The following abbreviations are used throughout this manual: R&S®SMW200A is abbreviated as R&S SMW, R&S®WinIQSIM2TM is
abbreviated as R&S WinIQSIM2; the license types 02/03/07/11/12/13/16 are abbreviated as xx.
ContentsSatellite Navigation
Contents
1Welcome to the GNSS options............................................................. 9
The R&S SMW-K44/-K66/-K94/-K97/-K98/-K106/-K107/-K108/-K109/-K132/-K134/K135/-K136/-K137/-K138/-K139 are firmware applications that add functionality to generate signals in accordance with GPS, Galileo, GLONASS, NavIC, QZSS and COMPASS/BeiDou navigation systems and SBAS augmentation systems.
This user manual contains a description of the functionality that the application provides, including remote control operation.
All functions not discussed in this manual are the same as in the base unit and are
described in the R&S SMW user manual. The latest version is available at:
www.rohde-schwarz.com/manual/SMW200A
Installation
You can find detailed installation instructions in the delivery of the option or in the
R&S SMW service manual.
●Notes on screenshots............................................................................................. 14
1.1Key features
The global navigation satellite system (GNSS) solution for the R&S SMW is suitable for
R&D lab tests or production tests. Supported are all possible scenarios, from simple
setups with individual satellites all the way to flexible scenarios generated in real time.
Real-time scenarios offer simulation of up to several hundred satellites for navigation
systems GPS, Galileo, GLONASS, BeiDou, NavIC and QZSS depending on the installed options.
Key features
The GNSS options key features are:
●
Support of multiple GNSS and regional navigation satellite systems (RNSS) and
signals including mixed constellations (Table 1-1)
●
Support of satellite-based augmentation systems (SBAS) and signals including
mixed constellations (Table 1-2)
●
Configuring the state of a particular signal component individually
●
Real-time simulation of mixed constellations and unlimited simulation time
●
Flexible scenario generation including moving scenarios, dynamic power control
and atmospheric modeling
9User Manual 1178.6379.02 ─ 13
Welcome to the GNSS optionsSatellite Navigation
Key features
●
Configuration of realistic user environments, including obscuration and multipath,
antenna characteristics and vehicle attitude
●
Navigation test mode for satellite constellation simulation, position fixing and time
to first fix (TTFF) testing
●
Tracking test mode for signal acquisition and tracking tests
●
Simulation of orbit perturbations and pseudorange errors
●
Support of ranging, correction and integrity services for SBAS
●
Configuration suitable for basic receiver testing using signals with zero, constant or
varying Doppler profiles
●
Common configuration of multi-frequency GNSS scenarios
●
Support of assisted GNSS test scenarios, including generation of assistance data
for GPS, Galileo, GLONASS and BeiDou
●
Logging of user motion and satellite-related parameters
●
Real-time external trajectory feed for hardware in the loop (HIL) applications
●
High signal dynamics, simulation of spinning vehicles to support aerospace and
defense applications
Table 1-1: Supported GNSS/RNSS, frequency bands and signals
GNSS/RNSSL1 bandL2 bandL5 band
GPSC/A, PC/A, P, L2CL5
GalileoE1E6E5a, E5b
GLONASS
BeiDouB1I, B1CB3IB2I, B2a
QZSSC/AL2CL5
NavIC--SPS
1)
The modernized GLONASS signals CDMA L1 and CDMA L2 are for experimental
C/A, CDMA L1
1)
C/A, CDMA L2
1)
CDMA L3
use only. Any compliance with GLONASS ICD CDMA open service navigation signal in
L1 frequency band or GLONASS ICD CDMA open service navigation signal in L2 frequency band is not guaranteed. See also Table 2-7.
Table 1-2: Supported SBAS, frequency bands and signals
SBASL1 bandL2 bandL5 band
EGNOSC/A-
WAASC/A-
MSASC/A--
Exp L5
Exp L5
1)
1)
GAGANC/A--
1)
SBAS "Exp L5" signals are for experimental use only. These signals do not comply
with SBAS interface control document (ICD) specifications. See also Table 2-11.
