ITU-T G 747-1993 Second Order Digital Multiplex Equipment Operating at 6312 kbit s and Multiplexing Three Tributaries at 2048 kbit s - General Aspects of Digital Transmission Syste.pdf

上传人:brainfellow396 文档编号:796471 上传时间:2019-02-02 格式:PDF 页数:8 大小:65.98KB
下载 相关 举报
ITU-T G 747-1993 Second Order Digital Multiplex Equipment Operating at 6312 kbit s and Multiplexing Three Tributaries at 2048 kbit s - General Aspects of Digital Transmission Syste.pdf_第1页
第1页 / 共8页
ITU-T G 747-1993 Second Order Digital Multiplex Equipment Operating at 6312 kbit s and Multiplexing Three Tributaries at 2048 kbit s - General Aspects of Digital Transmission Syste.pdf_第2页
第2页 / 共8页
ITU-T G 747-1993 Second Order Digital Multiplex Equipment Operating at 6312 kbit s and Multiplexing Three Tributaries at 2048 kbit s - General Aspects of Digital Transmission Syste.pdf_第3页
第3页 / 共8页
ITU-T G 747-1993 Second Order Digital Multiplex Equipment Operating at 6312 kbit s and Multiplexing Three Tributaries at 2048 kbit s - General Aspects of Digital Transmission Syste.pdf_第4页
第4页 / 共8页
ITU-T G 747-1993 Second Order Digital Multiplex Equipment Operating at 6312 kbit s and Multiplexing Three Tributaries at 2048 kbit s - General Aspects of Digital Transmission Syste.pdf_第5页
第5页 / 共8页
点击查看更多>>
资源描述

1、INTERNATIONAL TELECOMMUNICATION UNION)45G134 TELECOMMUNICATIONSTANDARDIZATION SECTOROF ITU%.%2!,G0G0!30%#43G0G0/ i = 1, 2, 3) (see Note 5 toTable 1/G.747).Positive justification should be indicated by the justification control signal 111 and no justification by the signal000. Majority decision is re

2、commended.Table 1/G.747 gives the maximum justification rate per tributary and the nominal justification ratio.2 Fascicle III.4 - Rec. G.747TABLE 1/G.7476312 kbit/s multiplexing frame structureNominal tributary bit rate (kbit/s) 2048Number of tributaries 3Frame structure Bit numberFrame alignment si

3、gnal (111010000)Bits from tributariesAlarm indication to the remote multiplex equipment (Note 1)Parity bit (Notes 2 and 3)Bit reserved for future use (Note 4)Bits from tributariesJustification control bits Cj1 (Note 5)Bits from tributariesJustification control bits Cj2 (Note 5)Bits from tributariesJ

4、ustification control bits Cj3(Note 5)Bits from tributaries available for justificationBits from tributariesSet I1 to 910 to 168Set II1234 to 168Set III1 to 34 to 168Set IV1 to 34 to 168Set V1 to 34 to 67 to 168Frame lengthBits per tributary in a frameMaximum justification rate per tributaryNominal j

5、ustification ratio840 bits273 bits7.5 kbit/s0.453Note 1 - See 10.2.1.Note 2 - The parity bit = 1 if the number of marks in all tributary bits including the bits in the justifiabletime-slots in the preceding frame is odd; the parity bit = 0 if the number of marks in all tributary bitsincluding the bi

6、ts in the justifiable time-slots in the preceding frame is even.Note 3 - The implementation and the use of this parity bit procedure are for further study.Note 4 - This bit should be set to 1 when not used.Note 5 - Cji(j = 1, 2, 3; i = 1, 2, 3) indicates the ith justification control bit of the jth

7、tributary.6 jitter6.1 Muldex jitter transfer characteristicA 2048 kbit/s signal, modulated by sinusoidal jitter, should be subject to a muldex jitter transfer characteristicFascicle III.4 - Rec. G.747 3within the gain/frequency limits given in Figure 1/G.747. The equivalent binary content of the tes

