub-test 3

Information Element	Units	Value/remark GNSS All
GANSS ID		1 (Modernized GPS)

GANSS ID: sub-tests 9 and 10

Information Element	Units	Value/remark GNSS All
GANSS ID		4 (BDS)

6.2.7.4 Contents of Information elements for A-GNSS Minimum performance testing in TS 37.571-1 subclauses 7 and 13

6.2.7.4.1 GNSS REFERENCE TIME:

GNSS-ReferenceTime (GPS): sub-tests 1, 4, 5, 8, 10, 11, 12 and 13

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
gnss-SystemTime
gnss-TimeID		0 (gps)	0 (gps)	0 (gps)
gnss-DayNumber	days	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
gnss-TimeOfDay	s	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (Note 1)
gnss-TimeOfDayFrac-msec	ms	0 (Note 1)	0 (Note 1)	0 (Note 1)
notificationOfLeapSecond		Not present	Not present	Not present
gps-TOW-Assist
satelliteID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
tlmWord		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
antiSpoof		1 (for all PRNs)	1 (for all PRNs)	1 (for all PRNs)
alert		0 (for all PRNs)	0 (for all PRNs)	0 (for all PRNs)
tlmRsvdBits		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
referenceTimeUnc		‘117’ (2.274 seconds) Absent for Sensitivity Fine Time Assistance test case. Present otherwise	‘117’ (2.274 seconds) Absent for Sensitivity Fine Time Assistance test case. Present otherwise	‘117’ (2.274 seconds)
gnss-ReferenceTimeForCells		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
GNSS-ReferenceTimeForOneCell
networkTime
secondsFromFrameStructureStart	s	Note 2	Note 2
fractionalSecondsFromFrameStructureStart	250ns	Note 2	Note 2
frameDrift		0	0
cellID
CHOICE eUTRA		For TS 37.571-1 subclause 7, or subclause 13 Test Configuration A	For TS 37.571-1 subclause 7, or subclause 13 Test Configuration A
physCellId		0	0
cellGlobalIdEUTRA		‘0000 0000’B	‘0000 0000’B
earfcn/earfcn-v9a0		Note 3	Note 3
CHOICE nr-r15		For TS 37.571-1 subclause 13 Test Configuration B	For TS 37.571-1 subclause 13 Test Configuration B
nrPhysCellId-r15		0	0
nrCellGlobalID-r15		‘0000 0000’B	‘0000 0000’B
nrARFCN-r15		Note 4	Note 4
referenceTimeUnc		‘24’ (11.11us)	‘24’ (11.11us)
Note 1: gnss-TimeOfDay and gnss-TimeOfDayFrac-msec. This is the value of gnss-TimeOfDay and gnss-TimeOfDayFrac-msec when the GNSS scenario is initially started in the GNSS simulator. For all TTFF test cases, each time a GNSS scenario is used, the GNSS 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. The actual value of gnss-TimeOfDay and gnss-TimeOfDayFrac-msec to be used in the Reference Time IE (before the addition of the random offset, if applicable) 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. The accuracy shall be such that the Maximum Test System Uncertainty for Coarse Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. For all TTFF test cases a random offset is then added to the value of gnss-TimeOfDay and gnss-TimeOfDayFrac-msec as described in subclause 6.2.7.2. Note 2: secondsFromFrameStructureStart and fractionalSecondsFromFrameStructureStart. The values of secondsFromFrameStructureStart and fractionalSecondsFromFrameStructureStart (before the addition of the random offset) shall be calculated at the time the IE is required. The accuracy of the values used shall be such that the Maximum Test System Uncertainty for Fine Time Assistance, specified in Table C.1.2 of 37.571-1 [6], shall be met. A random offset is then added to the value of secondsFromFrameStructureStart and fractionalSecondsFromFrameStructureStart as described in subclause 6.2.7.2. Note 3: earfcn/earfcn-v9a0 is defined in TS 36.508 [20] subclause 4.3.1 for the frequency band under test (see TS 37.571-1 [6] subclause 4.4.1) Note 4: nrARFCN is defined in TS 38.508-1 [24] subclause 6.2.3 for the frequency band under test (see TS 37.571-1 [6] subclause 4.12.1)

GNSS-ReferenceTime (GLONASS): sub-test 2

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
gnss-SystemTime
gnss-TimeID		4 (glonass)	4 (glonass)	4 (glonass)
gnss-DayNumber	days	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
gnss-TimeOfDay	s	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (Note 1)
gnss-TimeOfDayFrac-msec	ms	0 (Note 1)	0 (Note 1)	0 (Note 1)
notificationOfLeapSecond		00	00	00
gps-TOW-Assist		Not present	Not present	Not present
referenceTimeUnc		‘117’ (2.274 seconds) Absent for Sensitivity Fine Time Assistance test case. Present otherwise	‘117’ (2.274 seconds) Absent for Sensitivity Fine Time Assistance test case. Present otherwise	‘117’ (2.274 seconds)
gnss-ReferenceTimeForCells		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
GNSS-ReferenceTimeForOneCell
networkTime
secondsFromFrameStructureStart	s	Note 2	Note 2
fractionalSecondsFromFrameStructureStart	250ns	Note 2	Note 2
frameDrift		0	0
cellID
CHOICE eUTRA		For TS 37.571-1 subclause 7, or subclause 13 Test Configuration A	For TS 37.571-1 subclause 7, or subclause 13 Test Configuration A
physCellId		0	0
cellGlobalIdEUTRA		‘0000 0000’B	‘0000 0000’B
earfcn/earfcn-v9a0		Note 3	Note 3
CHOICE nr-r15		For TS 37.571-1 subclause 13 Test Configuration B	For TS 37.571-1 subclause 13 Test Configuration B
nrPhysCellId-r15		0	0
nrCellGlobalID-r15		‘0000 0000’B	‘0000 0000’B
nrARFCN-r15		Note 4	Note 4
referenceTimeUnc		‘24’ (11.11us)	‘24’ (11.11us)
Note 1: gnss-TimeOfDay and gnss-TimeOfDayFrac-msec This is the value of gnss-TimeOfDay and gnss-TimeOfDayFrac-msec when the GNSS scenario is initially started in the GNSS simulator. For all TTFF test cases, each time a GNSS scenario is used, the GNSS 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. The actual value of gnss-TimeOfDay and gnss-TimeOfDayFrac-msec to be used in the Reference Time IE (before the addition of the random offset, if applicable) 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. The accuracy shall be such that the Maximum Test System Uncertainty for Coarse Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. For all TTFF test cases a random offset is then added to the value of gnss-TimeOfDay and gnss-TimeOfDayFrac-msec as described in subclause 6.2.7.2. Note 2: secondsFromFrameStructureStart and fractionalSecondsFromFrameStructureStart. The values of secondsFromFrameStructureStart and fractionalSecondsFromFrameStructureStart (before the addition of the random offset) shall be calculated at the time the IE is required. The accuracy of the values used shall be such that the Maximum Test System Uncertainty for Fine Time Assistance, specified in Table C.1.2 of 37.571-1 [6], shall be met. A random offset is then added to the value of secondsFromFrameStructureStart and fractionalSecondsFromFrameStructureStart as described in subclause 6.2.7.2. Note 3: earfcn/earfcn-v9a0 is defined in TS 36.508 [20] subclause 4.3.1 for the frequency band under test (see TS 37.571-1 [6] subclause 4.4.1) Note 4: nrARFCN is defined in TS 38.508-1 [24] subclause 6.2.3 for the frequency band under test (see TS 37.571-1 [6] subclause 4.12.1)

