GNSS simulation for Rohde & Schwarz signal generators Specifications

Transcription

1 GNSS simulation for Rohde & Schwarz signal generators Specifications R&S SMW200A vector signal generator Data Sheet Version 02.00

2 CONTENTS Definitions... 3 Overview... 4 Abbreviations... 4 Minimum hardware configuration... 4 Signals and systems... 5 Key features... 5 Common specifications for all GNSS options... 6 Simulation configuration... 6 Simulation monitoring... 8 Simulation data logging... 8 Allocation of GNSS channels... 9 General rules... 9 Configuration examples Specifications for GNSS options GPS (R&S SMW-K44 option) Modernized GPS (R&S SMW-K98 option) Galileo (R&S SMW-K66 option) Glonass (R&S SMW-K94 option) BeiDou (R&S SMW-K107 option) SBAS/QZSS (R&S SMW-K106 option) Extension to 48 channels per baseband (R&S SMW-K99 option) Real world scenarios (R&S SMW-K108 option) Realtime GNSS interfaces (R&S SMW-K109 option) Advanced GNSS applications (R&S SMW-K120 option) Ordering information Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators

3 Definitions General Product data applies under the following conditions: Three hours storage at ambient temperature followed by 30 minutes warm-up operation Specified environmental conditions met Recommended calibration interval adhered to All internal automatic adjustments performed, if applicable Specifications with limits Represent warranted product performance by means of a range of values for the specified parameter. These specifications are marked with limiting symbols such as <,, >,, ±, or descriptions such as maximum, limit of, minimum. Compliance is ensured by testing or is derived from the design. Test limits are narrowed by guard bands to take into account measurement uncertainties, drift and aging, if applicable. Specifications without limits Represent warranted product performance for the specified parameter. These specifications are not specially marked and represent values with no or negligible deviations from the given value (e.g. dimensions or resolution of a setting parameter). Compliance is ensured by design. Typical data (typ.) Characterizes product performance by means of representative information for the given parameter. When marked with <, > or as a range, it represents the performance met by approximately 80 % of the instruments at production time. Otherwise, it represents the mean value. Nominal values (nom.) Characterize product performance by means of a representative value for the given parameter (e.g. nominal impedance). In contrast to typical data, a statistical evaluation does not take place and the parameter is not tested during production. Measured values (meas.) Characterize expected product performance by means of measurement results gained from individual samples. Uncertainties Represent limits of measurement uncertainty for a given measurand. Uncertainty is defined with a coverage factor of 2 and has been calculated in line with the rules of the Guide to the Expression of Uncertainty in Measurement (GUM), taking into account environmental conditions, aging, wear and tear. Device settings and GUI parameters are indicated as follows: parameter: value. Typical data as well as nominal and measured values are not warranted by Rohde & Schwarz. Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators 3

