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 PRELIMINARY
OCTOBER 2003
XRT75R12D
REV. P1.0.1
TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
GENERAL DESCRIPTION
The XRT75R12D is a twelve channel fully integrated Line Interface Unit (LIU) featuring EXAR's R3 Technology (Reconfigurable, Relayless Redundancy) for E3/DS3/STS-1 applications. The LIU incorporates 12 independent Receivers, Transmitters and Jitter Attenuators in a single 420 Lead TBGA package. Each channel of the XRT75R12D can be independently configured to operate in E3 (34.368 MHz), DS3 (44.736 MHz) or STS-1 (51.84 MHz). Each transmitter can be turned off and tri-stated for redundancy support or for conserving power. The XRT75R12D's differential receiver provides high noise interference margin and is able to receive data over 1000 feet of cable or with up to 12 dB of cable attenuation. The XRT75R12D incorporates an advanced crystalless jitter attenuator per channel that can be selected either in the transmit or receive path. The jitter attenuator performance meets the ETSI TBR-24 and FIGURE 1. BLOCK DIAGRAM OF THE XRT 75R12D
Bellcore GR-499 specifications. Also, the jitter attenuators can be used for clock smoothing in SONET STS-1 to DS-3 de-mapping. The XRT75R12D provides a Parallel Microprocessor Interface for programming and control. The XRT75R12D supports analog, remote and digital loop-backs. The device also has a built-in Pseudo Random Binary Sequence (PRBS) generator and detector with the ability to insert and detect single bit error for diagnostic purposes.
APPLICATIONS * E3/DS3 Access Equipment * DSLAMs * Digital Cross Connect Systems * CSU/DSU Equipment * Routers * Fiber Optic Terminals
CS RD WR Addr[7:0] D[7:0] PCLK RDY INT Pmode RESET
XRT75R12D XRT75R12D
Processor Interface
CLKOUT_n SFM_en RLOL_n E3Clk DS3Clk STS-Clk/12M
MUX
Peak Detector Slicer Clock & Data Recovery LOS Detector
Clock Synthesizer Jitter Attenuator HDB3/ B3ZS Decoder
RTIP_n RRing_n
AGC/ Equalizer
RxClk_n RxPOS_n RxNEG/LCV_n
Local LoopBack
Remote LoopBack RLOS_n TxClk_n TxPOS_n TxNEG_n
TTIP_n TRing_n MTIP_n MRing_n DMO_n ICT
Line Driver
Tx Pulse Shaping
Timing Control
Jitter Attenuator
MUX
HDB3/ B3ZS Encoder
Device Monitor
Tx Control
TxON Channel 0 Channel n... Channel 11
ORDERING INFORMATION
PART NUMBER XRT75R12DIB PACKAGE 420 Lead TBGA OPERATING TEMPERATURE RANGE -40C to +85C
Exar Corporation 48720 Kato Road, Fremont CA, 94538 * (510) 668-7000 * FAX (510) 668-7017 * www.exar.com
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
FEATURES
RECEIVER
* R3
Technology Redundancy) input jitter tolerance
(Reconfigurable,
Relayless
* Single 3.3 V 5% power supply * 5 V Tolerant digital inputs * Available in 420 pin TBGA Thermally enhanced
Package
* On chip Clock and Data Recovery circuit for high * Meets E3/DS3/STS-1 Jitter Tolerance Requirement * Detects and Clears LOS as per G.775 * Receiver Monitor mode handles up to 20 dB flat
loss with 6 dB cable attenuation
* - 40C to 85C Industrial Temperature Range
TRANSMIT INTERFACE CHARACTERISTICS
* Accepts either Single-Rail or Dual-Rail data from
Terminal Equipment and generates a bipolar signal to the line
* On chip B3ZS/HDB3 encoder and decoder that can
be either enabled or disabled
* Integrated Pulse Shaping Circuit * Built-in B3ZS/HDB3 Encoder (which can be
disabled)
* On-chip clock synthesizer provides the appropriate
rate clock from a single 12.288 MHz Clock
* Accepts Transmit Clock with duty cycle of 30%70%
* Provides low jitter output clock
TRANSMITTER
* Generates pulses that comply with the ITU-T G.703
pulse template for E3 applications Relayless
* R3
Technology Redundancy)
(Reconfigurable,
* Generates pulses that comply with the DSX-3 pulse
template, as specified in Bellcore GR-499-CORE and ANSI T1.102_1993
* Compliant with Bellcore GR-499, GR-253 and ANSI
T1.102 Specification for transmit pulse
* Generates pulses that comply with the STSX-1
pulse template, as specified in Bellcore GR-253CORE
* Tri-state Transmit output capability for redundancy
applications
* Each Transmitter can be turned on or off * Transmitters provide Current Output Drive
JITTER ATTENUATOR
* Transmitter can be turned off in order to support
redundancy designs RECEIVE INTERFACE CHARACTERISTICS
* On chip advanced crystal-less Jitter Attenuator for
each channel
* Integrated Adaptive Receive Equalization (optional)
for optimal Clock and Data Recovery
* Jitter Attenuator can be selected in Receive,
Transmit path, or disabled
* Declares and Clears the LOS defect per ITU-T
G.775 requirements for E3 and DS3 applications
* Meets ETSI TBR 24 Jitter Transfer Requirements * Compliant with jitter transfer template outlined in
ITU G.751, G.752, G.755 and GR-499-CORE,1995 standards
* Meets Jitter Tolerance Requirements, as specified
in ITU-T G.823_1993 for E3 Applications
* Meets Jitter Tolerance Requirements, as specified
in Bellcore GR-499-CORE for DS3 Applications
* 16 or 32 bits selectable FIFO size
CONTROL AND DIAGNOSTICS
* Declares Loss of Lock (LOL) Alarm * Built-in B3ZS/HDB3 Decoder (which can be
disabled)
* Parallel Microprocessor Interface for control and
configuration
* Recovered Data can be muted while the LOS
Condition is declared
* Supports
monitoring
optional
internal
Transmit
driver
* Outputs either Single-Rail or Dual-Rail data to the
Terminal Equipment
* Each channel supports Analog, Remote and Digital
Loop-backs
2
XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
PRELIMINARY TABLE OF CONTENTS
REV. P1.0.1
GENERAL DESCRIPTION.............................................................................................................. 1
APPLICATIONS ............................................................................................................................................................... 1
FIGURE 1. BLOCK DIAGRAM OF THE XRT 75R12D.................................................................................................................................. 1
ORDERING INFORMATION .................................................................................................................... 1
FEATURES..................................................................................................................................................................... 2 TRANSMIT INTERFACE CHARACTERISTICS ....................................................................................................................... 2 RECEIVE INTERFACE CHARACTERISTICS ......................................................................................................................... 2
PIN DESCRIPTIONS (BY FUNCTION) ........................................................................................... 3
SYSTEM-SIDE TRANSMIT INPUT AND TRANSMIT CONTROL PINS....................................................................................... 3 SYSTEM-SIDE RECEIVE OUTPUT AND RECEIVE CONTROL PINS ....................................................................................... 6 RECEIVE LINE SIDE PINS ............................................................................................................................................... 8 CLOCK INTERFACE......................................................................................................................................................... 9 GENERAL CONTROL PINS ............................................................................................................................................ 10 POWER SUPPLY PINS .................................................................................................................................................. 12 GROUND PINS ............................................................................................................................................................. 13
FUNCTIONAL DESCRIPTION ...................................................................................................... 18
1.0 R3 TECHNOLOGY (RECONFIGURABLE, RELAYLESS REDUNDANCY) ....................................... 18
1.1 NETWORK ARCHITECTURE ......................................................................................................................... 18
FIGURE 2. NETWORK REDUNDANCY ARCHITECTURE ............................................................................................................................. 18
2.0 CLOCK SYNTHESIZER ....................................................................................................................... 19
2.1 CLOCK DISTRIBUTION ................................................................................................................................. 19
FIGURE 4. CLOCK DISTRIBUTION CONGIFURED IN E3 MODE WITHOUT USING SFM ................................................................................ 19 FIGURE 3. SIMPLIFIED BLOCK DIAGRAM OF THE INPUT CLOCK CIRCUITRY DRIVING THE MICROPROCESSOR ............................................ 19
3.0 THE RECEIVER SECTION .................................................................................................................. 20
FIGURE 5. RECEIVE PATH BLOCK DIAGRAM .......................................................................................................................................... 20
3.1 RECEIVE LINE INTERFACE .......................................................................................................................... 20
FIGURE 6. RECEIVE LINE INTERFACECONNECTION................................................................................................................................. 20
3.2 ADAPTIVE GAIN CONTROL (AGC) .............................................................................................................. 21 3.3 RECEIVE EQUALIZER ................................................................................................................................... 21
FIGURE 7. ACG/EQUALIZER BLCOK DIAGRAM ....................................................................................................................................... 21 3.3.1 RECOMMENDATIONS FOR EQUALIZER SETTINGS .............................................................................................. 21
3.4 CLOCK AND DATA RECOVERY ................................................................................................................... 21
3.4.1 DATA/CLOCK RECOVERY MODE ............................................................................................................................ 21 3.4.2 TRAINING MODE........................................................................................................................................................ 21
3.5 LOS (LOSS OF SIGNAL) DETECTOR ........................................................................................................... 22
3.5.1 DS3/STS-1 LOS CONDITION ..................................................................................................................................... 22 3.5.2 DISABLING ALOS/DLOS DETECTION ..................................................................................................................... 22 TABLE 2: THE ALOS (ANALOG LOS) DECLARATION AND CLEARANCE THRESHOLDS FOR A GIVEN SETTING OF LOSTHR AND REQEN (DS3 AND STS-1 APPLICATIONS) .......................................................................................................................................................... 22 3.5.3 E3 LOS CONDITION:.................................................................................................................................................. 23 FIGURE 8. LOSS OF SIGNAL DEFINITION FOR E3 AS PER ITU-T G.775 .................................................................................................. 23 FIGURE 9. LOSS OF SIGNAL DEFINITION FOR E3 AS PER ITU-T G.775................................................................................................... 23 3.5.4 INTERFERENCE TOLERANCE.................................................................................................................................. 24 FIGURE 10. INTERFERENCE MARGIN TEST SET UP FOR DS3/STS-1 ...................................................................................................... 24 FIGURE 11. INTERFERENCE MARGIN TEST SET UP FOR E3. ................................................................................................................... 24 TABLE 3: INTERFERENCE MARGIN TEST RESULTS ................................................................................................................................. 25 3.5.5 MUTING THE RECOVERED DATA WITH LOS CONDITION:................................................................................... 26
3.6 B3ZS/HDB3 DECODER .................................................................................................................................. 26
FIGURE 12. RECEIVER DATA OUTPUT AND CODE VIOLATION TIMING ........................................................................................................ 26
4.0 THE TRANSMITTER SECTION ........................................................................................................... 27
FIGURE 13. TRANSMIT PATH BLOCK DIAGRAM ...................................................................................................................................... 27
4.1 TRANSMIT DIGITAL INPUT INTERFACE ..................................................................................................... 27
FIGURE 14. TYPICAL INTERFACE BETWEEN TERMINAL EQUIPMENT AND THE XRT75R12D (DUAL-RAIL DATA)............................................ 27 FIGURE 15. TRANSMITTER TERMINAL INPUT TIMING............................................................................................................................... 28 FIGURE 16. SINGLE-RAIL OR NRZ DATA FORMAT (ENCODER AND DECODER ARE ENABLED) .................................................................. 28
4.2 TRANSMIT CLOCK ........................................................................................................................................ 29 4.3 B3ZS/HDB3 ENCODER .................................................................................................................................. 29
4.3.1 B3ZS ENCODING ....................................................................................................................................................... 29 4.3.2 HDB3 ENCODING....................................................................................................................................................... 29
I
XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
REV. P1.0.1
PRELIMINARY
FIGURE 17. DUAL-RAIL DATA FORMAT (ENCODER AND DECODER ARE DISABLED).................................................................................... 29 FIGURE 18. B3ZS ENCODING FORMAT ................................................................................................................................................. 29
4.4 TRANSMIT PULSE SHAPER ......................................................................................................................... 30
FIGURE 20. TRANSMIT PULSE SHAPE TEST CIRCUIT.............................................................................................................................. 30 4.4.1 GUIDELINES FOR USING TRANSMIT BUILD OUT CIRCUIT .................................................................................. 30 FIGURE 19. HDB3 ENCODING FORMAT ................................................................................................................................................. 30
4.5 E3 LINE SIDE PARAMETERS ........................................................................................................................ 31
FIGURE 21. PULSE MASK FOR E3 (34.368 MBITS/S) INTERFACE AS PER ITU-T G.703 ............................................................................. 31 TABLE 4: E3 TRANSMITTER LINE SIDE OUTPUT AND RECEIVER LINE SIDE INPUT SPECIFICATIONS .............................................................. 32 FIGURE 22. BELLCORE GR-253 CORE TRANSMIT OUTPUT PULSE TEMPLATE FOR SONET STS-1 APPLICATIONS ................................. 33 TABLE 5: STS-1 PULSE MASK EQUATIONS ........................................................................................................................................... 33 TABLE 6: STS-1 TRANSMITTER LINE SIDE OUTPUT AND RECEIVER LINE SIDE INPUT SPECIFICATIONS (GR-253)..................................... 34 FIGURE 23. TRANSMIT OUPUT PULSE TEMPLATE FOR DS3 AS PER BELLCORE GR-499 ......................................................................... 34 TABLE 8: DS3 TRANSMITTER LINE SIDE OUTPUT AND RECEIVER LINE SIDE INPUT SPECIFICATIONS (GR-499) ........................................ 35 TABLE 7: DS3 PULSE MASK EQUATIONS............................................................................................................................................... 35
4.6 TRANSMIT DRIVE MONITOR ........................................................................................................................ 36 4.7 TRANSMITTER SECTION ON/OFF ............................................................................................................... 36
FIGURE 24. TRANSMIT DRIVER MONITOR SET-UP................................................................................................................................... 36
5.0 JITTER ..................................................................................................................................................37
5.1 JITTER TOLERANCE ..................................................................................................................................... 37
5.1.1 DS3/STS-1 JITTER TOLERANCE REQUIREMENTS ................................................................................................ 37 FIGURE 25. JITTER TOLERANCE MEASUREMENTS .................................................................................................................................. 37 5.1.2 E3 JITTER TOLERANCE REQUIREMENTS .............................................................................................................. 38 FIGURE 26. INPUT JITTER TOLERANCE FOR DS3/STS-1 ...................................................................................................................... 38 FIGURE 27. INPUT JITTER TOLERANCE FOR E3..................................................................................................................................... 38
5.2 JITTER TRANSFER ........................................................................................................................................ 39 5.3 JITTER ATTENUATOR ................................................................................................................................... 39
TABLE 9: JITTER AMPLITUDE VERSUS MODULATION FREQUENCY (JITTER TOLERANCE) ........................................................................... 39 TABLE 10: JITTER TRANSFER SPECIFICATION/REFERENCES ................................................................................................................... 39 5.3.1 JITTER GENERATION................................................................................................................................................ 40 TABLE 11: JITTER TRANSFER PASS MASKS ........................................................................................................................................... 40 FIGURE 28. JITTER TRANSFER REQUIREMENTS AND JITTER ATTENUATOR PERFORMANCE ...................................................................... 40
6.0 DIAGNOSTIC FEATURES ...................................................................................................................41
6.1 PRBS GENERATOR AND DETECTOR ......................................................................................................... 41
FIGURE 29. PRBS MODE ................................................................................................................................................................... 41
6.2 LOOPBACKS .................................................................................................................................................. 42
6.2.1 ANALOG LOOPBACK ................................................................................................................................................ 42 FIGURE 30. ANALOG LOOPBACK ........................................................................................................................................................... 42 6.2.2 DIGITAL LOOPBACK ................................................................................................................................................. 43 6.2.3 REMOTE LOOPBACK ................................................................................................................................................ 43 FIGURE 31. DIGITAL LOOPBACK ............................................................................................................................................................ 43 FIGURE 32. REMOTE LOOPBACK ........................................................................................................................................................... 43
6.3 TRANSMIT ALL ONES (TAOS) ...................................................................................................................... 44
FIGURE 33. TRANSMIT ALL ONES (TAOS) ............................................................................................................................................ 44
7.0 MICROPROCESSOR INTERFACE BLOCK ........................................................................................45
TABLE 12: SELECTING THE MICROPROCESSOR INTERFACE MODE .......................................................................................................... 45 FIGURE 34. SIMPLIFIED BLOCK DIAGRAM OF THE MICROPROCESSOR INTERFACE BLOCK ........................................................................ 45
7.1 THE MICROPROCESSOR INTERFACE BLOCK SIGNALS ......................................................................... 46
TABLE 13: XRT75R12D MICROPROCESSOR INTERFACE SIGNALS ......................................................................................................... 46
7.2 ASYNCHRONOUS AND SYNCHRONOUS DESCRIPTION .......................................................................... 47
TABLE 14: ASYNCHRONOUS TIMING SPECIFICATIONS............................................................................................................................. 48 FIGURE 35. ASYNCHRONOUS P INTERFACE SIGNALS DURING PROGRAMMED I/O READ AND WRITE OPERATIONS.................................. 48 FIGURE 36. SYNCHRONOUS P INTERFACE SIGNALS DURING PROGRAMMED I/O READ AND WRITE OPERATIONS.................................... 49 TABLE 15: SYNCHRONOUS TIMING SPECIFICATIONS............................................................................................................................... 49
7.3 REGISTER MAP ............................................................................................................................................. 50
TABLE 16: COMMAND REGISTER ADDRESS MAP, WITHIN THE XRT75R12D ......................................................................................... 50
THE GLOBAL/CHIP-LEVEL REGISTERS ................................................................................................................ 59 REGISTER DESCRIPTION - GLOBAL REGISTERS ............................................................................................... 59
TABLE 17: TABLE 18: TABLE 19: TABLE 20: TABLE 21: LIST AND ADDRESS LOCATIONS OF GLOBAL REGISTERS........................................................................................................ 59 APS/REDUNDANCY TRANSMIT CONTROL REGISTER - CR0 (ADDRESS LOCATION = 0X00) ..................................................... 59 APS/REDUNDANCY TRANSMIT CONTROL REGISTER - CR8 (ADDRESS LOCATION = 0X08) ..................................................... 60 CHANNEL LEVEL INTERRUPT ENABLE REGISTER - CR96 (ADDRESS LOCATION = 0X60) ......................................................... 61 CHANNEL LEVEL INTERRUPT ENABLE REGISTER - CR224 (ADDRESS LOCATION = 0XE0)....................................................... 62
II
XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
PRELIMINARY
TABLE 22: TABLE 23: TABLE 24: TABLE 25:
REV. P1.0.1
THE ABOVE IS: CHANNEL LEVEL INTERRUPT STATUS REGISTER - CR97 (ADDRESS LOCATION = 0X61) .................................. 63 CHANNEL LEVEL INTERRUPT STATUS REGISTER - CR225 (ADDRESS LOCATION = 0XE1)....................................................... 63 DEVICE/PART NUMBER REGISTER - CR110 (ADDRESS LOCATION = 0X6E) ........................................................................... 64 CHIP REVISION NUMBER REGISTER - CR111 (ADDRESS LOCATION = 0X6F) ......................................................................... 64
THE PER-CHANNEL REGISTERS........................................................................................................................... 65 REGISTER DESCRIPTION - PER CHANNEL REGISTERS .................................................................................... 66
TABLE 26: TABLE 27: TABLE 28: TABLE 29: TABLE 30: TABLE 31: TABLE 32: TABLE 33: TABLE 34: TABLE 35: TABLE 36: TABLE 37: TABLE 38: TABLE 39: TABLE 40: TABLE 41: TABLE 42: TABLE 43: TABLE 44: TABLE 45: XRT75R12D REGISTER MAP SHOWING INTERRUPT ENABLE REGISTERS (IER_N) ............................................................... 66 SOURCE LEVEL INTERRUPT ENABLE REGISTER - CHANNEL N ADDRESS LOCATION = 0XM1 .................................................... 66 XRT75R12D REGISTER MAP SHOWING INTERRUPT STATUS REGISTERS (ISR_N) ............................................................... 68 SOURCE LEVEL INTERRUPT STATUS REGISTER - CHANNEL N ADDRESS LOCATION = 0XM2 .................................................... 68 XRT75R12D REGISTER MAP SHOWING ALARM STATUS REGISTERS (AS_N)........................................................................ 70 ALARM STATUS REGISTER - CHANNEL N ADDRESS LOCATION = 0XM3................................................................................... 70 XRT75R12D REGISTER MAP SHOWING TRANSMIT CONTROL REGISTERS (TC_N) ................................................................ 74 TRANSMIT CONTROL REGISTER - CHANNEL N ADDRESS LOCATION = 0XM4 ........................................................................... 74 XRT75R12D REGISTER MAP SHOWING RECEIVE CONTROL REGISTERS (RC_N).................................................................. 76 RECEIVE CONTROL REGISTER - CHANNEL N ADDRESS LOCATION = 0XM5 ............................................................................. 76 XRT75R12D REGISTER MAP SHOWING CHANNEL CONTROL REGISTERS (CC_N)................................................................. 77 CHANNEL CONTROL REGISTER - CHANNEL N ADDRESS LOCATION = 0XM6 ............................................................................ 77 XRT75R12D REGISTER MAP SHOWING JITTER ATTENUATOR CONTROL REGISTERS (JA_N)................................................. 80 JITTER ATTENUATOR CONTROL REGISTER - CHANNEL N ADDRESS LOCATION = 0XM7 ........................................................... 80 XRT75R12D REGISTER MAP SHOWING ERROR COUNTER MSBYTE REGISTERS (EM_N) ..................................................... 81 ERROR COUNTER MSBYTE REGISTER - CHANNEL N ADDRESS LOCATION = 0XMA................................................................. 81 XRT75R12D REGISTER MAP SHOWING ERROR COUNTER LSBYTE REGISTERS (EL_N) ....................................................... 82 ERROR COUNTER LSBYTE REGISTER - CHANNEL N ADDRESS LOCATION = 0XMB.................................................................. 82 XRT75R12D REGISTER MAP SHOWING ERROR COUNTER HOLDING REGISTERS (EH_N) ..................................................... 82 ERROR COUNTER HOLDING REGISTER - CHANNEL N ADDRESS LOCATION = 0XMC ................................................................ 83
