ETSI TS 102 188-5-2004 Satellite Earth Stations and Systems (SES) Regenerative Satellite Mesh - A (RSM-A) air interface Physical layer specification Part 5 Radio transmission and r_1.pdf

1、 ETSI TS 102 188-5 V1.1.2 (2004-07)Technical Specification Satellite Earth Stations and Systems (SES);Regenerative Satellite Mesh - A (RSM-A) air interface;Physical layer specification;Part 5: Radio transmission and receptionETSI ETSI TS 102 188-5 V1.1.2 (2004-07) 2 Reference RTS/SES-00207-5 Keyword

2、s air interface, broadband, IP, multimedia, satellite ETSI 650 Route des Lucioles F-06921 Sophia Antipolis Cedex - FRANCE Tel.: +33 4 92 94 42 00 Fax: +33 4 93 65 47 16 Siret N 348 623 562 00017 - NAF 742 C Association but non lucratif enregistre la Sous-Prfecture de Grasse (06) N 7803/88 Important

3、notice Individual copies of the present document can be downloaded from: http:/www.etsi.org The present document may be made available in more than one electronic version or in print. In any case of existing or perceived difference in contents between such versions, the reference version is the Port

4、able Document Format (PDF). In case of dispute, the reference shall be the printing on ETSI printers of the PDF version kept on a specific network drive within ETSI Secretariat. Users of the present document should be aware that the document may be subject to revision or change of status. Informatio

5、n on the current status of this and other ETSI documents is available at http:/portal.etsi.org/tb/status/status.asp If you find errors in the present document, send your comment to: editoretsi.org Copyright Notification No part may be reproduced except as authorized by written permission. The copyri

6、ght and the foregoing restriction extend to reproduction in all media. European Telecommunications Standards Institute 2004. All rights reserved. DECTTM, PLUGTESTSTM and UMTSTM are Trade Marks of ETSI registered for the benefit of its Members. TIPHONTMand the TIPHON logo are Trade Marks currently be

7、ing registered by ETSI for the benefit of its Members. 3GPPTM is a Trade Mark of ETSI registered for the benefit of its Members and of the 3GPP Organizational Partners. ETSI ETSI TS 102 188-5 V1.1.2 (2004-07) 3 Contents Intellectual Property Rights5 Foreword.5 1 Scope 6 2 References 6 3 Definitions,

8、 symbols and abbreviations .7 3.1 Definitions7 3.2 Symbols7 3.3 Abbreviations .7 4 Introduction to radio transmission and reception .8 5 Frequency bands and channel arrangement9 5.1 Frequency bands.9 5.2 Downlink channel arrangement9 5.2.1 Downlink TDM carriers9 5.3 Uplink channel arrangement.9 5.3.

9、1 Uplink sub-bands 9 5.3.2 Uplink FDMA carrier modes10 5.3.2.1 Uplink allocated bandwidths and configurations 10 5.3.2.2 Uplink carrier centre frequency.10 6 Stability requirements.13 6.1 Frequency and symbol timing stability 13 6.2 Transmit signal accuracy13 6.2.1 Uplink input phase non-linearity 1

10、4 6.2.2 Uplink input amplitude non-linearity14 6.2.3 Uplink output amplitude non-linearity15 6.2.4 In-band spurs 15 6.2.5 Phase noise15 6.3 Frequency and mode switching16 6.3.1 Transmit frequency switching.16 6.3.2 Receiver carrier mode switching 16 7 Transmitter characteristics .17 7.1 Output power

11、17 7.1.1 ST power class17 7.1.2 Power control range17 7.1.3 Off-axis eirp18 7.1.3.1 Co-polar limits 18 7.1.3.2 Cross-polar limits18 7.2 Transmit antenna characteristics 19 7.2.1 Antenna radiation pattern19 7.2.2 Transmit polarization19 7.2.3 Transmit antenna losses 19 7.2.3.1 Wet antenna losses 19 7

