Spirent Scenario Package for testing GOST R … › resources › sites › SPIRENT...GOST R...

SSP0001 GOST R 55534-2103

Professional Services and Solutions

PROPRIETARY INFORMATION THE INFORMATION CONTAINED IN THIS DOCUMENT IS THE PROPERTY OF SPIRENT COMMUNICATIONS PLC. EXCEPT AS SPECIFICALLY AUTHORISED IN WRITING BY SPIRENT COMMUNICATIONS PLC, THE HOLDER OF THIS DOCUMENT SHALL KEEP ALL INFORMATION CONTAINED HEREIN CONFIDENTIAL AND SHALL PROTECT SAME IN WHOLE OR IN PART FROM DISCLOSURE AND DISSEMINATION TO ALL THIRD PARTIES TO THE SAME DEGREE IT PROTECTS ITS OWN CONFIDENTIAL INFORMATION. © COPYRIGHT SPIRENT COMMUNICATIONS PLC 2016 - 2016. N.B. Only documents bearing the Document Status ‘APPROVED SPIRENT DOCUMENTATION’ in the panel below are deemed official literature. This Issue Originated by: Approved by: Document Status:

M Hunter D.Lewis APPROVED SPIRENT DOCUMENTATION

Title: Technical Lead for Professional Services Title: Member of Technical Staff

Issue 1-00, 14 April 2016

Page 1 of 29

Spirent Scenario Package for testing

GOST R 55534-2103

Abstract

This document defines the scenarios used for verifying compliance to the National Standard of the Russian Federation

GOST R 55534-2013

SSP0001 GOST R 55534-2103

Spirent Scenario Package for testing GOST R 55534-2103 Issue 1-00, 14 April 2016

Page 2 of 29

RECORD OF ISSUE

Issue Date Author Reason for Change

1-00 14-APR-2016 MAH First issue

SSP0001 GOST R 55534-2103


Page 3 of 29

TABLE OF CONTENTS 1 PURPOSE OF THIS DOCUMENT ..................................................................................................... 6 1.1 SCOPE & APPLICABILITY ............................................................................................................ 6 1.2 REFERENCED DOCUMENTS ...................................................................................................... 6 1.3 GLOSSARY OF TERMS ................................................................................................................ 6 2 INTRODUCTION ................................................................................................................................. 7 2.1 COMMON SCENARIO PARAMETERS ........................................................................................ 7 2.1.1 ATMOSPHERIC SIMULATION ........................................................................................... 9 2.1.2 C2 MOTION PARAMETERS ............................................................................................. 10 2.1.3 C3 MOTION PARAMETERS ............................................................................................. 11 2.2 UTC OFFSETS ............................................................................................................................ 12 2.2.1 GPS UTC OFFSETS ......................................................................................................... 12 2.2.2 GLONASS UTC OFFSETS ............................................................................................... 12 2.3 ANTENNA PATTERN .................................................................................................................. 12 2.4 ALMANACS ................................................................................................................................. 12 2.4.1 GPS ALMANAC ................................................................................................................. 12 2.4.2 GLONASS ALMANAC ....................................................................................................... 13 2.5 EARTH OBSCURATION ANGLE ................................................................................................ 13 2.6 SIGNAL STRENGTH ................................................................................................................... 13 2.7 MOTION TRUTH DATA ............................................................................................................... 13 3 INDIVIDUAL SCENARIO DETAIL .................................................................................................... 14 3.1 GOST_5_1 ................................................................................................................................... 14 3.2 GOST_5_2 ................................................................................................................................... 14 3.3 GOST_5_3 ................................................................................................................................... 14 3.4 GOST_5_4 ................................................................................................................................... 14 3.5 GOST_5_5 ................................................................................................................................... 14 3.6 GOST_5_6 ................................................................................................................................... 15 3.7 GOST_5_7_3 ............................................................................................................................... 15 3.8 GOST_5_7_10 ............................................................................................................................. 15 3.9 GOST_5_7_11 ............................................................................................................................. 15 3.10 GOST_5_8_3 ............................................................................................................................... 15 3.11 GOST_5_8_9 ............................................................................................................................... 15 3.12 GOST_5_8_10 ............................................................................................................................. 15 3.13 GOST_5_8_13_C3_GLO ............................................................................................................. 15 3.14 GOST_5_8_13_C3_GPS ............................................................................................................. 15 3.15 GOST_5_8_13_C3_GLO_GPS ................................................................................................... 16 3.16 GOST_5_8_13_C4_GLO ............................................................................................................. 16 3.17 GOST_5_8_13_C4_GPS ............................................................................................................. 16 3.18 GOST_5_8_13_C4_GLO_GPS ................................................................................................... 16 3.19 GOST_5_10_1 ............................................................................................................................. 16 3.20 GOST_5_10_8 ............................................................................................................................. 16

SSP0001 GOST R 55534-2103


Page 4 of 29

3.21 GOST_5_10_9 .............................................................................................................................16 3.22 GOST_5_11_1 .............................................................................................................................16 3.23 GOST_5_11_6 .............................................................................................................................16 3.24 GOST_5_11_7 .............................................................................................................................17 3.25 GOST_5_12_6 .............................................................................................................................17 3.26 GOST_5_13_4 .............................................................................................................................17 3.27 GOST_5_14_5 .............................................................................................................................17 3.28 GOST_5_14_7 .............................................................................................................................17 4 INTERFERENCE TESTS ..................................................................................................................18 4.1 GOST 5.16 ...................................................................................................................................18 4.1.1 GOST 5.16.5 GLONASS TESTING ...................................................................................18 4.1.2 GOST 5.16.6 GPS TESTING.............................................................................................19 4.2 GOST_5_17_6 .............................................................................................................................19 APPENDIX A : GPS ALMANAC .......................................................................................................................21 APPENDIX B : GLONASS ALMANAC (.AGL FORMAT) .................................................................................25 APPENDIX C D1 GLONASS INTERFERENCE PROFILE ..............................................................................27 APPENDIX D D1 GPS INTERFERENCE PROFILE ........................................................................................28

SSP0001 GOST R 55534-2103


Page 5 of 29

TABLE OF TABLES Table 1 C1 Fixed Spatial Location ..................................................................................................................... 7 Table 2 C2 Simulation of speed up to maximum velocity .................................................................................. 7 Table 3 C3 Simulation of movement with manoeuvring ..................................................................................... 8 Table 4 C4 Simulation of movement in blockage and poor reception zones ..................................................... 8 Table 5 Ionospheric parameters ......................................................................................................................... 9 Table 6 C2 local velocity and acceleration values ........................................................................................... 10

TABLE OF FIGURES Figure 1 C3 motion profile ................................................................................................................................ 11 Figure 2 C3 motion trajectory ........................................................................................................................... 12 Figure 3 Adding Interference ............................................................................................................................ 18

SSP0001 GOST R 55534-2103


Page 6 of 29

1 PURPOSE OF THIS DOCUMENT This document defines a series of test scenarios that have been derived from section 5 of the Russian Federation GOSTR55534-2013 test document (reference a) These scenarios can be executed on any Spirent Simulator that runs the “Positioning Application” software suite and has both GPS and GLONASS constellations enabled.