4 Overview With the GNSS simulator solution for the R&S SMW200A, dynamic scenarios with GPS/SBAS/QZSS, Galileo, Glonass and BeiDou signals can be generated in realtime including moving scenarios, multipath, dynamic power control and atmospheric modeling. For moving scenarios, the effects of antenna pattern and vehicle body mask can be simulated in realtime with dynamic variation of the vehicle s attitude. The R&S SMW200A can be equipped with several basebands and RF outputs. This allows to simulate complex coexistence scenarios to test the receiver s resilience against unwanted interference or jamming attacks. Above and beyond GNSS signal generation, the R&S SMW200A is a flexible vector signal generator with excellent RF performance. It offers options for generating standard-compliant signals for all important digital communications standards (GSM, WCDMA, HSPA+, LTE, WiMAX TM, WLAN, etc.) and radio standards (DAB, Sirius XM Satellite Radio, HD Radio TM, FM stereo). This versatility allows mobile phone or car infotainment system manufacturers that integrate GNSS modules into their products to test the GNSS functionality and the normal functionality of their products with only one instrument. This document contains the functional specifications of the GNSS-related software options for the R&S SMW200A: R&S SMW-K44 GPS R&S SMW-K98 Modernized GPS R&S SMW-K66 Galileo R&S SMW-K94 Glonass R&S SMW-K107 BeiDou R&S SMW-K106 SBAS/QZSS R&S SMW-K99 Extension to 48 GNSS channels per baseband R&S SMW-K108 Real world scenarios R&S SMW-K109 Realtime GNSS interfaces R&S SMW-K120 Advanced GNSS applications For information on other digital standards or signal quality such as phase noise or spurious, see the following Rohde & Schwarz documents: R&S SMW200A data sheet, PD R&S SMW200A product brochure, PD Digital Standards for Signal Generators data sheet, PD Abbreviations The following abbreviations are used in this document: The R&S SMW-K44 is referred to as K44 The R&S SMW-K98 is referred to as K98 The R&S SMW-K66 is referred to as K66 The R&S SMW-K94 is referred to as K94 The R&S SMW-K107 is referred to as K107 The R&S SMW-K106 is referred to as K106 The R&S SMW-K99 is referred to as K99 The R&S SMW-K108 is referred to as K108 The R&S SMW-K109 is referred to as K109 The R&S SMW-K120 is referred to as K120 Minimum hardware configuration The following minimum hardware configuration is required for the R&S SMW200A as a prerequisite for testing GNSS functionality: R&S SMW-B103 R&S SMW-B13 R&S SMW-B10 frequency option, RF path A, 100 khz to 3 GHz signal routing and baseband main module, one I/Q path to RF baseband generator with ARB (64 Msample) and realtime coder, 120 MHz RF bandwidth WiMAX Forum is a registered trademark of the WiMAX Forum. WiMAX, the WiMAX Forum logo, WiMAX Forum Certified, and the WiMAX Forum Certified logo are trademarks of the WiMAX Forum. 4 Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators

5 Signals and systems System Frequency band Supported signals Option GNSS GPS L1 L2 C/A code, P code C/A code, P code, L2C R&S SMW-K44 R&S SMW-K98 (for L2C) Glonass L1 C/A code R&S SMW-K94 L2 C/A code Galileo E1 OS data/pilot R&S SMW-K66 BeiDou B1 B1-I R&S SMW-K107 B2 B2-I SBAS QZSS L1 C/A code R&S SMW-K106 WAAS L1 C/A code R&S SMW-K106 EGNOS L1 C/A code R&S SMW-K106 MSAS L1 C/A code R&S SMW-K106 GAGAN L1 C/A code R&S SMW-K106 Key features Support of all global satellite navigation (GNSS) and satellite-based augmentation systems (SBAS) 24 to 144 GNSS channels GNSS signals can be routed to 4 RF outputs Supported hardware for RF path 3 and 4: R&S SGT100A Automatic configuration of connected RF path extensions Support of multi-constellation, multi-frequency GNSS simulations Simulation of up to 4 antennas and up to 2 independent vehicles for high-end multi-antenna and multi-vehicle GNSS applications Static and dynamic GNSS scenarios Moving receiver simulations based on predefined and user-defined waypoints with additional support of NMEA and KML files and waypoint smoothing using vehicle description files Interactive power control of individual satellites Simulation of up to 7 internal interferer sources in addition to the GNSS signals for complex coexistence scenarios to test the receiver s resilience against unwanted interference or jamming attacks Optional internal noise generator Integrated GNSS simulation software with user-friendly simulation configuration, monitoring and interactive control capabilities using the instrument s large touchscreen Logging of user motion and satellite-related parameters Scenario generation can be fully automated using extensive remote control capabilities via Ethernet, USB or GPIB Support of A-GNSS test scenarios, including generation of A-GNSS assistance data Realistic GNSS scenarios with consideration of Orbit perturbations and clock errors Tropospheric and ionospheric effects Signal obscuration and multipath Antenna gain and phase patterns User trajectories with consideration of vehicle attitude Pseudorange steps and ramps for RAIM testing Measured worst case pseudorange accuracy < 10 cm (RMS) High hardware update rate of 100 Hz Simulations with high signal dynamics (velocities up to m/s 1, accelerations up to 1600 m/s², jerk up to 400 m/s³) Hardware-in-the-loop (HIL) realtime feed of vehicle s motion and attitude data (position, velocity, acceleration and jerk), configurable HIL streaming rate of up to 100 Hz HIL execution synchronous to 1 PPS with 20 ms system latency 1 Requires R&S SMW-B10F (subject to export restrictions); the standard baseband hardware (R&S SMW-B10) supports velocities up to 599 m/s. Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators 5