10User Manual 1178.6379.02 ─ 13
1.2Accessing the GNSS dialog
To open the dialog with GNSS settings
► In the block diagram of the R&S SMW, select "Baseband > GNSS".
A dialog box opens that displays the provided general settings.
The signal generation is not started immediately. To start signal generation with the
default settings, select "State > On".
1.3What's new
This manual describes firmware version FW 5.00.166.xx and later of the
R&S®SMW200A.
Compared to the previous version, it provides the new features listed below:
●
GLONASS CDMA signal generation in L1, L2 and L5 bands, see "Signals"
on page 68.
●
QZSS L1C signal generation, see "Signals"on page 68.
●
Individual mapping of SBAS space vehicles with SBAS systems, see "SBAS PRN
assignments"on page 201.
●
3GPP FDD 2020 and EUTRA/LTE 2020 assisted GNSS test scenarios added, see
Chapter E.3, "Assisted GNSS 2020 test scenarios", on page 611.
●
Extended attenuation range for editing antenna pattern and body mask files, see
"Edit > Body Mask/Antenna Pattern File"on page 127.
●
Date and time expressions conforming with ISO 8601. For example, see "Simula-
tion Start"on page 46.
●
Corrected minimum value of 20ms for the system latency, see [:SOURce<hw>]:
BB:GNSS:RECeiver[:V<st>]:HIL:SLATency on page 292.
Welcome to the GNSS optionsSatellite Navigation
Documentation overview
1.4Documentation overview
This section provides an overview of the R&S SMW user documentation. Unless specified otherwise, you find the documents on the R&S SMW product page at:
www.rohde-schwarz.com/manual/smw200a
1.4.1Getting started manual
Introduces the R&S SMW and describes how to set up and start working with the product. Includes basic operations, typical measurement examples, and general information, e.g. safety instructions, etc. A printed version is delivered with the instrument.
11User Manual 1178.6379.02 ─ 13
1.4.2User manuals and help
Separate manuals for the base unit and the software options are provided for download:
●
Base unit manual
Contains the description of all instrument modes and functions. It also provides an
introduction to remote control, a complete description of the remote control commands with programming examples, and information on maintenance, instrument
interfaces and error messages. Includes the contents of the getting started manual.
●
Software option manual
Contains the description of the specific functions of an option. Basic information on
operating the R&S SMW is not included.
The contents of the user manuals are available as help in the R&S SMW. The help
offers quick, context-sensitive access to the complete information for the base unit and
the software options.
All user manuals are also available for download or for immediate display on the Internet.
Welcome to the GNSS optionsSatellite Navigation
Documentation overview
1.4.3Tutorials
The R&S SMW provides interactive examples and demonstrations on operating the
instrument in form of tutorials. A set of tutorials is available directly on the instrument.
1.4.4Service manual
Describes the performance test for checking compliance with rated specifications, firmware update, troubleshooting, adjustments, installing options and maintenance.
The service manual is available for registered users on the global Rohde & Schwarz
information system (GLORIS):
https://gloris.rohde-schwarz.com
1.4.5Instrument security procedures
Deals with security issues when working with the R&S SMW in secure areas. It is available for download on the Internet.
1.4.6Printed safety instructions
Provides safety information in many languages. The printed document is delivered with
the product.
12User Manual 1178.6379.02 ─ 13
Welcome to the GNSS optionsSatellite Navigation
1.4.7Data sheets and brochures
The data sheet contains the technical specifications of the R&S SMW. It also lists the
options and their order numbers and optional accessories.
The brochure provides an overview of the instrument and deals with the specific characteristics.
See www.rohde-schwarz.com/brochure-datasheet/smw200a
1.4.8Release notes and open source acknowledgment (OSA)
The release notes list new features, improvements and known issues of the current
firmware version, and describe the firmware installation.
The open-source acknowledgment document provides verbatim license texts of the
used open source software.
See www.rohde-schwarz.com/firmware/smw200a
Scope
1.4.9Application notes, application cards, white papers, etc.
These documents deal with special applications or background information on particular topics.