8.0 THE SONET/SDH DE-SYNC FUNCTION WITHIN THE LIU ............................................................... 85
8.1 BACKGROUND AND DETAILED INFORMATION - SONET DE-SYNC APPLICATIONS ........................... 85
FIGURE 37. A SIMPLE ILLUSTRATION OF A DS3 SIGNAL BEING MAPPED INTO AND TRANSPORTED OVER THE SONET NETWORK ............... 86
8.2 MAPPING/DE-MAPPING JITTER/WANDER ................................................................................................. 87
8.2.1 HOW DS3 DATA IS MAPPED INTO SONET ............................................................................................................. 87 FIGURE 38. A SIMPLE ILLUSTRATION OF THE SONET STS-1 FRAME..................................................................................................... 88 FIGURE 39. A SIMPLE ILLUSTRATION OF THE STS-1 FRAME STRUCTURE WITH THE TOH AND THE ENVELOPE CAPACITY BYTES DESIGNATED 89 FIGURE 40. THE BYTE-FORMAT OF THE TOH WITHIN AN STS-1 FRAME................................................................................................. 90 FIGURE 41. THE BYTE-FORMAT OF THE TOH WITHIN AN STS-1 FRAME................................................................................................. 91 FIGURE 42. ILLUSTRATION OF THE BYTE STRUCTURE OF THE STS-1 SPE ............................................................................................. 92 FIGURE 43. AN ILLUSTRATION OF TELCORDIA GR-253-CORE'S RECOMMENDATION ON HOW MAP DS3 DATA INTO AN STS-1 SPE ......... 93 FIGURE 44. A SIMPLIFIED "BIT-ORIENTED" VERSION OF TELCORDIA GR-253-CORE'S RECOMMENDATION ON HOW TO MAP DS3 DATA INTO AN STS-1 SPE.......................................................................................................................................................................... 93 8.2.2 DS3 FREQUENCY OFFSETS AND THE USE OF THE "STUFF OPPORTUNITY" BITS ......................................... 94 FIGURE 45. A SIMPLE ILLUSTRATION OF A DS3 DATA-STREAM BEING MAPPED INTO AN STS-1 SPE, VIA A PTE .................................... 95 FIGURE 46. AN ILLUSTRATION OF THE STS-1 SPE TRAFFIC THAT WILL BE GENERATED BY THE "SOURCE" PTE, WHEN MAPPING IN A DS3 SIGNAL THAT HAS A BIT RATE OF 44.736MBPS + 1PPM, INTO AN STS-1 SIGNAL .................................................................................. 96
8.3
JITTER/WANDER DUE TO POINTER ADJUSTMENTS .............................................................................. 98
8.3.1 THE CONCEPT OF AN STS-1 SPE POINTER........................................................................................................... 98 FIGURE 47. AN ILLUSTRATION OF THE STS-1 SPE TRAFFIC THAT WILL BE GENERATED BY THE SOURCE PTE, WHEN MAPPING A DS3 SIGNAL THAT HAS A BIT RATE OF 44.736MBPS - 1PPM, INTO AN STS-1 SIGNAL................................................................................... 98 FIGURE 48. AN ILLUSTRATION OF AN STS-1 SPE STRADDLING ACROSS TWO CONSECUTIVE STS-1 FRAMES ........................................... 99 8.3.2 POINTER ADJUSTMENTS WITHIN THE SONET NETWORK ................................................................................ 100 FIGURE 49. THE BIT-FORMAT OF THE 16-BIT WORD (CONSISTING OF THE H1 AND H2 BYTES) WITH THE 10 BITS, REFLECTING THE LOCATION OF THE J1 BYTE, DESIGNATED .................................................................................................................................................. 100 FIGURE 50. THE RELATIONSHIP BETWEEN THE CONTENTS OF THE "POINTER BITS" (E.G., THE 10-BIT EXPRESSION WITHIN THE H1 AND H2 BYTES) AND THE LOCATION OF THE J1 BYTE WITHIN THE ENVELOPE CAPACITY OF AN STS-1 FRAME ................................................ 100 8.3.3 CAUSES OF POINTER ADJUSTMENTS ................................................................................................................. 101 FIGURE 51. AN ILLUSTRATION OF AN STS-1 SIGNAL BEING PROCESSED VIA A SLIP BUFFER.................................................................. 102 FIGURE 52. AN ILLUSTRATION OF THE BIT FORMAT WITHIN THE 16-BIT WORD (CONSISTING OF THE H1 AND H2 BYTES) WITH THE "I" BITS DESIGNATED ............................................................................................................................................................................. 103 FIGURE 53. AN ILLUSTRATION OF THE BIT-FORMAT WITHIN THE 16-BIT WORD (CONSISTING OF THE H1 AND H2 BYTES) WITH THE "D" BITS DESIGNATED ............................................................................................................................................................................. 104 8.3.4 WHY ARE WE TALKING ABOUT POINTER ADJUSTMENTS? ............................................................................. 105
8.4 CLOCK GAPPING JITTER ........................................................................................................................... 105
FIGURE 54. ILLUSTRATION OF THE TYPICAL APPLICATIONS FOR THE LIU IN A SONET DE-SYNC APPLICATION ...................................... 105
8.5 A REVIEW OF THE CATEGORY I INTRINSIC JITTER REQUIREMENTS (PER TELCORDIA GR-253-CORE)
III
XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
REV. P1.0.1
PRELIMINARY
FOR DS3 APPLICATIONS ........................................................................................................................... 106
TABLE 46: SUMMARY OF "CATEGORY I INTRINSIC JITTER REQUIREMENT PER TELCORDIA GR-253-CORE, FOR DS3 APPLICATIONS ...... 106 8.5.1 DS3 DE-MAPPING JITTER....................................................................................................................................... 107 8.5.2 SINGLE POINTER ADJUSTMENT ........................................................................................................................... 107 8.5.3 POINTER BURST...................................................................................................................................................... 107 FIGURE 55. ILLUSTRATION OF SINGLE POINTER ADJUSTMENT SCENARIO.............................................................................................. 107 8.5.4 PHASE TRANSIENTS............................................................................................................................................... 108 FIGURE 56. ILLUSTRATION OF BURST OF POINTER ADJUSTMENT SCENARIO ......................................................................................... 108 FIGURE 57. ILLUSTRATION OF "PHASE-TRANSIENT" POINTER ADJUSTMENT SCENARIO .......................................................................... 108 8.5.5 87-3 PATTERN.......................................................................................................................................................... 109 8.5.6 87-3 ADD ................................................................................................................................................................... 109 FIGURE 58. AN ILLUSTRATION OF THE 87-3 CONTINUOUS POINTER ADJUSTMENT PATTERN .................................................................. 109 8.5.7 87-3 CANCEL ............................................................................................................................................................ 110 FIGURE 59. ILLUSTRATION OF THE 87-3 ADD POINTER ADJUSTMENT PATTERN..................................................................................... 110 FIGURE 60. ILLUSTRATION OF 87-3 CANCEL POINTER ADJUSTMENT SCENARIO .................................................................................... 110 8.5.8 CONTINUOUS PATTERN......................................................................................................................................... 111 8.5.9 CONTINUOUS ADD ................................................................................................................................................. 111 FIGURE 61. ILLUSTRATION OF CONTINUOUS PERIODIC POINTER ADJUSTMENT SCENARIO .................................................................... 111 8.5.10 CONTINUOUS CANCEL ......................................................................................................................................... 112 FIGURE 62. ILLUSTRATION OF CONTINUOUS-ADD POINTER ADJUSTMENT SCENARIO ............................................................................. 112 FIGURE 63. ILLUSTRATION OF CONTINUOUS-CANCEL POINTER ADJUSTMENT SCENARIO ....................................................................... 112
8.6 A REVIEW OF THE DS3 WANDER REQUIREMENTS PER ANSI T1.105.03B-1997. ................................ 113 8.7 A REVIEW OF THE INTRINSIC JITTER AND WANDER CAPABILITIES OF THE LIU IN A TYPICAL SYSTEM APPLICATION .............................................................................................................................................. 113
8.7.1 INTRINSIC JITTER TEST RESULTS........................................................................................................................ 113 TABLE 47: SUMMARY OF "CATEGORY I INTRINSIC JITTER TEST RESULTS" FOR SONET/DS3 APPLICATIONS ......................................... 113 8.7.2 WANDER MEASUREMENT TEST RESULTS.......................................................................................................... 114
8.8 DESIGNING WITH THE LIU ......................................................................................................................... 114
8.8.1 HOW TO DESIGN AND CONFIGURE THE LIU TO PERMIT A SYSTEM TO MEET THE ABOVE-MENTIONED INTRINSIC JITTER AND WANDER REQUIREMENTS........................................................................................................... 114 FIGURE 64. ILLUSTRATION OF THE LIU BEING CONNECTED TO A MAPPER IC FOR SONET DE-SYNC APPLICATIONS .............................. 114
CHANNEL CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X06................................................................... 115 CHANNEL 1 ADDRESS LOCATION = 0X0E .......................................................... 115 CHANNEL 2 ADDRESS LOCATION = 0X16 ........................................................... 115 CHANNEL CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X06................................................................... 116 CHANNEL 1 ADDRESS LOCATION = 0X0E ............................................................... 116 CHANNEL 2 ADDRESS LOCATION = 0X16 ................................................................. 116 JITTER ATTENUATOR CONTROL REGISTER - (CHANNEL 0 ADDRESS LOCATION = 0X07................................................. 116 CHANNEL 1 ADDRESS LOCATION = 0X0F.................................................... 116 CHANNEL 2 ADDRESS LOCATION = 0X17 .................................................... 116
8.8.2 RECOMMENDATIONS ON PRE-PROCESSING THE GAPPED CLOCKS (FROM THE MAPPER/ASIC DEVICE) PRIOR TO ROUTING THIS DS3 CLOCK AND DATA-SIGNALS TO THE TRANSMIT INPUTS OF THE LIU ...................... 117
JITTER ATTENUATOR CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X07.................................................. 117 CHANNEL 1 ADDRESS LOCATION = 0X0F.............................................. 117 CHANNEL 2 ADDRESS LOCATION = 0X17 .............................................. 117 JITTER ATTENUATOR CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X07.................................................. 117 CHANNEL 1 ADDRESS LOCATION = 0X0F............................................. 117 CHANNEL 2 ADDRESS LOCATION = 0X17 ............................................. 117
FIGURE 65. ILLUSTRATION OF MINOR PATTERN P1 ......................................................................................................................... 118 FIGURE 66. ILLUSTRATION OF MINOR PATTERN P2 ......................................................................................................................... 119 FIGURE 67. ILLUSTRATION OF PROCEDURE WHICH IS USED TO SYNTHESIZE MAJOR PATTERN A....................................................... 119 FIGURE 68. ILLUSTRATION OF MINOR PATTERN P3 ......................................................................................................................... 120 FIGURE 69. ILLUSTRATION OF PROCEDURE WHICH IS USED TO SYNTHESIZE PATTERN B ................................................................... 120 8.8.3 HOW DOES THE LIU PERMIT THE USER TO COMPLY WITH THE SONET APS RECOVERY TIME REQUIREMENTS OF 50MS (PER TELCORDIA GR-253-CORE)? .......................................................................................................... 121 FIGURE 70. ILLUSTRATION OF THE SUPER PATTERN WHICH IS OUTPUT VIA THE "OC-N TO DS3" MAPPER IC ................................... 121 FIGURE 71. SIMPLE ILLUSTRATION OF THE LIU BEING USED IN A SONET DE-SYNCHRONIZER" APPLICATION......................................... 121 TABLE 48: MEASURED APS RECOVERY TIME AS A FUNCTION OF DS3 PPM OFFSET ............................................................................. 122
JITTER ATTENUATOR CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X07.................................................. 122 CHANNEL 1 ADDRESS LOCATION = 0X0F............................................. 122 CHANNEL 2 ADDRESS LOCATION = 0X17 ............................................. 122
8.8.4 HOW SHOULD ONE CONFIGURE THE LIU, IF ONE NEEDS TO SUPPORT "DAISY-CHAIN" TESTING AT THE END CUSTOMER'S SITE? ................................................................................................................................................... 123
IV
XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
PRELIMINARY
REV. P1.0.1
JITTER ATTENUATOR CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X07.................................................. 123 CHANNEL 1 ADDRESS LOCATION = 0X0F ................................................... 123 CHANNEL 2 ADDRESS LOCATION = 0X17.................................................... 123
9.0 ELECTRICAL CHARACTERISTICS ................................................................................................. 124
TABLE 49: ABSOLUTE MAXIMUM RATINGS ........................................................................................................................................... 124 TABLE 50: DC ELECTRICAL CHARACTERISTICS:................................................................................................................................... 124
ORDERING INFORMATION ................................................................................................................ 125
PACKAGE DIMENSIONS - ............................................................................................................................................ 125 REVISIONS ................................................................................................................................................................ 126
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
PIN DESCRIPTIONS (BY FUNCTION)
SYSTEM-SIDE TRANSMIT INPUT AND TRANSMIT CONTROL PINS
PIN # P4 SIGNAL NAME TYPE I DESCRIPTION
TxON
Transmit On/Off Input Upon power up, the transmitters are powered on. Turning the transmitters On or Off is selected through the microprocessor interface by programming the appropriate channel register if this pin is pulled "High". If the TxON pin is pulled "Low", all 12 transmitters are powered off.
NOTE:
TxON is ideal for redundancy applications. See the R3 Technology section of this datasheet for more details. Internally pulled "High".
F22 AA22 H22 Y23 G26 AA25 G1 AA2 H5 Y4 F5 AA5 E23 AB24 J22 AA23 G25 AA26 G2 AA1 J5 AA4 E4 AB3
TxCLK0 TxCLK1 TxCLK2 TxCLK3 TxCLK4 TxCLK5 TxCLK6 TxCLK7 TxCLK8 TxCLK9 TxCLK10 TxCLK11 TxPOS0 TxPOS1 TxPOS2 TxPOS3 TxPOS4 TxPOS5 TxPOS6 TxPOS7 TxPOS8 TxPOS9 TxPOS10 TxPOS11
I
Transmit Clock Input
These input pins have three functions:
* They function as the timing source for the Transmit Section of the
corresponding channel within the XRT75R12D.
* They are used by the Transmit Section of the LIU IC to sample the
corresponding TxPOS_n and TxNEG_n input pins.
* They are used to clock the PRBS generator
NOTE: The user is expected to supply a 44.736MHz 20ppm clock signal (for DS3 applications), 34.368MHz 20 ppm clock signal (for E3 applications) or a 51.84MHz 4.6ppm clock signal (for STS-1, Stratum 3E or better applications).
I
Transmit Positive Data Input
The function of these digitial input pins depends upon whether the corresponding channel has been configured to operate in the Single-Rail or Dual-Rail Mode. Single Rail Mode - Transmit Data Input Operating in the Single-Rail Mode; all transmit input data will be serially applied to this input pin. This signal will be latched into the Transmit Section circuitry on the active edge of the TxCLK_n signal. The Transmit Section of the LIU IC will then encode this data into either the B3ZS line code (for DS3 and STS-1 applications) or the HDB3 line code (for E3 applications). Dual Rail Mode - Transmit Positive Data Input In the Dual-Rail Mode, the user should apply a pulse to this input pin when a positive-polarity pulse is to be transmitted onto the line. This signal will be latched into the Transmit Section circuitry upon the active edge of the TxCLK_n signal,. The Transmit Section of the LIU IC will NOT encode this data into either the B3ZS or HDB3 line codes. If the user configures the LIU IC to operate in the Dual-Rail Mode, B3ZS/HDB3 encoding must have already been done prior to this input.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
SYSTEM-SIDE TRANSMIT INPUT AND TRANSMIT CONTROL PINS
PIN # C25 AB25 H23 W23 H24 Y26 H3 Y1 H4 W4 C2 AB2 B24 AE24 C20 AD20 C16 AD16 C11 AD11 C7 AD7 C3 AD3 SIGNAL NAME TYPE I DESCRIPTION
TxNEG0 TxNEG1 TxNEG2 TxNEG3 TxNEG4 TxNEG5 TxNEG6 TxNEG7 TxNEG8 TxNEG9 TxNEG10 TxNEG11 TTip0 TTip1 TTip2 TTip3 TTip4 TTip5 TTip6 TTip7 TTip8 TTip9 TTip10 TTip11
Transmit Negative Data Input
When a Channel has been configured to operate in the Dual-Rail Mode, the user should apply a pulse to this input pin anytime the Transmit Section of the LIU IC to generate a negative-polarity pulse onto the line. This signal will be latched into the Transmit Section circuitry upon the active edge of the TxCLK_n signal.
NOTE: In the Single-Rail Mode, this input pin has no function, and should be tied to GND.
O
Transmit TTIP Output - Positive Polarity Signal
These output pins along with the corresponding TRING_n output pins, function as the Transmit DS3/E3/STS-1 Line output signal drivers for a given channel of the XRT75R12D. Connect this signal and the corresponding TRING_n output signal to a 1:1 transformer. Whenever the Transmit Section of the Channel generates and transmits a positivepolarity pulse onto the line, this output pin will be pulsed to a high ervoltage than its corresponding TRING_n output pins. Conversely, whenever the Transmit Section of the Channel generates and transmit a negative-polarity pulse onto the line, this output pin will be pulsed to a lower voltage than its corresponding TRING_n output pin.
NOTE: This output pin will be tri-stated whenever the TxON input pin or bit-field is set to "0".
O
C24 AD24 B20 AE20 B16 AE16 B11 AE11 B7 AE7 B3 AE3
TRing0 TRing1 TRing2 TRing3 TRing4 TRing5 TRing6 TRing7 TRing8 TRing9 TRing10 TRing11
Transmit Ring Output - Negative Polarity Signal
These output pins along with the corresponding TTIP_n output pins, function as the Transmit DS3/E3/STS-1 Line output signal drivers for a given channel, within the XRT75R12D. Connect this signal and the corresponding TTIP_n output signal to a 1:1 transformer. Whenever the Transmit Section of the Channel generates and transmits a positivepolarity pulse onto the line, this output pin will be pulsed to a lower voltage than its corresponding TTIP_n output pin. Conversely, whenever the Transmit Section of the Channel generates and transmit a negative-polarity pulse onto the line, this output pin will be pulsed to a higher voltage than its corresponding TTIP_n output pin.
NOTE: This output pin will be tri-stated whenever the TxON input pin or bit-field is set to "0".
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
SYSTEM-SIDE TRANSMIT INPUT AND TRANSMIT CONTROL PINS
PIN # C23 AD23 D19 AC19 D15 AC15 E11 AB11 E8 AB8 C4 AD4 D23 AC23 E19 AB19 E16 AB16 D10 AC10 D8 AC8 D4 AC4 N3 N4 N5 N1 M1 L2 M2 M3 M4 M5 K2 J1 SIGNAL NAME TYPE I DESCRIPTION
MTip0 MTip1 MTip2 MTip3 MTip4 MTip5 MTip6 MTip7 MTip8 MTip9 MTip10 MTip11 MRing0 MRing1 MRing2 MRing3 MRing4 MRing5 MRing6 MRing7 MRing8 MRing9 MRing10 MRing11 DMO0 DMO1 DMO2 DMO3 DMO4 DMO5 DMO6 DMO7 DMO8 DMO9 DMO10 DMO11
Monitor Tip Input - Positive Polarity Signal
These input pins along with MRing_n function as the Transmit Drive Monitor Output (DMO) input monitoring pins. (1) To monitor the Transmit Output line signal and (2) to perform this monitoring externally, then this pin MUST be connected to the corresponding TTIP_n output pin via a 270 series resistor. Similarly, the MRING_n input pin MUST also be connected to its corresponding TRING_n output pin via a 270 series resistor. The MTIP_n and MRING_n input pins will continuously monitor the Transmit Output line signal via the TTIP_n and TRING_n output pins for bipolar activity. If these pins do not detect any bipolar activity for 128 bit periods, then the Transmit Drive Monitor circuit will drive the corresponding DMO_n output pin "High" in order to denote a possible fault condition in the Transmit Output Line signal path.
NOTE:
I
These input pins are inactive if the user chooses to internally monitor the Transmit Output line signal.
Monitor Ring Input
These input pins along with MTIP_n function as the Transmit Drive Monitor Output (DMO) input monitoring pins. (1) To monitor the Transmit Output line signal and (2) to perform this monitoring externally, then this input pin MUST be connected to the corresponding TRING_n output pin via a 270 series resistor. Similarly, the MTIP_n input pin MUST be connected to its corresponding TTIP_n output pin via a 270 series resistor. The MTIP_n and MRING_n input pins will continuously monitor the Transmit Output line signal via the TTIP_n and TRING_n output pins for bipolar activity. If these pins do not detect any bipolar activity for 128 bit periods, then the Transmit Drive Monitor circuit will drive the corresponding DMO_n output pin "High" to indicate a possible fault condition in the Transmit Output Line signal path.
NOTE:
O
These input pins are inactive if the user chooses to internally monitor the Transmit Output line signal.
Drive Monitor Output These output signals are used to indicate a fault condition within the Transmit Output signal path.
This output pin will toggle "High" anytime the Transmit Drive Monitor circuitry either, via the corresponding MTIP and MRING input pins or internally, detects no bipolar pulses via the Transmit Output line signal (e.g., via the TTIP_m and TRING_m output pins) for 128 bit-periods. This output pin will be driven "Low" anytime the Transmit Drive Monitor circuitry has detected at least one bipolar pulse via the Transmit Output line signal within the last 128 bit periods.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
SYSTEM-SIDE RECEIVE OUTPUT AND RECEIVE CONTROL PINS
PIN # D25 AD25 G23 AA24 J24 U24 J3 U3 G4 AA3 D2 AD2 G22 AB26 K22 U22 L24 W25 L3 W2 K5 U5 G5 AB1 E25 AD26 G24 Y24 L22 T22 L5 T5 G3 Y3 E2 AD1 SIGNAL NAME TYPE O DESCRIPTION
RLOS0 RLOS1 RLOS2 RLOS3 RLOS4 RLOS5 RLOS6 RLOS7 RLOS8 RLOS9 RLOS10 RLOS11 RLOL0 RLOL1 RLOL2 RLOL3 RLOL4 RLOL5 RLOL6 RLOL7 RLOL8 RLOL9 RLOL10 RLOL11 RxPOS0 RxPOS1 RxPOS2 RxPOS3 RxPOS4 RxPOS5 RxPOS6 RxPOS7 RxPOS8 RxPOS9 RxPOS10 RxPOS11
Receive Loss of Signal Output Indicator
This output pin indicates Loss of Signal (LOS) Defect condition for the corresponding channel. "Low" - Indicates that the corresponding Channel is NOT currently declaring the LOS defect condition. "High" - Indicates that the corresponding Channel is currently declaring the LOS defect condition.
O
Receive Loss of Lock Output Indicator
This output pin indicates Loss of Lock (LOL) condition for the corresponding channel. "Low" - Indicates that the corresponding Channel is NOT declaring the LOL condition. "High" - Indicates that the corresponding Channel is currently declaring the LOL condition.
NOTE: The Receive Section of a given channel will declare the LOL condition anytime the frequency of the Recovered Clock (RCLK) signal differs from that of the reference clock programmed for that channel by 0.5% or more.
O
Receive Positive Data Output
The function of these output pins depends upon whether the channel has been configured to operate in the Single-Rail or Dual-Rail Mode. Dual-Rail Mode - Receive Positive Polarity Data Output If the channel has been configured to operate in the Dual-Rail Mode, then all positive-polarity data will be output via this pin. The negative-polarity data will be output via the corresponding RxNEG_n pin. In other words, the Receive Section of the corresponding Channel will pulse this output pin "High" for one period of RCLK_n anytime it receives a positive-polarity pulse via the RTIP/ RRING input pins. The data output via this pin is updated upon the active edge of RxCLK_n output clock signal. Single-Rail Mode - Receive Data Output In the Single-Rail Mode, all Receive (or Recovered) data will be output via this pin. The data output via this pin is updated upon the active edge of the RCLK_n output clock signal.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
SYSTEM-SIDE RECEIVE OUTPUT AND RECEIVE CONTROL PINS
PIN # F23 AC26 F24 U23 L23 T24 L4 T3 F3 U4 F4 AC1 SIGNAL NAME TYPE O DESCRIPTION
RxNEG/LCV0 RxNEG/LCV1 RxNEG/LCV2 RxNEG/LCV3 RxNEG/LCV4 RxNEG/LCV5 RxNEG/LCV6 RxNEG/LCV7 RxNEG/LCV8 RxNEG/LCV9 RxNEG/LCV10 RxNEG/LCV11
Receive Negative Data Output/Line Code Violation
The function of these pins depends on whether the XRT75R12D is configured in Single Rail or Dual Rail mode. Dual-Rail Mode - Receive Negative Polarity Data Output In the Dual-Rail Mode, all negative-polarity data will be output via this pin. The positive-polarity data will be output via the corresponding RxPOS_n output pin. In other words, the Receive Section of the corresponding Channel will pulse this output pin "High" for one period of RxCLK_n anytime it receives a negativepolarity pulse via the RTIP/RRING input pins. The data output via this pin is updated upon the active edge of the RCLK_n output clock signal. Single-Rail Mode - Line Code Violation Indicator Output In the Single-Rail Mode, this output pin will function as the Line Code Violation indicator output. In this configuration, the Receive Section of the Channel will pulse this output pin "High" for at least one RCLK period whenever it detects either an LCV (Line Code Violation) or an EXZ (Excessive Zero Event). The data that is output via this pin is updated upon the active edge of the RCLK_n output clock signal.