6 Common specifications for all GNSS options Simulation configuration Simulation time flexible date and time (UTC) or GNSS resolution of 1 ms system time configuration leap second simulation Simulation modes/test modes tracking signal generation with constant or custom Doppler profiles for individual satellites navigation simulation of receiver positioning with realistic Doppler profiles relative to the motion of satellites and simulated user receiver Coordinate systems for configuring static locations or user trajectories ECEF WGS84 PZ altitude: m to m in steps of 0.1 m latitude: 90 to +90 in steps of longitude: 180 to +180 in steps of Trajectory configuration waypoint files with multiple formats XTD (proprietary trajectory format, see user manual for format description), KML, NMEA formats possibility to smooth the trajectory depending on vehicle dynamics Constellation configuration and navigation data sources default constellations available that will be internally extrapolated for different simulation start times data can be imported from multiple publicly available file formats RINEX, YUMA, SEM, AGL, XML Channel selection criteria satellite visibility time automatic exchange of invisible satellites with visible ones, with preference to those with longest visibility duration at the current position Visible satellites can be turned off and on without interrupting the simulation. satellite elevation same as above, with preference on satellites of higher elevation manual The satellites can be arbitrarily turned on and off without any automatic exchange. Elevation mask earth tangent, local horizon excludes satellites below a specific elevation; range: 10 to +90 Tropospheric models none possibility of removing troposphere errors STANAG STANAG Doc MOPS 229D minimum operational performance standard for GPS/SBAS airborne equipment Ionospheric models none possibility of removing ionosphere errors STANAG STANAG Doc NeQuick NeQuick ionosphere model MOPS 229D minimum operational performance standard for GPS/SBAS airborne equipment Satellite vehicle parameters state switch satellites on/off, modifiable on-the-fly 6 Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators

7 Power configuration reference power received power per signal assuming all offsets are zero (setting range: 145 dbm to 20 dbm) satellite vehicle power offset attenuation for all signals transmitted from a single satellite, modifiable on-the-fly free space path-loss automatically calculated attenuation due to the line of sight distance between transmit and receive antenna signal power offset additional attenuation of a specific signal ( 21 db to 0 db, updated in realtime without restarting the simulation) Connectivity Marker Triggering pseudorange errors in navigation mode constant signal dynamics in tracking mode high order signal dynamics in tracking mode see R&S SMW200A data sheet, I/Q baseband generator section constant bias, modifiable on-the-fly profile (steps, ramps): suitable for testing receiver autonomous integrity monitoring (RAIM) synced to corrections broadcasted in SBAS: The ionosphere errors will match the MOPS Grid broadcasted by SBAS. Moreover, for GPS satellite, the deviation between the simulated orbits and clock and those broadcasted by the satellites will match the amount of differential correction broadcasted in SBAS message about the individual GPS SVs. pseudorange (0 to km) pseudorange rate ( 100 km/s to 100 km/s) carrier Doppler is coupled with pseudorange rate initial carrier phase: 0 to 2π rad periodic profiles with acceleration, constant velocity and deceleration 1 PPS 1 PP2S 10 PPS pulse pattern on/off ratio trigger Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators 7