See www.rohde-schwarz.com/application/smw200a and www.rohde-schwarz.com/
manual/smw200a
1.5Scope
Tasks (in manual or remote operation) that are also performed in the base unit in the
same way are not described here.
In particular, it includes:
●
Managing settings and data lists, like saving and loading settings, creating and
accessing data lists, or accessing files in a particular directory.
●
Information on regular trigger, marker and clock signals and filter settings, if appropriate.
●
General instrument configuration, such as checking the system configuration, configuring networks and remote operation
●
Using the common status registers
For a description of such tasks, see the R&S SMW user manual.
13User Manual 1178.6379.02 ─ 13
1.6Notes on screenshots
When describing the functions of the product, we use sample screenshots. These
screenshots are meant to illustrate as many as possible of the provided functions and
possible interdependencies between parameters. The shown values may not represent
realistic usage scenarios.
The screenshots usually show a fully equipped product, that is: with all options installed. Thus, some functions shown in the screenshots may not be available in your particular product configuration.
Welcome to the GNSS optionsSatellite Navigation
Notes on screenshots
14User Manual 1178.6379.02 ─ 13
About the GNSS optionsSatellite Navigation
Required options
2About the GNSS options
Global navigation satellite system (GNSS) employs the radio signals of several navigation standards, like GPS, Galileo, GLONASS and BeiDou and NavIC. For several
years, GPS used to be the only standard available for civilian navigation through its
C/A civilian code.
Nowadays, the GNSS signals and systems are undergoing fast development, some
systems are getting modernized and some are new. In the foreseeable future, several
more GNSS satellites utilizing more signals and new frequencies are available.
The GNSS implementation in the R&S SMW enables you to generate composite signals of GNSS satellites, depending on the installed options. Signal generation is performed in real time and thus not limited to a certain time period.
The following chapters provide background information on required options, basic
terms and principles in the context of GNSS signal generation. For detailed information
on the GNSS standards, see the corresponding specifications.
2.1Required options
The basic equipment layout for generating GNSS signals includes:
●
Standard or wideband baseband generator (R&SSMW-B10/-B9)
●
Baseband main module (R&S SMW-B13/-B13T) or wideband baseband main module (R&S SMW-B13XT)
●
Frequency option (e.g. R&SSMW-B1003)
●
At least one basic or modernized GNSS option, per signal path, see Table 2-1. The
modernized GNSS options do not require a basic GNSS option.
●
Optional enhanced simulation capability options, per signal path, see Table 2-2.
–R&S SMW-B10: Standard GNSS, one simulation capability option per signal
path
–R&S SMW-B9: Advanced GNSS, one simulation capability option only
●
Optional enhanced simulation capacity options, see Table 2-3:
Table 2-1: GNSS system options
OptionDesignationRemark
R&S SMW-K44GPSC/A and P signals in L1 and L2 bands
R&S SMW-K66GalileoE1 OS, E6, E5a and E5b signals in L1, L2 and L5 bands
R&S SMW-K94GLONASSC/A signal in L1 and L2 bands
R&S SMW-K97NavIC/IRNSSSPS signal in L5 band
R&S SMW-K98Modernized GPSL1C, L2C and L5 signals in L1, L2 and L5 bands
There is a limitation on the maximum number of satellite signals that can be simulated
simultaneously. For more information, see Chapter G, "Channel budget", on page 616.
The column "Licenses" lists the number of installed options.
16User Manual 1178.6379.02 ─ 13
To play back GNSS waveforms
You can generate signals via play-back of waveform files at the signal generator. To
create the waveform file using R&S WinIQSIM2, you do not need a specific option.
To play back the waveform file at the signal generator, you have two options:
●
Install the R&S WinIQSIM2 option of the digital standard, e.g. R&S SMW-K255 for
playing LTE waveforms
●
If supported, install the real-time option of the digital standard, e.g. R&S SMW-K55
for playing LTE waveforms
For more information, see data sheet.