E24 AC25 J23 V23 K24 T23 K3 T4 J4 V4 E3 AC2
RxCLK0 RxCLK1 RxCLK2 RxCLK3 RxCLK4 RxCLK5 RxCLK6 RxCLK7 RxCLK8 RxCLK9 RxCLK10 RxCLK11
O
Receive Clock Output
This output pin functions as the Receive or recovered clock signal. All Receive (or recovered) data will output via the RxPOS_n and RxNEG_n outputs upon the active edge of this clock signal. Additionally, if the device/channel has been configured to operate in the SingleRail Mode, then the RNEG_n/LCV_n output pins will also be updated upon the active edge of this clock signal.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
RECEIVE LINE SIDE PINS
PIN # B22 AE22 B18 AE18 A14 AF14 D13 AC13 B9 AE9 B5 AE5 C22 AD22 C18 AD18 B14 AE14 C13 AD13 C9 AD9 C5 AD5 SIGNAL NAME TYPE I DESCRIPTION
RTip0 RTip1 RTip2 RTip3 RTip4 RTip5 RTip6 RTip7 RTip8 RTip9 RTip10 RTip11 RRing0 RRing1 RRing2 RRing3 RRing4 RRing5 RRing6 RRing7 RRing8 RRing9 RRing10 RRing11
Receive TIP Input
These input pins along with the corresponding RRing_n input pin function as the Receive DS3/E3/STS-1 Line input signal for a given channel of the XRT75R12D. Cconnect this signal and the corresponding RRING_n input signal to a 1:1 transformer. Whenever the RTIP/RRING input pins are receiving a positive-polarity pulse within the incoming DS3, E3 or STS-1 line signal, this input pin will be pulsed to a higher voltage than its corresponding RRING_n input pin. Conversely, whenever the RTIP/RRING input pins are receiving a negativepolarity pulse within the incoming DS3, E3 or STS-1 line signal, this input pin will be pulsed to a lower voltage than its corresponding RRING_n input pin.
I
Receive Ring Input
These input pins along with the corresponding RTIP_n input pin function as the Receive DS3/E3/STS-1 Line input signal for a given channel of the XRT75R12D. Connect this signal and the corresponding RTIP_n input signal to a 1:1 transformer. (See Figure 6) Whenever the RTIP/RRING input pins are receiving a positive-polarity pulse within the incoming DS3, E3 or STS-1 line signal, then this input pin will be pulsed to a lower voltage than its corresponding RTIP_n input pin. Conversely, whenever the RTIP/RRING input pins are receiving a negativepolarity pulse within the incoming DS3, E3 or STS-1 line signal, then this input pin will be pulsed to a higher voltage than its corresponding RTIP_n input pin.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
CLOCK INTERFACE
PIN # R5 SIGNAL NAME TYPE I DESCRIPTION Single Frequency Mode Enable This input pin is used to configure the XRT75R12D to operate in the SFM (Single Frequency Mode). When this feature is invoked, the SFM Synthesizer will become active. By applying a 12.288MHz clock signal to the STS-1Clk/12M pin, the XRT75R12D will generate all of the appropriate clock signals (e.g., 34.368MHz, 44.736MHz or 51.84). The XRT75R12D internal circuitry will route each of these synthesized clock signals to the appropriate nodes of the corresponding channels in the XRT75R12D. "Low" - Disables the Single Frequency Mode. In this setting, the user is required to supply to the E3CLK, DS3CLK or STS-1CLK input pins all of the relevant clock signals that are to be used within the chip. "High" - Enables the Single-Frequency Mode.
SFM_EN
NOTE: This input pin is internally pulled low.
R1
E3Clk
I
E3 Clock Input (34.368 MHz 20 ppm) If any one of the channels is configured in E3 mode, a reference clock of 34.368 MHz 20 ppm is applied to this input pin. If the LIU is used in E3 mode only, this pin must be connected to the DS3Clk input pin to have access to the internal microprocessor.
NOTE: SFM mode negates the need for this clock
T1
DS3Clk
I
DS3 Clock Input (44.736 MHz 20 ppm) If any one of the channels is configured in DS3 mode, a reference clock of 44.736 MHz 20 ppm is applied to this input pin.
NOTE: SFM mode negates the need for this clock
U1
STS-1Clk/12M
I
STS-1 Clock Input (51.84 MHz 20 ppm) If any one of the channels is configured in STS-1 mode, a reference clock of 51.84MHz 20 ppm is applied to this input pin. If the LIU is used in STS-1 mode only, this pin must be connected to the DS3Clk input pin to have access to the internal microprocessor. Single Frequency Mode Clock (12.288MHz) Input In Single Frequency Mode, a reference clock of 12.288 MHz 20 ppm is connected to this pin and the internal clock synthesizer generates the appropriate clock frequencies based on the configuration of the rates (E3, DS3 or STS-1). Reference clock out A reference clock pin is provided for each channel that will supply a precise data rate frequency derived from either the Clock input pin (E3Clk, DS3Clk, or STS1Clk) or the 12.288MHz input in SFM mode. This frequency will be as stable as the original source. It is designed to provide the attached framer with its appropriate reference clock.
C26 W22 K23 W24 J25 V25 J2 V2 K4 W3 C1 W5
CLKOUT0 CLKOUT1 CLKOUT2 CLKOUT3 CLKOUT4 CLKOUT5 CLKOUT6 CLKOUT7 CLKOUT8 CLKOUT9 CLKOUT10 CLKOUT11
O
9
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
GENERAL CONTROL PINS
PIN # P3 SIGNAL NAME TYPE **** DESCRIPTION Factory Test Mode Input Pin This pin must be connected to GND for normal operation.
TEST
NOTE: This input pin is internally pulled "Low".
AE25
TRST TMS TCK TDI TDO
I
Test Reset Test Boundary Scan Test Mose Select Test Boundary Scan Test Clock Test Boundary Scan Test Data Input Test Boundary Scan Test Data Output Test Boundary Scan
AB23
I
AB5
I
AB4
I
AE2
O
MICROPROCESSOR PARALLEL INTERFACE PIN # J26 SIGNAL NAME TYPE I DESCRIPTION
Pmode
This pin controls the Microprocessor Parallel Interface mode. "High" sets a Synchronous clocked interface mode with a clock from the Host. "Low" sets an Asynchronous mode where a clock internal to the XRT75R12D will time the operations.
P24 N24
PCLK CS
I I
High speed clock supplied by the Host to provide timing in the Synchronous Interface mode. This signal must be a square-wave. Chip select input (active low) Initiates a read or write operation. When "High", no parallel communication is active between the LIU and the Host.
N22
WR
I
Write input (active low) Enables the Host to write data D[7:0] into the LIU register space at address Addr[7:0].
N23
RD
I
Read input (active low) Commands the LIU to transfer the contents of a register specified by Addr[7:0] to the Host.
N25
RDY
O
Ready line output (active low) Provides a handshake between the LIU and the Host that communicates when an operation has been completed.
This pin must be pulled "High" with a 3k 1% resistor.
10
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER MICROPROCESSOR PARALLEL INTERFACE PIN # K25 M22 M23 M24 K26 L26 M26 N26 P22 R26 T26 U26 R25 R24 R23 R22 P26 SIGNAL NAME TYPE I DESCRIPTION
Addr0 Addr1 Addr2 Addr3 Addr4 Addr5 Addr6 Addr7 D0 D1 D2 D3 D4 D5 D6 D7 INT
An eight bit direct address bus that specifies the source/destination register for a Read or Write operation.
I/O
An eight bit bi-directional data bus that provides the data into the LIU for a Write operation or the data out to the Host for a Read operation.
O
Interrupt active Output (active low) Normally, this output pin will be pulled "High". However, if the user enables interrupts within the LIU, and if those conditions occur, the XRT75R12D will signal an interrupt from the Microprocessor by pulling this output pin "Low". The Host Microprocessor must ascertain the source of the interrupt and service it. Reading the source of the interupt will clear the flag and the INT pin will go back high unless another interrupt has gone active.
NOTES:
1. This pin will remain "Low" until the Interrupt has been serviced.
2. This pin must be pulled "High" with a 3k 1% resistor.
N2
RESET
I
RESET Input Pulsing this input "Low" causes the XRT75R12D to reset the contents of the on-chip Command Registers to their default values. As a consequence, the XRT75R12D will then also be operating in its default condition. For normal operation this input pin should be at a logic "High".
NOTE: This input pin is internally pulled high.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
POWER SUPPLY PINS
PIN NAME RVDD0 RVDD1 RVDD2 RVDD3 RVDD4 RVDD5 RVDD6 RVDD7 RVDD8 RVDD9 RVDD10 RVDD11 TVDD0 TVDD1 TVDD2 TVDD3 TVDD4 TVDD5 TVDD6 TVDD7 TVDD8 TVDD9 TVDD10 TVDD11 AVDD PIN NUMBERS DESCRIPTION Receive Analog Power Supply (3.3V 5%) RVDD should not be shared with other power supplies. It is recommended that RVDD be isolated from the digital power supply DVDD and the analog power supply TVDD. For best results, use an internal power plane for isolation. If an internal power plane is not available, a ferrite bead can be used. Each power supply pin should be bypassed to ground through an external 0.1F capacitor.
D22 AC22 D18 AC18 E15 AB15 E12 AB12 A9 AF9 D5 AC5 B23 AE23 B19 AE19 B15 AE15 B10 AE10 A6 AF6 B4 AE4 M25, T25, AB21, AB18, AF13, AF12, AB9, AB6, R4, K1, E6, E9, A12, A13, E18, E21, D26, F25, H25, P25, W26, V24, Y22, AF21, AF20, AF17, AF16, AD14, AD12, AF11, AF8, AF7, AF24, AD6, AF3, Y5, V3, W1, P5, P2, H2, F2, D1, C6, A7, A3, A8, A11, C12, C14, A16, A17, A20, A21, A24
Transmit Analog Power Supply (3.3V 5%) TVDD can be shared with DVDD. However, it is recommended that TVDD be isolated from the analog power supply RVDD. For best results, use an internal power plane for isolation. If an internal power plane is not available, a ferrite bead can be used. Each power supply pin should be bypassed to ground through an external 0.1F capacitor.
Analog Power Supply (3.3V 5%) AVDD should be isolated from the digital power supplies. For best results, use an internal power plane for isolation. If an internal power plane is not available, a ferrite bead can be used. Each power supply pin should be bypassed to ground through at least one 0.1F capacitor. Digital Power Supply (3.3V 5%) DVDD should be isolated from the analog power supplies. For best results, use an internal power plane for isolation. If an internal power plane is not available, a ferrite bead can be used. Every two DVDD power supply pins should be bypassed to ground through at least one 0.1F capacitor.
DVDD
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER GROUND PINS
PIN NAME RGND0 RGND1 RGND2 RGND3 RGND4 RGND5 RGND6 RGND7 RGND8 RGND9 RGND10 RGND11 TGND0 TGND1 TGND2 TGND3 TGND4 TGND5 TGND6 TGND7 TGND8 TGND9 TGND10 TGND11 AGND PIN NUMBERS DESCRIPTION Receive Analog Ground It's recommended that all ground pins of this device be tied together.
A22 AF22 A18 AF18 E14 AB14 E13 AB13 D9 AC9 A5 AF5 A23 AF23 A19 AF19 A15 AF15 A10 AF10 B6 AE6 A4 AF4
Transmit Analog Ground It's recommended that all ground pins of this device be tied together.
A1, A2, A25, A26, B1, B2, Analog Ground B25, B26, C8, C10, C17, It's recommended that all ground pins of this device be tied together. C19, C21, D17, D21, E5, E22, L25, U25, AB22, AB20, AB17, AB10, AB7, R3, L1, E7, E10, B12, B13, E17, E20, T2, U2, AC17, AC21, AD8, AD10, AD15, AD17, AD19, AD21, AE1, AE26, AE12, AE13, AF1, AF2, AF25, AF26, C15 E26, F26, H26, P23, , V26, Digital Ground Y25, V22, AC24, AC20, It's recommended that all ground pins of this device be tied together. AC16, AC14, AC12, AC11, AE8, AE17, AE21, AC7, AC6, AC3, V5, Y2, V1, R2, P1, H1, F1, E1, D3, D7, B8, D6, D11, D12, D14, D16, B17, D20, B21, D24
DGND
13
XRT75R12D
TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
PRELIMINARY
TABLE 1: LIST BY PIN NUMBER
PIN A1 A2 A3 A4 A5 A6 A7 A8 A9 A10 A11 A12 A13 A14 A15 A16 A17 A18 A19 A20 A21 A22 A23 A24 A25 A26 B1 B2 B3 B4 B5 PIN NAME AGND AGND DVDD TGND10 RGND10 TVDD8 DVDD DVDD RVDD8 TGND6 DVDD AVDD AVDD RTip4 TGND4 DVDD DVDD RGND2 TGND2 DVDD DVDD RGND0 TGND0 DVDD AGND AGND AGND AGND TRing10 TVDD10 RTip10 PIN B6 B7 B8 B9 B10 B11 B12 B13 B14 B15 B16 B17 B18 B19 B20 B21 B22 B23 B24 B25 B26 C1 C2 C3 C4 C5 C6 C7 C8 C9 C10 C11 C12 PIN NAME TGND8 TRing8 DGND RTip8 TVDD6 TRing6 AGND AGND RRing4 TVDD4 TRing4 DGND RTip2 TVDD2 TRing2 DGND RTip0 TVDD0 TTip0 AGND AGND CLKOUT10 TxNEG10 TTip10 MTip10 RRing10 DVDD TTip8 AGND RRing8 AGND TTip6 DVDD PIN C13 C14 C15 C16 C17 C18 C19 C20 C21 C22 C23 C24 C25 C26 D1 D2 D3 D4 D5 D6 D7 D8 D9 D10 D11 D12 D13 D14 D15 D16 D17 D18 D19 PIN NAME RRing6 DVDD AGND TTip4 AGND RRing2 AGND TTip2 AGND RRing0 MTip0 TRing0 TxNEG0 CLKOUT0 DVDD RLOS10 DGND MRing10 RVDD10 DGND DGND MRing8 RGND8 MRing6 DGND DGND RTip6 DGND MTip4 DGND AGND RVDD2 MTip2 PIN D20 D21 D22 D23 D24 D25 D26 E1 E2 E3 E4 E5 E6 E7 E8 E9 E10 E11 E12 E13 E14 E15 E16 E17 E18 E19 E20 E21 E22 E23 E24 E25 E26
REV. P1.0.1
PIN NAME DGND AGND RVDD0 MRing0 DGND RLOS0 DVDD DGND RxPOS10 RxCLK10 TxPOS10 AGND AVDD AGND MTip8 AVDD AGND MTip6 RVDD6 RGND6 RGND4 RVDD4 MRing4 AGND AVDD MRing2 AGND AVDD AGND TxPOS0 RxCLK0 RxPOS0 DGND
14
XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
REV. P1.0.1
PRELIMINARY
PIN NAME DGND DVDD RxNEG/LCV8 RxNEG/LCV10 TxCLK10 TxCLK0 RxNEG/LCV0 RxNEG/LCV2 DVDD DGND TxCLK6 TxPOS6 RxPOS8 RLOS8 RLOL10 RLOL0 RLOS2 RxPOS2 TxPOS4 TxCLK4 DGND DVDD TxNEG6 TxNEG8 TxCLK8 TxCLK2 TxNEG2 TxNEG4 DVDD DGND DMO11 CLKOUT6 RLOS6 PIN J4 J5 J22 J23 J24 J25 J26 K1 K2 K3 K4 K5 K22 K23 K24 K25 K26 L1 L2 L3 L4 L5 L22 L23 L24 L25 L26 M1 M2 M3 M4 M5 M22 PIN NAME RxCLK8 TxPOS8 TxPOS2 RxCLK2 RLOS4 CLKOUT4 Pmode AVDD DMO10 RxCLK6 CLKOUT8 RLOL8 RLOL2 CLKOUT2 RxCLK4 Addr0 Addr4 AGND DMO5 RLOL6 RxNEG/LCV6 RxPOS6 RxPOS4 RxNEG/LCV4 RLOL4 AGND Addr5 DMO4 DMO6 DMO7 DMO8 DMO9 Addr1 PIN M23 M24 M25 M26 N1 N2 N3 N4 N5 N22 N23 N24 N25 N26 P1 P2 P3 P4 P5 P22 P23 P24 P25 P26 R1 R2 R3 R4 R5 R22 R23 R24 R25 PIN NAME Addr2 Addr3 AVDD Addr6 DMO3 RESET DMO0 DMO1 DMO2 WR RD CS RDY Addr7 DGND DVDD TEST TxON DVDD D0 DGND PCLK DVDD INT E3Clk DGND AGND AVDD SFM_EN D7 D6 D5 D4 PIN R26 T1 T2 T3 T4 T5 T22 T23 T24 T25 T26 U1 U2 U3 U4 U5 U22 U23 U24 U25 U26 V1 V2 V3 V4 V5 V22 V23 V24 V25 V26 W1 W2 PIN NAME D1 DS3Clk AGND RxNEG/LCV7 RxCLK7 RxPOS7 RxPOS5 RxCLK5 RxNEG/LCV5 AVDD D2 STS-1Clk/12M AGND RLOS7 RxNEG/LCV9 RLOL9 RLOL3 RxNEG/LCV3 RLOS5 AGND D3 DGND CLKOUT7 DVDD RxCLK9 DGND DGND RxCLK3 DVDD CLKOUT5 DGND DVDD RLOL7
PIN F1 F2 F3 F4 F5 F22 F23 F24 F25 F26 G1 G2 G3 G4 G5 G22 G23 G24 G25 G26 H1 H2 H3 H4 H5 H22 H23 H24 H25 H26 J1 J2 J3
15
XRT75R12D
TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
PRELIMINARY
PIN W3 W4 W5 W22 W23 W24 W25 W26 Y1 Y2 Y3 Y4 Y5 Y22 Y23 Y24 Y25 Y26 AA1 AA2 AA3 AA4 AA5 AA22 AA23 AA24 AA25 AA26 AB1 AB2 AB3 AB4 AB5 PIN NAME CLKOUT9 TxNEG9 CLKOUT11 CLKOUT1 TxNEG3 CLKOUT3 RLOL5 DVDD TxNEG7 DGND RxPOS9 TxCLK9 DVDD DVDD TxCLK3 RxPOS3 DGND TxNEG5 TxPOS7 TxCLK7 RLOS9 TxPOS9 TxCLK11 TxCLK1 TxPOS3 RLOS3 TxCLK5 TxPOS5 RLOL11 TxNEG11 TxPOS11 TDI TCK PIN AB6 AB7 AB8 AB9 AB10 AB11 AB12 AB13 AB14 AB15 AB16 AB17 AB18 AB19 AB20 AB21 AB22 AB23 AB24 AB25 AB26 AC1 AC2 AC3 AC4 AC5 AC6 AC7 AC8 AC9 AC10 AC11 AC12 PIN NAME AVDD AGND MTip9 AVDD AGND MTip7 RVDD7 RGND7 RGND5 RVDD5 MRing5 AGND AVDD MRing3 AGND AVDD AGND TMS TxPOS1 TxNEG1 RLOL1 RxNEG/LCV11 RxCLK11 DGND MRing11 RVDD11 DGND DGND MRing9 RGND9 MRing7 DGND DGND PIN AC13 AC14 AC15 AC16 AC17 AC18 AC19 AC20 AC21 AC22 AC23 AC24 AC25 AC26 AD1 AD2 AD3 AD4 AD5 AD6 AD7 AD8 AD9 AD10 AD11 AD12 AD13 AD14 AD15 AD16 AD17 AD18 AD19 PIN NAME RTip7 DGND MTip5 DGND AGND RVDD3 MTip3 DGND AGND RVDD1 MRing1 DGND RxCLK1 RxNEG/LCV1 RxPOS11 RLOS11 TTip11 MTip11 RRing11 DVDD TTip9 AGND RRing9 AGND TTip7 DVDD RRing7 DVDD AGND TTip5 AGND RRing3 AGND PIN AD20 AD21 AD22 AD23 AD24 AD25 AD26 AE1 AE2 AE3 AE4 AE5 AE6 AE7 AE8 AE9 AE10 AE11 AE12 AE13 AE14 AE15 AE16 AE17 AE18 AE19 AE20 AE21 AE22 AE23 AE24 AE25 AE26
REV. P1.0.1
PIN NAME TTip3 AGND RRing1 MTip1 TRing1 RLOS1 RxPOS1 AGND TDO TRing11 TVDD11 RTip11 TGND9 TRing9 DGND RTip9 TVDD7 TRing7 AGND AGND RRing5 TVDD5 TRing5 DGND RTip3 TVDD3 TRing3 DGND RTip1 TVDD1 TTip1 TRST AGND
16
XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
REV. P1.0.1
PRELIMINARY
PIN NAME AGND AGND DVDD TGND11 RGND11 TVDD9 DVDD DVDD RVDD9 TGND7 DVDD AVDD AVDD RTip5 TGND5 DVDD DVDD RGND3 TGND3 DVDD DVDD RGND1 TGND1 DVDD AGND AGND
PIN AF1 AF2 AF3 AF4 AF5 AF6 AF7 AF8 AF9 AF10 AF11 AF12 AF13 AF14 AF15 AF16 AF17 AF18 AF19 AF20 AF21 AF22 AF23 AF24 AF25 AF26
17
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
FUNCTIONAL DESCRIPTION
The XRT75R12D is a twelve channel fully integrated Line Interface Unit featuring EXAR's R3 Technology (Reconfigurable, Relayless Redundancy) for E3/DS3/STS-1 applications. The LIU incorporates 12 independent Receivers, Transmitters and Jitter Attenuators in a single 420 Lead TBGA package. Each channel can be independently programmed to support E3, DS-3 or STS-1 line rates using one input clock reference of 12.288MHz in Single Frequency Mode (SFM). The LIU is responsible for provding the physical connection between a line interface and an aggregate mapper or framing device. Along with the analog-todigital processing, the LIU offers monitoring and diagnostic features to help optimize network design implementation. A key characteristic within the network topology is Automatic Protection Switching (APS). EXAR's proven expertise in providing redundany solutions has paved the way for R3 Technology. 1.0 R3 TECHNOLOGY (RECONFIGURABLE, RELAYLESS REDUNDANCY) Redundancy is used to introduce reliability and protection into network card design. The redundant card in many cases is an exact replicate of the primary card, such that when a failure occurs the network processor can automatically switch to the backup card. EXAR's R3 technology has re-defined E3/DS-3/STS-1 LIU design for 1:1 and 1+1 redundancy applications. Without relays and one Bill of Materials, EXAR offers multi-port, integrated LIU solutions to assist high density aggregate applications and framing requirements with reliability. The following section can be used as a reference for implementing R3 Technology with EXAR's world leading line interface units. 1.1 Network Architecture A common network design that supports 1:1 or 1+1 redundancy consists of N primary cards along with N backup cards that connect into a mid-plane or back-plane architecture without transformers installed on the network cards. In addition to the network cards, the design has a line interface card with one source of transformers, connectors, and protection components that are common to both network cards. Wtih this design, the bill of materials is reduced to the fewest amount of components. See Figure 2. for a simplified block diagram of a typical redundancy design. FIGURE 2. NETWORK REDUNDANCY ARCHITECTURE
GND 37.5 0.01F Rx 0.01F 31.6 31.6 37.5
1:1
Framer/ Mapper
LIU
Tx
1:1
Primary Line Card
Line Interface Card
0.01F Rx 0.01F 31.6 31.6
Framer/ Mapper
LIU
Tx
Redundant Line Card Back Plane or Mid Plane
18
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 2.0 CLOCK SYNTHESIZER The LIU uses a flexible user interface for accepting clock references to generate the internal master clocks used to drive the LIU. The reference clock used to supply the microprocessor timing is generated from the DS3 or SFM clock input. Therefore, if the chip is configured for STS-1 only or E3 only, then the DS-3 input pin must be connected to the STS-1 pin or E3 pin respectively. In DS-3 mode or when SFM is used, the STS-1 and E3 input pins can be left unconnected. If SFM is enabled by pulling the SFM_EN pin "High", 12.288MHz is the only clock reference necessary to generate DS-3, E3, or STS-1 line rates and the microprocessor timing. A simplified block diagram of the clock synthesizer is shown in Figure 3 FIGURE 3. SIMPLIFIED BLOCK DIAGRAM OF THE INPUT CLOCK CIRCUITRY DRIVING THE MICROPROCESSOR
SFM_EN STS-1Clk/12M DS3Clk E3Clk
Clock Synthesizer
CLKOUT_n LOL_n
0 1
Processor
2.1
Clock Distribution
Network cards that are designed to support multiple line rates which are not configured for single frequency mode should ensure that a clock is applied to the DS3Clk input pin. For example: If the network card being supplied to an ISP requires E3 only, the DS-3 input clock reference is still necessary to provide read and write access to the internal microprocessor. Therefore, the E3 mode requires two input clock references. If however, multiple line rates will not be supported, i.e. E3 only, then the DS3Clk input pin may be hard wire connected to the E3Clk input pin. FIGURE 4. CLOCK DISTRIBUTION CONGIFURED IN E3 MODE WITHOUT USING SFM
DS3Clk
E3Clk
Clock Synthesizer
CLKOUT_n LOL_n
Processor
NOTE: For one input clock reference, the single frequency mode should be used.