1.1 SCOPE & APPLICABILITY

Users with either a SimREPLAY or SimREPLAYplus licence can run all of the scenarios provided apart from those detailed in section 4 Interference Tests since this functionality is not supported on this platform; users with a GSS7765 Interference system (reference b) are able to complete this section too. Spirent provides motion truth data for each of the 4 default profiles (see section 2.1) both in WGS-84 and NMEA format. It is up to the user to interpret their receiver “truth” data and determine an appropriate pass/fail status. The scenario pack is provided under the terms defined in reference d).

1.2 REFERENCED DOCUMENTS

a) GOST R 55534/2013 Global Navigation Satellite System ROAD ACCIDENT EMERGENCY RESPONSE SYSTEM Test methods for navigation modules of in-vehicle emergency Official Edition English Version Approved by Interstandard

b) MS3055 Interference Simulation System Datasheet Specification c) STANAG 4294 NAVSTAR GLOBAL POSITIONING (GPS) SYSTEM CHARACTERISTICS d) DGP00956AAA Spirent Software Licence

1.3 GLOSSARY OF TERMS

CW Continuous Wave EUT Equipment under Test g Acceleration due to gravity GPS Global Positioning System GLONASS GLObal NAvigation Satellite System

(Russian Federation) GNSS Global Navigation Satellite System NMEA National Marine Electronics Association RAIM Receiver Autonomous Integrity Monitoring RF Radio Frequency SV GNSS Space Vehicle UTC Universal Time Coordinated WGS-84 World Geodetic System 1984 update

SSP0001 GOST R 55534-2103


Page 7 of 29

2 INTRODUCTION The test pack consists of 28 scenarios (plus the interference section 1 scenario and user action files) that are specifically named to cross-reference to section 5 of reference a). Some subsections of that document define multiple scenarios within the same subsection, the difference being the number and type of GNSS defined. Consequently particular scenario names may end in an addition appendage defining the GNSS enabled in that scenario. Unless otherwise stated in section 3 Individual Scenario Detail the scenario parameters used are defined below.

2.1 COMMON SCENARIO PARAMETERS

Appendix C of reference a) defines four sets of basic parameters, one of which is called for in each test case. These tables C1 through to C4, are reproduced below with the addition of Spirent comments on implementation where needed, if the parameter is not included in the table then no implementation note was needed:

Simulated Parameter Value from GOST Value to be used in software

Start Date and Time none 30th March 2016 12:00:00

IVS Location in: -WGS-84 CS -PZ-90

Central Russia Central Russia

Transformation matrix used PZ-90.11

Static location none 55°45’N 37° 33’ E

Atmospheric Parameters -troposphere -ionosphere

Standard “Autumn” Model

See section 2.1.1

Table 1 C1 Fixed Spatial Location



IVS initial point in: -WGS-84 CS -PZ-90



IVS movement model: -speed up to maximum velocity -acceleration,g

250 km/h 2 g

See section 2.1.2


Standard “Autumn” Model

See section 2.1.1

Table 2 C2 Simulation of speed up to maximum velocity

SSP0001 GOST R 55534-2103


Page 8 of 29






IVS movement model: -velocity -radius of turns -acceleration at turns

10 m/s 500 m 0.2 m/s2

See section 2.1.3


Standard “Spring” Model

See section 2.1.1

Table 3 C3 Simulation of movement with manoeuvring







Standard “Spring” Model

See section 2.1.1

Table 4 C4 Simulation of movement in blockage and poor reception zones

SSP0001 GOST R 55534-2103


Page 9 of 29

2.1.1 ATMOSPHERIC SIMULATION

Spirent interprets a “standard” troposphere for all test cases to mean that the tropospheric delay model used is STANAG with a surface refractivity index of 324.8 Spirent interprets the “Autumn” and “Spring” ionospheric model to mean use the Alpha and Beta Klobuchar parameters from Appendix 6 of the STANAG 4294 document (reference c). However due to bit limitation in the GPS navigation data, quantisation of these values is observed. So as not to introduce errors into the scenario that the receiver cannot correct for the same quantised broadcast values are also used in applying the delay model at RF. The original spring and autumn values from reference c) are shown below along with the quantised values used both in the RF model and the broadcast navigation data:

TERM Units * Spring Autumn

STANAG value Scenario value STANAG

value Scenario value

Alpha 0 sec 9.2E-9 9.3132257E-009 1.2E-8 1.2107193E-8

Alpha 1 sec/SC 1.8E-8 1.4901161E-008 -2.3E-9 0

Alpha 2 sec/SC2 -7.2E-8 -5.96046E-008 -9.2E-8 -1.19209e-7

Alpha 3 sec/SC3 -1.2E-7 -1.19209E-007 2.1E-8 0

Beta 0 sec 8.7E+4 86016 9.3E+4 92160

Beta 1 sec/SC 5.0E+4 49152 -1.5E+3 0

Beta 2 sec/SC2 -1.6E+5 -131072 -2.2E+5 -196608

Beta 3 sec/SC3 -3.3E+5 -327680 1.5E+4 0

* sec = seconds SC= semicircles (1SC = 180 degrees) E = exponent

Table 5 Ionospheric parameters

SSP0001 GOST R 55534-2103


Page 10 of 29

2.1.2 C2 MOTION PARAMETERS

The specification defines a trajectory of a maximum speed of 250km/h via a 2g’s acceleration. Spirent assumes the following:

• the vehicle is initially at rest for 5 minutes • 2g acceleration is not instantaneous

o The acceleration profile ramps up and down to 2g.in 0.1 seconds using a cubic spline fit.

