4.11 GNSS Requirements for V2X and MCS testing

36.5083GPPCommon test environments for User Equipment (UE) conformance testingEvolved Universal Terrestrial Radio Access (E-UTRA) and Evolved Packet Core (EPC)Release 17TS

4.11.1 General

This clause defines the GNSS scenarios and requirements which apply for all V2X and MCS test cases that require simulated GNSS signals, unless otherwise specified.

The term SV ID used in this clause is defined as the satellite PRN for GPS and Modernized GPS, as Code Number for Galileo, as the satellite Slot Number for GLONASS and as the Ranging Code Number for BDS.

4.11.2 GNSS Scenarios

The PIXIT px_GnssScenario2012 is specified in TS 37.571-5 [68] clause 6.1.2.

If px_GnssScenario2012 = FALSE, the following GNSS scenarios shall be used.

– Rinex navigation data: the required navigation data file(s) available in the GNSS orbital data sig zip file specified in TS 37.571-5 [68] Annex B are given in Table 4.11.2-1.

Table 4.11.2-1: Rinex navigation data files for V2X and MCS testing

GNSS supported by UE

Rinex file(s) (1)

GPS

Sig GNSS GPS 2020_9_17 Rinex.txt

GLONASS

Sig GNSS GLONASS 2020_9_17 Rinex.txt

Galileo

Sig GNSS Galileo 2020_9_17 Rinex.txt

BDS

Sig GNSS BDS 2020_9_17 Rinex.txt

Note 1: Where the UE supports more than one GNSS then all the relevant Rinex navigation data files are used

– UE location(s) and motion:

Latitude: the simulated latitude(s) are given in Table 4.11.2-3

Longitude: the simulated longitude(s) are given in Table 4.11.2-3

Height: the simulated height is 30m

Motion: the simulated motion(s) are given in Table 4.11.2-2

Table 4.11.2-2: UE location(s) and motion(s) for V2X and MCS testing

Scenario number and description

Step #

Action (Location details given in Table 4.11.2-3)

Notes

Scenario #1: static in Geographical area #1 Note 1

1

Static at location #1

Scenario #2: move from inside Geographical area #1 to outside Geographical area #1 Note 1

1

Static at location #1

2

Trigger from test case to move in a straight line at 15m/s from current location to next location

Simulation leaves Geographical area #1 after 905 m, 60s after the trigger. An additional 1s is added to allow for UE position accuracy of +/- 15m. An additional 10s is added to allow for UE position update. Total time 71s

3

Static at location #2

Scenario #3: move from zone id0 to zone id1 to zone id3 to zone id2

1

Static at location #3

2

Trigger from test case to move in a straight line at 2m/s from current location to next location

Simulation crosses the boundary between zone id0 and zone id1 47s after the trigger. An additional 7.5s is added to allow for UE position accuracy of +/- 15m. An additional 10s is added to allow for UE position update. Total time 64.5s

3

Static at location #4

4

Trigger from test case to move in a straight line at 2m/s from current location to next location

Simulation crosses the boundary between zone id1 and zone id3 42s after the trigger. An additional 7.5s is added to allow for UE position accuracy of +/- 15m. An additional 10s is added to allow for UE position update. Total time 59.5s

5

Static at location #5

6

Trigger from test case to move in a straight line at 2m/s from current location to next location

Simulation crosses the boundary between zone id3 and zone id2 47s after the trigger. An additional 7.5s is added to allow for UE position accuracy of +/- 15m. An additional 10s is added to allow for UE position update. Total time 64.5s

7

Static at location #6

Scenario #4: move from inside Geographical area #1 to location #7 and then location #8 inside Geographical area #1 Note 1

1

Static at location #1

2

Trigger from test case to move in a straight line at 10m/s from current location to next location

Simulation takes approximately 10 secs to move from location #1 to location #7

3

Static at location #7

4

Trigger from test case to move in a straight line at 10m/s from current location to next location

Simulation takes approximately 10 secs to move from location #7 to location #8

5

Static at location #8

Note 1: Geographical area #1 is defined in clause 4.9.3.1 and is defined by four points with the following coordinates:

Point 1: latitude: 35.753056, longitude: 139.689167

Point 2: latitude: 35.735278, longitude: 139.689167

Point 3: latitude: 35.744167, longitude: 139.709167

Point 4: latitude: 35.753056, longitude: 139.709167

Table 4.11.2-3: Location descriptions for V2X and MCS testing

Location number

Description for information only

Latitude (degrees)

Longitude (degrees)

#1

Approximate centre of Geographical area #1

35.74428

139.69916

#2

Approximately 1720m due west of location #1, outside Geographical area #1

35.74428

139.68017

#3

Centre of zone id0 inside Geographical area #1, see Table 4.11.2-4 and Figure 4.11.2-1

35.74478

139.70333

#4

Centre of zone id1 inside Geographical area #1, see Table 4.11.2-4 and Figure 4.11.2-1

35.74478

139.70540

#5

Centre of zone id3 inside Geographical area #1, see Table 4.11.2-4 and Figure 4.11.2-1

35.74523

139.70716

#6

Centre of zone id2 inside Geographical area #1, see Table 4.11.2-4 and Figure 4.11.2-1

35.74523

139.70508

#7

Approximately 100m due west of location #1, inside Geographical area #1

35.74428

139.69806

#8

Approximately 100m due west of location #7, inside Geographical area #1

35.74428

139.69695

Table 4.11.2-4: Zone id calculations for V2X testing

Description

Latitude (degrees)

Longitude (degrees)