19
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
3.0 THE RECEIVER SECTION The receiver is designed so that the LIU can recover clock and data from an attenuated line signal caused by cable loss or flat loss according to industry specifications. Once data is recovered, it is processed and presented at the receiver outputs according to the format chosen to interface with a Framer/Mapper or ASIC. This section describes the detailed operation of various blocks within the receive path. A simplified block diagram of the receive path is shown in Figure 5. FIGURE 5. RECEIVE PATH BLOCK DIAGRAM
Peak Detector Slicer Clock & Data Recovery LOS Detector Channel n Jitter Attenuator HDB3/ B3ZS Decoder RxClk_n RxPOS_n RxNEG/LCV_n RLOS_n
RTIP_n RRing_n
AGC/ Equalizer
MUX
3.1
Receive Line Interface
Physical Layer devices are AC coupled to a line interface through a 1:1 transformer. The transformer provides isolation and a level shift by blocking the DC offset of the incoming data stream. The typical medium for the line interface is a 75 coxial cable. Whether using E3, DS-3 or STS-1, the LIU requires the same bill of materials, see Figure 6. FIGURE 6. RECEIVE LINE INTERFACECONNECTION
1:1 RTIP_n Receiver 75 RRing_n
DS-3/E3/STS-1
37.5
37.5
0.01F RLOS_n
20
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 3.2 Adaptive Gain Control (AGC)
The Adaptive Gain Control circuit amplifies the incoming analog signal and compensates for the various flat losses and also for the loss at one-half symbol rate. The AGC has a dynamic range of 30 dB. The peak detector provides feedback to the equalizer before slicing occurs. 3.3 Receive Equalizer The Equalizer restores the integrity of the signal and compensates for the frequency dependent attenuation of up to 900 feet of coaxial cable (1300 feet for E3). The Equalizer also boosts the high frequency content of the signal to reduce Inter-Symbol Interference (ISI) so that the slicer slices the signal at 50% of peak voltage to generate Positive and Negative data. The equalizer can be disabled by programming the appropriate register. FIGURE 7. ACG/EQUALIZER BLCOK DIAGRAM
Peak Detector Slicer LOS Detector
RTIP_n RRing_n
AGC/ Equalizer
3.3.1
Recommendations for Equalizer Settings
The Equalizer has two gain settings to provide optimum equalization. In the case of normally shaped DS3/ STS-1 pulses (pulses that meet the template requirements) that has been driven through 0 to 900 feet of cable, the Equalizer can be enabled. However, for square-shaped pulses such as E3 or for DS3/STS-1 high pulses (that does not meet the pulse template requirements), it is recommended that the Equalizer be disabled for cable length less than 300 feet. This would help to prevent over-equalization of the signal and thus optimize the performance in terms of better jitter transfer characteristics. The Equalizer also contains an additional 20 dB gain stage to provide the line monitoring capability of the resistively attenuated signals which may have 20dB flat loss. The equalizer gain mode can be enabled by programming the appropriate register.
NOTE: The results of extensive testing indicate that even when the Equalizer was enabled, regardless of the cable length, the integrity of the E3 signal was restored properly over 0 to 12 dB cable loss at Industrial Temperature.
3.4
Clock and Data Recovery
The Clock and Data Recovery Circuit extracts the embedded clock, RxClk_n from the sliced digital data stream and provides the retimed data to the B3ZS (HDB3) decoder. The Clock Recovery PLL can be in one of the following two modes: 3.4.1 Data/Clock Recovery Mode In the presence of input line signals on the RTIP_n and RRing_n input pins and when the frequency difference between the recovered clock signal and the reference clock signal is less than 0.5%, the clock that is output on the RxClk_n out pins is the Recovered Clock signal. 3.4.2 Training Mode In the absence of input signals at RTIP_n and RRing_n pins, or when the frequency difference between the recovered line clock signal and the reference clock applied on the ExClk_n input pins exceed 0.5%, a Loss of Lock condition is declared by toggling RLOL_n output pin "High" or setting the RLOL_n bit to "1" in the control register. Also, the clock output on the RxClk_n pins are the same as the reference channel clock.
21
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
3.5 3.5.1 LOS (Loss of Signal) Detector DS3/STS-1 LOS Condition
A Digital Loss of SIgnal (DLOS) condition occurs when a string of 175 75 consecutive zeros occur on the line. When the DLOS condition occurs, the DLOS_n bit is set to "1" in the status control register. DLOS condition is cleared when the detected average pulse density is greater than 33% for 175 75 pulses. Analog Loss of Signal (ALOS) condition occurs when the amplitude of the incoming line signal is below the threshold as shown in the Table 2.The status of the ALOS condition is reflected in the ALOS_n status control register. RLOS is the logical OR of the DLOS and ALOS states. When the RLOS condition occurs the RLOS_n output pin is toggled "High" and the RLOS_n bit is set to "1" in the status control register. TABLE 2: THE ALOS (ANALOG LOS) DECLARATION AND CLEARANCE THRESHOLDS FOR A GIVEN SETTING OF LOSTHR AND REQEN (DS3 AND STS-1 APPLICATIONS)
APPLICATION REQEN SETTING LOSTHR SETTING DS3 0 1 0 1 STS-1 0 1 0 1 0 0 1 1 0 0 1 1 SIGNAL LEVEL TO DECLARE ALOS DEFECT < 75mVpk < 45mVpk < 120mVpk < 55mVpk < 120mVpk < 50mVpk < 125mVpk < 55mVpk SIGNAL LEVEL TO CLEAR ALOS DEFECT > 130mVpk > 60mVpk > 45mVpk > 180mVpk > 170mVpk > 75mVpk > 205mVpk > 90mVpk
3.5.2
Disabling ALOS/DLOS Detection
For debugging purposes it is useful to disable the ALOS and/or DLOS detection. Writing a "1" to both ALOSDIS_n and DLOSDIS_n bits disables the LOS detection on a per channel basis.
22
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 3.5.3 E3 LOS Condition:
If the level of incoming line signal drops below the threshold as described in the ITU-T G.775 standard, the LOS condition is detected. Loss of signal is defined as no transitions for 10 to 255 consecutive zeros. No transitions is defined as a signal level between 15 and 35 dB below the normal. This is illustrated in Figure 8. The LOS condition is cleared within 10 to 255 UI after restoration of the incoming line signal. Figure 9 shows the LOS declaration and clearance conditions. FIGURE 8. LOSS OF SIGNAL DEFINITION FOR E3 AS PER ITU-T G.775
0 dB
Maximum Cable Loss for E3
LOS Signal Must be Cleared
-12 dB -15dB
LOS Signal may be Cleared or Declared
-35dB
LOS Signal Must be Declared
FIGURE 9. LOSS OF SIGNAL DEFINITION FOR E3 AS PER ITU-T G.775.
Actual Occurrence of LOS Condition RTIP/ RRing Line Signal is Restored
10 UI
255 UI
Time Range for LOS Declaration
10 UI
255 UI
RLOS Output Pin 0 UI G.775 Compliance 0 UI Time Range for LOS Clearance G.775 Compliance
23
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
3.5.4 Interference Tolerance For E3 mode, ITU-T G.703 Recommendation specifies that the receiver be able to recover error free clock and data in the presence of a sinusoidal interfering tone signal. For DS3 and STS-1 modes, the same recommendation is being used. Figure 10 shows the configuration to test the interference margin for DS3/ STS1. Figure 11 shows the set up for E3. FIGURE 10. INTERFERENCE MARGIN TEST SET UP FOR DS3/STS-1
Attenuator Sine Wave Generator N
DS3 = 22.368 MHz STS-1 = 25.92 MHz
Cable Simulator Pattern Generator 2 23 -1 PRBS S
DUT XRT75R12D
Test Equipment
FIGURE 11. INTERFERENCE MARGIN TEST SET UP FOR E3.
Attenuator 1 Sine Wave Generator 17.184mHz N Attenuator 2
Signal Source 223-1 PRBS Cable Simulator S
DUT XRT75R12D Test Equipment
24
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
TABLE 3: INTERFERENCE MARGIN TEST RESULTS
MODE CABLE LENGTH (ATTENUATION) INTERFERENCE TOLERANCE Equalizer "IN" E3 0 dB 12 dB 0 feet DS3 225 feet 450 feet 0 feet STS-1 225 feet 450 feet -17 dB -14 dB -15 dB -15 dB -14 dB -15 dB -14 dB -14 dB
25
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
3.5.5 Muting the Recovered Data with LOS condition: When the LOS condition is declared, the clock recovery circuit locks into the reference clock applied to the internal master clock outputs this clock onto the RxClk_n output pin. The data on the RxPOS_n and RxNEG_n pins can be forced to zero by setting the LOSMUT_n bits in the individual channel control register to "1".
NOTE: When the LOS condition is cleared, the recovered data is output on RxPOS_n and RxNEG_n pins.
FIGURE 12. RECEIVER DATA OUTPUT AND CODE VIOLATION TIMING
tRRX RxClk tLCVO LCV tCO RPOS or RNEG
tFRX
SYMBOL
PARAMETER
MIN
TYP
MAX
UNITS
RxClk
Duty Cycle RxClk Frequency E3 DS-3 STS-1
45
50
55
%
34.368 44.736 51.84 2 2 4 4 4 2.5
MHz MHz MHz ns ns ns ns
tRRX tFRX tCO tLCVO
RxClk rise time (10% o 90%) RxClk falling time (10% to 90%) RxClk to RPOS/RNEG delay time RxClk to rising edge of LCV output delay
3.6
B3ZS/HDB3 Decoder
The decoder block takes the output from the clock and data recovery block and decodes the B3ZS (for DS3 or STS-1) or HDB3 (for E3) encoded line signal and detects any coding errors or excessive zeros in the data stream. Whenever the input signal violates the B3ZS or HDB3 coding sequence for bipolar violation or contains three (for B3ZS) or four (for HDB3) or more consecutive zeros, an active "High" pulse is generated on the RLCV_n output pins to indicate line code violation.
26
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 4.0 THE TRANSMITTER SECTION The transmitter is designed so that the LIU can accept serial data from a local device, encode the data properly, and then output an analog pulse according to the pulse shape chosen in the appropriate registers. This section describes the detailed operation of various blocks within the transmit path. A simplified block diagram of the transmit path is shown in Figure 13. FIGURE 13. TRANSMIT PATH BLOCK DIAGRAM
TTIP_n TRing_n MTIP_n MRing_n DMO_n
Line Driver
Tx Pulse Shaping
Timing Control
Jitter Attenuator
MUX
HDB3/ B3ZS Encoder
TxClk_n TxPOS_n TxNEG_n
Device Monitor
Tx Control Channel n
TxON
4.1
Transmit Digital Input Interface
The method for applying data to the transmit inputs of the LIU is a serial interface consisting of TxClk, TxPOS, and TxNEG. For single rail mode, only TxClk and TxPOS are necessary for providing the local data from a Framer device or ASIC. Data can be sampled on either edge of the input clock signal by programming the appropriate register. A typical interface is shown in Figure 14. FIGURE 14. TYPICAL INTERFACE BETWEEN TERMINAL EQUIPMENT AND THE XRT75R12D (DUAL-RAIL DATA)
TxPOS Terminal Equipment (E3/DS3 or STS-1 Framer) TxNEG TxLineClk
TPData TNData TxClk
Transmit Logic Block
Exar E3/DS3/STS-1 LIU
27
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
FIGURE 15. TRANSMITTER TERMINAL INPUT TIMING
tRTX TxClk tTSU TPData or TNData TTIP or TRing tTHO tFTX
SYMBOL
PARAMETER
MIN
TYP
MAX
UNITS
TxClk
Duty Cycle TxClk Frequency E3 DS-3 STS-1
30
50
70
%
34.368 44.736 51.84 4 4 3 3
MHz MHz MHz ns ns ns ns
tRTX tFTX tTSU tTHO
TxClk Rise Time (10% to 90%) TxClk Fall Time (10% to 90%) TPData/TNData to TxClk falling set up time TPData/TNData to TxClk falling hold time
FIGURE 16. SINGLE-RAIL OR NRZ DATA FORMAT (ENCODER AND DECODER ARE ENABLED)
Data
1
1
0
TPData TxClk
28
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER FIGURE 17. DUAL-RAIL DATA FORMAT (ENCODER AND DECODER ARE DISABLED)
Data
1
1
0
TPData TNData TxClk
4.2
Transmit Clock
The Transmit Clock applied via TxClk_n pins, for the selected data rate (for E3 = 34.368 MHz, DS3 = 44.736 MHz or STS-1 = 51.84 MHz), is duty cycle corrected by the internal PLL circuit to provide a 50% duty cycle clock to the pulse shaping circuit. This allows a 30% to 70% duty cycle Transmit Clock to be supplied. 4.3 B3ZS/HDB3 ENCODER When the Single-Rail (NRZ) data format is selected, the Encoder Block encodes the data into either B3ZS format (for either DS3 or STS-1) or HDB3 format (for E3). 4.3.1 B3ZS Encoding An example of B3ZS encoding is shown in Figure 18. If the encoder detects an occurrence of three consecutive zeros in the data stream, it is replaced with either B0V or 00V, where `B' refers to Bipolar pulse that is compliant with the Alternating polarity requirement of the AMI (Alternate Mark Inversion) line code and `V' refers to a Bipolar Violation (e.g., a bipolar pulse that violates the AMI line code). The substitution of B0V or 00V is made so that an odd number of bipolar pulses exist between any two consecutive violation (V) pulses. This avoids the introduction of a DC component into the line signal. FIGURE 18. B3ZS ENCODING FORMAT
TClk TPDATA Line Signal
1 1 0 0 1 11 1 0 0 1 0 0 V 0 0 B 0 0 0 V B V 0 0 0
0 0
0 0
0 V
0 0
1
4.3.2
HDB3 Encoding
An example of the HDB3 encoding is shown in Figure 19. If the HDB3 encoder detects an occurrence of four consecutive zeros in the data stream, then the four zeros are substituted with either 000V or B00V pattern. The substitution code is made in such a way that an odd number of pulses exist between any consecutive V pulses. This avoids the introduction of DC component into the analog signal.
29
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
FIGURE 19. HDB3 ENCODING FORMAT
TClk TPDATA Line Signal
1 1 0 0 1 11 1 0 0 0 0 0 0 0 V 1 1 0 0 0 0 0 0 V 0 0 B 0 0 0 0 0 V
4.4
TRANSMIT PULSE SHAPER
The Transmit Pulse Shaper converts the B3ZS encoded digital pulses into a single analog Alternate Mark Inversion (AMI) pulse that meets the industry standard mask template requirements for STS-1 and DS3. For E3 mode, the pulse shaper converts the HDB3 encoded pulses into a single full amplitude square shaped pulse with very little slope. The Pulse Shaper Block also includes a Transmit Build Out Circuit, which can either be disabled or enabled by setting the TxLEV_n bit to "1" or "0" in the control register. For DS3/STS-1 rates, the Transmit Build Out Circuit is used to shape the transmit waveform that ensures that transmit pulse template requirements are met at the Cross-Connect system. The distance between the transmitter output and the Cross-Connect system can be between 0 to 450 feet. For E3 rate, since the output pulse template is measured at the secondary of the transformer and since there is no Cross-Connect system pulse template requirements, the Transmit Build Out Circuit is always disabled. The differential line driver increases the transmit waveform to appropriate level and drives into the 75 load as shown in Figure 20. FIGURE 20. TRANSMIT PULSE SHAPE TEST CIRCUIT
R1
TxPOS(n) TxNEG(n) TxLineClk(n)
TPData(n) TNData(n) TxClk(n) TRing(n)
TTIP(n)
31.6 +1%
R2
31.6 + 1%
R3 75 1:1
4.4.1
Guidelines for using Transmit Build Out Circuit
If the distance between the transmitter and the DSX3 or STSX-1, Cross-Connect system, is less than 225 feet, enable the Transmit Build Out Circuit by setting the TxLEV_n control bit to "0". If the distance between the transmitter and the DSX3 or STSX-1 is greater than 225 feet, disable the Transmit Build Out Circuit.
30
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 4.5 E3 line side parameters
The XRT75R12D line output at the transformer output meets the pulse shape specified in ITU-T G.703 for 34.368 Mbits/s operation. The pulse mask as specified in ITU-T G.703 for 34.368 Mbits/s is shown in Figure 7. FIGURE 21. PULSE MASK FOR E3 (34.368 MBITS/S) INTERFACE AS PER ITU-T G.703
17 ns (14.55 + 2.45)
V = 100%
8.65 ns
Nominal Pulse
50%
14.55ns 12.1ns (14.55 - 2.45) 10% 20%
10% 0%
31
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
TABLE 4: E3 TRANSMITTER LINE SIDE OUTPUT AND RECEIVER LINE SIDE INPUT SPECIFICATIONS
PARAMETER MIN TYP MAX UNITS
TRANSMITTER LINE SIDE OUTPUT CHARACTERISTICS Transmit Output Pulse Amplitude (Measured at secondary of the transformer) Transmit Output Pulse Amplitude Ratio Transmit Output Pulse Width Transmit Intrinsic Jitter RECEIVER LINE SIDE INPUT CHARACTERISTICS Receiver Sensitivity (length of cable) Interference Margin Jitter Tolerance @ Jitter Frequency 800KHz Signal level to Declare Loss of Signal Signal Level to Clear Loss of Signal Occurence of LOS to LOS Declaration Time Termination of LOS to LOS Clearance Time -15 10 10 255 255 900 -20 0.15 1200 -14 0.28 -35 feet dB UI PP dB dB UI UI 0.95 12.5 1.00 14.55 0.02 1.05 16.5 0.05 ns UIPP 0.90 1.00 1.10 Vpk
NOTE: The above values are at TA = 250C and VDD = 3.3 V 5%.
32
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER FIGURE 22. BELLCORE GR-253 CORE TRANSMIT OUTPUT PULSE TEMPLATE FOR SONET STS-1 APPLICATIONS
ST S-1 Pulse T emplate
1.2
1
0.8 Norm a liz e d Am plitude
0.6 Lower Curve Upper Curve 0.4
0.2
0
-0.2
0
-1
1
2
3
4
5
6
7
8
9
1
1
2
3 1.
9
8
7
6
5
4
3
2
1
0.
0.
0.
0.
0.
0.
0.
0.
0.
1.
1.
-0 .
-0 .
-0 .
-0 .
-0 .
-0 .
-0 .
-0 .
-0 .
Time, in UI
TABLE 5: STS-1 PULSE MASK EQUATIONS
TIME IN UNIT INTERVALS LOWER CURVE -0.85 < T < -0.38 -0.38 - 0.03 NORMALIZED AMPLITUDE
< T < 0.36
* T 0.5 1 + sin -- 1 + ---------- - 0.03 0.18 2
- 0.03 UPPER CURVE
0.36 < T < 1.4
-0.85 < T < -0.68 -0.68 < T < 0.26
0.03
* T 0.5 1 + sin -- 1 + ---------- + 0.03 0.34 2 0.1 + 0.61 x e-2.4[T-0.26]
0.26 < T < 1.4
33
1.
4
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
TABLE 6: STS-1 TRANSMITTER LINE SIDE OUTPUT AND RECEIVER LINE SIDE INPUT SPECIFICATIONS (GR-253)
PARAMETER MIN TYP MAX UNITS
TRANSMITTER LINE SIDE OUTPUT CHARACTERISTICS Transmit Output Pulse Amplitude (measured with TxLEV = 0) Transmit Output Pulse Amplitude (measured with TxLEV = 1) Transmit Output Pulse Width Transmit Output Pulse Amplitude Ratio Transmit Intrinsic Jitter RECEIVER LINE SIDE INPUT CHARACTERISTICS Receiver Sensitivity (length of cable) Jitter Tolerance @ Jitter Frequency 400 KHz Signal Level to Declare Loss of Signal Signal Level to Clear Loss of Signal 900 0.15 Refer to Table 10 Refer to Table 10 1100 feet UIpp 8.6 0.90 9.65 1.00 0.02 10.6 1.10 0.05 UIpp ns 0.90 1.00 1.10 Vpk 0.65 0.75 0.90 Vpk
NOTE: The above values are at TA = 250C and VDD = 3.3 V 5%.
FIGURE 23. TRANSMIT OUPUT PULSE TEMPLATE FOR DS3 AS PER BELLCORE GR-499
DS3 Pulse T emplate
1.2
1
0.8 Norm a lize d Am plitude
0.6 Lower Curve Upper Curve 0.4
0.2
0
-0.2
-1
0
9
8
7
6
5
4
3
2
1
1
2
3
4
5
6
7
8
9
1
1
2
3 1.
0.
0.
0.
0.
0.
0.
0.
0.
0.
1.
1.
-0 .
-0 .
-0 .
-0 .
-0 .
-0 .
-0 .
-0 .
-0 .
Tim e , in UI
34
1.
4
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER TABLE 7: DS3 PULSE MASK EQUATIONS
TIME IN UNIT INTERVALS LOWER CURVE -0.85 < T < -0.36 -0.36 - 0.03 NORMALIZED AMPLITUDE
< T < 0.36
* T 0.5 1 + sin -- 1 + ---------- - 0.03 0.18 2
- 0.03 UPPER CURVE
0.36 < T < 1.4
-0.85 < T < -0.68 -0.68 < T < 0.36
0.03
* T 0.5 1 + sin -- 1 + ---------- + 0.03 2 0.34 0.08 + 0.407 x e-1.84[T-0.36]
0.36 < T < 1.4
TABLE 8: DS3 TRANSMITTER LINE SIDE OUTPUT AND RECEIVER LINE SIDE INPUT SPECIFICATIONS (GR-499)
PARAMETER MIN TYP MAX UNITS
TRANSMITTER LINE SIDE OUTPUT CHARACTERISTICS Transmit Output Pulse Amplitude (measured with TxLEV = 0) Transmit Output Pulse Amplitude (measured with TxLEV = 1) Transmit Output Pulse Width Transmit Output Pulse Amplitude Ratio Transmit Intrinsic Jitter RECEIVER LINE SIDE INPUT CHARACTERISTICS Receiver Sensitivity (length of cable) Jitter Tolerance @ 400 KHz (Cat II) Signal Level to Declare Loss of Signal Signal Level to Clear Loss of Signal 900 0.15 Refer to Table 10 Refer to Table 10 1100 feet UIpp 10.10 0.90 11.18 1.00 0.02 12.28 1.10 0.05 UIpp ns 0.90 1.00 1.10 Vpk 0.65 0.75 0.85 Vpk
NOTE: The above values are at TA = 250C and VDD = 3.3V 5%.
35
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
4.6 Transmit Drive Monitor This feature is used for monitoring the transmit line for occurrence of fault conditions such as a short circuit on the line or a defective line driver. To activate this function, connect MTIP_n pins to the TTIP_n lines via a 270 resistor and MRing_n pins to TRing_n lines via 270 resistor as shown in Figure 24. FIGURE 24. TRANSMIT DRIVER MONITOR SET-UP.
R1
TTIP(n)
31.6 +1%
R2
R3 75 1:1
TxPOS(n) TxNEG(n) TxLineClk(n)
TRing(n)
TPData(n) TNData(n) TxClk(n)
31.6 + 1%
R1
MTIP(n)
270
R2
MRing(n)
270
When the MTIP_n and MRing_n are connected to the TTIP_n and TRing_n lines, the drive monitor circuit monitors the line for transitions. The DMO_n (Drive Monitor Output) will be asserted "Low" as long as the transitions on the line are detected via MTIP_n and MRing_n. If no transitions on the line are detected for 128 32 TxClk_n periods, the DMO_n output toggles "High" and when the transitions are detected again, DMO_n toggles "Low".
NOTE: The Drive Monitor Circuit is only for diagnostic purpose and does not have to be used to operate the transmitter.
4.7
Transmitter Section On/Off
The transmitter section of each channel can either be turned on or off. To turn on the transmitter, set the input pin TxON to "High" and write a "1" to the TxON_n control bit. When the transmitter is turned off, TTIP_n and TRing_n are tri-stated.
NOTES: 1. 2. This feature provides support for Redundancy. If the XRT75R12D is configured in Host mode, to permit a system designed for redundancy to quickly shut-off the defective line card and turn on the back-up line card, writing a "1" to the TxON_n control bits transfers the control to TxON pin.