GNSS-ReferenceTime (Galileo): sub-test 3

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
gnss-SystemTime
gnss-TimeID		3 (galileo)	3 (galileo)	3 (galileo)
gnss-DayNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
gnss-TimeOfDay		Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (Note 1)
gnss-TimeOfDayFrac-msec		0 (Note 1)	0 (Note 1)	0 (Note 1)
notificationOfLeapSecond		Not present	Not present	Not present
gps-TOW-Assist		Not present	Not present	Not present
referenceTimeUnc		‘117’ (2.274 seconds) Absent for Sensitivity Fine Time Assistance test case. Present otherwise	‘117’ (2.274 seconds) Absent for Sensitivity Fine Time Assistance test case. Present otherwise	‘117’ (2.274 seconds)
gnss-ReferenceTimeForCells		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
GNSS-ReferenceTimeForOneCell
networkTime
secondsFromFrameStructureStart	s	Note 2	Note 2
fractionalSecondsFromFrameStructureStart	250ns	Note 2	Note 2
frameDrift		0	0
cellID
CHOICE eUTRA		For TS 37.571-1 subclause 7, or subclause 13 Test Configuration A	For TS 37.571-1 subclause 7, or subclause 13 Test Configuration A
physCellId		0	0
cellGlobalIdEUTRA		‘0000 0000’B	‘0000 0000’B
earfcn/earfcn-v9a0		Note 3	Note 3
CHOICE nr-r15		For TS 37.571-1 subclause 13 Test Configuration B	For TS 37.571-1 subclause 13 Test Configuration B
nrPhysCellId-r15		0	0
nrCellGlobalID-r15		‘0000 0000’B	‘0000 0000’B
nrARFCN-r15		Note 4	Note 4
referenceTimeUnc		‘24’ (11.11us)	‘24’ (11.11us)
Note 1: gnss-TimeOfDay and gnss-TimeOfDayFrac-msec This is the value of gnss-TimeOfDay and gnss-TimeOfDayFrac-msec when the GNSS scenario is initially started in the GNSS simulator. For all TTFF test cases, each time a GNSS scenario is used, the GNSS 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. The actual value of gnss-TimeOfDay and gnss-TimeOfDayFrac-msec to be used in the Reference Time IE (before the addition of the random offset, if applicable) 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. The accuracy shall be such that the Maximum Test System Uncertainty for Coarse Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. For all TTFF test cases a random offset is then added to the value of gnss-TimeOfDay and gnss-TimeOfDayFrac-msec as described in subclause 6.2.7.2. Note 2: secondsFromFrameStructureStart and fractionalSecondsFromFrameStructureStart. The values of secondsFromFrameStructureStart and fractionalSecondsFromFrameStructureStart (before the addition of the random offset) shall be calculated at the time the IE is required. The accuracy of the values used shall be such that the Maximum Test System Uncertainty for Fine Time Assistance, specified in Table C.1.2 of 37.571-1 [6], shall be met. A random offset is then added to the value of secondsFromFrameStructureStart and fractionalSecondsFromFrameStructureStart as described in subclause 6.2.7.2. Note 3: earfcn/earfcn-v9a0 is defined in TS 36.508 [20] subclause 4.3.1 for the frequency band under test (see TS 37.571-1 [6] subclause 4.4.1) Note 4: nrARFCN is defined in TS 38.508-1 [24] subclause 6.2.3 for the frequency band under test (see TS 37.571-1 [6] subclause 4.12.1)

