ITU-R S 1557-2002 Operational requirements and characteristics of fixed-satellite service systems operating in the 50 40 GHz bands for use in sharing studies between the fixed-sate.pdf

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1、 Rec. ITU-R S.1557 1 RECOMMENDATION ITU-R S.1557 Operational requirements and characteristics of fixed-satellite service systems operating in the 50/40 GHz bands for use in sharing studies between the fixed-satellite service and the fixed service*(Question ITU-R 250-1/4) (2002) The ITU Radiocommunic

2、ation Assembly, considering a) that the band 37.5-42.5 GHz is allocated to the fixed service and the fixed-satellite service (FSS) (space-to-Earth) on a co-primary basis; b) that some FSS systems plan to provide data rates ranging from synchronous transfer mode 1 (STM-1) or higher, up to 10 STM-4; c

3、) that most FSS systems propose using small earth station antennas, less than 1 m in diameter for the user link, to provide end-to-end link availability of at least 99.7%; d) that FSS systems may need to use larger earth terminal antennas, of up to 3 m in diameter, for gateway applications involving

4、 individually-coordinated earth stations at geographically dispersed hubs or fibre access points (FAPs) and that these applications will require the end-to-end link availability of at least 99.9%; e) that the feasibility of using larger antennas having a diameter greater than 2.4 m (D/ 300), given t

5、he effects of main reflector distortion, surface roughness, radome attenuation and auto tracking facilities capable of minimizing pointing loss in this band, remains to be determined; f) that some proposed FSS systems operating in this band use on-board processing for small earth terminal users, and

6、 use a transparent transponder for gateway or hub/FAP applications; g) that the propagation impairments are very severe in this frequency range; h) that most FSS systems plan to provide a clear-air bit error ratio (BER) of the order of 1 107to 1 1010; j) that current planned FSS systems use quadratu

7、re phase shift keying (QPSK) modulation, and future FSS systems may use higher order modulation schemes such as 8-PSK or quadrature amplitude modulation, 16-QAM, _ *This Recommendation should be brought to the attention of Radiocommunication Study Groups 7, 8 and 9 and Joint Working Party 4-9S. 2 Re

8、c. ITU-R S.1557 recommends 1 that FSS system design and sharing studies in the band 37.5-42.5 GHz should take into account the operational requirements in Annexes 1 and 2; 2 that FSS characteristics in Annexes 3 through 6 which contain technical information on some FSS systems operating in the 37.5-

9、42.5 GHz band, should be taken into consideration when conducting sharing studies between the 50/40 GHz FSS service and co-frequency, co-primary services; 3 that administrations planning modifications to these systems or proposing future satellite networks in the 50/40 GHz bands should submit FSS ne

10、twork technical characteristics to ITU-R to update the Annexes. ANNEX 1 Required downlink parameters of FSS systems operating in the 37.5-42.5 GHz band 1 Introduction This Annex presents data on the required downlink power flux-density (pfd) in the 37.5-42.5 GHz band to allow FSS systems operating i

11、n this band to operate with various earth terminal antenna sizes. The study is based on the proposed FSS operating in the 50/40 GHz bands. Based on the ITU filing, a considerable number of FSS systems, planned to operate within the bands 37.5-42.5 GHz and 47.2-50.2 GHz, have been received. These sys

12、tems plan to provide data rates ranging from video-conferencing quality through very high speed transmission of STM-1 (155 Mbit/s) or higher, up to 10 STM-1, to earth terminal antennas ranging in size from 1 m to 3 m. Most FSS systems propose using small earth terminals, less than 1 m in diameter, t

13、o provide 99.7% link availability, and the systems using bigger earth terminal antenna sizes, from 1.5-3 m for gateway-to-gateway or hub-to-hub applications, will require higher link availability. Because the propagation impairments are very severe in the 40/50 GHz bands, most proposed systems will

14、provide service at higher minimum elevation angles than FSS systems operating in frequency bands below 30 GHz. The typical minimum operational elevation angle at 40/50 GHz is 20; however, some systems, like the GSO SV plan to provide service at a 15 minimum elevation angle. Technical characteristics

15、 of several proposed FSS systems planning to operate in these bands have been included in Recommendation ITU-R S.1328. The purpose of this Annex is to provide additional technical characteristics of the FSS systems operating in the 40/50 GHz bands for use in future sharing studies in ITU-R. Rec. ITU

16、-R S.1557 3 2 Required earth terminal antenna size vs. downlink pfd This section contains computations of the downlink pfd levels that are required to allow the FSS satellite networks operating in the 40/50 GHz band to operate with various earth terminal antenna sizes and desired link availabilities

17、. The pfd at the Earths surface can be shown as: =+=spsBWfGSpfdSrxE1log10)(log2045.21/where: pfd : power flux-density (dB(W/(m2.MHz) S : receive signal strength (dBW) BW : transmit bandwidth (necessary bandwidth) (MHz) sps : symbol rate (Msymbols) f : frequency (GHz) GrxE/S: on-axis gain of receivin