2.2GNSS overview
This section provides an overview on the GNSS including the following:
●
Power spectral density and center frequencies
●
Characteristics of the satellite constellation
●
Signal plan for each GNSS
About the GNSS optionsSatellite Navigation
GNSS overview
The number of deployed satellites increases constantly. For the current deployment
status, see the official information of the GNSS providers.
The GNSS simulation capacity depends on installed options and the visibility state of
the individual satellite. For the number of satellites that can be present in the satellite
constellation, see Table 6-1.
Figure 2-1: Power spectral density and center frequencies of most important GNSS signals
Red= GPS L1, L2 and L5 signals, details in GPS signal plan
Blue = Galileo E1, E5 and E6 signals, details in Galileo signal plan
Green = GLONASS G1(L1), G2(L2) and G3(L5) signals, details in GLONASS FDMA signal plan
Yellow = BeiDou B1, B2 and B3 signals, details in BeiDou signal plan
GPS
The Global Positioning System (GPS) consists of several satellites circling the earth in
low orbits. The satellites transmit permanently information that can be used by the
receivers to calculate their current position (ephemeris) and about the orbits of all satellites (almanac). The 3D position of a receiver on the earth can be determined by carrying out delay measurements of at least four signals emitted by different satellites.
17User Manual 1178.6379.02 ─ 13
About the GNSS optionsSatellite Navigation
GNSS overview
Being transmitted on a single carrier frequency, the signals of the individual satellites
can be distinguished by correlation (gold) codes. These ranging codes are used as
spreading codes for the navigation message which is transmitted at a rate of 50 bauds.
The C/A codes are used to provide standard positioning service (SPS), the P(Y) codes
to provide precise positioning service (PPS).
Table 2-4: GPS signal plan
Service nameC/AP(Y)L1CL2CM codeL5I, L5Q
SignalC/APL1CL2C
1)
M
L5
Frequency bandL1L1
L2
Center frequency,
MHz
ModulationBPSK(1)BPSK(10)TMBOC
1)
M code signals are not supported with the GNSS firmware.
1575.421575.42
1227.6
L1L2L1
L2
1575.421227.61575.42
1227.6
BPSK(1)BOC(10,5)QPSK(10)
(6,1,1/11)
L5
1176.45
Galileo
Galileo is the European global navigation satellite system that provides global positioning service under civilian control. It is planed to be inter-operable with GPS and GLONASS and other global satellite navigation systems.
The fully deployed Galileo system consists of operational and spare satellites. Three
independent CDMA signals, named E5, E6 and E1, are permanently transmitted by all
Galileo satellites. The E5 signal is further subdivided into two signals denoted E5a and
E5b (see Figure 2-1). The Galileo system provides open service (OS), public regulated
service (PRS) to authorized, commercial service (CS) and search and rescue (SAR)
service.
L1 and L2 P code signals are not supported in the GNSS firmware.
2)
k is the frequency number (FDMA) with -7 ≤ k ≤ 13.
Table 2-7: GLONASS CDMA signal plan
SignalCDMA L1CDMA L2CDMA L3
Frequency bandL1L2L5
Center frequency,
MHz
ModulationTDMTDMQPSK
1600.9951248.061202.025
BPSK(5)
BeiDou
The fully deployed BeiDou navigation satellite system (BDS) is a Chinese satellite navigation system. This navigation system is also referred as BeiDou-2.
The BDS is a global satellite navigation system with a constellation of satellites (COMPASS satellites) to cover the globe. The constellation includes geostationary orbit satellites (GEO) and non-geostationary satellites. The non-geostationary satellites comprise medium earth orbit satellites (MEO) and inclined geosynchronous orbit (IGSO).
The BDS uses frequency allocated in the B1, B2 and B3 bands providing open service
(OS) and authorized service (AS).
Table 2-8: BeiDou signal plan
SignalB1CB1IB2aB2IB3I
Frequency bandB1
L1 (GPS)
Center frequency,
MHz
ModulationBOC(1,1)
1575.421561.0981176.451207.141268.52
QMBOC(6, 1,
4/33)
B1
L1 (GPS)
BPSK(2)BPSK(10)
B2
L5 (GPS)
BPSK(10)
B2
L5 (GPS)
BPSK(2)BPSK(10)
B3
L2 (GPS)
BeiDou B1Q, B2Q and B3Q AS signals are not supported in the GNSS firmware.