8、t signal should be1000.Note - In addition, the need to specify a demultiplexer tributary jitter transfer characteristic from the 6312 kbit/sdemultiplexer input to the 2048 kbit/s demultiplexer output is for further study.Note - The frequency f0should be as low as possible, taking into account the li

9、mitations of measuringequipment. In any case, f0should be no greater than 10 Hz. The selective measurement method should beused.FIGURE 1/G.747Muldex jitter transfer characteristic6.2 Output jitter6.2.1 Tributary output jitterWith no jitter applied to the input ports of the multiplexer and with the m

10、ultiplexer directly connected to thedemultiplexer, the peak-to-peak jitter at the tributary output port should not exceed 0.2 UI over a measurement intervalof one minute in the frequency range from f0to 100 kHz (see Note 1).When measured with an instrument incorporating a bandpass filter having a lo

11、wer cutoff frequency of 18 kHz,a roll-off of 20 dB/decade and an upper limit of 100 kHz, the peak-to-peak output jitter should not exceed 0.05 UI whenmeasured over a one minute interval (see Note 2).Note 1 - The frequency f0should be as low as possible, taking into account the limitations of measure

12、mentequipment. In any case f0should be no greater than 10 Hz.Note 2 - For interfaces meeting the national high Q option, detailed in Recommendation G.823, the lower cutofffrequency for the above measurement should be 700 Hz.6.2.2 Multiplexer output jitterThe peak-to-peak jitter at the 6312 kbit/s ou

13、tput port should not exceed 0.05 UI when it is measured over oneminute interval within the frequency range from f1= 10 Hz to f4= 60 kHz.6.3 Input jitter6.3.1 Tributary input jitterThe 2048 kbit/s input port should be capable of accommodating levels of input jitter up to the limits given in4 Fascicle

14、 III.4 - Rec. G.747Rec. G.823.6.3.2 Demultiplexer input jitterThe 6312 kbit/s input port should be capable of accommodating levels of input jitter up to the limits given inFigure 2/G.747.Note 1 - Current Recommendation G.703 does not refer to the jitter tolerated at the digital distribution frame at

15、6312 kbit/s nor at the input port of equipment connected to this distribution frame.Note 2 - The jitter accommodation requirement should be met when the jittered input signal is composed of themultiplexed tributary signals having any value of jitter allowed for the 2048 kbit/s.Peak-to-peak sinusoida

16、ljitter amplitudeFrequencyA1 (UI) A2(UI) f1 (Hz) f2 (Hz) f3 (kHz) f4 (kHz)5.0 0.15 10 120 4 60FIGURE 2/G.747Lower limit of maximum tolerable sinusoidal input jitterat 6312 kbit/s7 Digital interfacesThe digital interfaces at 2048 kbit/s and 6312 kbit/s should be in accordance with Recommendation G.70

17、3.8 Timing signalIf it is economically feasible, it may be desirable to be able to derive the multiplexing timing signal from anexternal source as well as from an internal source.Fascicle III.4 - Rec. G.747 59 Service digitsThree bits per frame are available for service functions (see Table 1/G.747)

18、: bit 1 of Set II is used to transmit analarm indication to the remote multiplex equipment when specific fault conditions are detected in the multiplexequipment (see 10 below); bit 2 of Set II may be used for a parity check; bit 3 of Set II is reserved for future use.10 Fault conditions and conseque

19、nt actions10.1 Fault conditions10.1.1 The digital multiplex equipment should detect the following fault conditions:1) failure of power supply;2) loss of an incoming 2048 kbit/s tributary signal at a multiplexer input port;3) loss of an incoming 6312 kbit/s multiplex signal at a demultiplexer input p