GNSS-ReferenceTime (BDS): sub-test 9

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
gnss-SystemTime
gnss-TimeID		5 (bds)	5 (bds)	5 (bds)
gnss-DayNumber	days	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
gnss-TimeOfDay	s	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (Note 1)	Start time derived from data in clause 6.2.1.2. (Note 1)
gnss-TimeOfDayFrac-msec	ms	0 (Note 1)	0 (Note 1)	0 (Note 1)
notificationOfLeapSecond		Not present	Not present	Not present
gps-TOW-Assist		Not present	Not present	Not present
referenceTimeUnc		‘117’ (2.274 seconds) Absent for Sensitivity Fine Time Assistance test case. Present otherwise	‘117’ (2.274 seconds) Absent for Sensitivity Fine Time Assistance test case. Present otherwise	‘117’ (2.274 seconds)
gnss-ReferenceTimeForCells		Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Present for Sensitivity Fine Time Assistance test case. Absent otherwise	Absent
GNSS-ReferenceTimeForOneCell
networkTime
secondsFromFrameStructureStart	s	Note 2	Note 2
fractionalSecondsFromFrameStructureStart	250ns	Note 2	Note 2
frameDrift		0	0
cellID
CHOICE eUTRA		For TS 37.571-1 subclause 7, or subclause 13 Test Configuration A	For TS 37.571-1 subclause 7, or subclause 13 Test Configuration A
physCellId		0	0
cellGlobalIdEUTRA		‘0000 0000’B	‘0000 0000’B
earfcn/earfcn-v9a0		Note 3	Note 3
CHOICE nr-r15		For TS 37.571-1 subclause 13 Test Configuration B	For TS 37.571-1 subclause 13 Test Configuration B
nrPhysCellId-r15		0	0
nrCellGlobalID-r15		‘0000 0000’B	‘0000 0000’B
nrARFCN-r15		Note 4	Note 4
referenceTimeUnc		‘24’ (11.11us)	‘24’ (11.11us)
Note 1: gnss-TimeOfDay and gnss-TimeOfDayFrac-msec. This is the value of gnss-TimeOfDay and gnss-TimeOfDayFrac-msec when the GNSS scenario is initially started in the GNSS simulator. For all TTFF test cases, each time a GNSS scenario is used, the GNSS 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. The actual value of gnss-TimeOfDay and gnss-TimeOfDayFrac-msec to be used in the Reference Time IE (before the addition of the random offset, if applicable) 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. The accuracy shall be such that the Maximum Test System Uncertainty for Coarse Time Assistance, specified in Table C.1.2 of TS 37.571-1 [6], shall be met. For all TTFF test cases a random offset is then added to the value of gnss-TimeOfDay and gnss-TimeOfDayFrac-msec as described in subclause 6.2.7.2. Note 2: secondsFromFrameStructureStart and fractionalSecondsFromFrameStructureStart. The values of secondsFromFrameStructureStart and fractionalSecondsFromFrameStructureStart (before the addition of the random offset) shall be calculated at the time the IE is required. The accuracy of the values used shall be such that the Maximum Test System Uncertainty for Fine Time Assistance, specified in Table C.1.2 of 37.571-1 [6], shall be met. A random offset is then added to the value of secondsFromFrameStructureStart and fractionalSecondsFromFrameStructureStart as described in subclause 6.2.7.2. Note 3: earfcn/earfcn-v9a0 is defined in TS 36.508 [20] subclause 4.3.1 for the frequency band under test (see TS 37.571-1 [6] subclause 4.4.1) Note 4: nrARFCN is defined in TS 38.508-1 [24] subclause 6.2.3 for the frequency band under test (see TS 37.571-1 [6] subclause 4.12.1)

6.2.7.4.2 GNSS REFERENCE LOCATION:

GNSS-ReferenceLocation

Derived from data in clause 6.2.1.2 and the following information:

Uncertainty of the semi-major axis: 3 km.

Uncertainty of the semi-minor axis: 3 km.

Orientation of the major axis: 0 degrees.

Uncertainty of the altitude information: 500 m.

Confidence factor: 68%.

6.2.7.4.3 GNSS IONOSPHERIC MODEL:

GNSS-IonosphericModel (Klobuchar Model): sub-tests 1, 2, 4 and 5

Derived from data in clause 6.2.1.2 and the following information:

dataID: 00

neQuickModel: not present

klobucharModel2: not present

GNSS-IonosphericModel (NeQuick Model): sub-test 3

Derived from data in clause 6.2.1.2 and the following information:

klobucharModel: not present

klobucharModel2: not present

GNSS-IonosphericModel (Klobuchar2 Model)

Derived from data in clause 6.2.1.2 and the following information:

klobucharModel: not present

neQuickModel: not present

GNSS-IonosphericModel: sub-tests 8 and 12

Information Element	Units	Value/remark GNSS All
GNSS-IonosphericModel
klobucharModel		See values for GNSS-IonosphericModel (Klobuchar)
neQuickModel		See values for GNSS-IonosphericModel (NeQuick)
klobucharModel2		Not present

GNSS-IonosphericModel: sub-tests 9, 10 and 11

Information Element	Units	Value/remark GNSS All
GNSS-IonosphericModel
klobucharModel		If BDS B1I supported. See values for GNSS-IonosphericModel (Klobuchar)
neQuickModel		Not present
klobucharModel2		If BDS B1C supported. See values for GNSS-IonosphericModel (Klobuchar2)

GNSS-IonosphericModel: sub-test 13

Information Element	Units	Value/remark GNSS All
GNSS-IonosphericModel
klobucharModel		If BDS B1I supported. See values for GNSS-IonosphericModel (Klobuchar)
neQuickModel		See values for GNSS-IonosphericModel (NeQuick)
klobucharModel2		If BDS B1C supported. See values for GNSS-IonosphericModel (Klobuchar2)

6.2.7.4.4 GNSS TIME MODEL LIST:

GNSS-TimeModelList (GPS – GLONASS): sub-test 5

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
gnss-TimeModelRefTime		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
tA0		0	0	0
gnss-TO-ID		1 (GPS)	1 (GPS)	1 (GPS)
weekNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
deltaT		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-TimeModelList (GPS – Galileo): sub-test 8

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
gnss-TimeModelRefTime		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
tA0		0	0	0
gnss-TO-ID		1 (GPS)	1 (GPS)	1 (GPS)
weekNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
deltaT		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-TimeModelList (GPS – BDS): sub-test 10

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
gnss-TimeModelRefTime		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
tA0		0	0	0
gnss-TO-ID		1 (GPS)	1 (GPS)	1 (GPS)
weekNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
deltaT		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-TimeModelList: sub-test 11

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 2
gnss-ID		4 (glonass)
GNSS-TimeModelList		See GNSS-TimeModelList (GPS – GLONASS)
gnss-ID		5 (bds)
GNSS-TimeModelList		See GNSS-TimeModelList (GPS – BDS)

GNSS-TimeModelList: sub-test 12

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 2
gnss-ID		3 (galileo)
GNSS- TimeModelList		See GNSS-TimeModelList (GPS – Galileo)
gnss-ID		4 (glonass)
GNSS- TimeModelList		See GNSS-TimeModelList (GPS – GLONASS)