8 Simulation monitoring Sky view available in test mode navigation shows the distribution of GNSS satellites in the sky Power view available in test mode navigation and tracking bar plot visualizing the signals power levels Satellite vehicle trajectory available in test mode navigation azimuth/elevation of individual SVs over 24 h relative to simulation start World map available in test mode navigation shows the simulated user position on a world map Map view available in test mode navigation shows the currently simulated user position along with a preview of the full trajectory Vehicle dynamics available in test mode navigation visualizes position, velocity and attitude information (heading, elevation and bank) in the form of an artificial horizon Hardware channels view available in test mode navigation and tracking visualizes the assignment of each GNSS signal in the hardware channels and its corresponding power (dbm) Each signal represents a unique combination of: vehicle antenna band multipath-ray signal type Simulation data logging Logging mode real-time log, offline log logs simulation data during the currently running simulation simulation run is performed as fast as possible without producing an RF signal for fast generation of logging data Log types satellite data elapsed time, UTC date and time, system/svid, elevation, azimuth, ECEF XYZ position [m], ECEF XYZ velocity [m/s], ECEF XYZ acceleration in [m/s 2 ], clock bias [m] signal level [dbm] range, pseudorange [m] range, pseudorange rates [m/s] pseudorange bias [m] pseudorange bias rate [m/s] Doppler shift [Hz] carrier phase [deg] tropospheric, ionospheric delays [m] vehicle motion elapsed time, UTC date and time latitude [deg] longitude [deg] altitude [m] position XYZ [m] velocity XYZ [m/s] acceleration XYZ [m/s 2 ] jerk XYZ [m/s 3 ] position east, north, upper [m] velocity east, north, upper [m/s] ground speed [m/s] attitude rate yaw, pitch, roll [deg] attitude rate yaw, pitch, roll [deg/s] attitude acceleration yaw, pitch, roll [deg/s 2 ] attitude jerk yaw, pitch, roll [deg/s 3 ] GDOP, PDOP, HDOP,VDOP,TDOP visible SVs 8 Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators

9 Allocation of GNSS channels General rules One channel is equivalent to a single signal component transmitted by a single satellite, e.g. GPS-L1C/A of SVID 1. This also means that for an SV transmitting two signals (such as GPS L1 C/A and GPS L2 C/A), two GNSS channels are required. 24 channels will be available when installing the first of the following basic GNSS options: R&S SMW-K44, R&S SMW-K98, R&S SMW-K66, R&S SMW-K94, R&S SMW-K107. All basic GNSS options can be installed twice (provided that two R&S SMW-B10(F) are available on the R&S SMW200A); if installed twice, the signals from that GNSS options can be used in baseband 1 and baseband GNSS channels are available in baseband 1, another 24 channels can be generated with baseband 2. When more than one basic option are used in the same baseband the total number of channels does not increase. Example: when licenses for GPS, Glonass, Galileo and BeiDou are installed in one baseband, the number of available GNSS channels is still 24. The number of available channels per baseband can be increased by installing the channel extension option R&S SMW-K99 (can be installed twice). For each installed extension option R&S SMW-K99, one baseband stream is extended from 24 to 48 channels. Restrictions apply when either GPS P code or L2C is enabled (see table below). The number of available SVs per system for a given instrument configuration depends on what constellations are active and what signals are to be simulated. Example: If GPS is the only active constellation, all available channels can be used for generating GPS L1 C/A signals; in this case, the number of available SVs equals the number of available channels. When simulating GPS L1 C/A and P code at the same time, the number of available SVs decreases as two channels per SVs are needed. Possible combinations of the basic GNSS options with the R&S SMW-K99 and R&S SMW-K120 options Without channel extension option R&S SMW-K99 With channel extension option R&S SMW-K99 (1 ) With channel extension option R&S SMW-K99 (2 ) One basic GNSS option without option R&S SMW-K120 one stream (vehicle, antenna, band) 24 channels where at most 12 channels can support GPS P code one stream (vehicle, antenna, band) 48 channels where at most 24 channels can support P code not supported Two or more basic GNSS options without option R&S SMW-K120 2 separate streams (vehicle, antenna, band) 2 24 channels where at most 2 12 channels can support GPS P code 2 separate streams (vehicle, antenna, band) channels where at most channels can support P code 2 separate streams (vehicle, antenna, band) 2 48 channels where at most 2 24 channels can support P code Two or more basic GNSS options with option R&S SMW-K120 up to 4 coupled streams (vehicle, antenna, band) total of 96 channels where at most 48 channels can support GPS P code not supported up to 4 streams (vehicle, antenna, band) total of 144 channels if no P code or L2C signals are enabled total of 96 channels if P code or L2C, where at most 48 channels can support P code Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators 9

