
Key features
R&S®SMBV-K361, R&S®SMBVB-K361, R&S®SMW-K361
5User Manual 1178.6591.02 ─ 09
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 compati-
bility of eCall in-vehicle systems with the positioning services provided by the Gali-
leo and the EGNOS systems
●United Nations regulation ECE/TRANS/WP.29/GRSG/2017/12, annex 8, Test meth-
ods 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, with-
out user interaction.
Table 1-1: Supported test cases
Test case Test purpose
1. Verify NMEA transmis-
sion from DUT
Checks that the GNSS receiver outputs the navigation parameter data to
external devices in NMEA-0183 format
2. Location accuracy (static
receiver)
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
3. Location accuracy (mov-
ing receiver) open sky
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
4. Location accuracy (mov-
ing receiver) intermitted
reception and urban can-
yon
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
5. Time-to-first fix (TTFF)
under cold start conditions
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.