Long distance from 0,0 in m (x) Note 1

Lat distance from 0,0 in m (y) Note 1

Values for zone_id calculation (Nx, Ny = 2, L = 100, W = 50 Note 2) Note 3

Centre of zone id0

35.74478

139.70333

11061850

3957225

y1= 0, x1= 0

Centre of zone id1

35.74478

139.70540

11061950

3957225

y1= 0, x1= 1

Centre of zone id2

35.74523

139.70508

11061850

3957275

y1= 1, x1= 0

Centre of zone id3

35.74523

139.70716

11061950

3957275

y1= 1, x1= 1

Note 1: all distances are +/- 1m

Note 2: zone length (longitude) is set to 100m, zone width (latitude) is set to 50m in accordance with TS 36.523-1 [18] Table 24.1.8.3.3-1 and Table 24.1.9.3.3-1, this allows for the accuracy with which a UE can define its position which is assumed to be +/- 15m. Zone id longitude modulus and zone id latitude modulus are set to 2 in accordance with TS 36.523-1 [18] Table 24.1.8.3.3-1 and Table 24.1.9.3.3-1.

Note 3: zone ids are calculated according to TS 36.331 [17] clause 5.10.13.2

Figure 4.11.2-1: Zones and motions for scenario #3 for V2X testing (not to scale)

– Nominal start time:

17th September 2020 23:40:00 (GPS time)\

– Visible satellites to be simulated are given in Table 4.11.2-5 and are above 15 degrees elevation with respect to the UE. These satellites have been selected to give a reasonable HDOP for the duration of the test.

Table 4.11.2-5: Satellites to be simulated for V2X and MCS testing

GNSS supported by UE

SV IDs of Satellites to be simulated (1)

GPS

3, 4, 6, 17, 19, 28

GLONASS

3, 4, 5, 10, 18, 19

Galileo

3, 5, 13, 15, 21, 27

BDS

38, 40, 42, 43, 59, 60

Note 1: Where the UE supports more than one GNSS then all the relevant satellites are simulated

Note 2: For BDS, the satellite types are as follows: GEO: 59, 60, IGSO: 38, 40, MEO: 42, 43

As an alternative, the contents of this clause in version 16.8.0 of this current specification may be used until September 2023.

– The levels of the simulated satellites are given in Table 4.11.2-6 and shall be generated with an accuracy of +/- 3 dB. These conditions are defined for when there is no GNSS assistance data available at the UE and are specified in TS 36.133 [39] clause B.6.

Table 4.11.2-6: GNSS Reference Signal Power Requirements

System

Parameters

Unit

Value

Number of generated satellites per system

6

GPS(1)

Reference signal power level for all satellites

dBm

-128.5

Galileo

Reference signal power level for all satellites

dBm

-127

GLONASS

Reference signal power level for all satellites

dBm

-131

BDS

Reference signal power level for all satellites

dBm

-133

NOTE 1: "GPS" here means GPS L1 C/A, Modernized GPS, or both, dependent on UE capabilities.

NOTE 2: The DUT UE shall support at least one system and will be configured for the supported system(s).

– Ionospheric model: simulated values are given in Tables 4.11.2-7 and 4.11.2-8.

Table 4.11.2-7: Klobuchar ionospheric model for GPS or GLONASS or BDS if supported by the UE

Model element

Units

Value/remark

alfa0

seconds

4.6566129 10E-9

alfa1

sec/semi-circle

1.4901161 10E-8

alfa2

sec/(semi-circle)2

-5.96046 10E-8

alfa3

sec/(semi-circle)3

-5.96046 10E-8

beta0

seconds

79872

beta1

sec/semi-circle

65536

beta2

sec/(semi-circle)2

-65536

beta3

sec/(semi-circle)3

-393216

Table 4.11.2-8: neQuick ionospheric model for Galileo if supported by the UE

Model Element

Units

Value/remark

ai0

solar flux unit

64.4

ai1

solar flux unit/degree

0

ai2

solar flux unit/degree2

0

– Tropospheric model: STANAG with SRI equal to 324.8, as defined in STANAG 4294 [70].

If px_GnssScenario2012 = TRUE, the following GNSS scenarios shall be used instead.

– Yuma / Rinex Almanac data: the required file(s) available in the GNSS data sig zip file specified in TS 37.571-5 [68] Annex B are given in Table 4.11.2-1.

Table 4.11.2-9: Yuma / Rinex Almanac data files for V2X and MCS testing

GNSS supported by UE

Yuma / Rinex file(s) (1)

GPS

Sig GNSS 1-3 Yuma.txt

GLONASS

Sig GNSS 1-1 AGL.txt

Galileo

Sig GNSS 1-2 Yuma.txt

BDS

Sig GNSS 1-9 Yuma.txt

Note 1: Where the UE supports more than one GNSS then all the relevant Yuma / AGL data files are used

– Nominal start time:

1st January 2012 00:31:00 (GPS time) (UTC time: TBD).

– Visible satellites to be simulated are given in Table 4.11.2-10 and are above 15 degrees elevation with respect to the UE. These satellites have been selected to give a reasonable HDOP for the duration of the test.

Table 4.11.2-10: Satellites to be simulated for V2X and MCS testing

GNSS supported by UE

SV IDs of Satellites to be simulated (1)

GPS

1, 11, 17, 20, 23, 28

GLONASS

3, 4, 9, 10, 18, 20

Galileo

5, 10, 11, 18, 19, 20

BDS

1,2,7,18,21,27

Note 1: Where the UE supports more than one GNSS then all the relevant satellites are simulated