10 Configuration examples 1 B10(F) + 1 K44 System GPS Signal L1 C/A Channel budget 24 SVs 24 1 B10(F) + 1 K K99 System GPS Signal L1 C/A Channel budget 48 SVs 37 (all possible PRNs) Note: The number of SVs is usually limited by the visibly in the navigation mode. Nevertheless, the channel budget might be higher in case of multipath simulation. 1 B10(F) + 1 K K K K107 System GPS Galileo Glonass BeiDou Signal L1CA L1CA B1 Channel budget SVs Total Note: As long as the total number of available channels is not exceeded, the SV/channel allocation can vary, e.g. 8 GPS + 4 Galileo + 7 Glonass + 5 BeiDou (this is also valid for the examples below). 1 B10(F) + 1 K K K K K99 System GPS Galileo Glonass BeiDou Signal L1CA L1CA B1 Channel budget SVs Total 2 B10(F) + 1 K K K120 (example with 4 streams, 2 RF bands and 2 antennas) System GPS Signal L1CA L2C Stream 1 channel budget (Antenna 1) Stream 2 channel budget (Antenna 1) Stream 3 channel budget (Antenna 2) Stream 4 channel budget (Antenna 2) SVs Total 2 B10(F) + 2 K K K120 (example with 4 streams, 2 RF bands and 2 antennas) System GPS Signal L1CA L1P L2C L2P Stream 1 channel budget (Antenna 1) Stream 2 channel budget (Antenna 1) Stream 3 channel budget (Antenna 2) Stream 4 channel budget (Antenna 2) SVs Total 2 B10(F) + 2 K K K K K K120 (example with 2 streams, 2 RF bands) System GPS Glonass BeiDou SBAS Signal L1CA L1P L2C L2P L1CA L2CA B1 B2 L1CA Stream 1 channel budget Stream 2 channel budget SVs Total 10 Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators

11 Specifications for GNSS options GPS (R&S SMW-K44 option) GPS in line with ICD-GPS-200 revision H Simulation configuration/monitoring/logging see Common specifications for all GNSS options section Channel budget see Channel budget section Frequency bands L1, L2 Center frequencies MHz, MHz Signals C/A code, P code Max. number of SVs 24 (37 with K99) Navigation data format LNAV Space vehicles PRNs 1 to 37 Modernized GPS (R&S SMW-K98 option) GPS in line with ICD-GPS-200 revision H Simulation configuration/monitoring/logging see Common specifications for all GNSS options section Channel budget see Channel budget section Frequency bands L2 Center frequencies MHz Signals L2C Max. number of SVs 24 (37 with K99) Navigation data format CNAV Space vehicles PRNs 1 to 37 Galileo (R&S SMW-K66 option) Galileo in line with OS SIS ICD, E1 band Simulation configuration/monitoring/logging see Common specifications for all GNSS options section Channel budget see Channel budget section Frequency bands E1 Center frequencies MHz Signals E1 open service Max. number of SVs 24 (30 with K99) Navigation data format I/NAV Space vehicles PRNs 1 to 30 Glonass (R&S SMW-K94 option) Glonass in line with Glonass ICD version 5.0 Simulation configuration/monitoring/logging see Common specifications for all GNSS options section Channel budget see Channel budget section Frequency bands L1, L2 Center frequencies MHz, MHz Signals coarse/acquisition C/A code Max. number of SVs 24 Navigation data format Glonass NAV Space vehicles PRNs 1 to 24 BeiDou (R&S SMW-K107 option) BeiDou in line with BDS-SIS-ICD-BI-2.0 Simulation configuration/monitoring/logging see Common specifications for all GNSS options section Channel budget see Channel budget section Frequency bands B1, B2 Center frequencies MHz, MHz Orbits GSO, IGSO, MEO Signals B1 I (GSO), B1 I (Non-GSO), B2 I (GSO), B2 I (Non-GSO), Max. number of SVs 24 (35 with K99) Navigation data format D1 NAV, D2 NAV Space vehicles PRNs 1 to 35 Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators 11