36
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 5.0 JITTER There are three fundamental parameters that describe circuit performance relative to jitter
* Jitter Tolerance * Jitter Transfer * Jitter Generation
5.1 JITTER TOLERANCE Jitter tolerance is a measure of how well a Clock and Data Recovery unit can successfully recover data in the presence of various forms of jitter. It is characterized by the amount of jitter required to produce a specified bit error rate. The tolerance depends on the frequency content of the jitter. Jitter Tolerance is measured as the jitter amplitude over a jitter spectrum for which the clock and data recovery unit achieves a specified bit error rate (BER). To measure the jitter tolerance as shown in Figure 25, jitter is introduced by the sinusoidal modulation of the serial data bit sequence. Input jitter tolerance requirements are specified in terms of compliance with jitter mask which is represented as a combination of points. Each point corresponds to a minimum amplitude of sinusoidal jitter at a given jitter frequency. FIGURE 25. JITTER TOLERANCE MEASUREMENTS
Pattern Generator
Data
DUT XRT75R12D
Error Detector
Clock Modulation Freq.
FREQ Synthesizer
5.1.1
DS3/STS-1 Jitter Tolerance Requirements
Bellcore GR-499 CORE specifies the minimum requirement of jitter tolerance for Category I and Category II. The jitter tolerance requirement for Category II is the most stringent. Figure 26 shows the jitter tolerance curve as per GR-499 specification.
37
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
FIGURE 26. INPUT JITTER TOLERANCE FOR DS3/STS-1
64 41 15 JITTER AMPLITUDE (UIpp) 10 5 1.5 0.3 0.15 0.1
GR-253 STS-1 GR-499 Cat II GR-499 Cat I XRT75R12D
0.01
0.03
0.3
2
20
100
JITTER FREQUENCY (kHz)
5.1.2
E3 Jitter Tolerance Requirements
ITU-T G.823 standard specifies that the clock and data recovery unit must be able to tolerate jitter up to certain specified limits. Figure 27 shows the tolerance curve. FIGURE 27. INPUT JITTER TOLERANCE FOR E3
64 JITTER AMPLITUDE (UIpp) 10 1.5
ITU-T G.823 XRT75R12D
0.3
0.1
1 JITTER FREQUENCY (kHz)
10
800
As shown in the Figures above, in the jitter tolerance measurement, the dark line indicates the minimum level of jitter that the E3/DS3/STS-1 compliant component must tolerate. Table 9 below shows the jitter amplitude versus the modulation frequency for various standards.
38
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER TABLE 9: JITTER AMPLITUDE VERSUS MODULATION FREQUENCY (JITTER TOLERANCE)
BIT RATE (KB/S) 34368 44736 44736 51840 INPUT JITTER AMPLITUDE (UI P-P) STANDARD A1 ITU-T G.823 GR-499 CORE Cat I GR-499 CORE Cat II GR-253 CORE Cat II 1.5 5 10 15 A2 0.15 0.1 0.3 1.5 A3 0.15
F1(HZ) F2(HZ) F3(KHZ) F4(KHZ) F5(KHZ)
MODULATION FREQUENCY
100 10 10 10
1000 2.3k 669 30
10 60 22.3 300
800 300 300 2
20
5.2
JITTER TRANSFER
Jitter Transfer function is defined as the ratio of jitter on the output relative to the jitter applied on the input versus frequency. There are two distinct characteristics in jitter transfer, jitter gain (jitter peaking) defined as the highest ratio above 0dB and jitter transfer bandwidth. The overall jitter transfer bandwidth is controlled by a low bandwidth loop, typically using a voltage-controlled crystal oscillator (VCXO). The jitter transfer function is a ratio between the jitter output and jitter input for a component, or system often expressed in dB. A negative dB jitter transfer indicates the element removed jitter. A positive dB jitter transfer indicates the element added jitter. A zero dB jitter transfer indicates the element had no effect on jitter. Table 10 shows the jitter transfer characteristics and/or jitter attenuation specifications for various data rates: TABLE 10: JITTER TRANSFER SPECIFICATION/REFERENCES
E3 ETSI TBR-24 DS3 GR-499 CORE section 7.3.2 Category I and Category II STS-1 GR-253 CORE section 5.6.2.1
NOTE: The above specifications can be met only with a jitter attenuator that supports E3/DS3/STS-1 rates.
5.3
Jitter Attenuator
An advanced crystal-less jitter attenuator per channel is included in the XRT75R12D. The jitter attenuator requires no external crystal nor high-frequency reference clock. By clearing or setting the JATx/Rx_n bits in the channel control registers selects the jitter attenuator either in the Receive or Transmit path on per channel basis. The FIFO size can be either 16-bit or 32-bit. The bits JA0_n and JA1_n can be set to appropriate combination to select the different FIFO sizes or to disable the Jitter Attenuator on a per channel basis. Data is clocked into the FIFO with the associated clock signal (TxClk or RxClk) and clocked out of the FIFO with the dejittered clock. When the FIFO is within two bits of overflowing or underflowing, the FIFO limit status bit, FL_n is set to "1" in the Alarm status register. Reading this bit clears the FIFO and resets the bit into default state.
NOTE: It is recommended to select the 16-bit FIFO for delay-sensitive applications as well as for removing smaller amounts of jitter. Table 11 specifies the jitter transfer mask requirements for various data rates:
39
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
TABLE 11: JITTER TRANSFER PASS MASKS
RATE (KBITS) 34368 44736 MASK G.823 ETSI-TBR-24 GR-499, Cat I GR-499, Cat II GR-253 CORE GR-253 CORE F1 (HZ) 100 F2 (HZ) 300 F3 (HZ) 3K F4 (KHZ) 800K A1(dB) 0.5 A2(dB) -19.5
10 10 10 10
10k 56.6k 40 40k
-
15k 300k 15k 400k
0.1 0.1 0.1 0.1
-
51840
The jitter attenuator within the XRT75R12D meets the latest jitter attenuation specifications and/or jitter transfer characteristics as shown in the Figure 28. FIGURE 28. JITTER TRANSFER REQUIREMENTS AND JITTER ATTENUATOR PERFORMANCE
JITTER AMPLITUDE
A1 A2
F1
F2
F3
F4
J IT T E R F R E Q U E N C Y (k H z )
5.3.1
JITTER GENERATION
Jitter Generation is defined as the process whereby jitter appears at the output port of the digital equipment in the absence of applied input jitter. Jitter Generation is measured by sending jitter free data to the clock and data recovery circuit and measuring the amount of jitter on the output clock or the re-timed data. Since this is essentially a noise measurement, it requires a definition of bandwidth to be meaningful. The bandwidth is set according to the data rate. In general, the jitter is measured over a band of frequencies.
40
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 6.0 DIAGNOSTIC FEATURES 6.1 PRBS Generator and Detector The XRT75R12D contains an on-chip Pseudo Random Binary Sequence (PRBS) generator and detector for diagnostic purpose. With the PRBSEN_n bit = "1", the transmitter will send out PRBS of 223-1 in E3 rate or 215-1 in STS-1/DS3 rate. At the same time, the receiver PRBS detector is also enabled. When the correct PRBS pattern is detected by the receiver, the RNEG/LCV pin will go "Low" to indicate PRBS synchronization has been achieved. When the PRBS detector is not in sync the PRBSLS bit will be set to "1" and RNEG/LCV pin will go "High". With the PRBS mode enabled, the user can also insert a single bit error by toggling "INSPRBS" bit. This is done by writing a "1" to INSPRBS bit. The receiver at RNEG/LCV pin will pulse "High" for one RxClk cycle for every bit error detected. Any subsequent single bit error insertion must be done by first writing a "0" to INSPRBS bit and followed by a "1". Figure 29 shows the status of RNEG/LCV pin when the XRT75R12D is configured in PRBS mode.
NOTE: In PRBS mode, the device is forced to operate in Single-Rail Mode.
FIGURE 29. PRBS MODE
RxClk
SYNC LOSS
RxNEG/LCV
PRBS SYNC Single Bit Error
41
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
6.2 LOOPBACKS The XRT75R12D offers three loopback modes for diagnostic purposes. The loopback modes are selected via the RLB_n and LLB_n bits n the Channel control registers select the loopback modes. 6.2.1 ANALOG LOOPBACK In this mode, the transmitter outputs TTIP_n and TRing_n are internally connected to the receiver inputs RTIP_n and RRing_n as shown in Figure 30. Data and clock are output at RxClk_n, RxPOS_n and RxNEG_n pins for the corresponding transceiver. Analog loopback exercises most of the functional blocks of the device including the jitter attenuator which can be selected in either the transmit or receive path.
NOTES: 1. In the Analog loopback mode, data is also output via TTIP_n and TRing_n pins. 2. Signals on the RTIP_n and RRing_n pins are ignored during analog loopback.
FIGURE 30. ANALOG LOOPBACK
TxClk TxPOS TxNEG HDB3/B3ZS ENCODER
JITTER ATTENUATOR
TIMING CONTROL
TTIP Tx TRing
RxClk RxPOS RxNEG HDB3/B3ZS DECODER
JITTER ATTENUATOR
DATA & CLOCK RECOVERY
RTIP Rx RRing
42
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 6.2.2 DIGITAL LOOPBACK
When the Digital Loopback is selected, the transmit clock TxClk_n and transmit data inputs (TxPOS_n & TxNEG_n are looped back and output onto the RxClk_n, RxPOS_n and RxNEG_n pins as shown in Figure 31. FIGURE 31. DIGITAL LOOPBACK
TxCLK TxPOS TxNEG HDB3/B3ZS ENCODER
JITTER ATTENUATOR
TIMING CONTROL
TTIP Tx TRing
RxCLK RxPOS RxNEG HDB3/B3ZS DECODER
JITTER ATTENUATOR
DATA & CLOCK RECOVERY
RTIP Rx RRing
6.2.3
REMOTE LOOPBACK
With Remote loopback activated as shown in Figure 32, the receive data on RTIP and RRing is looped back after the jitter attenuator (if selected in receive or transmit path) to the transmit path using RxClk as transmit timing. The receive data is also output via the RxPOS and RxNEG pins.
NOTE: Input signals on TxClk, TxPOS and TxNEG are ignored during Remote loopback.
FIGURE 32. REMOTE LOOPBACK
TxCLK TxPOS TxNEG HDB3/B3ZS ENCODER
JITTER ATTENUATOR
TIMING CONTROL
TTIP Tx TRing
RxCLK RxPOS RxNEG HDB3/B3ZS DECODER
JITTER ATTENUATOR
DATA & CLOCK RECOVERY
RTIP Rx RRing
43
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
6.3 TRANSMIT ALL ONES (TAOS) Transmit All Ones (TAOS) can be set by setting the TAOS_n control bits to "1" in the Channel control registers. When the TAOS is set, the Transmit Section generates and transmits a continuous AMI all "1's" pattern on TTIP_n and TRing_n pins. The frequency of this ones pattern is determined by TxClk_n. the TAOS data path is shown in Figure 33. TAOS does not operate in Analog loopback or Remote loopback modes, however will function in Digital loopback mode. FIGURE 33. TRANSMIT ALL ONES (TAOS)
TxCLK TxPOS TxNEG HDB3/B3ZS ENCODER
JITTER ATTENUATOR
TIMING CONTROL
Tx
TTIP Transmit All 1's TRing
TAOS
RxCLK RxPOS RxNEG HDB3/B3ZS DECODER
JITTER ATTENUATOR
DATA & CLOCK RECOVERY
RTIP Rx RRing
44
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 7.0 MICROPROCESSOR INTERFACE BLOCK The Microprocessor Interface section supports communication between the local microprocessor (P) and the LIU. The XRT75R12D supports a parallel interface asynchronously or synchronously timed to the LIU. The microprocessor interface is selected by the state of the Pmode input pin. Selecting the microprocessor interface mode is shown in Table 12. TABLE 12: SELECTING THE MICROPROCESSOR INTERFACE MODE
PMODE "Low" "High" MICROPROCESSOR MODE Asynchronous Mode Synchronous Mode
The local P configures the LIU by writing data into specific addressable, on-chip Read/Write registers. The P provides the signals which are required for a general purpose microprocessor to read or write data into these registers. The P also supports polled and interrupt driven environments. A simplified block diagram of the microprocessor is shown in Figure 34. FIGURE 34. SIMPLIFIED BLOCK DIAGRAM OF THE MICROPROCESSOR INTERFACE BLOCK
CS WR RD
Addr[7:0] D[7:0] PCLK Pmode RESET RDY INT
Microprocessor Interface
45
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
7.1 THE MICROPROCESSOR INTERFACE BLOCK SIGNALS The LIU may be configured into different operating modes and have its performance monitored by software through a standard microprocessor using data, address and control signals. These interface signals are described below in Table 13. The microprocessor interface can be configured to operate in Asynchronous mode or Synchronous mode. TABLE 13: XRT75R12D MICROPROCESSOR INTERFACE SIGNALS
PIN NAME TYPE I I/O I DESCRIPTION Microprocessor Interface Mode Select Input pin This pin is used to specify the microprocessor interface mode. Bi-Directional Data Bus for register "Read" or "Write" Operations. Eight-Bit Address Bus Inputs The XRT75R12D LIU microprocessor interface uses a direct address bus. This address bus is provided to permit the user to select an on-chip register for Read/Write access. Chip Select Input This active low signal selects the microprocessor interface of the XRT75R12D LIU and enables Read/Write operations with the on-chip register locations. Read Signal This active low input functions as the read signal from the local P. When this pin is pulled "Low" (if CS is "Low") the LIU is informed that a read operation has been requested and begins the process of the read cycle. Write Signal This active low input functions as the write signal from the local P. When this pin is pulled "Low" (if CS is "Low") the LIU is informed that a write operation has been requested and begins the process of the write cycle. Ready Output This active low signal is provided by the LIU device. It indicates that the current read or write cycle is complete, and the LIU is waiting for the next command. Interrupt Output This active low signal is provided by the LIU to alert the local mP that a change in alarm status has occured. This pin is Reset Upon Read (RUR) once the alarm status registers have been cleared. Reset Input This active low input pin is used to Reset the LIU.
Pmode
D[7:0] Addr[7:0]
CS
I
RD
I
WR
I
RDY INT
O O
RESET
I
46
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 7.2 ASYNCHRONOUS AND SYNCHRONOUS DESCRIPTION Whether the LIU is configured for Asynchronous or Synchronous mode, the following descriptions apply. The synchronous mode requires an input clock (PCLK) to be used as the microprocessor timing reference. Read and Write operations are described below. Read Cycle (For Pmode = "0" or "1") Whenever the local P wishes to read the contents of a register, it should do the following. 1. Place the address of the target register on the address bus input pins Addr[7:0]. 2. While the P is placing this address value on the address bus, the address decoding circuitry should assert the CS pin of the LIU, by toggling it "Low". This action enables communication between the P and the LIU microprocessor interface block. 3. Next, the P should indicate that this current bus cycle is a Read operation by toggling the RD input pin "Low". This action enables the bi-directional data bus output drivers of the LIU. 4. After the P toggles the Read signal "Low", the LIU will toggle the RDY output pin "Low". The LIU does this to inform the P that the data is available to be read by the P, and that it is ready for the next command. 5. After the P detects the RDY signal and has read the data, it can terminate the Read Cycle by toggling the RD input pin "High". 6. The CS input pin must be pulled "High" before a new command can be issued. Write Cycle (For Pmode = "0" or "1") Whenever a local P wishes to write a byte or word of data into a register within the LIU, it should do the following. 1. Place the address of the target register on the address bus input pins Addr[7:0]. 2. While the P is placing this address value on the address bus, the address decoding circuitry should assert the CS pin of the LIU, by toggling it "Low". This action enables communication between the P and the LIU microprocessor interface block. 3. The P should then place the byte or word that it intends to write into the target register, on the bi-directional data bus D[7:0]. 4. Next, the P should indicate that this current bus cycle is a Write operation by toggling the WR input pin "Low". This action enables the bi-directional data bus input drivers of the LIU. 5. After the P toggles the Write signal "Low", the LIU will toggle the RDY output pin "Low". The LIU does this to inform the P that the data has been written into the internal register location, and that it is ready for the next command. 6. The CS input pin must be pulled "High" before a new command can be issued.
47
PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
FIGURE 35. ASYNCHRONOUS P INTERFACE SIGNALS DURING PROGRAMMED I/O READ AND WRITE OPERATIONS
READ OPERATION
t0 Addr[7:0] Valid Address t0 Valid Address
WRITE OPERATION
CS
D[7:0] t1 RD
Valid Data for Readback
Data Available to Write Into the LIU
t3 WR t2 t4 RDY
TABLE 14: ASYNCHRONOUS TIMING SPECIFICATIONS
SYMBOL t0 t1 t2 NA t3 t4 NA PARAMETER Valid Address to CS Falling Edge CS Falling Edge to RD Assert RD Assert to RDY Assert RD Pulse Width (t2) CS Falling Edge to WR Assert WR Assert to RDY Assert WR Pulse Width (t4) MIN 0 0 70 0 70 MAX 65 65 ns ns ns ns ns ns ns UNITS
48
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER FIGURE 36. SYNCHRONOUS P INTERFACE SIGNALS DURING PROGRAMMED I/O READ AND WRITE OPERATIONS
READ OPERATION
PCLK t0 Addr[7:0] Valid Address t0 Valid Address
WRITE OPERATION
CS
D[7:0] t1 RD
Valid Data for Readback
Data Available to Write Into the LIU
t3 WR t2 t4 RDY
TABLE 15: SYNCHRONOUS TIMING SPECIFICATIONS
SYMBOL t0 t1 t2 NA t3 t4 NA PARAMETER Valid Address to CS Falling Edge CS Falling Edge to RD Assert RD Assert to RDY Assert RD Pulse Width (t2) CS Falling Edge to WR Assert WR Assert to RDY Assert WR Pulse Width (t4) PCLK Period PCLK Duty Cycle PCLK "High/Low" time MIN 0 0 40 0 40 15 MAX 35 35 ns ns ns, see note 1 ns ns ns, see note 1 ns ns UNITS
NOTE: 1. This timing parameter is based on the frequency of the synchronous clock (PCLK). To determine the access time, use the following formula: (PCLKperiod * 2) + 5ns
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
7.3 Register Map TABLE 16: COMMAND REGISTER ADDRESS MAP, WITHIN THE XRT75R12D
ADDRESS (HEX) 0x00 COMMAND REGISTER (DECIMAL) CR0 LABEL APST TYPE R/W REGISTER NAME APS Transmit Redundancy Control Register 0-5
CHANNEL 0 CONTROL REGISTERS 0x01 0x02 0x03 0x04 0x05 0x06 0x07 0x08 0x09 0x0A 0x0B 0x0C 0x0D 0x0E 0x0F 0x10 CHANNEL 1 CONTROL REGISTERS 0x11 0x12 0x13 0x14 0x15 0x16 0x17 0x18 0x19 0x1A 0x1B 0x1C CR26 CR27 CR28 EM1 EL1 EH1 R/W R/W R/W Error counter MSByte Ch 1 Error counter LSbyte Error counter Holding register CR17 CR18 CR19 CR20 CR21 CR22 CR23 IER1 ISR1 AS1 TC0 RC1 CC1 JA1 R/W RUR R/O R/W R/W R/W R/W Source Level Interrupt Enable Register - Ch 1 Source Level Interrupt Status Register - Ch 1 Alarm Status Register - Ch 1 Transmit Control Register - Ch 1 Receive Control Register - Ch 1 Channel Control Register - Ch 1 Jitter Attenuator Control Register - Ch 1 CR10 CR11 CR12 EM0 EL0 EH0 R/W R/W R/W Error counter MS Byte Ch 0 Error counter LS Byte Error counter Holding register CR1 CR2 CR3 CR4 CR5 CR6 CR7 CR8 IER0 ISR0 AS0 TC0 RC0 CC0 JA0 APSR R/W RUR R/O R/W R/W R/W R/W R/W Source Level Interrupt Enable Register - Ch 0 Source Level Interrupt Status Register Ch 0 Alarm Status Register - Ch 0 Transmit Control Register - Ch 0 Receive Control Register - Ch 0 Channel Control Register - Ch 0 Jitter Attenuator Control Register - Ch 0 APS Receive Redundancy Control Register 0-5
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
ADDRESS (HEX) 0x1D 0x1E 0x1F 0x20 CHANNEL 2 CONTROL REGISTERS 0x21 0x22 0x23 0x24 0x25 0x26 0x27 0x28 0x29 0x2A 0x2B 0x2C 0x2D 0x2E 0x2F 0x30 CHANNEL 3 CONTROL REGISTERS 0x31 0x32 0x33 0x34 0x35 0x36 0x37 0x38 0x39 0x3A 0x3B CR58 CR59 EM3 EL3 R/W R/W Error counter MSByte Ch 3 Error counter LSbyte CR49 CR50 CR51 CR52 CR53 CR54 CR55 IER3 ISR3 AS3 TC3 RC3 CC3 JA3 R/W RUR R/O R/W R/W R/W R/W Source Level Interrupt Enable Register - Ch 3 Source Level Interrupt Status Register - Ch 3 Alarm Status Register - Ch 3 Transmit Control Register - Ch 3 Receive Control Register - Ch 3 Channel Control Register - Ch 3 Jitter Attenuator Control Register - Ch 3 CR42 CR43 CR44 EM2 EL2 EH2 R/W R/W R/W Error counter MSByte Ch 2 Error counter LSbyte Error counter Holding register CR33 CR34 CR35 CR36 CR37 CR38 CR39 IER2 ISR2 AS2 TC2 RC2 CC2 JA2 R/W RUR R/O R/W R/W R/W R/W Source Level Interrupt Enable Register - Ch 2 Source Level Interrupt Status Register - Ch 2 Alarm Status Register - Ch 2 Transmit Control Register - Ch 2 Receive Control Register - Ch 2 Channel Control Register - Ch 2 Jitter Attenuator Control Register - Ch 2 COMMAND REGISTER (DECIMAL) LABEL TYPE REGISTER NAME
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
ADDRESS (HEX) 0x3C 0x3D 0x3E 0x3F 0x40 CHANNEL 4 CONTROL REGISTERS 0x41 0x42 0x43 0x44 0x45 0x46 0x47 0x48 0x49 0x4A 0x4B 0x4C 0x4D 0x4E 0x4F 0x50 CHANNEL 5 CONTROL REGISTERS 0x51 0x52 0x53 0x54 0x55 0x56 0x57 0x58 0x59 0x5A CR90 EM5 R/W Error counter MSByte Ch 5 CR81 CR82 CR83 CR84 CR85 CR86 CR87 IER5 ISR5 AS5 TC5 RC5 CC5 JA5 R/W RUR R/O R/W R/W R/W R/W Source Level Interrupt Enable Register - Ch 5 Source Level Interrupt Status Register - Ch 5 Alarm Status Register - Ch 5 Transmit Control Register - Ch 5 Receive Control Register - Ch 5 Channel Control Register - Ch 5 Jitter Attenuator Control Register - Ch 5 CR74 CR75 CR76 EM4 EL4 EH4 R/W R/W R/W Error counter MSByte Ch 4 Error counter LSbyte Error counter Holding register CR65 CR66 CR67 CR68 CR69 CR70 CR71 IER4 ISR4 AS4 TC4 RC4 CC4 JA4 R/W RUR R/O R/W R/W R/W R/W Source Level Interrupt Enable Register - Ch 4 Source Level Interrupt Status Register - Ch 4 Alarm Status Register - Ch 4 Transmit Control Register - Ch 4 Receive Control Register - Ch 4 Channel Control Register - Ch 4 Jitter Attenuator Control Register - Ch 4 COMMAND REGISTER (DECIMAL) CR60 LABEL EH3 TYPE R/W REGISTER NAME Error counter Holding register