12、.2.3.2 Pointing losses.19 7.2.4 Pointing accuracy19 7.3 Ramp-up and ramp-down.20 7.4 Output RF spectrum .21 7.4.1 Emissions due to modulation21 7.4.2 Adjacent channel interference.21 7.4.3 Carrier-off conditions .21 7.5 Spurious emissions.21 7.5.1 Transmitter spurious emissions.21 7.5.2 Off-axis spu

13、rious radiation .21 7.5.3 On-axis spurious radiation 22 ETSI ETSI TS 102 188-5 V1.1.2 (2004-07) 4 8 Receiver characteristics22 8.1 Receive antenna characteristics22 8.1.1 Receiver figure of merit22 8.1.2 Receiver discrimination 22 8.1.3 Receive polarization .23 8.1.4 Receive antenna losses23 8.1.4.1

14、 Wet antenna losses 23 8.1.4.2 Depointing losses 23 8.2 Receiver performance.23 8.2.1 Definitions 23 8.2.1.1 Received Isotropic Power (RIP)23 8.2.1.2 Packet Loss Rate (PLR) 23 8.2.2 Receiver sensitivity.23 8.2.2.1 Receiver packet loss rate for PTP transmissions.23 8.2.2.2 Receiver packet loss rate f

15、or Broadcast transmissions23 8.2.2.3 Receiver dynamic range24 8.3 Receive signal quality 24 8.3.1 Beacon measurements.24 8.3.2 PTP measurements24 Annex A (normative): Downlink telemetry signals.25 A.1 General .25 A.2 Downlink telemetry signals25 Annex B (informative): Bibliography.26 History 27 ETSI

16、 ETSI TS 102 188-5 V1.1.2 (2004-07) 5 Intellectual Property Rights IPRs essential or potentially essential to the present document may have been declared to ETSI. The information pertaining to these essential IPRs, if any, is publicly available for ETSI members and non-members, and can be found in E

17、TSI SR 000 314: “Intellectual Property Rights (IPRs); Essential, or potentially Essential, IPRs notified to ETSI in respect of ETSI standards“, which is available from the ETSI Secretariat. Latest updates are available on the ETSI Web server (http:/webapp.etsi.org/IPR/home.asp). Pursuant to the ETSI

18、 IPR Policy, no investigation, including IPR searches, has been carried out by ETSI. No guarantee can be given as to the existence of other IPRs not referenced in ETSI SR 000 314 (or the updates on the ETSI Web server) which are, or may be, or may become, essential to the present document. Foreword

19、This Technical Specification (TS) has been produced by ETSI Technical Committee Satellite Earth Stations and Systems (SES). The present document is part 5 of a multi-part deliverable covering the BSM Regenerative Satellite Mesh - A (RSM-A); air interface; Physical layer specification, as identified

20、below: Part 1: “General description“; Part 2: “Frame structure“; Part 3: “Channel coding“; Part 4: “Modulation“; Part 5: “Radio transmission and reception“; Part 6: “Radio link control“; Part 7: “Synchronization“. ETSI ETSI TS 102 188-5 V1.1.2 (2004-07) 6 1 Scope The present document defines the Rad

21、io Frequency (RF) requirements for the Satellite Terminal (ST) transceiver of the Regenerative Satellite Mesh - A (RSM-A); Air interface operating in the Fixed Satellite System (FSS) allocations at Ka-band as follows: ST reception is in the Fixed Satellite Service (FSS) frequency ranges from 17,70 G

22、Hz to 19,70 GHz and from 19,70 GHz to 20,20 GHz; ST transmission is in the frequency ranges allocated to FSS from 27,50 GHz to 29,50 GHz and from 29,50 GHz to 30,00 GHz. Requirements are defined for two categories of parameters: those that are required to provide compatibility between the radio chan

23、nels, connected either to separate or common antennas, that are used in the system. This category also includes parameters providing compatibility with existing systems in the same or adjacent frequency bands; those that define the transmission quality of the system. These requirements apply to all