The resulting local body acceleration and velocity profile in the direction of acceleration is as detailed below:

Time into run (s)

Acceleration m/s2

Velocity m/s

300 0 0 300.1 19.8411 0.992057 300.2 19.8411 2.976171 300.3 19.8411 4.960286 300.4 19.8411 6.9444 300.5 19.8411 8.928514 300.6 19.8411 10.91263 300.7 19.8411 12.89674 300.8 19.8411 14.88086 300.9 19.8411 16.86497 301 19.8411 18.84909

301.1 19.8411 20.8332 301.2 19.8411 22.81731 301.3 19.8411 24.80143 301.4 19.8411 26.78554 301.5 19.8411 28.76966 301.6 19.8411 30.75377 301.7 19.8411 32.73789 301.8 19.8411 34.722

Time into run

Acceleration m/s2

Velocity m/s

301.9 19.8411 36.70611 302 19.8411 38.69023

302.1 19.8411 40.67434 302.2 19.8411 42.65846 302.3 19.8411 44.64257 302.4 19.8411 46.62669 302.5 19.8411 48.6108 302.6 19.8411 50.59491 302.7 19.8411 52.57903 302.8 19.8411 54.56314 302.9 19.8411 56.54726 303 19.8411 58.53137

303.1 19.8411 60.51549 303.2 19.8411 62.4996 303.3 19.8411 64.48371 303.4 19.8411 66.46783 303.5 19.8411 68.45194 303.6 0 69.444 303.7 0 69.444

Table 6 C2 local velocity and acceleration values

Note due to the necessity of this acceleration taking place in a multiple of the system iteration rate (100ms) the acceleration seen is about 1.1% higher than the 2g specified.

SSP0001 GOST R 55534-2103


Page 11 of 29

2.1.3 C3 MOTION PARAMETERS

Spirent Implements the manoeuvring with the following commands in the airplane motion model, ensuring a constant speed of 10m/s, and a lateral acceleration on turning of 0.2m/s. These dynamics automatically ensure on turning that a turn radius of 500m is achieved:

Figure 1 C3 motion profile

SSP0001 GOST R 55534-2103


Page 12 of 29

The resulting trajectory is as shown below:

Figure 2 C3 motion trajectory

2.2 UTC OFFSETS

2.2.1 GPS UTC OFFSETS

GPS system time is aligned with UTC i.e.A0=0 s A1=0 s/s A2=0 s/s2

The GPS navigation data will transmit the appropriate GPS to UTC offset (leap second count) for the simulated date, for this release (v1) that value is 17 seconds

2.2.2 GLONASS UTC OFFSETS

GLONASS system time has a fixed offset with UTC(SU) defined as A0 = 1e-7 s

2.3 ANTENNA PATTERN

The default isotropic 0dBi pattern is used for both GPS and GLONASS resulting in signal minimums as defined in reference a)

2.4 ALMANACS

2.4.1 GPS ALMANAC

APPENDIX A details the GPS almanac used. There is also an electronic copy supplied with the scenario set.

SSP0001 GOST R 55534-2103


Page 13 of 29

2.4.2 GLONASS ALMANAC

APPENDIX B details the GLONASS almanac used. There is also an electronic copy supplied with the scenario set

2.5 EARTH OBSCURATION ANGLE

A standard earth obscuration angle of 5 degrees is used for both GPS and GLONASS. SV’s below this angle will not be simulated.

2.6 SIGNAL STRENGTH

The modelled option is chosen for both GPS and GLONASS. Consequently SV’s with a 90 degree elevation with respect to the modelled antenna have about a 2.5 dB gain compared to those on the horizon.

2.7 MOTION TRUTH DATA

For each of the four motion profiles detailed in tables C1 to C4 Spirent provides a “Motion Truth Data” folder with corresponding NMEA data (WGS -84 reference frame) and raw WGS-84 ECEF data for each profile is provided.

SSP0001 GOST R 55534-2103


Page 14 of 29

3 INDIVIDUAL SCENARIO DETAIL The actual scenario names detailed in this release have a “_v1” appendage i.e. GOST_5_1_v1

3.1 GOST_5_1

Checking that navigation signals of standard precision in L1 band of GLONASS GNSS may be received and processed in order to determine vehicle coordinates and its velocity components

• GLONASS only • Table C2 parameters i.e. Autumn and 2g acceleration

3.2 GOST_5_2

Checking that navigation signals of standard precision in L1 band of GPS GNSS may be received and processed in order to determine vehicle coordinates and its velocity components

• GPS only • Table C2 parameters i.e. Autumn and 2g acceleration

3.3 GOST_5_3

Checking that navigation signals of standard precision in L1 band of GPS GNSS may be received and processed in order to determine vehicle coordinates and its velocity components

• GLONASS and GPS • Table C2 parameters i.e. Autumn and 2g acceleration

3.4 GOST_5_4

Checking that navigation parameters data may be output to external devices in NMEA-0183 format • GLONASS and GPS • Table C1 parameters i.e. Autumn and fixed location

3.5 GOST_5_5

Checking receiver autonomous integrity monitoring (RAIM) algorithm • GLONASS and GPS • Table C1 parameters i.e. Autumn and fixed location

Unfortunately reference a) does not specify the magnitude of the “simulated errors in ephemeris and timing data” for the effected SV’s. Spirent uses the following (aggressive) pseudo-range ramp parameters:

• SV’s o GPS SV’s 13,15 and 28 o GLONASS 2,3 and 12

• Start time 10 mins • ramping of signal pseudo-range at a rate of 1 km/s for the next 50 minutes

Although the test section states “no SV signals are received while the errors are simulated”, signals will be still received; the pass criteria should be, for example, that once the errors are applied there should be no degradation in positional accuracy i.e. the RAIM algorithm has rejected the delayed signals.