18、g earth station (dBi). The received Eb/(N0+ I0) at the receiver can be computed as: )log(10)(0000sbpINSINEb+=+and )()(log10)(log20)(log204.20()(00/0000INfDGSINSINSSrxE+=+=+and +=+101000001010log10)(ININ where: N0= 228.6 + 10 log(T) (dB(W/Hz), thermal noise power density T : earth station receiver no

19、ise temperature + noise temperature increases due to rain (K) I0: self interference + interference from other FSS systems operating in the same band (dB(W/Hz) D : earth station antenna diameter (m) f : frequency (GHz) : earth station antenna efficiency bps : bit rate. 4 Rec. ITU-R S.1557 It is impor

20、tant to note that the FSS downlink must satisfy the pfd limits at all slant ranges and elevation angles, while the Eb/N0of interest to a designer is the minimum Eb/N0over all slant ranges, elevation angles, and positions within a beam. Also the calculated pfd at the Earths surface is based on the fr

21、ee-space propagation conditions. The received downlink Eb/N0at the FSS receiver, can be shown as: systemfadepscinatmbMMEOCLLINDbpsspspfdINE05.61)()log(10)log(20log10/0000+=+where: Latm/scin: atmospheric loss and scintillation loss. In this band, the atmospheric and scintillation loss are about 1.2 d

22、B Lp: depending on antenna size (dB) EOC : edge of coverage, typically 3.5 dB Mfade: required rain fade margin to achieve its link availability (dB) Msystem: system margin (2 dB is allocated to system margin). From the above expressions the receive earth terminal antenna size in metres can be shown

23、as: =+systemfadepscinatmbMMEOCLLINbpsspspfdINED/000005.61)()log(10log1020110 2.1 Downlink Eb/(N0+ I0) The required receive Eb/(N0+ I0) depends on the modulation (QPSK, 8-PSK, 16-QAM, etc.), BER, coding and implementation loss. Most of the proposed systems in these bands plan to use QPSK modulation a

24、nd to provide a BER of the order of 1 107to 1 109. The required Eb/(N0+ I0), including the implementation loss, is in the range from 7 dB to 9 dB depending on the coding. If the higher modulations such as 8-PSK, 16-QAM, etc. are used, the required Eb/(N0+ I0) is significantly higher. In this study,

25、both QPSK and 8-PSK modulations are used. The required downlink Eb/(N0+ I0) depends on whether the satellite payload functions as an on-board processor (OBP) or a transparent transponder (bent-pipe (BP). In the case of an OBP, the downlink Eb/(N0+ I0) is the same as the required Eb/(N0+ I0) to achie

26、ve its BER. When the satellite payload functions as a transparent transponder, the downlink Eb/(N0+ I0) can be computed as: +=+0000)1.0()1.0(001010log10INEINEbbbrequiredINERec. ITU-R S.1557 5 In this study, the downlink Eb/(N0+ I0) is assumed to be equal to uplink Eb/(N0+ I0). Therefore the downlink

27、 Eb/(N0+ I0) is 3 dB higher than the required receive Eb/(N0+ I0). 2.2 Thermal noise density, N0and interference noise density, I0Thermal noise density, N0, can be shown as: N0= 228.6 + 10 log(Trx+ Train) dB(W/Hz) where: Trx: earth station receive system noise temperature (K). Typical ground antenna

28、 system temperature is 800 K (antenna noise temperature = 70 K, Receiver noise figure = 4.5 dB, filter/diplexer = 0.7 dB and cable loss = 0.3 dB) Traincan be computed as: Train= 280 (1 100.1 (rain fade margin) For example, if the rain fade margin is 18 dB, the noise temperature increase due to rain

29、is 275 K. Interference noise density, I0: Calculated interference noise density should include intra- and inter-system noise density. In this study, 1.5 dB is allocated to the intra-system interference. Calculated inter-system interference from other FSS systems operating in the same frequency band

30、depends on the earth station antenna roll-off and the downlink pfd from other FSS systems. In this study, all FSS systems are assumed to operate at the same pfd and the geostationary-satellite orbit (GSO) is assumed to be populated at 4 intervals. For example, if all GSO FSS systems operate at a dow

31、nlink pfd of 105 dB (W/(m2 MHz), the received interference noise density of 1 m earth terminal operating in the 40 GHz band is 203.44 dB(W/Hz). 2.3 Required rain fade margin As mentioned above, most proposed systems plan to provide 99.7% link availability to the very small aperture terminal (VSAT) u

32、sers and provide higher link availability to gateway-to-gateway or hub-to-hub users. The required rain fade margin is shown in Fig. 1. In the calculation, 99.7% link availability and a 25 elevation angle are assumed. Figure 2 shows the link availability of FSS systems operating in the 40 GHz band wi

33、th an 18 dB rain fade margin. Figure 2 shows that the 18 dB rain fade margin will not achieve the 99.7% link availability for most locations around world. In addition, the systems that plan to provide service at elevation angles less than 25 must use mitigation techniques, such as variable data rate