24、types of ST that transmit a single modulated carrier, including STs with an antenna diameter greater than 1,8 m (or equivalent corresponding aperture). The technical requirements of the present document apply under the environmental profile for operation of the equipment, which shall be declared by

25、the manufacturer. The equipment shall comply with all the technical requirements of the present document at all times when operating within the boundary limits of the declared operational environmental profile. The environmental profile for operation of the equipment shall include the ranges of humi

26、dity, temperature and supply voltage. 2 References The following documents contain provisions which, through reference in this text, constitute provisions of the present document. References are either specific (identified by date of publication and/or edition number or version number) or non-specif

27、ic. For a specific reference, subsequent revisions do not apply. For a non-specific reference, the latest version applies. Referenced documents which are not found to be publicly available in the expected location might be found at http:/docbox.etsi.org/Reference. 1 ETSI EN 301 459 (V1.2.1): “Satell

28、ite Earth Stations and Systems (SES); Harmonized EN for Satellite Interactive Terminals (SIT) and Satellite User Terminals (SUT) transmitting towards satellites in geostationary orbit in the 29,5 to 30,0 GHz frequency bands covering essential requirements under article 3.2 of the R Guidance for gene

29、ral purpose earth stations transmitting in the 5,7 GHz to 30,0 GHz frequency bands towards geostationary satellites and not covered by other ETSI specifications or standards“. ETSI ETSI TS 102 188-5 V1.1.2 (2004-07) 7 3 Definitions, symbols and abbreviations 3.1 Definitions For the purposes of the p

30、resent document, the following terms and definitions apply: allocated bandwidth: width of the frequency band within 1,25 (symbol rate/2) of the carrier frequency carrier transmission bandwidth: width of the frequency band within 1,4 (symbol rate/2) of the carrier frequency necessary bandwidth: width

31、 of the frequency band which is just sufficient to ensure the transmission of information at the rate and with the quality required under specified conditions out-of-band emission: emission on a frequency or frequencies immediately outside the necessary bandwidth which results from the modulation pr

32、ocess, but excluding spurious emissions Received Isotropic Power (RIP): power that would be received by an isotropic antenna Packet Loss Rate (PLR): ratio of RSM-A packets that are lost relative to total number of RSM-A packets received NOTE: The PLR is measured after Forward Error Correction (FEC).

33、 satellite payload: part of the satellite that provides air interface functions NOTE: The satellite payload operates as a packet switch that provides direct unicast and multicast communication between STs at the link layer. Satellite Terminal (ST): terminal installed in the user premises spurious em

34、ission: emission on a frequency or frequencies which are outside the necessary bandwidth and the level of which may be reduced without affecting the corresponding transmission of information NOTE: Spurious emissions include harmonic emissions, parasitic emissions, intermodulation products and freque

35、ncy conversion products, but exclude out-of-band emissions. unwanted emissions: consist of spurious emissions and out-of-band emissions 3.2 Symbols For the purposes of the present document, the following symbols apply: kph klilometre per hour ms millisecond (10-3second) s microsecond (10-6second) 3.

36、3 Abbreviations For the purposes of the present document, the following abbreviations apply: ASK Amplitude Shift Keyed C/N Carrier to Noise C/No Carrier to Noise density FDMA Frequency Division Multiple Access FEC Forward Error Correction FSS Fixed Satellite Service G/T Gain/Temperature HPA High Pow

37、er Amplifier I In phase kbps kilo bits per second (thousands of bits per second) LHCP Left Hand Circular Polarization Mbps Mega bits per second (millions of bits per second) ETSI ETSI TS 102 188-5 V1.1.2 (2004-07) 8 PHY PHYsical PLR Packet Loss Rate p-p peak-to-peakPTP Point-to-Point Q Quadrature RF

38、 Radio Frequency RHCP Right Hand Circular Polarization RIP Received Isotropic Power RSM Regenerative Satellite Mesh Rx Receive SLC Satellite Link Control ST Satellite Terminal TDM Time Division Multiplex Tx Transmit ULPC UpLink Power Control 4 Introduction to radio transmission and reception The fun