GNSS-TimeModelList: sub-test 13

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 2
gnss-ID		3 (galileo)
GNSS- TimeModelList		See GNSS-TimeModelList (GPS – Galileo)
gnss-ID		5 (bds)
GNSS- TimeModelList		See GNSS-TimeModelList (GPS – BDS)

6.2.7.4.5 GNSS NAVIGATION MODEL:

GNSS-NavigationModel (GPS L1 C/A only): sub-test 1

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
nonBroadcastFlag		0	0	0
gnss-SatelliteList		(SIZE) 9	(SIZE) 9	(SIZE) 9

GNSS-NavModelSatelliteElement (GPS L1 C/A only): sub-test 1

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
svHealth		0	0	0
iod		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-NavModelSatelliteElement (GPS L1 C/A only): sub-test 1

Derived from data in clause 6.2.1.2 and the following information:

GNSS-ClockModel: nav-ClockModel, Model-2

GNSS-OrbitModel: nav-KeplerianSet, Model-2

GNSS-NavigationModel (GLONASS): sub-test 2

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
nonBroadcastFlag		0	0	0
gnss-SatelliteList		(SIZE) 8	(SIZE) 8	(SIZE) 8

GNSS-NavModelSatelliteElement (GLONASS): sub-test 2

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
svHealth		00000000	00000000	00000000
iod		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-NavModelSatelliteElement (GLONASS): sub-test 2

Derived from data in clause 6.2.1.2 and the following information:

GNSS-ClockModel: glonass-ClockModel, Model-4

GNSS-OrbitModel: glonass-ECEF, Model-4

GNSS-NavigationModel (Galileo): sub-test 3

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
nonBroadcastFlag		0	0	0
gnss-SatelliteList		(SIZE) 7	(SIZE) 7	(SIZE) 7

GNSS-NavModelSatelliteElement (Galileo): sub-test 3

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
svHealth		0	0	0
iod		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-NavModelSatelliteElement (Galileo): sub-test 3

Derived from data in clause 6.2.1.2 and the following information:

GNSS-ClockModel: standardClockModelList, Model-1.

standardClockModelList: (SIZE) 1 if the UE supports only Galileo E1, (SIZE) 2 if the UE supports multiple Galileo signals.

StandardClockModelElement (I/NAV):

stanClockTgd: Not present if the UE supports multiple Galileo signals.
stanModelID: 0 (I/NAV). Present only if the UE supports multiple Galileo signals

StandardClockModelElement (F/NAV): Present only if the UE supports multiple Galileo signals

stanClockTgd: Not present
stanModelID: 1 (F/NAV)

GNSS-OrbitModel: keplerianSet, Model-1

GNSS-NavigationModel: sub-test 4

The GNSS-NavigationModel(s) to be used depends on the GNSS-NavigationModel(s) supported by the UE. The allowed NavigationModels are as follows:

GNSS-NavigationModel (GPS)

GNSS-NavigationModel (Modernized GPS)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
nonBroadcastFlag		0	0	0
gnss-SatelliteList		(SIZE) 9	(SIZE) 10	(SIZE) 10

GNSS-NavModelSatelliteElement (Modernized GPS)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
svHealth		0	0	0
iod		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-NavModelSatelliteElement (Modernized GPS)

Derived from data in clause 6.2.1.2 and the following information:

GNSS-ClockModel: cnav-ClockModel, Model-3

GNSS-OrbitModel: cnav-KeplerianSet, Model-3

GNSS-NavigationModel: sub-test 5

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 2
gnss-ID		0 (gps)
GNSS-NavigationModel		See GNSS-NavigationModel (GPS) and/or GNSS-NavigationModel (Modernized GPS) depending on GNSS-NavigationModel supported by the UE
gnss-ID		4 (glonass)
GNSS-NavigationModel		See GNSS-NavigationModel (GLONASS)

GNSS-NavigationModel (GPS)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
nonBroadcastFlag		0	0	0
gnss-SatelliteList		(SIZE) 9	(SIZE) 10	(SIZE) 10

GNSS-NavModelSatelliteElement (GPS)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
svHealth		0	0	0
iod		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-NavModelSatelliteElement (GPS)

Derived from data in clause 6.2.1.2 and the following information:

GNSS-ClockModel: nav-ClockModel, Model-2

GNSS-OrbitModel: nav-KeplerianSet, Model-2

GNSS-NavigationModel: sub-test 8

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 2
gnss-ID		0 (gps)
GNSS-NavigationModel		See GNSS-NavigationModel (GPS) and/or GNSS-NavigationModel (Modernized GPS) depending on GNSS-NavigationModel supported by the UE
gnss-ID		3 (galileo)
GNSS-NavigationModel		See GNSS-NavigationModel (Galileo)

GNSS-NavigationModel: sub-test 9

The GNSS-NavigationModel(s) to be used depends on the GNSS-NavigationModel(s) supported by the UE. The allowed NavigationModels are as follows:

GNSS-NavigationModel (BDS B1I)

GNSS-NavigationModel (BDS B1C)

GNSS-NavigationModel (BDS B1I)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
nonBroadcastFlag		0	0	0
gnss-SatelliteList		(SIZE) 12	(SIZE) 9	(SIZE) 9

GNSS-NavModelSatelliteElement (BDS B1I)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
svHealth		0	0	0
iod		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-NavModelSatelliteElement (BDS B1I)

Derived from data in clause 6.2.1.2 and the following information:

GNSS-ClockModel: BDS-ClockModel-r12, Model-6

GNSS-OrbitModel: BDS-KeplerianSet-r12, Model-6

GNSS-NavigationModel (BDS B1C)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
nonBroadcastFlag		0	0	0
gnss-SatelliteList		(SIZE) 12	(SIZE) 9	(SIZE) 9

GNSS-NavModelSatelliteElement (BDS B1C)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
svHealth		0	0	0
iod		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-NavModelSatelliteElement (BDS B1C)

Derived from data in clause 6.2.1.2 and the following information:

