Rohde&Schwarz SMBV-K361, SMBVBK361, SMW-K361 User Manual

R&S®SMBV-K361, R&S®SMBVB­K361, R&S®SMW-K361
eCall Test Suite User Manual
(;ÜÏé2)
1178659102 Version 06
This manual describes the following R&S®CMWrun option for software version V1.9.9 or higher:
R&S®SMBV-K361 (eCall test suite)
R&S®SMBVB-K361 (eCall test suite)
R&S®SMW-K361 (eCall test suite)
© 2020 Rohde & Schwarz GmbH & Co. KG Mühldorfstr. 15, 81671 München, Germany Phone: +49 89 41 29 - 0 Email: info@rohde-schwarz.com Internet: www.rohde-schwarz.com Subject to change – data without tolerance limits is not binding. R&S® is a registered trademark of Rohde & Schwarz GmbH & Co. KG. Trade names are trademarks of the owners.
1178.6591.02 | Version 06 | R&S®SMBV-K361, R&S®SMBVB-K361, R&S®SMW-K361
The following abbreviations are used throughout this manual: Options R&S®SMBV-K361, R&S®SMBVB-K361, and R&S®SMW-K361 are abbreviated as R&S SMx-K361. R&S® is abbreviated as R&S. R&S®SMBV100A and R&S®SMBV100B are abbreviated as R&S SMBV.
R&S®SMBV-K361, R&S®SMBVB-K361, R&S®SMW-K361

Contents

1 Key Features...........................................................................................5
2 Prerequisites.......................................................................................... 7
3 Test Setup............................................................................................... 9
4 System Configuration..........................................................................10
4.1 Preparation of Controller PC......................................................................................10
4.2 Preparation of Instrument Connection..................................................................... 10
4.3 Preparation of IVS Connection.................................................................................. 11
5 Test Configuration............................................................................... 16
5.1 Vehicle Simulation Setting......................................................................................... 16
Contents
5.2 GNSS Simulation Setting........................................................................................... 18
5.3 Signal Power Setting.................................................................................................. 19
5.4 Test Case Setting........................................................................................................ 20
5.5 Advanced Settings......................................................................................................21
6 Test Results.......................................................................................... 25
7 Test Module Details..............................................................................27
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Contents
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1 Key Features

The test suites R&S SMx-K361 provide eCall tests with the sequencer tool R&S CMWrun. The tests are performed on a connected in-vehicle system (IVS). The tests are as closely aligned with the selected test specification as possible.
The following standards are supported:
European Union regulation 2017/79, annex VI, Technical requirements for compati­bility of eCall in-vehicle systems with the positioning services provided by the Gali­leo and the EGNOS systems
United Nations regulation ECE/TRANS/WP.29/GRSG/2017/12, annex 8, Test meth­ods for the navigation solutions
The test equipment simulates a global navigation satellite system (GNSS). The R&S CMWrun controls the test equipment via SCPI commands and the IVS typically via vendor-specific commands. The test cases can be performed fully automatic, with­out user interaction.
Table 1-1: Supported test cases
Key Features
Test case Test purpose
1. Verify NMEA transmis­sion from DUT
2. Location accuracy (static receiver)
3. Location accuracy (mov­ing receiver) open sky
4. Location accuracy (mov­ing receiver) intermitted reception and urban can­yon
5. Time-to-first fix (TTFF) under cold start conditions
Checks that the GNSS receiver outputs the navigation parameter data to external devices in NMEA-0183 format
Estimates the error in the evaluation of the plane view and altitude in the autonomous static mode. A static location is simulated and the error between actual and determined location is calculated
Estimates the error in the evaluation of the plane view, altitude and velocity in the dynamic mode. A certain trajectory is simulated and the error between actual and determined location as well as the velocity error is calculated
Estimates the error in the evaluation of the plane view, altitude and velocity in the dynamic mode with signal impairments. A certain trajectory is simulated, signal is faded and partly blocked. The velocity error and the error between actual and determined location as well as the velocity error is calculated
Determines the time to first navigation fix for a reset receiver. The ephemeris and almanac data from all satellites are cleared and thus, the receiver has to gain all data and the time to first fix is measured. One measurement step comprises signal acquisition at the TX level of -130 dBm and the cold start of the DUT, until it can acquire the signal again. The cold start is executed with specified repetitions. The same is executed with the TX level of -140 dBm. The averaged measurement time must not exceed 60 s for the signal level of
-130 dBm and 300 s the signal level of -140 dBm.
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Test case Test purpose
6. Reacquisition time Evaluates the restore time for signal tracking for a certain GNSS constella­tion after tracking was lost due to signal blockage. To simulate blockage, the radio frequency signal is switched off for a specified time and the recovery time is measured after the signal was switched on. One measurement step comprises signal off, signal on, until the DUT can acquire the signal again. Each step is executed with specified repetitions.
Key Features
7. Tracking and acquisition
sensitivity
Verifies the sensitivity of the GNSS navigation module in signal acquisition mode and in tracking mode. The acquisition time is measured with the signal level of -144 dBm. The tracking time is measured with the signal level of
-155 dBm. The reacquisition time is measured after configurable signal blockage with the signal level of -150 dBm. The acquisition, tracking and reacquisition time must be within the required limits of ≦3600 s for T ≧600 s for T
, and 60 s for T
Tracking
Reacquisition
.
Acquisition
,
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2 Prerequisites