SSP0001 GOST R 55534-2103


Page 15 of 29

3.6 GOST_5_6

Checking that the navigation parameters may be determined in PZ-90 and WGS-84 coordinate systems

• GLONASS only • Table C1 parameters i.e. Autumn and fixed location

3.7 GOST_5_7_3

Estimating error in evaluation of plane view coordinates and altitude in autonomous static mode • GLONASS only • Table C1 parameters i.e. Autumn and fixed location

3.8 GOST_5_7_10

Estimating error in evaluation of plane view coordinates and altitude in autonomous static mode • GPS only • Table C1 parameters i.e. Autumn and fixed location

3.9 GOST_5_7_11

Estimating error in evaluation of plane view coordinates and altitude in autonomous static mode • GLONASS and GPS • Table C1 parameters i.e. Autumn and fixed location

3.10 GOST_5_8_3

Estimating error in evaluation of plane view coordinates and altitude and velocity in dynamic mode • GLONASS only • Table C2 parameters i.e. Autumn and 2g acceleration

3.11 GOST_5_8_9

Estimating error in evaluation of plane view coordinates and altitude and velocity in dynamic mode • GPS only • Table C2 parameters i.e. Autumn and 2g acceleration

3.12 GOST_5_8_10

Estimating error in evaluation of plane view coordinates and altitude and velocity in dynamic mode • GLONASS and GPS • Table C2 parameters i.e. Autumn and 2g acceleration

3.13 GOST_5_8_13_C3_GLO

Estimating error in evaluation of plane view coordinates and altitude and velocity in dynamic mode • GLONASS only • Table C3 parameters i.e. Spring and manoeuvring

3.14 GOST_5_8_13_C3_GPS

Estimating error in evaluation of plane view coordinates and altitude and velocity in dynamic mode • GPS only • Table C3 parameters i.e. Spring and manoeuvring

SSP0001 GOST R 55534-2103


Page 16 of 29

3.15 GOST_5_8_13_C3_GLO_GPS

Estimating error in evaluation of plane view coordinates and altitude and velocity in dynamic mode • GLONASS and GPS • Table C3 parameters i.e. Spring and manoeuvring

3.16 GOST_5_8_13_C4_GLO

Estimating error in evaluation of plane view coordinates and altitude and velocity in dynamic mode • GLONASS only • Table C4 parameters i.e. Spring and 10 m/s with blockage

3.17 GOST_5_8_13_C4_GPS

Estimating error in evaluation of plane view coordinates and altitude and velocity in dynamic mode • GPS only • Table C4 parameters i.e. Spring and 10 m/s with blockage

3.18 GOST_5_8_13_C4_GLO_GPS

Estimating error in evaluation of plane view coordinates and altitude and velocity in dynamic mode • GLONASS and GPS • Table C4 parameters i.e. Spring and 10 m/s with blockage

3.19 GOST_5_10_1

Checking time to restore tracking signals of working NSC constellation after tracking fault caused by blockage.

• GLONASS and GPS • Assume C1 parameters i.e. Autumn and fixed spatial location

3.20 GOST_5_10_8


• GLONASS only • Assume C1 parameters i.e. Autumn and fixed spatial location

3.21 GOST_5_10_9


• GPS only • Assume C1 parameters i.e. Autumn and fixed spatial location

3.22 GOST_5_11_1

Evaluating time of navigation fix in cold start mode • GLONASS and GPS • Assume C1 parameters i.e. Autumn and fixed spatial location

3.23 GOST_5_11_6

Evaluating time of navigation fix in cold start mode • GLONASS only

SSP0001 GOST R 55534-2103


Page 17 of 29

• Assume C1 parameters i.e. Autumn and fixed spatial location

3.24 GOST_5_11_7

Evaluating time of navigation fix in cold start mode • GPS only • Assume C1 parameters i.e. Autumn and fixed spatial location

3.25 GOST_5_12_6

Evaluating sensitivity of GNSS navigation module in GNSS signal search (locking) mode and in GNSS hold (tracking) mode

• GLONASS and GPS • C1 parameters i.e. Autumn and fixed spatial location • Fixed power level per SV of -120dBm GPS and -122.5 GLONASS (offset from relative

minimum ICD power levels) Section 12 can be completed wholly via power level manipulation in the software rather than manipulation of an attenuation bank.

3.26 GOST_5_13_4

Checking that data output rate may be changed in required range using GNSS_DATA_RATE setup parameter

• GLONASS and GPS • Table C2 parameters i.e. Autumn and 2g acceleration

3.27 GOST_5_14_5

Checking minimum elevation (cut-off angle) for navigation spacecrafts • GLONASS and GPS • C1 parameters i.e. Autumn and fixed spatial location • Earth obscuration angle = 0 degrees

3.28 GOST_5_14_7

Checking minimum elevation (cut-off angle) for navigation spacecrafts • GLONASS and GPS • C1 parameters i.e. Autumn and fixed spatial location

SSP0001 GOST R 55534-2103


Page 18 of 29

4 INTERFERENCE TESTS Customers with access to reference can now complete GOST section 5.16 (harmonic interference) and 5.17 (pulsed interference) by adding the interference option to antenna1. Right click on antenna 1 and select “Edit” and make the selection as shown below:

Figure 3 Adding Interference

4.1 GOST 5.16

Checking conformity to requirements of intended use under exposure to harmonic interference

4.1.1 GOST 5.16.5 GLONASS TESTING

Add interference and users actions file “D1 GLONASS Interference profile.act” to each of these scenarios in turn and retest: GOST_5_1 GOST_5_5 GOST_5_7_3 GOST_5_8_3 GOST_5_8_13_C3_GLO GOST_5_8_14_C4_GLO GOST_5_10_8

SSP0001 GOST R 55534-2103


Page 19 of 29

GOST_5_11_6 User actions file “D1 GLONASS Interference profile.act” is documented in APPENDIX C

4.1.2 GOST 5.16.6 GPS TESTING

Add interference and users actions file “D1 GPS Interference profile.act” to each of these scenarios in turn and retest: GOST_5_2 GOST_5_5 GOST_5_7_10 GOST_5_8_9 GOST_5_8_13_C3_GPS GOST_5_8_14_C4_GPS GOST_5_10_9 GOST_5_11_7 User actions file “D1 GPS Interference profile.act” is documented in APPENDIX D

4.2 GOST_5_17_6

Checking that GNSS signals may be tracked under exposure to pulse interference

• Basic Configuration – Table C.1 • Signals Present – GPS & GLONASS • Additional configuration:

o GNSS base signal strength GPS -128.5 dBm GLONASS -131dBm

o User actions file configured as follows: 15minutes of static no changes to get GNSS signals and Nav data. Configure interference pulse generation as follows: Frequency range – 1565.42 to 1609.36 Threshold value of interference signals (peak pulse power) = (Maximum

0dBm) Pulse duration = <=1ms Pulse duty cycle = >=10

If the customer wanted to perform testing at +20dBm (-10dBW) then a +20dB amplifier on the output of the Agilent noise generator or a high output power option will be required (note the High output power option has not been tested with PosApp).