GNSS-ClockModel: bds-ClockModel2-r16, Model-7

GNSS-OrbitModel: bds-KeplerianSet2-r16, Model-7

GNSS-NavigationModel: sub-test 10

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 2
gnss-ID		0 (gps)
GNSS-NavigationModel		See GNSS-NavigationModel (GPS) and/or GNSS-NavigationModel (Modernized GPS) depending on GNSS-NavigationModel supported by the UE
gnss-ID		5 (bds)
GNSS-NavigationModel		See GNSS-NavigationModel (BDS B1I) and/or GNSS-NavigationModel (BDS B1C) depending on GNSS-NavigationModel supported by the UE

GNSS-NavigationModel: sub-test 11

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 3
gnss-ID		0 (gps)
GNSS-NavigationModel		See GNSS-NavigationModel (GPS) and/or GNSS-NavigationModel (Modernized GPS) depending on GNSS-NavigationModel supported by the UE
gnss-ID		4 (glonass)
GNSS-NavigationModel		See GNSS-NavigationModel (GLONASS)
gnss-ID		5 (bds)
GNSS-NavigationModel		See GNSS-NavigationModel (BDS B1I) and/or GNSS-NavigationModel (BDS B1C) depending on GNSS-NavigationModel supported by the UE

GNSS-NavigationModel: sub-test 12

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 3
gnss-ID		0 (gps)
GNSS-NavigationModel		See GNSS-NavigationModel (GPS) and/or GNSS-NavigationModel (Modernized GPS) depending on GNSS-NavigationModel supported by the UE
gnss-ID		3 (galileo)
GNSS-NavigationModel		See GNSS-NavigationModel (Galileo)
gnss-ID		4 (glonass)
GNSS-NavigationModel		See GNSS-NavigationModel (GLONASS)

GNSS-NavigationModel: sub-test 13

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 3
gnss-ID		0 (gps)
GNSS-NavigationModel		See GNSS-NavigationModel (GPS) and/or GNSS-NavigationModel (Modernized GPS) depending on GNSS-NavigationModel supported by the UE
gnss-ID		3 (galileo)
GNSS-NavigationModel		See GNSS-NavigationModel (Galileo)
gnss-ID		5 (bds)
GNSS-NavigationModel		See GNSS-NavigationModel (BDS B1I) and/or GNSS-NavigationModel (BDS B1C) depending on GNSS-NavigationModel supported by the UE

6.2.7.4.6 GNSS ACQUISITION ASSISTANCE:

GNSS-AcquisitionAssistance (GPS L1 C/A only): sub-test 1

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-AcquisitionAssistance
gnss-SignalID		0 (GPS L1 C/A)	0 (GPS L1 C/A	0 (GPS L1 C/A)
gnss-AcquisitionAssistList		(SIZE) 9	(SIZE) 9	(SIZE) 9
confidence-r10	%	98	98	98

GNSS-AcquisitionAssistElement (GPS L1 C/A only): sub-test 1

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AcquisitionAssistElement (GPS L1 C/A only): sub-test 1

These fields are time varying (see clause 6.2.7.1) and are derived from data in clause 6.2.1.2 and the following information:

Doppler uncertainty: 40 m/s

Code Phase Search Window: derived for each satellite using a 3 km radius UE position uncertainty

GNSS-AcquisitionAssistance (GLONASS): sub-test 2

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-AcquisitionAssistance
gnss-SignalID		0 (GLONASS G1)	0 (GLONASS G1)	0 (GLONASS G1)
gnss-AcquisitionAssistList		(SIZE) 8	(SIZE) 8	(SIZE) 8
confidence-r10	%	98	98	98

GNSS-AcquisitionAssistElement (GLONASS): sub-test 2

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AcquisitionAssistElement (GLONASS): sub-test 2

These fields are time varying (see clause 6.2.7.1) and are derived from data in clause 6.2.1.2 and the following information:

Doppler uncertainty: 40 m/s

Code Phase Search Window: derived for each satellite using a 3 km radius UE position uncertainty

GNSS-AcquisitionAssistance: sub-test 3

The GNSS-AcquisitionAssistance(s) to be used depends on the GNSS-AcquisitionAssistance(s) supported by the UE. The allowed GNSS-AcquisitionAssistances are as follows:

GNSS-AcquisitionAssistance (Galileo E1)

GNSS-AcquisitionAssistance (Galileo E5A)

Data for other Galileo signals are FFS

GNSS-AcquisitionAssistance (Galileo E1)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-AcquisitionAssistance
gnss-SignalID		0 (Galileo E1)	0 (Galileo E1)	0 (Galileo E1)
gnss-AcquisitionAssistList		(SIZE) 7	(SIZE) 7	(SIZE) 7
confidence-r10	%	98	98	98

GNSS-AcquisitionAssistElement (Galileo E1)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AcquisitionAssistElement (Galileo E1)

These fields are time varying (see clause 6.2.7.1) and are derived from data in clause 6.2.1.2 and the following information:

Doppler uncertainty: 40 m/s

Code Phase Search Window: derived for each satellite using a 3 km radius UE position uncertainty

GNSS-AcquisitionAssistance (Galileo E5A)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-AcquisitionAssistance
gnss-SignalID		1 (Galileo E5A)	1 (Galileo E5A)	1 (Galileo E5A)
gnss-AcquisitionAssistList		(SIZE) 7	(SIZE) 7	(SIZE) 7
confidence-r10	%	98	98	98

GNSS-AcquisitionAssistElement (Galileo E5A)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AcquisitionAssistElement (Galileo E5A)

These fields are time varying (see clause 6.2.7.1) and are derived from data in clause 6.2.1.2 and the following information:

Doppler uncertainty: 40 m/s

Code Phase Search Window: derived for each satellite using a 3 km radius UE position uncertainty

GNSS-AcquisitionAssistance: sub-test 4

The GNSS-AcquisitionAssistance(s) to be used depends on the GNSS-AcquisitionAssistance(s) supported by the UE. The allowed GNSS-AcquisitionAssistances are as follows:

GNSS-AcquisitionAssistance (GPS L1 C/A)