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
ADDRESS (HEX) 0x5B 0x5C 0x5D 0x5E 0x5F 0x60 0x61 0x62 0x63 0x64 0x65 0x66 0x67 0x68 0x65 0x69 0x6A 0x6B 0x6C 0x6D 0x6E 0x6F 0x70 0x71 0x72 0x73 0x74 0x75 0x76 0x77 0x78 0x75 0x79 CR110 CR111 PN VN R/O R/O Device Part Number Register Chip Revision Number Register CR96 CR97 CIE CIS R/W R/O Channel 0-5 Interrupt Enable flags Channel 0-5 Interrupt status flags COMMAND REGISTER (DECIMAL) CR91 CR92 LABEL EL5 EH5 TYPE R/W R/W REGISTER NAME Error counter LSbyte Error counter Holding register
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
ADDRESS (HEX) 0x7A 0x7B 0x7C 0x7D 0x7E 0x7F 0x80 CR128 APST R/W APS Transmit Redundancy Control Register 6-11 COMMAND REGISTER (DECIMAL) LABEL TYPE REGISTER NAME
CHANNEL 6 CONTROL REGISTERS 0x81 0x82 0x83 0x84 0x85 0x86 0x87 0x88 0x89 0x8A 0x8B 0x8C 0x8D 0x8E 0x8F 0x90 CHANNEL 7 CONTROL REGISTERS 0x91 0x92 0x93 0x94 0x95 0x96 0x97 0x98 CR145 CR146 CR147 CR148 CR149 CR150 CR151 IER7 ISR7 AS7 TC7 RC7 CC7 JA7 R/W RUR R/O R/W R/W R/W R/W Source Level Interrupt Enable Register - Ch 7 Source Level Interrupt Status Register - Ch 7 Alarm Status Register - Ch 7 Transmit Control Register - Ch 7 Receive Control Register - Ch 7 Channel Control Register - Ch 7 Jitter Attenuator Control Register - Ch 7 CR138 CR139 CR140 EM6 EL6 EH6 R/W R/W R/W Error counter MSByte Ch 6 Error counter LSbyte Error counter Holding register CR129 CR130 CR131 CR132 CR133 CR134 CR135 CR136 IER6 ISR6 AS6 TC6 RC6 CC6 JA6 APSR R/W RUR R/O R/W R/W R/W R/W R/W Source Level Interrupt Enable Register - Ch 6 Source Level Interrupt Status Register - Ch 6 Alarm Status Register - Ch 6 Transmit Control Register - Ch 6 Receive Control Register - Ch 6 Channel Control Register - Ch 6 Jitter Attenuator Control Register - Ch 6 APS Receive Redundancy Control Register 6-11
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
ADDRESS (HEX) 0x99 0x9A 0x9B 0x9C 0x9D 0x9E 0x9F 0xA0 CHANNEL 8 CONTROL REGISTERS 0xA1 0xA2 0xA3 0xA4 0xA5 0xA6 0xA7 0xA8 0xA9 0xAA 0xAB 0xAC 0xAD 0xAE 0xAF 0xB0 CHANNEL 9 CONTROL REGISTERS 0xB1 0xB2 0xB3 0xB4 0xB5 0xB6 0xB7 CR177 CR178 CR179 CR180 CR181 CR182 CR183 IER9 ISR9 AS9 TC9 RC9 CC9 JA9 R/W RUR R/O R/W R/W R/W R/W Source Level Interrupt Enable Register - Ch 9 Source Level Interrupt Status Register - Ch 9 Alarm Status Register - Ch 9 Transmit Control Register - Ch 9 Receive Control Register - Ch 9 Channel Control Register - Ch 9 Jitter Attenuator Control Register - Ch 9 CR170 CR171 CR172 EM8 EL8 EH8 R/W R/W R/W Error counter MSByte Ch 8 Error counter LSbyte Error counter Holding register CR161 CR162 CR163 CR164 CR165 CR166 CR167 IER8 ISR8 AS8 TC8 RC8 CC8 JA8 R/W RUR R/O R/W R/W R/W R/W Source Level Interrupt Enable Register - Ch 8 Source Level Interrupt Status Register - Ch 8 Alarm Status Register - Ch 8 Transmit Control Register - Ch 8 Receive Control Register - Ch 8 Channel Control Register - Ch 8 Jitter Attenuator Control Register - Ch 8 CR154 CR155 CR156 EM7 EL7 EH7 R/W R/W R/W Error counter MSByte Ch 7 Error counter LSbyte Error counter Holding register COMMAND REGISTER (DECIMAL) LABEL TYPE REGISTER NAME
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
ADDRESS (HEX) 0xB8 0xB9 0xBA 0xBB 0xBC 0xBD 0xBE 0xBF 0xC0 CHANNEL 10 CONTROL REGISTERS 0xC1 0xC2 0xC3 0xC4 0xC5 0xC6 0xC7 0xC8 0xC9 0xCA 0xCB 0xCC 0xCD 0xCE 0xCF 0xD0 CHANNEL 11 CONTROL REGISTERS 0xD1 0xD2 0xD3 0xD4 0xD5 0xD6 CR209 CR210 CR211 CR212 CR213 CR214 IER11 ISR11 AS11 TC11 RC11 CC11 R/W RUR R/O R/W R/W R/W Source Level Interrupt Enable Register - Ch 11 Source Level Interrupt Status Register - Ch 11 Alarm Status Register - Ch 11 Transmit Control Register - Ch 11 Receive Control Register - Ch 11 Channel Control Register - Ch 11 CR202 CR203 CR204 EM10 EL10 EH10 R/W R/W R/W Error counter MSByte Ch 10 Error counter LSbyte Error counter Holding register CR193 CR194 CR195 CR196 CR197 CR198 CR199 IER10 ISR10 AS10 TC10 RC10 CC10 JA10 R/W RUR R/O R/W R/W R/W R/W Source Level Interrupt Enable Register - Ch 10 Source Level Interrupt Status Register - Ch 10 Alarm Status Register - Ch 10 Transmit Control Register - Ch 10 Receive Control Register - Ch 10 Channel Control Register - Ch 10 Jitter Attenuator Control Register - Ch 10 CR186 CR187 CR188 EM9 EL9 EH9 R/W R/W R/W Error counter MSByte Ch 9 Error counter LSbyte Error counter Holding register COMMAND REGISTER (DECIMAL) LABEL TYPE REGISTER NAME
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
ADDRESS (HEX) 0xD7 0xD8 0xD9 0xDA 0xDB 0xDC 0xDD 0xDE 0xDF 0xE0 0xE1 0xE2 0xE3 0xE4 0xE5 0xE6 0xE7 0xE8 0xE5 0xE9 0xEA 0xEB 0xEC 0xED 0xEE 0xEF 0xF0 0xF1 0xF2 0xF3 0xF4 0xF5 0xF6 CR224 CR225 CIE CIS R/W R/O Channel 6-11 Interrupt enable flags Channel 6-11 Interrupt status flags CR218 CR219 CR229 EM11 EL11 EH11 R/W R/W R/W Error counter MSByte Ch 11 Error counter LSbyte Error counter Holding register COMMAND REGISTER (DECIMAL) CR215 LABEL JA11 TYPE R/W REGISTER NAME Jitter Attenuator Control Register - Ch 11
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
ADDRESS (HEX) 0xF7 0xF8 0xF5 0xF9 0xFA 0xFB 0xFC 0xFD 0xFE 0xFF COMMAND REGISTER (DECIMAL) LABEL TYPE REGISTER NAME
58
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER THE GLOBAL/CHIP-LEVEL REGISTERS The register set, within the XRT75R12D contains ten global or chip-level registers. These registers control operations in more than one channel or apply to the complete chip. This section will present detailed information on the Global Registers. TABLE 17: LIST AND ADDRESS LOCATIONS OF GLOBAL REGISTERS
ADDRESS 0x00 0x08 0x80 0x88 0x60 0x61 0xE0 0xE1 0x6E 0x6F COMMAND REGISTER CR0 CR8 CR128 CR136 CR96 CR97 CR224 CR225 CR110 CR111 LABEL APST APSR APST APSR CIE CIS CIE CIS PN VN TYPE R/W R/W R/W R/W R/W R/O R/W R/O ROM ROM REGISTER NAME APS Transmit Redundancy Control Register 0-5 APS Receive Redundancy Control Register 0-5 APS Transmit Redundancy Control Register 6-11 APS Receive Redundancy Control Register 6-11 Channel 0-5 Interrupt Enable flags Channel 0-5 Interrupt status flags Channel 6-11 Interrupt enable flags Channel 6-11 Interrupt status flags Device Part Number Register Chip Revision/Version Number Register
REGISTER DESCRIPTION - GLOBAL REGISTERS TABLE 18: APS/REDUNDANCY TRANSMIT CONTROL REGISTER - CR0 (ADDRESS LOCATION = 0X00)
BIT 7 Reserved BIT 6 Reserved BIT 5 TxON Ch 5 R/W BIT 4 TxON Ch 4 R/W BIT 3 TxON Ch 3 R/W BIT 2 TxON Ch 2 R/W BIT 1 TxON Ch 1 R/W BIT 0 TxON Ch 0 R/W
BIT NUMBER 7,6 5 4 3 2 1 0
NAME Reserved TxON Ch 5 TxON Ch 4 TxON Ch 3 TxON Ch 2 TxON Ch 1 TxON Ch 0
TYPE
DESCRIPTION
R/W
Transmit Section ON - Channel n This READ/WRITE bit-field is used to turn on or turn off the Transmit Driver associated with Channel n. If the user turns on the Transmit Driver, then Channel n will transmit DS3, E3 or STS-1 pulses on the line via the TTIP_n and TRING_ n output pins. Conversely, if the user turns off the Transmit Driver, then the TTIP_n and TRING_n output pins will be tri-stated. 0 - Shuts off the Transmit Driver associated with Channel n and tristates the TTIP_n and TRING_ n output pins. 1 - Turns on the Transmit Driver associated with Channel n.
NOTE: The master TxON control pin(pin # P4) must be in a high state (logic 1) for this operation to turn on any channel.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
TABLE 19: APS/REDUNDANCY TRANSMIT CONTROL REGISTER - CR8 (ADDRESS LOCATION = 0X08)
BIT 7 Reserved BIT 6 Reserved BIT 5 TxON Ch 11 R/W BIT 4 TxON Ch 10 R/W BIT 3 TxON Ch 9 R/W BIT 2 TxON Ch 8 R/W BIT 1 TxON Ch 7 R/W BIT 0 TxON Ch 6 R/W
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
BIT NUMBER 7,6 5 4 3 2 1 0
NAME Reserved TxON Ch 11 TxON Ch 10 TxON Ch 9 TxON Ch 8 TxON Ch 7 TxON Ch 6
TYPE
DESCRIPTION
R/W
Transmit Section ON - Channel n This READ/WRITE bit-field is used to turn on or turn off the Transmit Driver associated with Channel n on a per channel basis. If the user turns on the Transmit Driver, then Channel n will transmit DS3, E3 or STS-1 pulses on the line via the TTIP_n and TRING_ n output pins. Conversely, if the user turns off the Transmit Driver (for channel n), the TTIP_n and TRING_n output pins will be tri-stated. 0 - Shuts off the Transmit Driver associated with Channel n and tristates the TTIP_n and TRING_ n output pins. 1 - Turns on the Transmit Driver associated with Channel n.
NOTE: The master TxON control (pin # P4) must be in a high state (logic 1) for this operation to turn on any channel.
TABLE 20: CHANNEL LEVEL INTERRUPT ENABLE REGISTER - CR96 (ADDRESS LOCATION = 0X60)
BIT 7 Reserved BIT 6 Reserved BIT 5 Channel 5 Interrupt Enable R/W BIT 4 Channel 4 Interrupt Enable R/W BIT 3 Channel 3 Interrupt Enable R/W BIT 2 Channel 2 Interrupt Enable R/W BIT 1 Channel 1 Interrupt Enable R/W BIT 0 Channel 0 Interrupt Enable R/W
BIT NUMBER 7,6 5 4 3 2 1 0
NAME Unused Channel 5 Interrupt Enable Channel 4 Interrupt Enable Channel 3 Interrupt Enable Channel 2 Interrupt Enable Channel 1 Interrupt Enable Channel 0 Interrupt Enable
TYPE
DESCRIPTION
R/W
Channel n Interrupt Enable Bit: This READ/WRITE bit is used to:
* To enable Channel n for Interrupt Generation at the Channel
Level
* To disable all Interrupts associated with Channel n within the
XRT75R12D This is a "master" enable bit for each channel. This bit allows control on a per channel basis to signal the Host of selected error conditions. If a bit is cleared, no interrupts from that channel will be sent to the Host via the INT. If the bit is set (logic 1), any generated interrupt in channel n that has been enabled in the Interrupt Enable register (IERn) for the channel will activate the INT pin to the Host. 0 - Disables all Channel n related Interrupts. 1 - Enables Channel n-related Interrupts. The user must enable individual Channel n related Interrupts at the source level, before they are can generate an interrupt.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
TABLE 21: CHANNEL LEVEL INTERRUPT ENABLE REGISTER - CR224 (ADDRESS LOCATION = 0XE0)
BIT 7 Reserved BIT 6 Reserved BIT 5 Channel 11 Interrupt Enable R/W BIT NUMBER 7,6 5 4 3 2 1 0 BIT 4 Channel 10 Interrupt Enable R/W BIT 3 Channel 9 Interrupt Enable R/W BIT 2 Channel 8 Interrupt Enable R/W BIT 1 Channel 7 Interrupt Enable R/W BIT 0 Channel 6 Interrupt Enable R/W
NAME Reserved Channel 11 Interrupt Enable Channel 10 Interrupt Enable Channel 9 Interrupt Enable Channel 8 Interrupt Enable Channel 7 Interrupt Enable Channel 6 Interrupt Enable
TYPE
DESCRIPTION
R/W
Channel n Interrupt Enable Bit: This READ/WRITE bit is used to:
* To enable Channel n for Interrupt Generation at the Channel
Level
* To disable all Interrupts associated with Channel n within the
XRT75R12D This is a "master" enable bit for each channel. This bit allows control on a per channel basis to signal the Host of selected error conditions. If a bit is cleared, no interrupts from that channel will be sent to the Host via the INT pin. If the bit is set (logic 1), any generated interrupt in channel n that has been enabled in the Interrupt Enable register (IERn) for the channel will activate the INT pin to the Host. 0 - Disables all Channel n related Interrupts. 1 - Enables Channel n-related Interrupts. The user must enable individual Channel n related Interrupts at the source level, before they are can generate an interrupt.
BIT 7
BIT 6
BIT 5
BIT 4
BIT 3
BIT 2
BIT 1
BIT 0
Reserved Reserved
Channel 5 Channel 4 Channel 3 Channel 2 Channel 1 Channel 0 Interrupt Status Interrupt Status Interrupt Status Interrupt Status Interrupt Status Interrupt Status R/O R/O R/O R/O R/O R/O
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
BIT NUMBER 7, 6 5 4 3 2 1 0 NAME Reserved Channel 5 Interrupt Status Channel 4 Interrupt Status Channel 3 Interrupt Status Channel 2 Interrupt Status Channel 1 Interrupt Status Channel 0 Interrupt Status R/O Channel n Interrupt Status Bit: This READ-ONLY bit-field indicates whether the XRT75R12D has a pending Channel n-related interrupt that is awaiting service. The first six channels are serviced through this location and the other six at address 0xE1. These two registers are used by the Host to identify the source channel of an active interrupt. 0 - Indicates that there is NO Channel n-related Interrupt awaiting service. 1 - Indicates that there is at least one Channel n-related Interrupt awaiting service. In this case, the user's Interrupt Service routine should be written such that the Microprocessor will now proceed to read out the contents of the Source Level Interrupt Status Register Channel n (Address Locations = 0xn2) to determine the exact source of the interrupt request. TYPE DESCRIPTION
NOTE: Once this bit-field is set to "1", it will not be cleared back to "0" until the user has read out the contents of the SourceLevel Interrupt Status Register bit, that corresponds to the interrupt request channel.
TABLE 22: The above is: CHANNEL LEVEL INTERRUPT STATUS REGISTER - CR97 (ADDRESS LOCATION = 0X61) TABLE 23: CHANNEL LEVEL INTERRUPT STATUS REGISTER - CR225 (ADDRESS LOCATION = 0XE1)
BIT 7 BIT 6 BIT 5 BIT 4 BIT 3 BIT 2 BIT 1 BIT 0
Reserved Reserved
Channel 11 Channel 10 Channel 9 Channel 8 Channel 7 Channel 6 Interrupt Status Interrupt Status Interrupt Status Interrupt Status Interrupt Status Interrupt Status R/O R/O R/O R/O R/O R/O
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
BIT NUMBER 7, 6 5 4 3 2 1 0
NAME Reserved Channel 11 Interrupt Status Channel 10 Interrupt Status Channel 9 Interrupt Status Channel 8 Interrupt Status Channel 7 Interrupt Status Channel 6 Interrupt Status
TYPE
DESCRIPTION
R/O
Channel n Interrupt Status Bit: This READ-ONLY bit-field indicates whether the XRT75R12D has a pending Channel n-related interrupt that is awaiting service. The last six channels are serviced through this location and the other six at address 0x61. These two registers are used by the Host to identify the source channel of an active interrupt. 0 - Indicates that there is NO Channel n-related Interrupt awaiting service. 1 - Indicates that there is at least one Channel n-related Interrupt awaiting service. In this case, the user's Interrupt Service routine should be written such that the Microprocessor will now proceed to read out the contents of the Source Level Interrupt Status Register Channel n (Address Locations = 0xn2) to determine the exact source of the interrupt request.
NOTE: Once this bit-field is set to "1", it will not be cleared back to "0" until the user has read out the contents of the SourceLevel Interrupt Status Register bit, that corresponds to the interrupt request channel.
TABLE 24: DEVICE/PART NUMBER REGISTER - CR110 (ADDRESS LOCATION = 0X6E)
BIT 7 BIT 6 BIT 5 BIT 4 BIT 3 BIT 2 BIT 1 BIT 0
Part Number ID Value R/O 0 R/O 1 R/O 1 R/O 1 R/O 0 R/O 1 R/O 1 R/O 1
BIT NUMBER 7-0
NAME Part Number ID Value
TYPE R/O
DEFAULT VALUE 0x77
DESCRIPTION Part Number ID Value: This READ-ONLY register contains a unique value for the XRT75R12D. This value will always be 0x77.
TABLE 25: CHIP REVISION NUMBER REGISTER - CR111 (ADDRESS LOCATION = 0X6F)
BIT 7 BIT 6 BIT 5 BIT 4 BIT 3 BIT 2 BIT 1 BIT 0
Chip Revision Number Value R/O 0 R/O 0 R/O 0 R/O 0 R/O X R/O X R/O X R/O X
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
DEFAULT VALUE 0x0#
BIT NUMBER 7-0
NAME Chip Revision Number Value
TYPE R/O
DESCRIPTION Chip Revision Number Value: This READ-ONLY register contains a value that represents the current revision of this XRT75R12D. This revision number will always be in the form of "0x0#", where "#" is a hexadecimal value that specifies the current revision of the chip. For example, the very first revision of this chip will contain the value "0x01".
THE PER-CHANNEL REGISTERS The XRT75R12D consists of 120 per-Channel Registers (12 channels and 10 registers per channel). Table 9 presents the overall Register Map with the Per-Channel Registers unshaded.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
REGISTER DESCRIPTION - PER CHANNEL REGISTERS TABLE 26: XRT75R12D REGISTER MAP SHOWING INTERRUPT ENABLE REGISTERS (IER_N)
ADDRESS LOCATION 0x00X10x20x30x40x50x60x70x80X90xA0xB0xC0xD0xE0xFCIE APST CIE
0
APST
1 IER0 IER1 IER2 IER3 IER4 IER5 CIS
2 ISR0 ISR1 ISR2 ISR3 ISR4 ISR5
3 AS0 AS1 AS2 AS3 AS4 AS5
4 TC0 TC1 TC2 TC3 TC4 TC5
5 RC0 RC1 RC2 RC3 RC4 RC5
6 CC0 CC1 CC2 CC3 CC4 CC5
7 JA0 JA1 JA2 JA3 JA4 JA5
8
APSR
9
A EM0 EM1 EM2 EM3 EM4 EM5
B EL0 EL1 EL2 EL3 EL4 EL5
C EH0 EH1 EH2 EH3 EH4 EH5
DE F
PN VN
IER6 IER7 IER8 IER9 IER10 IER11 CIS
ISR6 ISR7 ISR8 ISR9 ISR10 ISR11
AS6 AS7 AS8 AS9 AS10 AS11
TC6 TC7 TC8 TC9 TC10 TC11
RC6 RC7 RC8 RC9 RC10 RC11
CC6 CC7 CC8 CC9 CC10 CC11
JA6 JA7 JA8 JA9 JA10 JA11
APSR
EM6 EM7 EM8 EM9 EM10 EM11
EL6 EL7 EL8 EL9 EL10 EL11
EH6 EH7 EH8 EH9 EH10 EH11
TABLE 27: SOURCE LEVEL INTERRUPT ENABLE REGISTER - CHANNEL N ADDRESS LOCATION = 0XM1 (m= 0-5 & 8-D)
BIT 7 BIT 6 BIT 5 BIT 4 BIT 3 BIT 2 BIT 1 BIT 0
Reserved
Change of FL Change of LOL Change of LOS Change of Condition Condition Condition DMO Condition Interrupt Enable Interrupt Enable Interrupt Enable Interrupt Enable Ch n Ch n Ch n Ch n R/W R/W R/W R/W
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
BIT NUMBER 7-4 3 NAME Reserved Change of FL Condition Interrupt Enable - Ch n TYPE R/O R/W Change of FL (FIFO Limit Alarm) Condition Interrupt Enable - Ch n: This READ/WRITE bit-field is used to enable or disable the Change of FIFO Limit Alarm Condition Interrupt. If the user enables this interrupt, the XRT75R12D will generate an interrupt if any of the following events occur. DESCRIPTION
* Whenever the Jitter Attenuator (within Channel n) declares the FL
(FIFO Limit Alarm) condition.
* Whenever the Jitter Attenuator (within Channel n) clears the FL
(FIFO Limit Alarm) condition. 0 - Disables the Change in FL Condition Interrupt. 1 - Enables the Change in FL Condition Interrupt. 2 Change of LOL Condition Interrupt Enable R/W Change of Receive LOL (Loss of Lock) Condition Interrupt Enable - Channel n: This READ/WRITE bit-field is used to enable or disable the Change of Receive LOL Condition Interrupt. If the user enables this interrupt, then the XRT75R12D will generate an interrupt any time any of the following events occur.
* Whenever the Receive Section (within Channel n) declares the Loss
of Lock Condition.
* Whenever the Receive Section (within Channel n) clears the Loss of
Lock Condition. 0 - Disables the Change in Receive LOL Condition Interrupt. 1 - Enables the Change in Receive LOL Condition Interrupt. 1 Change of LOS Condition Interrupt Enable R/W Change of the Receive LOS (Loss of Signal) Defect Condition Interrupt Enable - Ch 0: This READ/WRITE bit-field is used to enable or disable the Change of the Receive LOS Defect Condition Interrupt. If the user enables this interrupt, then the XRT75R12D will generate an interrupt any time any of the following events occur.
* Whenever the Receive Section (within Channel n) declares the LOS
Defect Condition.
* Whenever the Receive Section (within Channel n) clears the LOS
Defect condition. 0 - Disables the Change in the LOS Defect Condition Interrupt. 1 - Enables the Change in the LOS Defect Condition Interrupt. 0 Change of DMO Condition Interrupt Enable R/W Change of Transmit DMO (Drive Monitor Output) Condition Interrupt Enable - Ch n: This READ/WRITE bit-field is used to enable or disable the Change of Transmit DMO Condition Interrupt. If the user enables this interrupt, then the XRT75R12D will generate an interrupt any time any of the following events occur.
* Whenever the Transmit Section toggles the DMO output pin (or bitfield) to "1".
* Whenever the Transmit Section toggles the DMO output pin (or bitfield) to "0". 0 - Disables the Change in the DMO Condition Interrupt. 1 - Enables the Change in the DMO Condition Interrupt.
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TABLE 28: XRT75R12D REGISTER MAP SHOWING INTERRUPT STATUS REGISTERS (ISR_N) TABLE 29: SOURCE LEVEL INTERRUPT STATUS REGISTER - CHANNEL N ADDRESS LOCATION = 0XM2
BIT 7 BIT 6 BIT 5 BIT 4 BIT 3 BIT 2 BIT 1 BIT 0
Reserved
Change of FL Change of LOL Change of LOS Change of DMO Condition Condition Condition Condition Interrupt Status Interrupt Status nterrupt Status Interrupt Status Ch_n Ch_n Ch_n Ch_n RUR RUR RUR RUR
BIT NUMBER 7-4 3
NAME Reserved Change of FL Condition Interrupt Status
TYPE
DESCRIPTION
RUR
Change of FL (FIFO Limit Alarm) Condition Interrupt Status - Ch n: This RESET-upon-READ bit-field indicates whether or not the Change of FL Condition Interrupt (for Channel n) has occurred since the last read of this register. 0 - Indicates that the Change of FL Condition Interrupt has NOT occurred since the last read of this register. 1 - Indicates that the Change of FL Condition Interrupt has occurred since the last read of this register.