34、s, site diversity, frequency diversity, heavy coding, etc. to achieve the desired link availability. 6 Rec. ITU-R S.1557 1557-01180 140 100 60 20 20 60 100 140 180906030030609060 dB50 dB40 dB30 dB20 dB10 dB0 dBFIGURE 1Required rain fade margin(Frequency band = 40 GHz; elevation angle = 25; link avai

35、lability = 99.7%)1557-02180 140 100 60 20 20 60 100 140 1809060300306090FIGURE 2Link availability(Frequency band = 40 GHz; elevation angle = 25; rain fade margin = 18 dB)99.0%99.1%99.2%99.3%99.4%99.5%99.6%99.7%99.8%99.9%99.95%2.4 Pointing loss The off-axis antenna pointing loss (dB) for an idea unif

36、ormly-illuminated circular aperture can be derived from physical optics: 21)(2log10=xxJLoss Rec. ITU-R S.1557 7 where: )sin(=cDfx and f : frequency D : antenna diameter c : speed of light : off-axis angle J1(x) : first order of Bessell function. For an off-axis angle of 0.1 the pointing loss versus

37、earth terminal antenna size is shown in Fig. 3. In this study, 0.7 dB is allocated to earth terminal antenna pointing loss. 1557-031201234567FIGURE 3Antenna pointing loss vs. antenna size (off-axis angle = 0.1)Loss(dB)Antenna size (m)0.5 0.75 1.25 1.5 1.75 2.25 2.5 2.752.5 Results Figure 4 shows the

38、 required earth terminal antenna size versus the downlink pfd level. The calculation is based on the following assumptions: Rain fade margin = 18 dB Earth terminal receive noise temperature = 800 K Pointing loss = 0.7 dB Atmospheric and scintillation loss = 1.2 dB Degradation due to self-interferenc

39、e = 1.5 dB EOC = 3.5 dB Antenna efficiency = 70% Frequency = 40 GHz System margin = 2 dB 8 Rec. ITU-R S.1557 Required Eb/N0: OBP: QPSK = 7.0 dB 8-PSK = 10.5 dB BP (transparent transponder): QPSK = 10.0 dB 8-PSK = 13.5 dB. 1557-04125121086420120 115 110 105 100 9514161820FIGURE 4Earth terminal antenn

40、a size vs. downlinkpfd levelsAntenna diameter(m)pfd (dB(W/(m2 MHz)OBP/QPSKBP/QPSKOBP/8-PSKBP/8-PSK3 Discussion of results Most proposed FSS systems operating in the 40/50 GHz bands use OBP for VSAT users, and use a transparent transponder or BP for gateway-to-gateway or hub-to-hub users. The typical

41、 antenna diameter of VSAT users is in a range from 0.5 m to 1 m, and the antenna diameter of gateway-to-gateway or hub-to-hub users is in a range from 1 m to 3 m. Most proposed FSS systems in the 40/50 GHz do not plan to use earth terminal antennas bigger than 3 m because the complexity of an auto t

42、rack antenna capable of minimizing pointing loss in these frequency bands is very high. Figure 4 shows that for a QPSK system a downlink pfd level of 95 dB(W/(m2.MHz) will allow the use of a 1 m user terminal VSAT operating in this band. The 3 m gateway-to-gateway antenna size may close the link wit

43、h a pfd level of 105 dB(W/(m2.MHz). If the smaller antenna size is used, the pfd must be greater than 95 dB(W/(m2.MHz) for VSAT and 105 dB(W/(m2.MHz) for gateway users. However, required downlink pfd levels can be different depending on the rain region. Furthermore, if higher modulations, such as 8-

44、PSK, 16-QAM are used, the required downlink pfd levels will be significantly increased. Rec. ITU-R S.1557 9 4 Summary This Annex shows that, for the example system described, in order to allow 3 m gateway-to-gateway or hub-to-hub users to operate in the 40/50 GHz band, the downlink pfd level must be

45、 greater than or equal to 105 dB (W/(m2.MHz). This Annex also show that the downlink pfd level must be greater than or equal to 95 dB (W/(m2.MHz) in order to operate a 1 m VSAT in the same band. Even with these levels, it is shown that even with an 18 dB rain fade margin, the FSS systems still would

46、 not be able to achieve their desired 99.7% link availability for all locations around the world. However, required downlink pfd levels can be different, depending on the rain region. Finally, a system that plans to operate at higher-order modulations and/or low elevation angles and/or smaller anten

47、nas, would need to either operate at higher pfd levels or use mitigation techniques, such as site diversity or frequency diversity, in order to achieve its link availability. ANNEX 2 Examination of Table 21-4 of the Radio Regulations (RR) pfd values required for the GSO satellites in the FSS to oper

48、ate viable downlinks into gateway earth stations in the 37.5-40 GHz and 42-42.5 GHz frequency bands 1 Introduction This study examines the constraints imposed by both downlink pfd and the effect of elevation angle of the receiving gateway FSS earth station in the 37.5-40 GHz and the 42-42.5 GHz bands. FSS downlinks, all meeting the pfd limits from RR Table 21-4, having various forms of modulation and coding characteristics are examined by calculating link availabilities on GSO FSS downlinks to gateway earth stations ranging from 1.8 to 3 m in diameter over a ra