GNSS-AcquisitionAssistance (Modernized GPS L5)

Data for other GPS signals are FFS

GNSS-AcquisitionAssistance (Modernized GPS L5)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-AcquisitionAssistance
gnss-SignalID		3 (GPS L5)	3 (GPS L5)	3 (GPS L5)
gnss-AcquisitionAssistList		(SIZE) 9	(SIZE) 10	(SIZE) 10
confidence-r10	%	98	98	98

GNSS-AcquisitionAssistElement (Modernized GPS L5)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AcquisitionAssistElement (Modernized GPS L5)

These fields are time varying (see clause 6.2.7.1) and are derived from data in clause 6.2.1.2 and the following information:

Doppler uncertainty: 40 m/s

Code Phase Search Window: derived for each satellite using a 3 km radius UE position uncertainty

GNSS-AcquisitionAssistance: sub-test 5

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 2
gnss-ID		0 (gps)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (GPS L1 C/A) and/or GNSS-AcquisitionAssistance (Modernized GPS L5) depending on GNSS-AcquisitionAssistance supported by the UE
gnss-ID		4 (glonass)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (GLONASS)

GNSS-AcquisitionAssistance (GPS L1 C/A)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-AcquisitionAssistance
gnss-SignalID		0 (GPS L1 C/A)	0 (GPS L1 C/A	0 (GPS L1 C/A)
gnss-AcquisitionAssistList		(SIZE) 9	(SIZE) 10	(SIZE) 10
confidence-r10	%	98	98	98

GNSS-AcquisitionAssistElement (GPS L1 C/A)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AcquisitionAssistElement (GPS L1 C/A)

These fields are time varying (see clause 6.2.7.1) and are derived from data in clause 6.2.1.2 and the following information:

Doppler uncertainty: 40 m/s

Code Phase Search Window: derived for each satellite using a 3 km radius UE position uncertainty

GNSS-AcquisitionAssistance: sub-test 8

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 2
gnss-ID		0 (gps)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (GPS L1 C/A) and/or GNSS-AcquisitionAssistance (Modernized GPS L5) depending on GNSS-AcquisitionAssistance supported by the UE
gnss-ID		3 (galileo)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (Galileo E1) and/or GNSS-AcquisitionAssistance (Galileo E5A) depending on GNSS-AcquisitionAssistance supported by the UE

GNSS-AcquisitionAssistance: sub-test 9

The GNSS-AcquisitionAssistance(s) to be used depends on the GNSS-AcquisitionAssistance(s) supported by the UE. The allowed GNSS-AcquisitionAssistances are as follows:

GNSS-AcquisitionAssistance (BDS B1I)

GNSS-AcquisitionAssistance (BDS B1C)

GNSS-AcquisitionAssistElement (BDS B1I)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AcquisitionAssistElement (BDS B1I)

These fields are time varying (see clause 6.2.7.1) and are derived from data in clause 6.2.1.2 and the following information:

Doppler uncertainty: 40 m/s

Code Phase Search Window: derived for each satellite using a 3 km radius UE position uncertainty

GNSS-AcquisitionAssistElement (BDS B1C)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AcquisitionAssistElement (BDS B1C)

These fields are time varying (see clause 6.2.7.1) and are derived from data in clause 6.2.1.2 and the following information:

Doppler uncertainty: 40 m/s

Code Phase Search Window: derived for each satellite using a 3 km radius UE position uncertainty

GNSS-AcquisitionAssistance: sub-test 10

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 2
gnss-ID		0 (gps)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (GPS L1 C/A) and/or GNSS-AcquisitionAssistance (Modernized GPS L5) depending on GNSS-AcquisitionAssistance supported by the UE
gnss-ID		5 (bds)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (BDS B1I) and/or GNSS-AcquisitionAssistance (BDS B1C) depending on GNSS-AcquisitionAssistance supported by the UE

GNSS-AcquisitionAssistance: sub-test 11

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 3
gnss-ID		0 (gps)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (GPS L1 C/A) and/or GNSS-AcquisitionAssistance (Modernized GPS L5) depending on GNSS-AcquisitionAssistance supported by the UE
gnss-ID		4 (glonass)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (GLONASS)
gnss-ID		5 (bds)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (BDS B1I) and/or GNSS-AcquisitionAssistance (BDS B1C) depending on GNSS-AcquisitionAssistance supported by the UE

GNSS-AcquisitionAssistance: sub-test 12

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 3
gnss-ID		0 (gps)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (GPS L1 C/A) and/or GNSS-AcquisitionAssistance (Modernized GPS L5) depending on GNSS-AcquisitionAssistance supported by the UE
gnss-ID		3 (galileo)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (Galileo E1) and/or GNSS-AcquisitionAssistance (Galileo E5A) depending on GNSS-AcquisitionAssistance supported by the UE
gnss-ID		4 (glonass)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (GLONASS)

GNSS-AcquisitionAssistance: sub-test 13

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 3
gnss-ID		0 (gps)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (GPS L1 C/A) and/or GNSS-AcquisitionAssistance (Modernized GPS L5) depending on GNSS-AcquisitionAssistance supported by the UE
gnss-ID		3 (galileo)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (Galileo E1) and/or GNSS-AcquisitionAssistance (Galileo E5A) depending on GNSS-AcquisitionAssistance supported by the UE
gnss-ID		5 (bds)
GNSS-AcquisitionAssistance		See GNSS-AcquisitionAssistance (BDS B1I) and/or GNSS-AcquisitionAssistance (BDS B1C) depending on GNSS-AcquisitionAssistance supported by the UE

6.2.7.4.7 GNSS ALMANAC:

GNSS-Almanac (GPS L1 C/A only): sub-test 1

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-Almanac
weekNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
toa		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
ioda		Not present	Not present	Not present
completeAlmanacProvided		1 (TRUE)	1 (TRUE)	1 (TRUE)
gnss-AlmanacList		(SIZE) 24	(SIZE) 24	(SIZE) 24