SSP0001 GOST R 55534-2103


Page 20 of 29

SSP0001 GOST R 55534-2103


Page 21 of 29

APPENDIX A : GPS ALMANAC ******** Week 866 almanac for PRN-01 ******** ID: 01 Health: 000 Eccentricity: 0.5217075348E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9637977322 Rate of Right Ascen(r/s): -0.7828897534E-008 SQRT(A) (m 1/2): 5153.602539 Right Ascen at Week(rad): -0.1158766690E+001 Argument of Perigee(rad): 0.451503426 Mean Anom(rad): -0.2085681323E+001 Af0(s): 0.1621246338E-004 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-02 ******** ID: 02 Health: 000 Eccentricity: 0.1561641693E-001 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9425257330 Rate of Right Ascen(r/s): -0.8023191341E-008 SQRT(A) (m 1/2): 5153.697754 Right Ascen at Week(rad): -0.1203085478E+001 Argument of Perigee(rad): -2.138623509 Mean Anom(rad): -0.1677678011E+001 Af0(s): 0.5989074707E-003 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-03 ******** ID: 03 Health: 000 Eccentricity: 0.2431869507E-003 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9596751588 Rate of Right Ascen(r/s): -0.7874613724E-008 SQRT(A) (m 1/2): 5153.681641 Right Ascen at Week(rad): -0.1175191820E+000 Argument of Perigee(rad): -2.654391966 Mean Anom(rad): -0.8258891143E-001 Af0(s): -0.4291534424E-004 Af1(s/s): -0.3637978807E-011 week: 866 ******** Week 866 almanac for PRN-05 ******** ID: 05 Health: 000 Eccentricity: 0.4567623138E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9467621565 Rate of Right Ascen(r/s): -0.8000333246E-008 SQRT(A) (m 1/2): 5153.704590 Right Ascen at Week(rad): -0.1286690052E+000 Argument of Perigee(rad): 0.466892295 Mean Anom(rad): 0.8149317876E+000 Af0(s): -0.1325607300E-003 Af1(s/s): 0.3637978807E-011 week: 866 ******** Week 866 almanac for PRN-06 ******** ID: 06 Health: 000 Eccentricity: 0.4229545593E-003 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9636299530 Rate of Right Ascen(r/s): -0.7828897534E-008 SQRT(A) (m 1/2): 5153.617676 Right Ascen at Week(rad): -0.1167210326E+001 Argument of Perigee(rad): -1.651495850

Mean Anom(rad): -0.1531606413E+001 Af0(s): 0.1697540283E-003 Af1(s/s): 0.7275957614E-011 week: 866 ******** Week 866 almanac for PRN-07 ******** ID: 07 Health: 000 Eccentricity: 0.9196281433E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9667338673 Rate of Right Ascen(r/s): -0.7817468486E-008 SQRT(A) (m 1/2): 5153.615723 Right Ascen at Week(rad): 0.2000559620E+001 Argument of Perigee(rad): -2.681704389 Mean Anom(rad): -0.2813372072E+001 Af0(s): 0.4625320435E-003 Af1(s/s): -0.3637978807E-011 week: 866 ******** Week 866 almanac for PRN-08 ******** ID: 08 Health: 000 Eccentricity: 0.1825332642E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9625633570 Rate of Right Ascen(r/s): -0.8148910863E-008 SQRT(A) (m 1/2): 5153.616699 Right Ascen at Week(rad): -0.2219099077E+001 Argument of Perigee(rad): -1.232277551 Mean Anom(rad): 0.1043138020E+001 Af0(s): -0.2956390381E-004 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-09 ******** ID: 09 Health: 000 Eccentricity: 0.6465911865E-003 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9554327432 Rate of Right Ascen(r/s): -0.8080336578E-008 SQRT(A) (m 1/2): 5153.550293 Right Ascen at Week(rad): 0.9221786163E+000 Argument of Perigee(rad): 2.035474161 Mean Anom(rad): -0.1098769915E+000 Af0(s): 0.1010894775E-003 Af1(s/s): 0.7275957614E-011 week: 866 ******** Week 866 almanac for PRN-10 ******** ID: 10 Health: 000 Eccentricity: 0.1341819763E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9599268275 Rate of Right Ascen(r/s): -0.7874613724E-008 SQRT(A) (m 1/2): 5153.631348 Right Ascen at Week(rad): -0.1215724715E+000 Argument of Perigee(rad): -2.793115736 Mean Anom(rad): 0.1929271833E+001 Af0(s): 0.1335144043E-004 Af1(s/s): -0.1091393642E-010 week: 866 ******** Week 866 almanac for PRN-11 ******** ID: 11 Health: 000 Eccentricity: 0.1624584198E-001 Time of Applicability(s): 503808.0000

SSP0001 GOST R 55534-2103


Page 22 of 29

Orbital Inclination(rad): 0.8957692795 Rate of Right Ascen(r/s): -0.8606072763E-008 SQRT(A) (m 1/2): 5153.591309 Right Ascen at Week(rad): -0.1531956952E+001 Argument of Perigee(rad): 1.512255261 Mean Anom(rad): -0.2693532070E+001 Af0(s): -0.6389617920E-003 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-12 ******** ID: 12 Health: 000 Eccentricity: 0.6048679352E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9905884670 Rate of Right Ascen(r/s): -0.7737465154E-008 SQRT(A) (m 1/2): 5153.717285 Right Ascen at Week(rad): 0.3075321762E+001 Argument of Perigee(rad): 0.702235882 Mean Anom(rad): 0.2996809734E+001 Af0(s): 0.3747940063E-003 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-13 ******** ID: 13 Health: 000 Eccentricity: 0.4575252533E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9717912102 Rate of Right Ascen(r/s): -0.7886042771E-008 SQRT(A) (m 1/2): 5153.626953 Right Ascen at Week(rad): 0.1042074420E+001 Argument of Perigee(rad): 1.987702419 Mean Anom(rad): -0.1866079764E+001 Af0(s): -0.7629394531E-005 Af1(s/s): -0.3637978807E-011 week: 866 ******** Week 866 almanac for PRN-14 ******** ID: 14 Health: 000 Eccentricity: 0.8412361145E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9643070617 Rate of Right Ascen(r/s): -0.7977475151E-008 SQRT(A) (m 1/2): 5153.937988 Right Ascen at Week(rad): 0.1005376851E+001 Argument of Perigee(rad): -1.964500960 Mean Anom(rad): -0.4467793946E-001 Af0(s): -0.5722045898E-005 Af1(s/s): -0.3637978807E-011 week: 866 ******** Week 866 almanac for PRN-15 ******** ID: 15 Health: 000 Eccentricity: 0.8094310760E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9312186168 Rate of Right Ascen(r/s): -0.8320346576E-008 SQRT(A) (m 1/2): 5153.500488 Right Ascen at Week(rad): 0.8709718958E+000 Argument of Perigee(rad): 0.479959968 Mean Anom(rad): -0.8367134909E+000 Af0(s): -0.3042221069E-003 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-16 ******** ID: 16 Health: 000 Eccentricity: 0.8730411530E-002 Time of Applicability(s): 503808.0000