Required equipment for R&S SMBV-K361:
R&S SMBV100A for GNSS simulation must be equipped with the following options: Hardware: – HW option R&S SMBV-B10 – HW option R&S SMBV-B103/-B106 Minimum required options: – R&S SMBV-K44, GPS – R&S SMBV-K66, Galileo – R&S SMBV-K91, extension to 12 satellites – R&S SMBV-K92, GNSS enhanced (motion files, atmospheric effects) – R&S SMBV-K96, extension to 24 satellites – R&S SMBV-K110, SBAS Additional options for full test coverage: – R&S SMBV-K102, antenna pattern and R&S SMBV-K103, spinning and attitude
simulation for test location accuracy with moving receiver - intermitted recep­tion and urban canyon (test case 4)
R&S SMBV-K94, GLONASS for testing in line with UN specification (test cases
1 to 7)
R&S CMWrun base software, version 1.8.10 or higher. No smart card and no licenses are required for R&S CMWrun.
Prerequisites
Required equipment for R&S SMBVB-K361:
R&S SMBV100B for GNSS simulation must be equipped with the following options: Hardware: – HW option R&S SMBVB-B103 Minimum required options: – R&S SMBVB-K520 real-time extension – R&S SMBVB-K44, GPS – R&S SMBVB-K66, Galileo – R&S SMBVB-K106, SBAS Additional options for full test coverage: – R&S SMBVB-K108, antenna pattern, spinning and attitude simulation for test
location accuracy with moving receiver - intermitted reception and urban can­yon (test case 4)
R&S SMBVB-K94, GLONASS for testing in line with UN specification (test
cases 1 to 7)
R&S CMWrun base software, version 1.9.6 or higher. No smart card and no licenses are required for R&S CMWrun.
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Required equipment for R&S SMW-K361:
R&S SMW200A for GNSS simulation must be equipped with the following options: Hardware: – HW option R&S SMW-B10 – HW option R&S SMW-B103/-B203 Minimum required options: – R&S SMW-K44, GPS – R&S SMW-K66, Galileo – R&S SMW-K106, SBAS Additional options for full test coverage: – R&S SMW-K108, antenna pattern, spinning and attitude simulation for test
location accuracy with moving receiver - intermitted reception and urban can­yon (test case 4)
R&S SMW-K94, GLONASS for testing in line with UN specification (test cases
1 to 7)
R&S CMWrun base software, version 1.9.5 or higher. No smart card and no licenses are required for R&S CMWrun.
Prerequisites
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3 Test Setup

The following figure provides an overview of the test setup. In this example, the instru­ment R&S SMBV100A is used. The test setup with another supported instrument is similar.
Test Setup
The test setup comprises the following components:
An instrument, providing GNSS signals to the IVS for positioning. Connect the RF output port of the instrument to the RF port of the IVS (GNSS receiver).
A computer executing the R&S CMWrun. The computer controls the instrument via SCPI connections (typically LAN). It con­trols the IVS typically via vendor-specific commands on a serial port interface.
External attenuator is recommended for levels below -120 dBm, refer to "External
Power Attenuation" on page 19.
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