20、ort;4) loss of frame alignment signal at a demultiplexer input port;5) detection of an alarm indication received from the remote multiplex equipment at a demultiplexer inputport;6) detection of alarm indication signal (AIS) at a demultiplexer input port.Note 1 - The equivalent binary content of the

21、AIS at 2048 and 6312 kbit/s should be a continuous stream ofbinary 1s (marks) as recommended in Recommendation M.20.Note 2 - Some current 44 736/6312 kbit/s demultiplexers do not issue a 6312 kbit/s AIS. Thus no detection cantake place in that case.Note 3 - The strategy for detecting the presence of

22、 the AIS should be such that the AIS is detectable even in thepresence of an error ratio of 1 10-3. However, a signal with all bits except the frame alignment signal in the state of 1should not be mistaken as an AIS.10.1.2 The need to monitor the degradation of the incoming 6312 kbit/s signal for th

23、e purpose of end-to-end errorperformance monitoring of the 6132 kbit/s digital block as well as the procedure for detecting such degradation, are forfurther study.10.2 Consequent actionsFurther to the detection of a fault condition, the appropriate actions should be taken as specified inTable 2/G.74

24、7.Note 1 - The concept and definition of prompt maintenance alarm indication is given in Recommendation M.20.Note 2 - When the alarm indication signal (AIS) is detected at the input of the demultiplexer, the promptmaintenance alarm indication associated with loss of frame alignment should be inhibit

25、ed, while the rest of theconsequent actions are in accordance with those associated in Table 2/G.747 with the fault condition.10.2.1 Alarm indication to the remote multiplex equipment should be generated by changing bit 1 of Set II (seeTable 1/G.747) from the state 0 to the state 1.10.2.2 AIS should

26、 be applied to the following as specified in Table 2/G.747.- all three 2048 kbit/s tributary outputs from the demultiplexer;- 6312 kbit/s output of the multiplexer;- the time slots of the 6312 kbit/s signal at the output of the multiplexer, corresponding to the relevant2048 kbit/s tributary.6 Fascic

27、le III.4 - Rec. G.747TABLE 2/G.747Fault conditions and consequent actionsConsequent actions (see 10.2)AIS appliedEquipmentpartFault condition(see 10.1)PromptmaintenancealarmindicationgeneratedAlarmindication tothe remotemultiplexequipmentgeneratedTo all thetributariesTo thecompositesignalTo the rele

28、vanttime slotsof thecompositesignalMultiplexeranddemultiplexerFailureof power supplyYes Yes(if practicable)Yes(if practicable)MultiplexeronlyLoss of incoming signalon a tributaryYes YesLoss of incoming signalat 6312 kbit/sYes Yes YesDemultiplexerLoss of frame alignment Yes Yes YesonlyAlarm indicatio

29、nreceived fromthe remote multiplexequipmentNote - A Yes in the table signifies that a certain action should be taken as a consequence of the relevant fault condition. An open spacein the table signifies that the relevant action should not be taken as a consequence of the relevant fault condition, if this condition isthe only one present. If more than one fault condition is simultaneously present the relevant action should be taken if, for at least oneof the conditions, a Yes is defined in relation to this action.