19User Manual 1178.6379.02 ─ 13
About the GNSS optionsSatellite Navigation
GNSS overview
QZSS
The Quasi-Zenith satellite system (QZSS) is a regional space-based positioning system deployed in 2013.
In its final deployment stage, the QZSS uses a total number of three regional non-geostationary and highly inclined satellites and one geostationary orbit (GEO) satellite. The
QZSS does not aim to cover the globe but to increase the availability of GPS in Japan,
especially in the larger towns.
The QZSS uses signals that are similar to the GPS public signals.
Table 2-9: QZSS signal plan
Service nameC/AL1C
SignalC/AL1C-L2CL5-
Frequency bandL1L1L1L2L5E6
SAIF
1)
L2CM,
L2CL
L5I, L5Q
LEX
1)
Center frequency,
MHz
ModulationBPSK(1)TMBOC
1575.421575.421575.421227.61176.451278.75
BPSK(1)BPSK(1)BPSK(10)BPSK(5)
(6,1,1/11)
QZSS SAIF and E6 LEX signals are not supported in the GNSS firmware.
NavIC
NavIC (Navigation Indian Constellation) is the Indian navigation satellite system, formerly denoted IRNSS (Indian Regional Navigational Satellite System).
NavIC is a regional satellite navigation system with a constellation of satellites to cover
an area of 1500 km surrounding India (2016). The constellation includes geostationary
orbit (GEO) satellites and inclined geosynchronous orbit (IGSO) satellites.
The NavIC system uses frequencies allocated in the L5 and S bands providing special
positioning service (SPS) and precision service (PS).
Table 2-10: NavIC signal plan
SignalSPS
Frequency bandL5S
Center frequency,
MHz
1176.452491.75
PS
1)
ModulationBPSK(1)N/A
1)
NavIC PS signal is not supported in the GNSS firmware.
Assisted GNSS (A-GNSS)
Assisted GNSS (A-GNSS) was introduced to different mobile communication standards to reduce the time to first fix (TTFF) of a user equipment (UE) containing a GNSS
receiver. The reduction is achieved by transmitting information (assistance data) mainly
about the satellites directly from a base station to the UE.
20User Manual 1178.6379.02 ─ 13
For example, a standalone GPS receiver needs about 30 to 60 seconds for a first fix
and up to 12.5 minutes to get all information (almanac).
In A-GNSS "UE-based mode", the base station assists the UE by providing the complete navigation message along with a list of visible satellites and ephemeris data. In
addition to this information, the UE gets the location and the current time at the base
station. That speeds up both acquisition and navigation processes of the GPS receiver
and reduces TTFF to a few seconds.
In A-GNSS "UE assisted mode", the base station is even responsible for the calculation of the UE's exact location. The base station takes over the navigation based on the
raw measurements provided by the UE. Since the acquisition assistance data provided
by the base station already serves speeding up the acquisition process, the UE only
has to track the code and carrier phase.
2.3SBAS overview
Satellite-based augmentation systems (SBAS) use geostationary satellites (GEO) to
broadcast GNSS coarse integrity and wide area correction data (error estimations),
and ranging signal to augment the GNSS.
About the GNSS optionsSatellite Navigation
SBAS overview
SBAS broadcast augmentation data in the GPS frequency band L1 using the C/A code
of GPS. For experimental use, the R&S SMW provides modulation of SBAS L1 navigation message data in the GPS L5 band for SBAS systems EGNOS and WAAS. Thus,
the signal "Exp L5" is a pure copy of L1 data and does not comply with SBAS interface
control document (ICD) specifications.
Table 2-11: SBAS signal plan
SignalC/AExp L5
Frequency bandL1L5
Center frequency, MHz1575.421176.45
ModulationBPSK(1)N/A
The SBAS provides data for a maximum of 51 satellites. In the SBAS, the term
"pseudo random number" (PRN) is used instead of the term space vehicle (SV). There
are 90 PRN numbers reserved for SBAS, where the numbering starts at 120.