12 SBAS/QZSS (R&S SMW-K106 option) Requires the R&S SMW-K44 option. SBAS in line with: DO-229D, minimum operational performance standard for global positioning system/wide area augmentation system airborne equipment Simulation configuration/monitoring/logging see Common specifications for all GNSS options section Channel budget see Channel budget section Frequency bands L1 Center frequencies MHz Signals coarse/acquisition C/A code Max. number of SVs 5 Navigation data format SBAS-L1-NAV Regional systems WAAS EGNOS MSAS GAGAN Space vehicles PRN: 120, 124, 126, 131, 136, 122, 133, 134, 135, 138, 129, 137 Differential corrections automatically generated The broadcasted corrections reflect the simulated errors in the GNSS constellation: Ionosphere model, pseudorange error, orbit and clock deviations. Message types replay of historical data with possibility to edit almanac ephemeris time conversion to UTC ionosphere corrections PRN mask fast corrections long-term corrections degradation parameters clock and ephemeris covariance matrix loading of downloaded daily data from EGNOS and WAAS FTP servers: EGNOS message server EMS format and WAAS real-time data NSTB format. MSAS and GAGAN raw data are not supported. Optionally the ionosphere model pseudo-range error GPS satellite can be synchronized to the imported data. MT 17 MT 9 MT 12 MT 18 and 26 MT 1 MT 2, 3, 4, 5, 6 and 24 MT 25 and 24 MT 7 and 10 MT 28 QZSS in line with IS-QZSS V1.6 Simulation configuration/monitoring/logging see Common specifications for all GNSS options section Channel budget see Channel budget section Frequency bands L1 Center frequencies MHz Signals coarse/acquisition C/A code Max. number of SVs 5 Navigation data format QZSS-L1-NAV Space vehicles PRN: 193, 194, 195, 196, Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators

13 Extension to 48 channels per baseband (R&S SMW-K99 option) Extends the number of available channels per baseband to 48. For more detailed information on available number of channels for different instrument configurations, please see Allocation of GNSS channel section. Requires at least one GNSS option (R&S SMW- K44 or R&S SMW-K98 or R&S SMW-K66 or R&S SMW-K94 or R&S SMW-K107) and can be installed twice. Real world scenarios (R&S SMW-K108 option) This option adds the following simulation features to the basic options R&S SMW-K44, R&S SMW-K98, R&S SMW-K66, R&S SMW-K94, R&S SMW-K107 or R&S SMW-K106: Receiver antenna pattern and body mask maximum of one active antenna per option four configurable antennas, two of them can be activated antenna to vehicle attitude offsets e.g. if the antenna frame is not aligned with the vehicle body frame. Note that antenna to vehicle position offsets are available in the basic options. Separate files can be used for antenna patterns and body masks. XML file format with a resolution down to 1 (see user manual for format description) Receiver attitude (heading, elevation and bank) constant The vehicle will remain in the same orientation with respect to the earth-fixedearth-centered (ECEF) frame. from file The vehicle will change attitude with a resolution up to the hardware update rate. The values are imported from an external file. spinning The vehicle will change bank at constant rate defined by the user (max. 50 Hz). Receiver environment static multipath user-defined initial code phase, code phase drift, power offset, initial carrier phase, Doppler shift, elevation/azimuth angles of arrival Realtime GNSS interfaces (R&S SMW-K109 option) This option adds the following simulation features to the basic options R&S SMW-K44, R&S SMW-K98, R&S SMW-K66, R&S SMW-K94, R&S SMW-K107 or R&S SMW-K106: Realtime trajectory feed Realtime attitude feed Spinning Streaming rate Latency realtime feed of vehicle motion data (position, velocity, acceleration and jerk) for hardware in the loop applications realtime feed of vehicle attitude data (yaw, pitch and roll) for hardware in the loop applications up to 100 Hz up to 100 Hz down to 20 ms Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators 13