NOTE: The user can determine the current state of the FIFO Alarm condition by reading out the contents of Bit 3 (FL Alarm Declared) within the Alarm Status Register.(n)
2 Change of LOL Condition Interrupt Status RUR Change of Receive LOL (Loss of Lock) Condition Interrupt Status - Ch n: This RESET-upon-READ bit-field indicates whether or not the Change of Receive LOL Condition Interrupt (for Channel n) has occurred since the last read of this register. 0 - Indicates that the Change of Receive LOL Condition Interrupt has NOT occurred since the last read of this register. 1 - Indicates that the Change of Receive LOL Condition Interrupt has occurred since the last read of this register.
NOTE: The user can determine the current state of the Receive LOL Defect condition by reading out the contents of Bit 2 (Receive LOL Defect Declared) within the Alarm Status Register.(n)
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BIT NUMBER 1 NAME Change of LOS Condition Interrupt Status TYPE RUR DESCRIPTION Change of Receive LOS (Loss of Signal) Defect Condition Interrupt Status: This RESET-upon-READ bit-field indicates whether or not the Change of the Receive LOS Defect Condition Interrupt (for Channel n) has occurred since the last read of this register. 0 - Indicates that the Change of the Receive LOS Defect Condition Interrupt has NOT occurred since the last read of this register. 1 - Indicates that the Change of the Receive LOS Defect Condition Interrupt has occurred since the last read of this register.
NOTE: The user can determine the current state of the Receive LOS Defect condition by reading out the contents of Bit 1 (Receive LOS Defect Declared) within the Alarm Status Register.(n)
0 Change of DMO Condition Interrupt Status RUR Change of Transmit DMO (Drive Monitor Output) Condition Interrupt Status - Ch n: This RESET-upon-READ bit-field indicates whether or not the Change of the Transmit DMO Condition Interrupt (for Channel n) has occurred since the last read of this register. 0 - Indicates that the Change of the Transmit DMO Condition Interrupt has NOT occurred since the last read of this register. 1 - Indicates that the Change of the Transmit DMO Condition Interrupt has occurred since the last read of this register.
NOTE: The user can determine the current state of the Transmit DMO Condition by reading out the contents of Bit 0 (Transmit DMO Condition) within the Alarm Status Register.(n)
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TABLE 30: XRT75R12D REGISTER MAP SHOWING ALARM STATUS REGISTERS (AS_N) TABLE 31: ALARM STATUS REGISTER - CHANNEL N ADDRESS LOCATION = 0XM3
BIT 7 Reserved
BIT 6 Loss of PRBS Pattern Sync
BIT 5 Digital LOS Defect Declared
BIT 4 Analog LOS Defect Declared
BIT 3 FL (FIFO Limit) Alarm Declared R/O
BIT 2
BIT 1
BIT 0 Transmit DMO Condition
Receive LOL Receive LOS Defect Defect Declared Declared
R/O
R/O
R/O
R/O
R/O
R/O
BIT NUMBER 7 6
NAME Reserved Loss of PRBS Pattern Lock
TYPE
DESCRIPTION
R/O
Loss of PRBS Pattern Lock Indicator: This READ-ONLY bit-field indicates whether or not the PRBS Receiver (within the Receive Section of Channel n) is declaring PRBS Lock within the incoming PRBS pattern. If the PRBS Receiver detects a very large number of bit-errors within its incoming data-stream, then it will declare the Loss of PRBS Lock Condition. Conversely, if the PRBS Receiver were to detect its pre-determined PRBS pattern with the incoming DS3, E3 or STS-1 data-stream, (with little or no bit errors) then the PRBS Receiver will clear the Loss of PRBS Lock condition. 0 - Indicates that the PRBS Receiver is currently declaring the PRBS Lock condition within the incoming DS3, E3 or STS-1 data-stream. 1 - Indicates that the PRBS Receiver is currently declaring the Loss of PRBS Lock condition within the incoming DS3, E3 or STs-1 datastream.
NOTE: This register bit is only valid if all of the following are true.
a. The PRBS Generator block (within the Transmit Section of the Chip is enabled). b. The PRBS Receiver is enabled. c. The PRBS Pattern (that is generated by the PRBS Generator) is somehow looped back into the Receive Path (via the Line-Side) and in-turn routed to the receive input of the PRBS Receiver.
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BIT NUMBER 5 NAME Digital LOS Defect Declared TYPE R/O DESCRIPTION Digital LOS Defect Declared: This READ-ONLY bit-field indicates whether or not the Digital LOS (Loss of Signal) detector is declaring the LOS Defect condition. For DS3 and STS-1 applications, the Digital LOS Detector will declare the LOS Defect condition whenever it detects an absence of pulses (within the incoming DS3 or STS-1 data-stream) for 160 consecutive bit-periods. Further, (again for DS3 and STS-1 applications) the Digital LOS Detector will clear the LOS Defect condition whenever it determines that the pulse density (within the incoming DS3 or STS-1 signal) is at least 33%. 0 - Indicates that the Digital LOS Detector is NOT declaring the LOS Defect Condition. 1 - Indicates that the Digital LOS Detector is currently declaring the LOS Defect condition.
NOTES: 1. LOS Detection (within each channel of the XRT75R12D) is performed by both an Analog LOS Detector and a Digital LOS Detector. The LOS state of a given Channel is simply a WIRED-OR of the LOS Defect Declare states of these two detectors. 2. The current LOS Defect Condition (for the channel) can be determined by reading out the contents of Bit 1 (Receive LOS Defect Declared) within this register.
4 Analog LOS Defect Declared R/O Analog LOS Defect Declared: This READ-ONLY bit-field indicates whether or not the Analog LOS (Loss of Signal) detector is declaring the LOS Defect condition. For DS3 and STS-1 applications, the Analog LOS Detector will declare the LOS Defect condition whenever it determines that the amplitude of the pulses (within the incoming DS3/STS-1 line signal) drops below a certain Analog LOS Defect Declaration threshold level. Conversely, (again for DS3 and STS-1 applications) the Analog LOS Detector will clear the LOS Defect condition whenever it determines that the amplitude of the pulses (within the incoming DS3/STS-1 line signal) has risen above a certain Analog LOS Defect Clearance threshold level. It should be noted that, in order to prevent "chattering" within the Analog LOS Detector output, there is some built-in hysteresis between the Analog LOS Defect Declaration and the Analog LOS Defect Clearance threshold levels. 0 - Indicates that the Analog LOS Detector is NOT declaring the LOS Defect Condition. 1 - Indicates that the Analog LOS Detector is currently declaring the LOS Defect condition.
NOTES: 1. LOS Detection (within each channel of the XRT75R12D) is performed by both an Analog LOS Detector and a Digital LOS Detector. The LOS state of a given Channel is simply a WIRED-OR of the LOS Defect Declare states of these two detectors. 2. The current LOS Defect Condition (for the channel) can be determined by reading out the contents of Bit 1 (Receive LOS Defect Declared) within this register.
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BIT NUMBER 3 NAME FL Alarm Declared TYPE R/O DESCRIPTION FL (FIFO Limit) Alarm Declared: This READ-ONLY bit-field indicates whether or not the Jitter Attenuator block (within Channel_n) is currently declaring the FIFO Limit Alarm. The Jitter Attenuator block will declare the FIFO Limit Alarm anytime the Jitter Attenuator FIFO comes within two bit-periods of either overflowing or under-running. Conversely, the Jitter Attenuator block will clear the FIFO Limit Alarm anytime the Jitter Attenuator FIFO is NO longer within two bit-periods of either overflowing or under-running. Typically, this Alarm will only be declared whenever there is a very serious problem with timing or jitter in the system. 0 - Indicates that the Jitter Attenuator block (within Channel_n) is NOT currently declaring the FIFO Limit Alarm condition. 1 - Indicates that the Jitter Attenuator block (within Channel_n) is currently declaring the FIFO Limit Alarm condition.
NOTE:
2 Receive LOL Condition Declared R/O
This bit-field is only active if the Jitter Attenuator (within Channel_n) has been enabled.
Receive LOL (Loss of Lock) Condition Declared: This READ-ONLY bit-field indicates whether or not the Receive Section (within Channel_n) is currently declaring the LOL (Loss of Lock) condition. The Receive Section (of Channel_n) will declare the LOL Condition, if the frequency of the Recovered Clock signal differs from that of the reference clock programmed for that channel (from the appropriate oscillator or the SFM clock synthesizer if in that mode) by 0.5% (or 5000ppm) or more . 0 - Indicates that the Receive Section of Channel_n is NOT currently declaring the LOL Condition. 1 - Indicates that the Receive Section of Channel_n is currently declaring the LOL Condition and the recovered clock differs by more than 0.5%..
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BIT NUMBER 1 NAME Receive LOS Defect Condition Declared TYPE R/O DESCRIPTION Receive LOS (Loss of Signal) Defect Condition Declared: This READ-ONLY bit-field indicates whether or not the Receive Section (within Channel_n) is currently declaring the LOS defect condition. The Receive Section (of Channel_n) will declare the LOS defect condition, if any one of the following conditions is met.
* If the Digital LOS Detector declares the LOS defect condition (for
DS3 or STS-1 applications)
* If the Analog LOS Detector declares the LOS defect condition (for
DS3 or STS-1 applications)
* If the ITU-T G.775 LOS Detector declares the LOS defect condition
(for E3 applications). 0 - Indicates that the Receive Section of Channel_n is NOT currently declaring the LOS Defect Condition. 1 - Indicates that the Receive Section of Channel_n is currently declaring the LOS Defect condition. 0 Transmit DMO Condition Declared R/O Transmit DMO (Drive Monitor Output) Condition Declared: This READ-ONLY bit-field indicates whether or not the Transmit Section of Channel_n is currently declaring the DMO Alarm condition. As configured, the Transmit Section will either internally (via the TTIP_n and TRING_n ) or externally (via the MTIP_n and MRING_n) check the Transmit Output DS3/E3/STS-1 Line signal for bipolar pulses. If the Transmit Section were to detect no bipolar for 128 consecutive bit-periods, then it will declare the Transmit DMO Alarm condition. This particular alarm can be used to check for fault conditions on the Transmit Output Line Signal path. The Transmit Section will clear the Transmit DMO Alarm condition upon detecting bipolar activity on the Transmit Output Line signal. 0 - Indicates that the Transmit Section of Channel_n is NOT currently declaring the Transmit DMO Alarm condition. 1 - Indicates that the Transmit Section of Channel_n is currently declaring the Transmit DMO Alarm condition.
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TABLE 32: XRT75R12D REGISTER MAP SHOWING TRANSMIT CONTROL REGISTERS (TC_N) TABLE 33: TRANSMIT CONTROL REGISTER - CHANNEL N ADDRESS LOCATION = 0XM4
BIT 7 Reserved BIT 6 BIT 5 Internal Transmit Drive Monitor R/W BIT 4 Insert PRBS Error BIT 3 Reserved BIT 2 TAOS BIT 1 TxCLKINV BIT 0 TxLEV
R/W
R/W
R/W
R/W
BIT NUMBER 7-6 5
NAME Reserved Internal Transmit Drive Monitor Enable
TYPE
DESCRIPTION
R/W
Internal Transmit Drive Monitor Enable - Channel_n: This READ/WRITE bit-field is used to configure the Transmit Section of Channel_n to either internally or externally monitor the TTIP_n and TRING_n output pins for bipolar pulses, in order to determine whether to declare the Transmit DMO Alarm condition. If the user configures the Transmit Section to externally monitor the TTIP_n and TRING_n output pins (for bipolar pulses) then the user must connect the MTIP_n and MRING_n input pins to their corresponding TTIP_n and TRING_n output pins (via a 270 ohm series resistor). If the user configures the Transmit Section to internally monitor the TTIP_n and TRING_n output pins (for bipolar pulses), the user does NOT need to conect the MTIP_n and MRING_n input pins. This monitoring will be performed internally at the TTIP_n and TRING_n pads. 0 - Configures the Transmit Drive Monitor to externally monitor the TTIP_n and TRING_n output pins for bipolar pulses. 1 - Configures the Transmit Drive Monitor to internally monitor the TTIP_n and TRING_n output pins for bipolar pulses. Insert PRBS Error - Channel_n: A "0 to 1" transition within this bit-field causes the PRBS Generator (within the Transmit Section of Channel_n) to generate a single bit error within the outbound PRBS pattern-stream.
4
Insert PRBS Error
R/W
NOTES: 1. This bit-field is only active if the PRBS Generator and Receiver have been enabled within the corresponding Channel. 2. After writing the "1" into this register, the user must execute a write operation to clear this particular register bit to "0" in order to facilitate the next "0 to 1" transition in this bit-field.
3 Reserved
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
BIT NUMBER 2 NAME TAOS TYPE R/W DESCRIPTION Transmit All OneS Pattern - Channel_n: This READ/WRITE bit-field is used to command the Transmit Section of Channel_n to generate and transmit an unframed, All Ones pattern via the DS3, E3 or STS-1 line signal (to the remote terminal equipment). Whenever the user implements this configuration setting, the Transmit Section will ignore the data that it is accepting from the System-side equipment and output the "All Ones" Pattern. 0 - Configures the Transmit Section to transmit the data that it accepts from the System-side Interface. 1 - Configures the Transmit Section to generate and transmit the Unframed, All Ones pattern. Transmit Clock Invert Select - Channel_n: This READ/WRITE bit-field is used to select the edge of the TxCLK_n input that the Transmit Section of Channel_n will use to sample the TxPOS_n and TxNEG_n input pins, as described below. 0 - Configures the Transmit Section (within the corresponding channel) to sample the TxPOS_n and TxNEG_n input pins upon the falling edge of TxCLK_n. 1 - Configures the Transmit Section (within the corresponding channel) to sample the TxPOS_n and TxNEG_n input pins upon the rising edge of TxCLK_n.
1
TxCLKINV
R/W
NOTE: This is done on a per-channel basis.
0 TxLEV R/W Transmit Line Build-Out Select - Channel_n: This READ/WRITE bit-field is used to enable or disable the Transmit Line Build-Out (e.g., pulse-shaping) circuit within the corresponding channel. The user should set this bit-field to either "0" or to "1" based upon the following guidelines. 0 - If the cable length between the Transmit Output (of the corresponding Channel) and the DSX-3/STSX-1 location is 225 feet or less. 1 - If the cable length between the Transmit Output (of the corresponding Channel) and the DSX-3/STSX-1 location is more than 225 feet . The user must follow these guidelines in order to insure that the Transmit Section (of Channel_n) will always generate a DS3 pulse that complies with the Isolated Pulse Template requirements per Bellcore GR499-CORE, or an STS-1 pulse that complies with the Pulse Template requirements per Telcordia GR-253-CORE.
NOTE: This bit-field is ignored if the channel has been configured to operate in the E3 Mode.
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TABLE 34: XRT75R12D REGISTER MAP SHOWING RECEIVE CONTROL REGISTERS (RC_N) TABLE 35: RECEIVE CONTROL REGISTER - CHANNEL N ADDRESS LOCATION = 0XM5
BIT 7 Reserved
BIT 6
BIT 5
BIT 4
BIT 3 RxCLKINV
BIT 2 LOSMUT Enable
BIT 1 Receive Monitor Mode Enable R/W
BIT 0 Receive Equalizer Enable R/W
Disable DLOS Disable ALOS Detector Detector
R/W
R/W
R/W
R/W
BIT NUMBER 7-6 5
NAME Reserved Disable DLOS Detector
TYPE
DESCRIPTION
R/W
Disable Digital LOS Detector - Channel_n: This READ/WRITE bit-field is used to enable or disable the Digital LOS (Loss of Signal) Detector within Channel_n, as described below. 0 - Enables the Digital LOS Detector within Channel_n. 1 - Disables the Digital LOS Detector within Channel_n.
NOTE: This bit-field is only active if Channel_n has been configured to operate in the DS3 or STS-1 Modes.
4 Disable ALOS Detector R/W Disable Analog LOS Detector - Channel_n: This READ/WRITE bit-field is used to either enable or disable the Analog LOS (Loss of Signal) Detector within Channel_n, as described below. 0 - Enables the Analog LOS Detector within Channel_n. 1 - Disables the Analog LOS Detector within Channel_n.
NOTE: This bit-field is only active if Channel_n has been configured to operate in the DS3 or STS-1 Modes.
3 RxCLKINV R/W Receive Clock Invert Select - Channel_n: This READ/WRITE bit-field is used to select the edge of the RxCLK_n output that the Receive Section of Channel_n will use to output the recovered data via the RxPOS_n and RxNEG_n output pins, as described below. 0 - Configures the Receive Section (within the corresponding channel) to output the recovered data via the RxPOS_n and RxNEG_n output pins upon the rising edge of RCLK_n. 1 - Configures the Receive Section (within the corresponding channel) to output the recovered data via the RxPOS_n and RxNEG_n output pins upon the falling edge of RCLK_n.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
BIT NUMBER 2 NAME LOSMUT Enable TYPE R/W DESCRIPTION Muting upon LOS Enable - Channel_n: This READ/WRITE bit-field is used to configure the Receive Section (within Channel_n) to automatically pull their corresponding Recovered Data Output pins (e.g., RxPOS_n and RxNEG_n) to GND for the duration that the Receive Section declares the LOS defect condition. In other words, this feature (if enabled) will cause the Receive Channel to automatically mute the Recovered data anytime the Receive Section declares the LOS defect condition. 0 - Disables the Muting upon LOS feature. In this setting the Receive Section will NOT automatically mute the Recovered Data whenever it is declaring the LOS defect condition. 1 - Enables the Muting upon LOS feature. In this setting the Receive Section will automatically mute the Recovered Data whenever it is declaring the LOS defect condition. Receive Monitor Mode Enable - Channel_n: This READ/WRITE bit-field is used to configure the Receive Section of Channel_n to operate in the Receive Monitor Mode. If the user configures the Receive Section to operate in the Receive Monitor Mode, then it will be able to receive a nominal DSX-3/STSX-1 signal that has been attenuator by 20dB of flat loss along with 6dB of cable loss, in an error-free manner, and without declaring the LOS defect condition. 0 - Configures the corresponding channel to operate in the Normal Mode. 1 - Configure the corresponding channel to operate in the Receive Monitor Mode. Receive Equalizer Enable - Channel_n: This READ/WRITE register bit is used to enable or disable the Receive Equalizer block within the Receive Section of Channel_n, as listed below. 0 - Disables the Receive Equalizer within the corresponding channel. 1 - Enables the Receive Equalizer within the corresponding channel.
1
Receive Monitor Mode Enable
R/W
0
Receive Equalizer Enable
R/W
NOTE: For virtually all applications, we recommend that the user set this bit-field to "1" (for all channels) and enable the Receive Equalizer.
TABLE 36: XRT75R12D REGISTER MAP SHOWING CHANNEL CONTROL REGISTERS (CC_N) TABLE 37: CHANNEL CONTROL REGISTER - CHANNEL N ADDRESS LOCATION = 0XM6
BIT 7 Reserved
BIT 6
BIT 5 PRBS Enable Ch_n R/W
BIT 4 RLB_n
BIT 3 LLB_n
BIT 2 E3_n
BIT 1 STS-1/DS3_n
BIT 0 SR/DR_n
R/W
R/W
R/W
R/W
R/W
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BIT NUMBER 7-6 5 NAME Reserved PRBS Enable R/W PRBS Generator and Receiver Enable - Channel_n: This READ/WRITE bit-field is used to enable or disable the PRBS Generator and Receiver within a given Channel of the XRT75R12D. If the user enables the PRBS Generator and Receiver, then the following will happen. 1. The PRBS Generator (which resides within the Transmit Section of the Channel) will begin to generate an unframed, 2^15-1 PRBS Pattern (for DS3 and STS-1 applications) and an unframed, 2^23-1 PRBS Pattern (for E3 applications). 2. The PRBS Receiver (which resides within the Receive Section of the Channel) will now be enabled and will begin to search the incoming data for the above-mentioned PRBS patterns. 0 - Disables both the PRBS Generator and PRBS Receiver within the corresponding channel. 1 - Enables both the PRBS Generator and PRBS Receiver within the corresponding channel. TYPE DESCRIPTION
NOTES: 1. To check and monitor PRBS Bit Errors, DR (Dual Rail) mode will be over-ridden and Single Rail mode forced for the duration of this mode. This will configure the RNEG/LCV_n output pin to function as a PRBS Error Indicator. All errors will be flagged on this pin. The errors will also be accumulated in the 16 bit Error counter for the channel. 2. If the user enables the PRBS Generator and PRBS Receiver, the Channel will ignore the data that is being accepted from the System-side Equipment (via the TxPOS_n and TxNEG_n input pins) and will overwrite this outbound data with the PRBS Pattern. 3. The system must provide an accurate and stable data-rate clock to the TxClk_n pin during this operation.
4 RLB_n R/W Loop-Back Select - RLB Bit - Channel_n: This READ/WRITE bit-field along with the corresponding LLB_n bitfield is used to configure a given channel into various loop-back modes ass shown by the following table.
LLB_n 0 0 1 1
RLB_n 0 1 0 1
Loop-back M ode Norm al (No Loop-back) Mode Rem ote Loop-back Mode Analog Local Loop-back Mode Digital Local Loop-back Mode
3
LLB_n
R/W
Loop-Back Select - LLB Bit-field - Channel_n: See the table (above) for RLB_n.
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BIT NUMBER 2 NAME E3_n TYPE R/W DESCRIPTION E3 Mode Select - Channel_n: This READ/WRITE bit-field, along with Bit 1 (STS-1/DS3_n) within this register, is used to configure a given channel into either the DS3, E3 or STS-1 Modes. 0 - Configures Channel_n to operate in either the DS3 or STS-1 Modes, depending upon the state of Bit 1 (STS-1/DS3_n) within this same register. 1- Configures Channel_n to operate in the E3 Mode. STS-1/DS3 Mode Select - Channel_n: This READ/WRITE bit-field, along with Bit 2 (E3_n) is used to configure a given channel into either the DS3, E3 or STS-1 Modes. This bit-field is ignored if Bit 2 (E3_n) has been set to "1". If Bit 2 (E3_n) is a 0: 0 - Configures Channel_n to operate in the DS3 Mode. 1 - Configures Channel_n to operate in the STS-1 Mode . Single-Rail/Dual-Rail Select - Channel_n: This READ/WRITE bit-field is used to configure Channel_n to operate in either the Single-Rail or Dual-Rail Mode. If the user configures the Channel to operate in the Single-Rail Mode, the following will happen.
1
STS-1/DS3_n
R/W
0
SR/DR_n
R/W
* The B3ZS/HDB3 Encoder and Decoder blocks (within Channel_n)
will be enabled.
* The Transmit Section of Channel_n will accept all of the outbound
data (from the System-side Equipment) via the TxPOS_n input pin.
* The Receive Section of each channel will output all of the recovered
data (to the System-side Equipment) via the RxPOS_n output pin.
* The corresponding RNEG/LCV_n output pin will now function as the
LCV (Line Code Violation or Excessive Zero Event) indicator output pin for Channel_n. If the user configures Channel_n to operate in the Dual-Rail Mode, the following will happen.
* The B3ZS/HDB3 Encoder and Decoder blocks of Channel_n will be
disabled.
* The Transmit Section of Channel_n will be configured to accept
positive-polarity data via the TxPOS_n input pin and negativepolarity data via the TxNEG_n input pin.
* The Receive Section of Channel_n will pulse the RxPOS_n output
pin "High" (for one period of RCLK_n) for each time a positivepolarity pulse is received via the RTIP_n/RRING_n input pins. Likewise, the Receive Section of each channel will pulse the RxNEG_n output pin "High" (for one period of RxCLK_n) for each time a negative-polarity pulse is received via the RTIP_n/RRING_n input pins. 0 - Configures Channel_n to operate in the Dual-Rail Mode. 1 - Configures Channel_n to operate in the Single-Rail Mode.
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TABLE 38: XRT75R12D REGISTER MAP SHOWING JITTER ATTENUATOR CONTROL REGISTERS (JA_N)
TABLE 39: JITTER ATTENUATOR CONTROL REGISTER - CHANNEL N ADDRESS LOCATION = 0XM7
BIT 7 BIT 6 Reserved BIT 5 BIT 4 BIT 3 JA RESET Ch_n R/W BIT 2 JA1 Ch_n BIT 1 JA in Tx Path Ch_n R/W BIT 0 JA0 Ch_n
R/W
R/W
BIT NUMBER 7-4 3
NAME Reserved JA RESET Ch_n
TYPE
DESCRIPTION
R/W
Jitter Attenuator RESET - Channel_n: Writing a "0 to 1" transition within this bit-field will configure the Jitter Attenuator (within Channel_n) to execute a RESET operation. Whenever the user executes a RESET operation, then following will occur.