Several SBAS systems are still in their development phase, like, for example, the
SDCM in Russia Federation, and GAGAN in India.
SBAS systems that are currently in operation argument the US GPS satellite navigation system, so that they are suitable, for example, for civil aviation navigation safety
needs. The following SBAS systems are supported by R&S SMW:
●
EGNOS
EGNOS (European geostationary navigation overlay service) EGNOS is the European SBAS system.
●
WAAS
WAAS (wide area augmentation system) is the SBAS system in United States.
21User Manual 1178.6379.02 ─ 13
●
MSAS
MSAS (multi-functional satellite augmentation system ) is the SBAS system working in Japan. It uses the multi-functional transport satellites (MTSAT) and supports
differential GPS.
●
GAGAN
GAGAN (GPS aided geo augmented navigation system) is the SBAS implementation by the Indian government.
2.4GNSS components overview
The GNSS system consists of three main components: the space segment, the ground
segment and the user segment.
About the GNSS optionsSatellite Navigation
GNSS components overview
Figure 2-2: GNSS system components (simplified)
1 = Space segment or satellites
2 = Ground segment or ground stations
3 = User segment or receivers
4 = Ephemeris (broadcasted satellites orbit and clock)
5 = Broadcasted navigation message
Space segment
The space segment consists of the satellites that orbit the earth on their individual
orbits. Satellites broadcast signals at specific frequency in the L band and spread by
predefined codes. For the GPS satellites using L1 frequency band, for instance, the
predefined codes are the coarse/acquisition (C/A) or the precision (P) codes.
22User Manual 1178.6379.02 ─ 13
About the GNSS optionsSatellite Navigation
How are the GNSS components simulated?
The transmitted signal carries the navigation message, on which each satellite broadcasts its major characteristics, its clock offsets and precise orbit description, where the
latter is called ephemeris. The navigation message contains also satellites status
information, ionospheric and time-related parameters, UTC information and orbit data
with reduced accuracy for all other satellites, commonly referred as almanac.
Ground segment
The ground segment is a network of ground stations whose primary goal is to measure constantly the satellites’ location, altitude and velocity, and the satellites signals.
The ground stations also estimate the influence of the ionosphere. They calculate the
precise orbit (and orbit perturbation) parameters and clock drifts parameters of
each satellite. This corrected highly accurate information is regularly broadcasted back
to the satellites so that their navigation messages can be updated.
User segment
Finally, the receiver decodes the navigation message (ephemeris and almanac)
broadcasted by the GNSS satellites, obtains information regarding the satellites orbit,
clock, health etc. and calculates the satellites coordinates. The receiver also measures
the signal propagation time (i.e. the pseudorange) of at least four satellites and estimates its own position.
2.5How are the GNSS components simulated?
In real life, the true satellite orbit can differ from the orbit information that the satellite
broadcasts.
In this implementation, the simulated orbit is the true orbit. Thus, the satellites motion
along their orbits, the clock they use and the current distance to each of them are referred to as simulated orbit, clock and pseudorange. They are set as retrieved from
the constellation data source and can be configured on a per satellite basis.
The navigation message of each of the satellites is per default identical to the simulated one. It is referred to as broadcasted navigation message, since it represents the
broadcasted satellite’s signal, see Figure 2-2. Per default, the broadcasted and the
simulated orbit and clock parameters match. Obviously, if the parameters in any of
those two groups are changed, a deviation between the sets is simulated.
The receiver is the device under test (DUT). In the simulation, the receiver is represented by its position, antenna configuration, environment, etc. The receiver is tested with
the GNSS that it would receive in a real-world situation if placed in the specified conditions.
Simulation date, time and location
The R&S SMW generates the signal for any simulation date and time, in the past or in
the future. The generated signal represents any location, on the earth or in the space,
for a static or moving receiver.
23User Manual 1178.6379.02 ─ 13
About the GNSS optionsSatellite Navigation
How are the GNSS components simulated?