Orbital Inclination(rad): 0.9911097807 Rate of Right Ascen(r/s): -0.7737465154E-008 SQRT(A) (m 1/2): 5153.691406 Right Ascen at Week(rad): 0.3094076325E+001 Argument of Perigee(rad): 0.352232099 Mean Anom(rad): 0.9499000011E+000 Af0(s): -0.2765655518E-004 Af1(s/s): 0.3637978807E-011 week: 866 ******** Week 866 almanac for PRN-17 ******** ID: 17 Health: 000 Eccentricity: 0.1098394394E-001 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9756800912 Rate of Right Ascen(r/s): -0.7977475151E-008 SQRT(A) (m 1/2): 5153.616211 Right Ascen at Week(rad): -0.2167265057E+001 Argument of Perigee(rad): -1.933866285 Mean Anom(rad): 0.2161092807E-001 Af0(s): -0.2031326294E-003 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-18 ******** ID: 18 Health: 000 Eccentricity: 0.1692819595E-001 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9253942835 Rate of Right Ascen(r/s): -0.8228914196E-008 SQRT(A) (m 1/2): 5153.610840 Right Ascen at Week(rad): -0.1485366031E+000 Argument of Perigee(rad): -1.900863228 Mean Anom(rad): 0.1581769008E+001 Af0(s): 0.4997253418E-003 Af1(s/s): 0.3637978807E-011 week: 866 ******** Week 866 almanac for PRN-19 ******** ID: 19 Health: 000 Eccentricity: 0.1074504852E-001 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9727379640 Rate of Right Ascen(r/s): -0.8000333246E-008 SQRT(A) (m 1/2): 5153.560547 Right Ascen at Week(rad): -0.2118337586E+001 Argument of Perigee(rad): 0.733958500 Mean Anom(rad): -0.3127502950E+001 Af0(s): -0.5254745483E-003 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-20 ******** ID: 20 Health: 000 Eccentricity: 0.4712581635E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9266286586 Rate of Right Ascen(r/s): -0.8183198006E-008 SQRT(A) (m 1/2): 5153.653320 Right Ascen at Week(rad): -0.2004166872E+000 Argument of Perigee(rad): 1.353437316 Mean Anom(rad): -0.7501810205E+000 Af0(s): 0.4034042358E-003 Af1(s/s): 0.3637978807E-011 week: 866 ******** Week 866 almanac for PRN-21 ******** ID: 21 Health: 000 Eccentricity: 0.2334308624E-001 Time of Applicability(s): 503808.0000

SSP0001 GOST R 55534-2103


Page 23 of 29

Orbital Inclination(rad): 0.9357186932 Rate of Right Ascen(r/s): -0.8068907531E-008 SQRT(A) (m 1/2): 5153.588379 Right Ascen at Week(rad): -0.1190706148E+001 Argument of Perigee(rad): -1.808868947 Mean Anom(rad): 0.2449736609E+001 Af0(s): -0.5178451538E-003 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-22 ******** ID: 22 Health: 000 Eccentricity: 0.7826805115E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9232610914 Rate of Right Ascen(r/s): -0.8206056101E-008 SQRT(A) (m 1/2): 5154.995117 Right Ascen at Week(rad): -0.1477988242E+000 Argument of Perigee(rad): -2.002095099 Mean Anom(rad): -0.1108409726E+000 Af0(s): 0.3709793091E-003 Af1(s/s): -0.7275957614E-011 week: 866 ******** Week 866 almanac for PRN-23 ******** ID: 23 Health: 000 Eccentricity: 0.1066064835E-001 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9463786613 Rate of Right Ascen(r/s): -0.8171768958E-008 SQRT(A) (m 1/2): 5153.641113 Right Ascen at Week(rad): 0.9279332913E+000 Argument of Perigee(rad): -2.599040202 Mean Anom(rad): -0.1268415233E+001 Af0(s): -0.1678466797E-003 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-24 ******** ID: 24 Health: 000 Eccentricity: 0.4390716553E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9498181338 Rate of Right Ascen(r/s): -0.8023191341E-008 SQRT(A) (m 1/2): 5153.576660 Right Ascen at Week(rad): 0.1954329349E+001 Argument of Perigee(rad): 0.402162125 Mean Anom(rad): -0.1882723605E+001 Af0(s): -0.1525878906E-004 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-25 ******** ID: 25 Health: 000 Eccentricity: 0.5472660065E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9788439266 Rate of Right Ascen(r/s): -0.7851755629E-008 SQRT(A) (m 1/2): 5153.731445 Right Ascen at Week(rad): 0.3025093629E+001 Argument of Perigee(rad): 0.733778736 Mean Anom(rad): 0.2457797123E+001 Af0(s): -0.1449584961E-003 Af1(s/s): -0.7275957614E-011 week: 866 ******** Week 866 almanac for PRN-26 ******** ID: 26 Health: 000 Eccentricity: 0.9903907776E-003 Time of Applicability(s): 503808.0000