14 Advanced GNSS applications (R&S SMW-K120 option) Requires the R&S SMW-B10(F) option (2 ), the R&S SMW-B13T option and least any two of the following GNSS options: R&S SMW-K44, R&S SMW-K98, R&S SMW-K66, R&S SMW-K94, R&S SMW-K107. It will augment these options with the following features: Baseband coupling turns the R&S SMW200A into a pure GNSS simulator with a GNSS GUI controlling the complete scenario and the entire instrument allows direct and easy scenario configuration for up to 4 coupled GNSS streams The following stream configurations/scenarios are possible: multi-frequency scenarios with L1 (stream 1) and L2 (stream 2) multi-antenna scenarios with up to 4 antennas (antenna 1 on stream 1, antenna 2 on stream 2, antenna 3 on stream 3, antenna 4 on stream 4) multi-vehicle scenarios with up to 2 vehicles (vehicle 1 on stream 1, vehicle 2 on stream 2); stream 3 and 4 can be used for simulating signals in a different frequency band or simulating two antennas per vehicle. max. number of channels for all streams: 144 (requires 2 R&S SMW-K99); max. number of SVs per scenario: 48 (requires 2 R&S SMW-K99) 14 Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators

15 Ordering information R&S SMW-Bxxx = hardware option R&S SMW-Kxxx = software/key code option Designation Type Order No. Vector Signal Generator, R&S SMW200A including power cable and quick start guide Minimum hardware configuration for GNSS Frequency Option, RF path A, 100 khz to 3 GHz R&S SMW-B Signal Routing and Baseband Main Module, R&S SMW-B one I/Q path to RF Baseband Generator with ARB (64 Msample) and realtime R&S SMW-B coder, 120 MHz RF bandwidth Baseband Generator with ARB (64 Msample) and realtime coder, 120 MHz RF bandwidth, supporting high signal dynamics R&S SMW-B10(F) Recommended hardware configuration for multi-frequency GNSS Frequency Option, RF path A, 100 khz to 3 GHz R&S SMW-B Frequency Option, RF path B, 100 khz to 3 GHz R&S SMW-B Signal Routing and Baseband Main Module, R&S SMW-B13T two I/Q paths to RF Baseband Generator with ARB (64 Msample) and realtime R&S SMW-B coder, 120 MHz RF bandwidth (2 ) Additional configuration options for GNSS Phase Coherence R&S SMW-B Additive White Gaussian Noise (AWGN) R&S SMW-K Multiple Entities (for coexistence tests) R&S SMW-K Software options for GNSS GPS R&S SMW-K Modernized GPS R&S SMW-K Galileo R&S SMW-K Glonass R&S SMW-K Extension to 48 GNSS channels per baseband R&S SMW-K BeiDou R&S SMW-K SBAS/QZSS R&S SMW-K Real World Scenarios R&S SMW-K Realtime GNSS interfaces R&S SMW-K Advanced GNSS Applications R&S SMW-K Recommended extras 19" Rack Adapter R&S ZZA-KN Cable for connecting Rohde & Schwarz digital baseband R&S SMU-Z interfaces USB Serial Adapter for RS-232 remote control R&S TS-USB Documentation Documentation of Calibration Values R&S DCV R&S SMW200A DAkkS Calibration (ISO 17025, ISO 9000) R&S SMW200ADKD Rohde & Schwarz GNSS simulation for Rohde & Schwarz signal generators 15

16 Service that adds value Worldwide Local and personalized Customized and flexible Uncompromising quality Long-term dependability Rohde & Schwarz The Rohde & Schwarz electronics group offers innovative solutions in the following business fields: test and measurement, broadcast and media, secure communications, cybersecurity, monitoring and network testing. Founded more than 80 years ago, the independent company which is headquartered in Munich, Germany, has an extensive sales and service network with locations in more than 70 countries. Sustainable product design Environmental compatibility and eco-footprint Energy efficiency and low emissions Longevity and optimized total cost of ownership Certified Quality Management ISO 9001 Certified Environmental Management ISO Rohde & Schwarz GmbH & Co. KG Rohde & Schwarz training Regional contact Europe, Africa, Middle East North America TEST RSA ( ) customer.support@rsa.rohde-schwarz.com Latin America customersupport.la@rohde-schwarz.com Asia Pacific customersupport.asia@rohde-schwarz.com China customersupport.china@rohde-schwarz.com R&S is a registered trademark of Rohde & Schwarz GmbH & Co. KG Trade names are trademarks of the owners PD Version April 2018 (fi) GNSS simulation for Rohde & Schwarz signal generators Data without tolerance limits is not binding Subject to change 2018 Rohde & Schwarz GmbH & Co. KG Munich, Germany PDP 1 en