GNSS-AlmanacElement (GPS L1 C/A only): sub-test 1

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
keplerianNAV-Almanac		Model-2	Model-2	Model-2
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AlmanacElement (GPS L1 C/A only): sub-test 1

FFS

GNSS-Almanac (GLONASS): sub-test 2

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-Almanac
completeAlmanacProvided		1 (TRUE)	1 (TRUE)	1 (TRUE)
gnss-AlmanacList		(SIZE) 24	(SIZE) 24	(SIZE) 24

GNSS-AlmanacElement (GLONASS): sub-test 2

FFS

GNSS-AlmanacElement: keplerianGLONASS (Model-5)

GNSS-Almanac (Galileo): sub-test 3

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-Almanac
weekNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
toa		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
ioda		0	0	0
completeAlmanacProvided		1 (TRUE)	1 (TRUE)	1 (TRUE)
gnss-AlmanacList		(SIZE) 27	(SIZE) 27	(SIZE) 27

GNSS-Almanac (Galileo): sub-test 3

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
keplerianAlmanacSet		Model-1	Model-1	Model-1
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AlmanacElement (Galileo): sub-test 3

FFS

kepSV-StatusFNAV: 0. Present only if the UE supports multiple Galileo signals

GNSS-Almanac: sub-test 4

The GNSS-Almanac(s) to be used depends on the GNSS-Almanac(s) supported by the UE. The allowed GNSS-Almanacs are as follows:

GNSS-Almanac (GPS)

GNSS-Almanac (Modernized GPS Reduced)

GNSS-Almanac (Modernized GPS Midi)

GNSS-Almanac (Modernized GPS Reduced)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-Almanac
weekNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
toa		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
ioda		Not present	Not present	Not present
completeAlmanacProvided		1 (TRUE)	1 (TRUE)	1 (TRUE)
gnss-AlmanacList		(SIZE) 27	(SIZE) 27	(SIZE) 27

GNSS-AlmanacElement (Modernized GPS Reduced)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
keplerianReducedAlmanac		Model-3	Model-3	Model-3
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AlmanacElement (Modernized GPS Reduced)

FFS

GNSS-Almanac (Modernized GPS Midi)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-Almanac
weekNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
toa		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
ioda		Not present	Not present	Not present
completeAlmanacProvided		1 (TRUE)	1 (TRUE)	1 (TRUE)
gnss-AlmanacList		(SIZE) 27	(SIZE) 27	(SIZE) 27

GNSS-AlmanacElement (Modernized GPS Midi)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
keplerianMidiAlmanac		Model-4	Model-4	Model-4
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AlmanacElement (Modernized GPS Midi)

FFS

GNSS-Almanac: sub-test 5

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 2
gnss-ID		0 (gps)
GNSS-Almanac		See GNSS-Almanac (GPS) and/or GNSS-Almanac (Modernized GPS Reduced) and/or GNSS-Almanac (Modernized GPS Midi) depending on GNSS-Almanac supported by the UE
gnss-ID		4 (glonass)
GNSS-Almanac		See GNSS-Almanac (GLONASS)

GNSS-Almanac (GPS)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-Almanac
weekNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
toa		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
ioda		Not present	Not present	Not present
completeAlmanacProvided		1 (TRUE)	1 (TRUE)	1 (TRUE)
gnss-AlmanacList		(SIZE) 27	(SIZE) 27	(SIZE) 27

GNSS-AlmanacElement (GPS)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
keplerianNAV-Almanac		Model-2	Model-2	Model-2
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AlmanacElement (GPS)

FFS

GNSS-Almanac: sub-test 8

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 2
gnss-ID		0 (gps)
GNSS-Almanac		See GNSS-Almanac (GPS) and/or GNSS-Almanac (Modernized GPS Reduced) and/or GNSS-Almanac (Modernized GPS Midi) depending on GNSS-Almanac supported by the UE
gnss-ID		3 (galileo)
GNSS-Almanac		See GNSS-Almanac (Galileo)

GNSS-Almanac: sub-test 9

The GNSS-Almanac(s) to be used depends on the GNSS-Almanac(s) supported by the UE. The allowed GNSS-Almanacs are as follows:

GNSS-Almanac (BDS B1I)

GNSS-Almanac (BDS B1C Reduced)

GNSS-Almanac (BDS B1C Midi)

GNSS-Almanac (BDS B1I)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-Almanac
weekNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
toa		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
ioda		Not present	Not present	Not present
completeAlmanacProvided		1 (TRUE)	1 (TRUE)	1 (TRUE)
gnss-AlmanacList		(SIZE) 35	(SIZE) 35	(SIZE) 35

GNSS-AlmanacElement (BDS B1I)

FFS

GNSS-AlmanacElement: BDS-AlmanacSet-r12 (Model-7)

GNSS-Almanac (BDS B1C Reduced)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-Almanac
weekNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
toa		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
ioda		Not present	Not present	Not present
completeAlmanacProvided		1 (TRUE)	1 (TRUE)	1 (TRUE)
gnss-AlmanacList		(SIZE) 35	(SIZE) 35	(SIZE) 35

GNSS-AlmanacElement (BDS B1C Reduced)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
keplerianReducedAlmanac		Model-3	Model-3	Model-3
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AlmanacElement (BDS B1C Reduced)

FFS

GNSS-Almanac (BDS B1C Midi)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-Almanac
weekNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
toa		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
ioda		Not present	Not present	Not present
completeAlmanacProvided		1 (TRUE)	1 (TRUE)	1 (TRUE)
gnss-AlmanacList		(SIZE) 35	(SIZE) 35	(SIZE) 35

GNSS-AlmanacElement (BDS B1C Midi)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
keplerianMidiAlmanac		Model-4	Model-4	Model-4
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AlmanacElement (BDS B1C Midi)

FFS

GNSS-Almanac: sub-test 10

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 2
gnss-ID		0 (gps)
GNSS-Almanac		See GNSS-Almanac (GPS) and/or GNSS-Almanac (Modernized GPS Reduced) and/or GNSS-Almanac (Modernized GPS Midi) depending on GNSS-Almanac supported by the UE
gnss-ID		5 (bds)
GNSS-Almanac		See GNSS-Almanac (BDS B1I) and/or GNSS-Almanac (BDS B1C Reduced) and/or GNSS-Almanac (BDS B1C Midi) depending on GNSS-Almanac supported by the UE