Orbital Inclination(rad): 0.9608316365 Rate of Right Ascen(r/s): -0.8034620388E-008 SQRT(A) (m 1/2): 5153.684570 Right Ascen at Week(rad): 0.3017103896E+001 Argument of Perigee(rad): 0.064435058 Mean Anom(rad): 0.1725278603E+001 Af0(s): -0.3147125244E-003 Af1(s/s): -0.1455191523E-010 week: 866 ******** Week 866 almanac for PRN-27 ******** ID: 27 Health: 000 Eccentricity: 0.3456115723E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9706527088 Rate of Right Ascen(r/s): -0.8057478483E-008 SQRT(A) (m 1/2): 5153.585938 Right Ascen at Week(rad): -0.2216842672E+001 Argument of Perigee(rad): 0.224509099 Mean Anom(rad): 0.6410736409E-001 Af0(s): 0.7820129395E-004 Af1(s/s): 0.3637978807E-011 week: 866 ******** Week 866 almanac for PRN-28 ******** ID: 28 Health: 000 Eccentricity: 0.1978206635E-001 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9897975081 Rate of Right Ascen(r/s): -0.7748894201E-008 SQRT(A) (m 1/2): 5153.584473 Right Ascen at Week(rad): 0.3099086106E+001 Argument of Perigee(rad): -1.618097688 Mean Anom(rad): 0.7889248961E+000 Af0(s): 0.5130767822E-003 Af1(s/s): 0.3637978807E-011 week: 866 ******** Week 866 almanac for PRN-29 ******** ID: 29 Health: 000 Eccentricity: 0.1057624817E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9766208528 Rate of Right Ascen(r/s): -0.7988904198E-008 SQRT(A) (m 1/2): 5153.543457 Right Ascen at Week(rad): -0.2157596784E+001 Argument of Perigee(rad): -0.438554097 Mean Anom(rad): 0.2498110558E+001 Af0(s): 0.6561279297E-003 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-30 ******** ID: 30 Health: 000 Eccentricity: 0.1849651337E-002 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9525385529 Rate of Right Ascen(r/s): -0.7954617056E-008 SQRT(A) (m 1/2): 5153.571777 Right Ascen at Week(rad): 0.2045510201E+001 Argument of Perigee(rad): 2.976603957 Mean Anom(rad): -0.2669070769E+001 Af0(s): 0.1125335693E-003 Af1(s/s): 0.3637978807E-011 week: 866 ******** Week 866 almanac for PRN-31 ******** ID: 31 Health: 000 Eccentricity: 0.8252143860E-002 Time of Applicability(s): 503808.0000

SSP0001 GOST R 55534-2103


Page 24 of 29

Orbital Inclination(rad): 0.9715695020 Rate of Right Ascen(r/s): -0.7760323249E-008 SQRT(A) (m 1/2): 5153.675293 Right Ascen at Week(rad): 0.2009665384E+001 Argument of Perigee(rad): -0.406641604 Mean Anom(rad): -0.2898616613E+001 Af0(s): 0.2756118774E-003 Af1(s/s): 0.0000000000E+000 week: 866 ******** Week 866 almanac for PRN-32 ******** ID: 32 Health: 000

Eccentricity: 0.1091957092E-003 Time of Applicability(s): 503808.0000 Orbital Inclination(rad): 0.9600406777 Rate of Right Ascen(r/s): -0.8023191341E-008 SQRT(A) (m 1/2): 5153.526855 Right Ascen at Week(rad): 0.9233006394E+000 Argument of Perigee(rad): -2.316074301 Mean Anom(rad): 0.2956953948E+000 Af0(s): 0.8583068848E-005 Af1(s/s): -0.3637978807E-011 week: 866

SSP0001 GOST R 55534-2103


Page 25 of 29

APPENDIX B : GLONASS ALMANAC (.AGL FORMAT) 30 03 2016 43200 1 1 1 30 03 2016 0.311715000E+05 0.000000000E+00 0.000000000E+00 0.141143799E-03 -0.4120054E+00 0.6711960E-02 -0.1791382E-01 0.3595352E-03 -0.2656176E+04 0.8544922E-03 30 03 2016 43201 2 -4 1 30 03 2016 0.364800625E+05 0.000000000E+00 0.000000000E+00 -0.183105469E-03 -0.5330372E+00 0.9342194E-02 -0.6798401E+00 0.1445770E-02 -0.2655951E+04 0.8544922E-03 30 03 2016 43202 3 5 1 30 03 2016 0.102203125E+04 0.000000000E+00 0.000000000E+00 -0.648498535E-04 0.2904472E+00 0.8404732E-02 -0.6440430E+00 0.1405716E-02 -0.2655996E+04 0.1159668E-02 30 03 2016 43203 4 6 1 30 03 2016 0.619046875E+04 0.000000000E+00 0.000000000E+00 -0.160217285E-03 0.1700058E+00 0.8515358E-02 -0.6274719E+00 0.5121231E-03 -0.2655969E+04 0.1220703E-02 30 03 2016 25204 5 1 1 30 03 2016 0.111274375E+05 0.000000000E+00 0.000000000E+00 0.381469727E-05 0.5292416E-01 0.6644249E-02 0.3413391E+00 0.3585815E-03 -0.2656045E+04 0.1037598E-02 30 03 2016 18814 6 -4 1 30 03 2016 0.164654375E+05 0.000000000E+00 0.000000000E+00 -0.839233398E-04 -0.7101822E-01 0.6612778E-02 0.7937927E+00 0.7486343E-03 -0.2655934E+04 0.9765625E-03 30 03 2016 18818 7 5 1 30 03 2016 0.213687812E+05 0.000000000E+00 0.000000000E+00 0.381469727E-05 -0.1816559E+00 0.8449554E-02 -0.6353760E+00 0.1203537E-02 -0.2655947E+04 0.9765625E-03 30 03 2016 18822 8 6 1 30 03 2016 0.263055312E+05 0.000000000E+00 0.000000000E+00 0.267028809E-04 -0.2963276E+00 0.8489609E-02 -0.4527283E+00 0.1761436E-02 -0.2655959E+04 0.9155273E-03 30 03 2016 18676 9 -6 1 30 03 2016 0.299038125E+05 0.000000000E+00 0.000000000E+00 -0.102996826E-03 0.2957907E+00 0.9177208E-02 -0.7069092E+00 0.1339912E-02 -0.2655738E+04 -0.1342773E-02 30 03 2016 43280 10 -7 1 30 03 2016 0.348216250E+05 0.000000000E+00 0.000000000E+00 -0.152587891E-04 0.1762466E+00 0.1487923E-01 0.8268738E+00 0.1654625E-02 -0.2655889E+04 -0.1281738E-02 30 03 2016 19144 11 0 1 30 03 2016 0.398703750E+05 0.000000000E+00 0.000000000E+00 -0.228881836E-04 0.5527782E-01 0.1273727E-01 0.3988647E-01 0.1928329E-02 -0.2655916E+04 -0.1281738E-02 30 03 2016 18698 12 -1 0 30 03 2016 0.449393750E+04 0.000000000E+00 0.000000000E+00 0.000000000E+00 0.8774529E+00 0.1044464E-01 0.8925171E+00 0.3373146E-02 -0.2655953E+04 -0.1342773E-02 30 03 2016 18702 13 -2 1 30 03 2016 0.969546875E+04 0.000000000E+00 0.000000000E+00 -0.762939453E-05 0.7555208E+00 0.1266289E-01 0.4612122E+00 0.7925034E-03 -0.2655900E+04 -0.1464844E-02 30 03 2016 18706 14 -7 1 30 03 2016 0.149427813E+05 0.000000000E+00 0.000000000E+00 -0.297546387E-03 0.6373196E+00 0.1479244E-01 0.8185120E+00 0.1605988E-02 -0.2655725E+04 -0.1464844E-02 30 03 2016 18710 15 0 1 30 03 2016 0.192088750E+05 0.000000000E+00 0.000000000E+00 -0.648498535E-04 0.5382318E+00 0.1478291E-01 -0.1525879E-01 0.2299309E-02 -0.2656260E+04 -0.1403809E-02 30 03 2016 18724 16 -1 1 30 03 2016 0.245991562E+05 0.000000000E+00 0.000000000E+00 -0.267028809E-04 0.4107065E+00 0.1048088E-01 0.1132507E+00 0.2592087E-02 -0.2655918E+04 -0.1464844E-02 30 03 2016 18728 17 4 1 30 03 2016 0.279656875E+05 0.000000000E+00 0.000000000E+00 0.228881836E-04 -0.9974432E+00 0.1004314E-01 -0.7627869E+00 0.7514954E-03 -0.2656287E+04 0.9155273E-03 30 03 2016 18732 18 -3 1 30 03 2016 0.327730000E+05 0.000000000E+00 0.000000000E+00 -0.915527344E-04 0.8893719E+00 0.1148796E-01 -0.1291809E+00 0.1705170E-02 -0.2656246E+04 0.9765625E-03 30 03 2016 18736