You have full control over the satellites’ constellation, the satellites signals and the navigation message of each satellite. Repeat measurement scenarios with same preconditions and vary the complexity or replay simulation events from the past.
For details, see:
●
Chapter 4, "Simulation time", on page 44
●
Chapter 5, "Receiver type and position", on page 50
●
Chapter 6, "Satellite constellation", on page 65
●
Chapter 7, "Space vehicle configuration", on page 78
Real-world scenarios through environmental effects
You can also simulate various different environmental conditions, like the effect of the
receiver’s antenna characteristic, vehicle movement, vehicle body mask, multipath
propagation, obstacles or the atmosphere.
For details, see Chapter 8, "Real-world environment", on page 102.
Ionospheric effects
You can also simulate the effect of the atmospheric (ionospheric and tropospheric)
errors on the positioning accuracy.
For details, see "Tropospheric and ionospheric models"on page 160.
GNSS errors sources
Additional to the real-world and the ionosphere effects, you can simulate signal errors
by manipulating the navigation messages of the satellites. Signal errors have a direct
impact on the receiver’s positioning accuracy.
You can observe the effect of the following common error sources:
●
Ephemeris errors: Orbit and orbit perturbation errors
●
Satellite clock and time conversion errors
●
Pseudorange errors
For details, see Chapter 10, "Perturbations and errors simulation", on page 153.
Historical constellations and navigation data
You can also replay historical satellite constellations, by loading constellation files and
navigation data files for all GNSS systems supported in the GNSS firmware.
For details, see:
●
"Constellation data and navigation message file formats"on page 268
●
Chapter 15.1, "Import GNSS constellation and navigation message data settings",
on page 270
Correction data
You can also correct navigation data by loading SBAS corrections.
24User Manual 1178.6379.02 ─ 13
About the GNSS optionsSatellite Navigation
How are the GNSS components simulated?
For details, see:
●
Chapter 11, "SBAS corrections", on page 200
●
Chapter 15.2, "Import SBAS constellation and correction data settings",
on page 272
25User Manual 1178.6379.02 ─ 13
Getting startedSatellite Navigation
Trying out the GNSS simulator
3Getting started
In its default configuration, the software generates GNSS signal that is sufficient for a
receiver to get a position fix. The simulated GNSS depends on the installed options.
For example, if R&S SMW-K44 is installed, it is GPS C/A signal in the L1 band.
For all GNSS, the simulation starts on 2014-02-19 at 6 am UTC time and the satellite
constellation corresponds to a constellation, that is visible for a static receiver located
in Munich.
To simulate a defined configuration, you can load predefined assistance GNSS scenarios or load a user-defined scenario. The software applies the configuration automatically, you can change related settings afterwards. For example, try out the receiver
templates and configure a receiver, moving in a circle in New York.
●Trying out the GNSS simulator............................................................................... 26
2. Select, e.g., "General > Predefined Scenarios > Assisted GNSS > 3GPP2 >
3GPP2C.S0036 2.1.2 Moving".
See also Chapter E, "List of predefined test scenarios", on page 605.
3. Select "General > State > On".
27User Manual 1178.6379.02 ─ 13
Getting startedSatellite Navigation
Trying out the GNSS simulator
The summary information confirms the used scenario. Configured is a single GPS
system signal in the L1 frequency band.
4. To observe current satellite constellation and the trajectory of the moving receiver,
select "Simulation Monitor > Display > Receiver > Map View".
The "Simulation Monitor" shows the trajectory of the moving receiver.
5. To observe the preconfigured receiver settings, select "Simulation Monitor > Config".
6. In the "Simulation Configuration > Receiver" dialog, select "Position Configuration".
Observe the configuration.
28User Manual 1178.6379.02 ─ 13
7. In the block diagram, select "RF > On".
Getting startedSatellite Navigation
Trying out the GNSS simulator
The signal generation starts.
The frequency and level of the generated RF signal are configured automatically.
Further settings are not required.
For description of the related settings, see:
●Chapter 3.2, "General settings", on page 31
●Chapter 3.3, "Simulation monitor", on page 34
●Chapter 5, "Receiver type and position", on page 50