GNSS-Almanac: sub-test 11

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 3
gnss-ID		0 (gps)
GNSS-Almanac		See GNSS-Almanac (GPS) and/or GNSS-Almanac (Modernized GPS Reduced) and/or GNSS-Almanac (Modernized GPS Midi) depending on GNSS-Almanac supported by the UE
gnss-ID		4 (glonass)
GNSS-Almanac		See GNSS-Almanac (GLONASS)
gnss-ID		5 (bds)
GNSS-Almanac		See GNSS-Almanac (BDS B1I) and/or GNSS-Almanac (BDS B1C Reduced) and/or GNSS-Almanac (BDS B1C Midi) depending on GNSS-Almanac supported by the UE

GNSS-Almanac: sub-test 12

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 3
gnss-ID		0 (gps)
GNSS-Almanac		See GNSS-Almanac (GPS) and/or GNSS-Almanac (Modernized GPS Reduced) and/or GNSS-Almanac (Modernized GPS Midi) depending on GNSS-Almanac supported by the UE
gnss-ID		3 (galileo)
GNSS-Almanac		See GNSS-Almanac (Galileo)
gnss-ID		4 (glonass)
GNSS-Almanac		See GNSS-Almanac (GLONASS)

GNSS-Almanac: sub-test 13

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 3
gnss-ID		0 (gps)
GNSS-Almanac		See GNSS-Almanac (GPS) and/or GNSS-Almanac (Modernized GPS Reduced) and/or GNSS-Almanac (Modernized GPS Midi) depending on GNSS-Almanac supported by the UE
gnss-ID		3 (galileo)
GNSS-Almanac		See GNSS-Almanac (Galileo)
gnss-ID		5 (bds)
GNSS-Almanac		See GNSS-Almanac (BDS B1I) and/or GNSS-Almanac (BDS B1C Reduced) and/or GNSS-Almanac (BDS B1C Midi) depending on GNSS-Almanac supported by the UE

6.2.7.4.8 GNSS UTC MODEL:

GNSS-UTC-Model: sub-tests 5, 11 and 12

Information Element	Units	Value/remark GNSS All
GNSS-UTC-Model
utcModel1		Model-1

UTC-ModelSet1: sub-tests 5, 11 and 12

Derived from data in clause 6.2.1.2 and the following information:

gnss-Utc-A1: 0

gnss-Utc-A0: 0

6.2.7.4.9 GNSS AUXILIARY INFORMATION:

GNSS-AuxiliaryInformation (GLONASS): sub-test 2

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-AuxiliaryInformation
gnss-ID-GLONASS		(SIZE) 8	(SIZE) 8	(SIZE) 8

GNSS-ID-GLONASS-SatElement (GLONASS): sub-test 2

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
signalsAvailable		G1	G1	G1
channelNumber		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AuxiliaryInformation (Modernized GPS): sub-test 4

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-AuxiliaryInformation
gnss-ID-GPS		(SIZE) 9	(SIZE) 10	(SIZE) 10

GNSS-ID-GPS-SatElement (Modernized GPS): sub-test 4

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
signalsAvailable		As supported by the UE	As supported by the UE	As supported by the UE

GNSS-AuxiliaryInformation: sub-test 8

GNSS-AuxiliaryInformation is used only if multiple GPS signals supported by the UE.

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 1 if UE supports multiple GPS signals
gnss-ID		0 (gps) if UE supports multiple GPS signals
GNSS-AuxiliaryInformation		See GNSS-AuxiliaryInformation (Modernized GPS)

GNSS-AuxiliaryInformation: sub-test 9

GNSS-AuxiliaryInformation is used only if BDS B1C is supported by the UE.

GNSS-AuxiliaryInformation (BDS B1C)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
GNSS-AuxiliaryInformation
gnss-ID-BDS-r16		(SIZE) 12	(SIZE) 9	(SIZE) 9

GNSS-ID-BDS-SatElement-r16 (BDS B1C)

Information Element	Units	Value/remark GNSS #1	Value/remark GNSS #2	Value/remark GNSS #5
svID-r16		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2
satType-r16		Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2	Derived from data in clause 6.2.1.2

GNSS-AuxiliaryInformation: sub-tests 5 and 12

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 1, or 2 if UE supports multiple GPS signals
gnss-ID		0 (gps) if UE supports multiple GPS signals
GNSS-AuxiliaryInformation		See GNSS-AuxiliaryInformation (Modernized GPS)
gnss-ID		4 (glonass)
GNSS-AuxiliaryInformation		See GNSS-AuxiliaryInformation (GLONASS)

GNSS-AuxiliaryInformation: sub-tests 10 and 13

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 1 if UE supports multiple GPS signals or BDS B1C, or 2 if UE supports multiple GPS signals and BDS B1C
gnss-ID		0 (gps) if UE supports multiple GPS signals
GNSS-AuxiliaryInformation		See GNSS-AuxiliaryInformation (Modernized GPS)
gnss-ID		5 (bds) if UE supports BDS B1C
GNSS-AuxiliaryInformation		See GNSS-AuxiliaryInformation (BDS B1C)

GNSS-AuxiliaryInformation: sub-test 11

Information Element	Units	Value/remark GNSS All
GNSS-GenericAssistData		(SIZE) 1, or 2 if UE supports multiple GPS signals or BDS B1C, or 3 if UE supports multiple GPS signals and BDS B1C
gnss-ID		0 (gps) if UE supports multiple GPS signals
GNSS-AuxiliaryInformation		See GNSS-AuxiliaryInformation (Modernized GPS)
gnss-ID		4 (glonass)
GNSS-AuxiliaryInformation		See GNSS-AuxiliaryInformation (GLONASS)
gnss-ID		5 (bds) if UE supports BDS B1C
GNSS-AuxiliaryInformation		See GNSS-AuxiliaryInformation (BDS B1C)