SSP0001 GOST R 55534-2103


Page 26 of 29

19 3 1 30 03 2016 0.381289063E+05 0.000000000E+00 0.000000000E+00 0.148773193E-03 0.7699308E+00 0.1270962E-01 -0.3051758E+00 0.2870560E-03 -0.2656477E+04 0.1037598E-02 30 03 2016 18740 20 2 1 30 03 2016 0.276596875E+04 0.000000000E+00 0.000000000E+00 0.225067139E-03 -0.4088068E+00 0.1277542E-01 -0.1058655E+00 0.1344681E-02 -0.2656330E+04 0.4882812E-03 30 03 2016 42304 21 4 1 30 03 2016 0.756540625E+04 0.000000000E+00 0.000000000E+00 -0.572204590E-04 -0.5252981E+00 0.1115513E-01 -0.8102417E+00 0.4358292E-03 -0.2656135E+04 0.5493164E-03 30 03 2016 42308 22 -3 1 30 03 2016 0.126722500E+05 0.000000000E+00 0.000000000E+00 -0.194549561E-03 -0.6437893E+00 0.1219749E-01 -0.3411865E-01 0.3011703E-02 -0.2655998E+04 0.7934570E-03 30 03 2016 42312 23 3 1 30 03 2016 0.180192812E+05 0.000000000E+00 0.000000000E+00 0.953674316E-04 -0.7681351E+00 0.1210403E-01 0.4797363E-01 0.1916885E-03 -0.2655924E+04 0.8544922E-03 30 03 2016 42316 24 2 1 30 03 2016 0.227588125E+05 0.000000000E+00 0.000000000E+00 0.133514404E-03 -0.8780346E+00 0.1215839E-01 0.3186646E+00 0.7171631E-03 -0.2656008E+04 0.8544922E-03

SSP0001 GOST R 55534-2103


Page 27 of 29

APPENDIX C D1 GLONASS INTERFERENCE PROFILE

SSP0001 GOST R 55534-2103


Page 28 of 29

APPENDIX D D1 GPS INTERFERENCE PROFILE

SSP0001 GOST R 55534-2103


Page 29 of 29

Spirent Global Services contact details: In the US, Government/Contractors and Universities Spirent Federal Systems Inc. 1402 W. State Rd. Pleasant Grove 84062 Utah USA Tel: +1 801 785 1448 Fax: +1 801 785 1294 E-mail: [email protected] In the US Commercial, and rest of Americas Spirent Communications Inc 541 Industrial Way West Eatontown, NJ 07724 USA Tel: 1.800.SPIRENT Fax: +1 732 544 8347 E-mail: [email protected] Asia Pacific (All Customers) Spirent Communications, Shining Tower, No. 35, Xueyuan Road, Room 1302, Beijing 100191, China Tel (Toll free mainland China): 400 810 9529 Tel (Outside mainland China): +86 400 810 9529 E-mail: [email protected] All other Regions and Customers Spirent Communications plc, Aspen Way, Paignton, Devon TQ4 7QR United Kingdom Tel: + 44 1803 546333 Fax: + 44 1803 546302 E-mail: [email protected]

spirent.com Spirent Communications plc, Aspen Way, Paignton, Devon TQ4 7QR, UK Tel +44 (0)1803 546300 Fax +44 (0)1803 546301 http://www.spirent.com/Solutions/GNSS-Developers Registered in England Number 00470893 Registered office: Northwood Park, Gatwick Road, Crawley, West Sussex RH10 9XN, UK © 2016 Spirent. All Rights Reserved. All of the company names and/or brand names and/or product names referred to in this document, in particular, the name “Spirent” and its logo device, are either registered trademarks or trademarks of Spirent plc and its subsidiaries, pending registration in accordance with relevant national laws. All other registered trademarks or trademarks are the property of their respective owners.

The information contained in this document is subject to change without notice and does not represent a commitment on the part of Spirent. The information in this document is believed to be accurate and reliable; however, Spirent assumes no responsibility or liability for any errors or inaccuracies that may appear in the document.

mailto:[email protected]



http://www.spirent.com/Solutions/GNSS-Developers

Date post:	26-Jun-2020
Category:	Documents
Upload:	others
View:	12 times
Download:	0 times

Spirent Scenario Package for testing GOST R … › resources › sites › SPIRENT...GOST R...

Documents