展开阅读全文
相关资源
猜你喜欢
  • ASD-STAN PREN 2240-023-1996 Aerospace Series Lamps Incandescent Part 023  Lamp Code 316 Product Standard (Edition P 1)《航空航天系列 白炽灯 第023部分 灯 型号316 产品标准 第P1版》.pdf ASD-STAN PREN 2240-023-1996 Aerospace Series Lamps Incandescent Part 023 Lamp Code 316 Product Standard (Edition P 1)《航空航天系列 白炽灯 第023部分 灯 型号316 产品标准 第P1版》.pdf
  • ASD-STAN PREN 2240-024-1996 Aerospace Series Lamps Incandescent Part 024  Lamp Code 327 Product Standard (Edition P 1)《航空航天系列 白炽灯 第024部分 灯 型号327 产品标准 第P1版》.pdf ASD-STAN PREN 2240-024-1996 Aerospace Series Lamps Incandescent Part 024 Lamp Code 327 Product Standard (Edition P 1)《航空航天系列 白炽灯 第024部分 灯 型号327 产品标准 第P1版》.pdf
  • ASD-STAN PREN 2240-025-1996 Aerospace Series Lamps Incandescent Part 025  Lamp Code 328 Product Standard (Edition P 1)《航空航天系列 白炽灯 第025部分 灯 型号328 产品标准 第P1版》.pdf ASD-STAN PREN 2240-025-1996 Aerospace Series Lamps Incandescent Part 025 Lamp Code 328 Product Standard (Edition P 1)《航空航天系列 白炽灯 第025部分 灯 型号328 产品标准 第P1版》.pdf
  • ASD-STAN PREN 2240-026-1996 Aerospace Series Lamps Incandescent Part 026  Lamp Code 330 Product Standard (Edition P 1)《航空航天系列 白炽灯 第026部分 灯 型号330 产品标准 第P1版》.pdf ASD-STAN PREN 2240-026-1996 Aerospace Series Lamps Incandescent Part 026 Lamp Code 330 Product Standard (Edition P 1)《航空航天系列 白炽灯 第026部分 灯 型号330 产品标准 第P1版》.pdf
  • ASD-STAN PREN 2240-027-1996 Aerospace Series Lamps Incandescent Part 027  Lamp Code 334 Product Standard (Edition P 1)《航空航天系列 白炽灯 第027部分 灯 型号334 产品标准 第P1版》.pdf ASD-STAN PREN 2240-027-1996 Aerospace Series Lamps Incandescent Part 027 Lamp Code 334 Product Standard (Edition P 1)《航空航天系列 白炽灯 第027部分 灯 型号334 产品标准 第P1版》.pdf
  • ASD-STAN PREN 2240-028-1996 Aerospace Series Lamps Incandescent Part 028  Lamp Code 337 Product Standard (Edition P 1)《航空航天系列 白炽灯 第028部分 灯 型号337 产品标准 第P1版》.pdf ASD-STAN PREN 2240-028-1996 Aerospace Series Lamps Incandescent Part 028 Lamp Code 337 Product Standard (Edition P 1)《航空航天系列 白炽灯 第028部分 灯 型号337 产品标准 第P1版》.pdf
  • ASD-STAN PREN 2240-029-1996 Aerospace Series Lamps Incandescent Part 029  Lamp Code 338 Product Standard (Edition P 1)《航空航天系列 白炽灯 第029部分 灯 型号338 产品标准 第P1版》.pdf ASD-STAN PREN 2240-029-1996 Aerospace Series Lamps Incandescent Part 029 Lamp Code 338 Product Standard (Edition P 1)《航空航天系列 白炽灯 第029部分 灯 型号338 产品标准 第P1版》.pdf
  • ASD-STAN PREN 2240-030-1996 Aerospace Series Lamps Incandescent Part 030  Lamp Code 345 Product Standard (Edition P 1)《航空航天系列 白炽灯 第030部分 灯 型号345 产品标准 第P1版》.pdf ASD-STAN PREN 2240-030-1996 Aerospace Series Lamps Incandescent Part 030 Lamp Code 345 Product Standard (Edition P 1)《航空航天系列 白炽灯 第030部分 灯 型号345 产品标准 第P1版》.pdf
  • ASD-STAN PREN 2240-031-1996 Aerospace Series Lamps Incandescent Part 031  Lamp Code 356 Product Standard (Edition P 1)《航空航天系列 白炽灯 第031部分 灯 型号356 产品标准 第P1版》.pdf ASD-STAN PREN 2240-031-1996 Aerospace Series Lamps Incandescent Part 031 Lamp Code 356 Product Standard (Edition P 1)《航空航天系列 白炽灯 第031部分 灯 型号356 产品标准 第P1版》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1