39、ctions of the physical layer are different for the uplink and downlink. The major functions are illustrated in figure 4. UPLINK DOWNLINK Part 3: Channel coding Part 2: Frame structure Part 4: Modulation Part 5: Radio transmission and reception tn Part 7: Synchronization Block interleaving Inner codi

40、ng (convolutional) Downlink burst building Downlink modulation (QPSK) ST receiver Scrambling Assemble packets into code blocks Outer coding (Reed-Solomon) No interleaving Inner coding (hamming) Uplink burst building Uplink modulation (OQPSK) Part6:Radio linkcontrolScrambling Timing and frequency con

41、trol ST transmitter Assemble packets into code blocks Outer coding (Reed-Solomon) Figure 4: Physical layer functions The present document describes the ST radio transmission and reception functions - this group of functions is highlighted in figure 4. Clause 5 describes the frequency bands and chann

42、el arrangements for the uplink and the downlink. ETSI ETSI TS 102 188-5 V1.1.2 (2004-07) 9 Clause 6 describes the ST stability requirements. Clause 7 describes the ST transmitter requirements. Clause 8 describes the ST receiver requirements. 5 Frequency bands and channel arrangement 5.1 Frequency ba

43、nds The operating frequency bands are defined in table 5.1. Table 5.1: Operating frequency bands Band designation Uplink frequency band Downlink frequency band Frequency band A 29,5 GHz to 30,0 GHz 19,7 GHz to 20,2 GHz 5.2 Downlink channel arrangement 5.2.1 Downlink TDM carriers The downlink Time Di

44、vision Multiplex (TDM) transmission uses a single carrier in one of two polarizations. The carrier transmits TDM timeslots in one of three possible operating modes. These modes are referred to as full-rate, 1/3-rate, and 1/4-rate corresponding to the burst rate of the carrier during that timeslot. T

45、he downlink carrier centre frequencies are defined in table 5.2.1. Table 5.2.1: Downlink carrier centre frequencies (Frequency band A) Carrier mode Carrier bandwidth (MHz) Centre frequency (GHz) Full-Rate 500 19,950 1/3-Rate 500 19,951/4-Ra 19,950 5.3 Uplink channel arrangement 5.3.1 Uplink sub-band

46、s An uplink sub-band is a contiguous 62,5 MHz spectrum portion within an uplink frequency band. There are eight possible 62,5 MHz sub-bands of spectrum in each polarization for the uplink frequency band. The uplink sub-bands allocated to the right-hand polarization are referred as sub-bands 0 throug

47、h 7. The uplink sub-bands allocated to the left-hand polarization are referred as sub-bands 8 through 15. The starting frequency (or the lower-band edge) and the centre frequency for each sub-band is as listed in table 5.3.1 for Uplink Frequency Band A. The sub-band starting frequency is derived fro

48、m the following equation: () MHz 5,62GHz 5,29band-sub offrequency Starting += KM where: K = M in modulo-8 M = sub-band designator, M = 0 to 15 Centre of Frequency of Sub-band (M) = Starting Frequency of Sub-band (M) + 31,25 MHz ETSI ETSI TS 102 188-5 V1.1.2 (2004-07) 10Table 5.3.1: Uplink sub-band s

49、tarting and centre frequencies (frequency band A) Sub-band designator Sub-band starting frequency in uplink frequency band A Sub-band centre frequency in uplink frequency band A RHCP LHCP (Hz) (Hz) 0 8 29,500000E+09 29,531250E+09 1 9 29,562500E+09 29,593750E+09 2 10 29,625000E+09 29,656250E+09 3 11 29,687500E+09 29,718750E+09 4 12 29,750000E+09 29,781250E+09 5 13 29,812500E+09 29,843750E+09 6 14 29,875000E+09 29,906250E+09 7 15 29,937500E+09 29,968750E+09 NOTE: All frequencies are defined with respect to a satellite master oscillator that has the stability p