* The READ and WRITE pointers (within the Jitter Attenuator FIFO)
will be reset to their default values.
* The contents of the Jitter Attenuator FIFO will be flushed.
NOTE: The user must follow up any "0 to 1" transition with the appropriate write operate to set this bit-field back to "0", in order to resume normal operation with the Jitter Attenuator.
2
JA1 Ch_n
R/W
Jitter Attenuator Configuration Select Input - Bit 1: This READ/WRITE bit-field, along with Bit 0 (JA0 Ch_n) is used to do any of the following.
* To enable or disable the Jitter Attenuator corresponding to
Channel_n.
* To select the FIFO Depth for the Jitter Attenuator within Channel_n.
The relationship between the settings of these two bit-fields and the Enable/Disable States, and FIFO Depths is presented below.
JA0 0 0 1 1
JA1 0 1 0 1
Jitter Attenuator M ode FIFO Depth = 16 bits FIFO Depth = 32 bits Disabled Disabled
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BIT NUMBER 1 NAME JA in Tx Path Ch_n TYPE R/W DESCRIPTION Jitter Attenuator in Transmit/Receive Path Select Bit: This input pin is used to configure the Jitter Attenuator (within Channel_n) to operate in either the Transmit or Receive path, as described below. 0 - Configures the Jitter Attenuator (within Channel_n) to operate in the Receive Path. 1 - Configures the Jitter Attenuator (within Channel_n) to operate in the Transmit Path. Jitter Attenuator Configuration Select Input - Bit 0: See the description for Bit 2 (JA1 Ch_n).
0
JA0 Ch_n
R/W
TABLE 40: XRT75R12D REGISTER MAP SHOWING ERROR COUNTER MSBYTE REGISTERS (EM_N)
ADDRESS LOCATION 0x00X10x20x30x40x50x60x70x80X90xA0xB0xC0xD0xE0xFCIE APST CIE
0
APST
1 IER0 IER1 IER2 IER3 IER4 IER5 CIS
2 ISR0 ISR1 ISR2 ISR3 ISR4 ISR5
3 AS0 AS1 AS2 AS3 AS4 AS5
4 TC0 TC1 TC2 TC3 TC4 TC5
5 RC0 RC1 RC2 RC3 RC4 RC5
6 CC0 CC1 CC2 CC3 CC4 CC5
7 JA0 JA1 JA2 JA3 JA4 JA5
8
APSR
9
A EM0 EM1 EM2 EM3 EM4 EM5
B EL0 EL1 EL2 EL3 EL4 EL5
C EH0 EH1 EH2 EH3 EH4 EH5
DE F
PN VN
IER6 IER7 IER8 IER9 IER10 IER11 CIS
ISR6 ISR7 ISR8 ISR9 ISR10 ISR11
AS6 AS7 AS8 AS9 AS10 AS11
TC6 TC7 TC8 TC9 TC10 TC11
RC6 RC7 RC8 RC9 RC10 RC11
CC6 CC7 CC8 CC9 CC10 CC11
JA6 JA7 JA8 JA9 JA10 JA11
APSR
EM6 EM7 EM8 EM9 EM10 EM11
EL6 EL7 EL8 EL9 EL10 EL11
EH6 EH7 EH8 EH9 EH10 EH11
TABLE 41: ERROR COUNTER MSBYTE REGISTER - CHANNEL N ADDRESS LOCATION = 0XMA
BIT 7 Msb R/W R/W R/W R/W R/W R/W R/W BIT 6 BIT 5 BIT 4 BIT 3 BIT 2 BIT 1 BIT 0 9th bit R/W
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
TABLE 42: XRT75R12D REGISTER MAP SHOWING ERROR COUNTER LSBYTE REGISTERS (EL_N)
ADDRESS LOCATION 0x00X10x20x30x40x50x60x70x80X90xA0xB0xC0xD0xE0xFCIE APST CIE
0
APST
1 IER0 IER1 IER2 IER3 IER4 IER5 CIS
2 ISR0 ISR1 ISR2 ISR3 ISR4 ISR5
3 AS0 AS1 AS2 AS3 AS4 AS5
4 TC0 TC1 TC2 TC3 TC4 TC5
5 RC0 RC1 RC2 RC3 RC4 RC5
6 CC0 CC1 CC2 CC3 CC4 CC5
7 JA0 JA1 JA2 JA3 JA4 JA5
8
APSR
9
A EM0 EM1 EM2 EM3 EM4 EM5
B EL0 EL1 EL2 EL3 EL4 EL5
C EH0 EH1 EH2 EH3 EH4 EH5
DE F
PN VN
IER6 IER7 IER8 IER9 IER10 IER11 CIS
ISR6 ISR7 ISR8 ISR9 ISR10 ISR11
AS6 AS7 AS8 AS9 AS10 AS11
TC6 TC7 TC8 TC9 TC10 TC11
RC6 RC7 RC8 RC9 RC10 RC11
CC6 CC7 CC8 CC9 CC10 CC11
JA6 JA7 JA8 JA9 JA10 JA11
APSR
EM6 EM7 EM8 EM9 EM10 EM11
EL6 EL7 EL8 EL9 EL10 EL11
EH6 EH7 EH8 EH9 EH10 EH11
TABLE 43: ERROR COUNTER LSBYTE REGISTER - CHANNEL N ADDRESS LOCATION = 0XMB
BIT 7 8th bit R/W R/W R/W R/W R/W R/W R/W BIT 6 BIT 5 BIT 4 BIT 3 BIT 2 BIT 1 BIT 0 Ls bit R/W
TABLE 44: XRT75R12D REGISTER MAP SHOWING ERROR COUNTER HOLDING REGISTERS (EH_N)
ADDRESS LOCATION 0x00X10x20x30x40x50x6CIE
0
APST
1 IER0 IER1 IER2 IER3 IER4 IER5 CIS
2 ISR0 ISR1 ISR2 ISR3 ISR4 ISR5
3 AS0 AS1 AS2 AS3 AS4 AS5
4 TC0 TC1 TC2 TC3 TC4 TC5
5 RC0 RC1 RC2 RC3 RC4 RC5
6 CC0 CC1 CC2 CC3 CC4 CC5
7 JA0 JA1 JA2 JA3 JA4 JA5
8
APSR
9
A EM0 EM1 EM2 EM3 EM4 EM5
B EL0 EL1 EL2 EL3 EL4 EL5
C EH0 EH1 EH2 EH3 EH4 EH5
DE F
PN VN
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
ADDRESS LOCATION 0x70x80X90xA0xB0xC0xD0xE0xFCIE APST
0
1
2
3
4
5
6
7
8
9
A
B
C
DE F
IER6 IER7 IER8 IER9 IER10 IER11 CIS
ISR6 ISR7 ISR8 ISR9 ISR10 ISR11
AS6 AS7 AS8 AS9 AS10 AS11
TC6 TC7 TC8 TC9 TC10 TC11
RC6 RC7 RC8 RC9 RC10 RC11
CC6 CC7 CC8 CC9 CC10 CC11
JA6 JA7 JA8 JA9 JA10 JA11
APSR
EM6 EM7 EM8 EM9 EM10 EM11
EL6 EL7 EL8 EL9 EL10 EL11
EH6 EH7 EH8 EH9 EH10 EH11
TABLE 45: ERROR COUNTER HOLDING REGISTER - CHANNEL N ADDRESS LOCATION = 0XMC
BIT 7 Msb R/W R/W R/W R/W R/W R/W R/W BIT 6 BIT 5 BIT 4 BIT 3 BIT 2 BIT 1 BIT 0 Ls bit R/W
Each channel contains a dedicated 16 bit PRBS error counter. When enabled this counter will accumulate PRBS errors (as well as excess zeros and LCVs). The LS byte will "carry" a one over to the MS byte each time it rolls over from 255 to zero until the MS byte also reaches 255. When both counters reach 255, no further errors will be accumulated and "all ones" will signify an overflow condition. The counter can be read while in the active count mode. Either register may be read "on the fly" and the other byte will be simultaneously transferred into the channel's Error Holding register. The holding register may then be read to supply the Host with a correct 16 bit count (as of the instant of reading). With this mechanism, the Host could rapidly cycle thru reading all twelve counters in order (storing the read byte in scratch RAM) and then come back and read the second byte from each holding register to form the 16 bit accumulation in the Host system.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
84
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 8.0 THE SONET/SDH DE-SYNC FUNCTION WITHIN THE LIU The LIU with D-SYNC is very similar to the non D-SYNC LIU in that they both contain Jitter Attenuator blocks within each channel. They are also pin to pin compatible with each other. However, the Jitter Attenuators within the D-SYNC have some enhancements over and above those within the non D-SYNC device. The Jitter Attenuator blocks will support all of the modes and features that exist in the non D-SYNC device and in addition they also support a SONET/SDH De-Sync Mode.
NOTE: The "D" suffix within the part number stands for "De-Sync".
The SONET/SDH De-Sync feature of the Jitter Attenuator blocks permits the user to design a SONET/SDH PTE (Path Terminating Equipment) that will comply with all of the following Intrinsic Jitter and Wander requirements.
* For SONET Applications
s s
Category I Intrinsic Jitter Requirements per Telcordia GR-253-CORE (for DS3 Applications) ANSI T1.105.03b-1997 - SONET Jitter at Network Interfaces - DS3 Wander Supplement Jitter and Wander Generation Requirements per ITU-T G.783 (for DS3 and E3 Applications)
* For SDH Applications
s
Specifically, if the user designs in the LIU along with a SONET/SDH Mapper IC (which can be realized as either a standard product or as a custom logic solution, in an ASIC or FPGA), then the following can be accomplished.
* The Mapper can receive an STS-N or an STM-M signal (which is carrying asynchronously-mapped DS3 and/
or E3 signals) and byte de-interleave this data into N STS-1 or 3*M VC-3 signals
* The Mapper will then terminate these STS-1 or VC-3 signals and will de-map out this DS3 or E3 data from
the incoming STS-1 SPEs or VC-3s, and output this DS3 or E3 to the DS3/E3 Facility-side towards the LIU
* This DS3 or E3 signal (as it is output from these Mapper devices) will contain a large amount of intrinsic jitter
and wander due to (1) the process of asynchronously mapping a DS3 or E3 signal into a SONET or SDH signal, (2) the occurrence of Pointer Adjustments within the SONET or SDH signal (transporting these DS3 or E3 signals) as it traverses the SONET/SDH network, and (3) clock gapping.
* When the LIU has been configured to operate in the "SONET/SDH De-Sync" Mode, then it will (1) accept this
jittery DS3 or E3 clock and data signal from the Mapper device (via the Transmit System-side interface) and (2) through the Jitter Attenuator, the LIU will reduce the Jitter and Wander amplitude within these DS3 or E3 signals such that they (when output onto the line) will comply with the above-mentioned intrinsic jitter and wander specifications. 8.1
BACKGROUND AND DETAILED INFORMATION - SONET DE-SYNC APPLICATIONS
This section provides an in-depth discussion on the mechanisms that will cause Jitter and Wander within a DS3 or E3 signal that is being transported across a SONET or SDH Network. A lot of this material is introductory, and can be skipped by the engineer that is already experienced in SONET/SDH designs. In the wide-area network (WAN) in North America it is often necessary to transport a DS3 signal over a long distance (perhaps over a thousand miles) in order to support a particular service. Now rather than realizing this transport of DS3 data, by using over a thousand miles of coaxial cable (interspaced by a large number of DS3 repeaters) a common thing to do is to route this DS3 signal to a piece of equipment (such as a Terminal MUX, which in the "SONET Community" is known as a PTE or Path Terminating Equipment). This Terminal MUX will asynchronously map the DS3 signal into a SONET signal. At this point, the SONET network will now transport this asynchronously mapped DS3 signal from one PTE to another PTE (which is located at the other end of the SONET network). Once this SONET signal arrives at the remote PTE, this DS3 signal will then be extracted from the SONET signal, and will be output to some other DS3 Terminal Equipment for further processing. Similar things are done outside of North America. In this case, this DS3 or E3 signal is routed to a PTE, where it is asynchronously mapped into an SDH signal. This asynchronously mapped DS3 or E3 signal is then transported across the SDH network (from one PTE to the PTE at the other end of the SDH network). Once
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
this SDH signal arrives at the remote PTE, this DS3 or E3 signal will then be extracted from the SDH signal, and will be output to some other DS3/E3 Terminal Equipment for further processing. Figure 37 presents an illustration of this approach to transporting DS3 data over a SONET Network FIGURE 37. A SIMPLE ILLUSTRATION OF A DS3 SIGNAL BEING MAPPED INTO AND TRANSPORTED OVER THE SONET NETWORK
SONET Network
DS3 Data
PTE PTE
PTE PTE
DS3 Data
As mentioned above a DS3 or E3 signal will be asynchronously mapped into a SONET or SDH signal and then transported over the SONET or SDH network. At the remote PTE this DS3 or E3 signal will be extracted (or de-mapped) from this SONET or SDH signal, where it will then be routed to DS3 or E3 terminal equipment for further processing. In order to insure that this "de-mapped" DS3 or E3 signal can be routed to any industry-standard DS3 or E3 terminal equipment, without any complications or adverse effect on the network, the Telcordia and ITU-T standard committees have specified some limits on both the Intrinsic Jitter and Wander that may exist within these DS3 or E3 signals as they are de-mapped from SONET/SDH. As a consequence, all PTEs that maps and de-mapped DS3/E3 signals into/from SONET/SDH must be designed such that the DS3 or E3 data that is de-mapped from SONET/SDH by these PTEs must meet these Intrinsic Jitter and Wander requirements. As mentioned above, the LIU can assist the System Designer (of SONET/SDH PTE) by ensuring that their design will meet these Intrinsic Jitter and Wander requirements. This section of the data sheet will present the following information to the user.
* Some background information on Mapping DS3/E3 signals into SONET/SDH and de-mapping DS3/E3
signals from SONET/SDH.
* A brief discussion on the causes of jitter and wander within a DS3 or E3 signal that mapped into a SONET/
SDH signal, and is transported across the SONET/SDH Network.
* A brief review of these Intrinsic Jitter and Wander requirements in both SONET and SDH applications. * A brief review on the Intrinsic Jitter and Wander measurement results (of a de-mapped DS3 or E3 signal)
whenever the LIU device is used in a system design.
* A detailed discussion on how to design with and configure the LIU device such that the end-system will meet
these Intrinsic Jitter and Wander requirements.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER In a SONET system, the relevant specification requirements for Intrinsic Jitter and Wander (within a DS3 signal that is mapped into and then de-mapped from SONET) are listed below.
* Telcordia GR-253-CORE Category I Intrinsic Jitter Requirements for DS3 Applications (Section 5.6), and * ANSI T1.105.03b-1997 - SONET Jitter at Network Interfaces - DS3 Wander Supplement
In general, there are three (3) sources of Jitter and Wander within an asynchronously-mapped DS3 signal that the system designer must be aware of. These sources are listed below.
* Mapping/De-Mapping Jitter * Pointer Adjustments * Clock Gapping
Each of these sources of jitter/wander will be defined and discussed in considerable detail within this Section. In order to accomplish all of this, this particular section will discuss all of the following topics in details.
* How DS3 data is mapped into SONET, and how this mapping operation contributes to Jitter and Wander
within this "eventually de-mapped" DS3 signal.
* How this asynchronously-mapped DS3 data is transported throughout the SONET Network, and how
occurrences on the SONET network (such as pointer adjustments) will further contributes to Jitter and Wander within the "eventually de-mapped" DS3 signal.
* A review of the Category I Intrinsic Jitter Requirements (per Telcordia GR-253-CORE) for DS3 applications * A review of the DS3 Wander requirements per ANSI T1.105.03b-1997 * A review of the Intrinsic Jitter and Wander Capabilities of the LIU in a typical system application * An in-depth discussion on how to design with and configure the LIU to permit the system to the meet the
above-mentioned Intrinsic Jitter and Wander requirements
NOTE: An in-depth discussion on SDH De-Sync Applications will be presented in the next revision of this data sheet.
8.2
MAPPING/DE-MAPPING JITTER/WANDER
Mapping/De-Mapping Jitter (or Wander) is defined as that intrinsic jitter (or wander) that is induced into a DS3 signal by the "Asynchronous Mapping" process. This section will discuss all of the following aspects of Mapping/De-Mapping Jitter.
* How DS3 data is mapped into an STS-1 SPE * How frequency offsets within either the DS3 signal (being mapped into SONET) or within the STS-1 signal
itself contributes to intrinsic jitter/wander within the DS3 signal (being transported via the SONET network). 8.2.1 HOW DS3 DATA IS MAPPED INTO SONET Whenever a DS3 signal is asynchronously mapped into SONET, this mapping is typically accomplished by a PTE accepting DS3 data (from some remote terminal) and then loading this data into certain bit-fields within a given STS-1 SPE (or Synchronous Payload Envelope). At this point, this DS3 signal has now been asynchronously mapped into an STS-1 signal. In most applications, the SONET Network will then take this particular STS-1 signal and will map it into "higher-speed" SONET signals (e.g., STS-3, STS-12, STS-48, etc.) and will then transport this asynchronously mapped DS3 signal across the SONET network, in this manner. As this "asynchronously-mapped" DS3 signal approaches its "destination" PTE, this STS-1 signal will eventually be de-mapped from this STS-N signal. Finally, once this STS-1 signal reaches the "destination" PTE, then this asynchronously-mapped DS3 signal will be extracted from this STS-1 signal. 8.2.1.1
A Brief Description of an STS-1 Frame
In order to be able to describe how a DS3 signal is asynchronously mapped into an STS-1 SPE, it is important to define and understand all of the following.
* The STS-1 frame structure * The STS-1 SPE (Synchronous Payload Envelope)
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
* Telcordia GR-253-CORE's recommendation on mapping DS3 data into an STS-1 SPE
An STS-1 frame is a data-structure that consists of 810 bytes (or 6480 bits). A given STS-1 frame can be viewed as being a 9 row by 90 byte column array (making up the 810 bytes). The frame-repetition rate (for an STS-1 frame) is 8000 frames/second. Therefore, the bit-rate for an STS-1 signal is (6480 bits/frame * 8000 frames/sec =) 51.84Mbps. A simple illustration of this SONET STS-1 frame is presented below in Figure 38. FIGURE 38. A SIMPLE ILLUSTRATION OF THE SONET STS-1 FRAME
90 Bytes
9 Rows
STS-1 Frame (810 Bytes)
Last Byte of the STS-1 Frame First Byte of the STS-1 Frame
Figure 38 indicates that the very first byte of a given STS-1 frame (to be transmitted or received) is located in the extreme upper left hand corner of the 90 column by 9 row array, and that the very last byte of a given STS1 frame is located in the extreme lower right-hand corner of the frame structure. Whenever a Network Element transmits a SONET STS-1 frame, it starts by transmitting all of the data, residing within the top row of the STS1 frame structure (beginning with the left-most byte, and then transmitting the very next byte, to the right). After the Network Equipment has completed its transmission of the top or first row, it will then proceed to transmit the second row of data (again starting with the left-most byte, first). Once the Network Equipment has transmitted the last byte of a given STS-1 frame, it will proceed to start transmitting the very next STS-1 frame. The illustration of the STS-1 frame (in Figure 38) is very simplistic, for multiple reasons. One major reason is that the STS-1 frame consists of numerous types of bytes. For the sake of discussion within this data sheet, the STS-1 frame will be described as consisting of the following types (or groups) of bytes.
* The Transport Overheads (or TOH) Bytes * The Envelope Capacity Bytes
8.2.1.1.1 The Transport Overhead (TOH) Bytes The Transport Overhead or TOH bytes occupy the very first three (3) byte columns within each STS-1 frame. Figure 39 presents another simple illustration of an STS-1 frame structure. However, in this case, both the TOH and the Envelope Capacity bytes are designated in this Figure.
88
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER FIGURE 39. A SIMPLE ILLUSTRATION OF THE STS-1 FRAME STRUCTURE WITH THE TOH AND THE ENVELOPE CAPACITY BYTES DESIGNATED
90 Bytes
3 Bytes
87 Bytes
TOH
Envelope Capacity
9 Row
Since the TOH bytes occupy the first three byte columns of each STS-1 frame, and since each STS-1 frame consists of nine (9) rows, then we can state that the TOH (within each STS-1 frame) consists of 3 byte columns x 9 rows = 27 bytes. The byte format of the TOH is presented below in Figure 40.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
FIGURE 40. THE BYTE-FORMAT OF THE TOH WITHIN AN STS-1 FRAME
3 Byte Columns
87 Byte Columns
A1 A1 B1 B1 D1 D1 H1 H1
9 Rows
A2 A2 E1 E1 D2 D2 H2 H2 K1 K1 D5 D5 D8 D8 D11 D11 M0 M0
C1 C1 F1 F1 D3 D3 H3 H3 K2 K2 D6 D6 D9 D9 D12 D12 E2 E2 The TOH Bytes Envelope Capacity Envelope Capacity Bytes Bytes
B2 B2 D4 D4 D7 D7 D10 D10 S1 S1
In general, the role/purpose of the TOH bytes is to fulfill the following functions.
* To support STS-1 Frame Synchronization * To support Error Detection within the STS-1 frame * To support the transmission of various alarm conditions such as RDI-L (Line - Remote Defect Indicator) and
REI-L (Line - Remote Error Indicator)
* To support the Transmission and Reception of "Section Trace" Messages * To support the Transmission and Reception of OAM&P Messages via the DCC Bytes (Data Communication
Channel bytes - D1 through D12 byte) The roles of most of the TOH bytes is beyond the scope of this Data Sheet and will not be discussed any further. However, there are a three TOH bytes that are important from the stand-point of this data sheet, and will discussed in considerable detail throughout this document. These are the H1 and H2 (e.g., the SPE Pointer) bytes and the H3 (e.g., the Pointer Action) byte. Figure 41 presents an illustration of the Byte-Format of the TOH within an STS-1 Frame, with the H1, H2 and H3 bytes highlighted.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER FIGURE 41. THE BYTE-FORMAT OF THE TOH WITHIN AN STS-1 FRAME
3 Byte Columns
87 Byte Columns
A1 A1 B1 B1 D1 D1 H1 H1
9 Rows
A2 A2 E1 E1 D2 D2 H2 H2 K1 K1 D5 D5 D8 D8 D11 D11 M0 M0
C1 C1 F1 F1 D3 D3 H3 H3 K2 K2 D6 D6 D9 D9 D12 D12 E2 E2 The TOH Bytes Envelope Capacity Envelope Capacity Bytes Bytes
B2 B2 D4 D4 D7 D7 D10 D10 S1 S1
Although the role of the H1, H2 and H3 bytes will be discussed in much greater detail in "Section 8.3, Jitter/ Wander due to Pointer Adjustments" on page 98. For now, we will simply state that the role of these bytes is two-fold.
* To permit a given PTE (Path Terminating Equipment) that is receiving an STS-1 data to be able to locate the
STS-1 SPE (Synchronous Payload Envelope) within the Envelope Capacity of this incoming STS-1 data stream and,
* To inform a given PTE whenever Pointer Adjustment and NDF (New Data Flag) events occur within the
incoming STS-1 data-stream. 8.2.1.1.2 The Envelope Capacity Bytes within an STS-1 Frame In general, the Envelope Capacity Bytes are any bytes (within an STS-1 frame) that exist outside of the TOH bytes. In short, the Envelope Capacity contains the STS-1 SPE (Synchronous Payload Envelope). In fact, every single byte that exists within the Envelope Capacity also exists within the STS-1 SPE. The only difference that exists between the "Envelope Capacity" as defined in Figure 40 and Figure 41 above and the STS-1 SPE is that the Envelope Capacity is aligned with the STS-1 framing boundaries and the TOH bytes; whereas the STS-1 SPE is NOT aligned with the STS-1 framing boundaries, nor the TOH bytes. The STS-1 SPE is an "87 byte column x 9 row" data-structure (which is the exact same size as is the Envelope Capacity) that is permitted to "float" within the "Envelope Capacity". As a consequence, the STS-1 SPE (within an STS-1 data-stream) will typically straddle across an STS-1 frame boundary. 8.2.1.1.3 The Byte Structure of the STS-1 SPE As mentioned above, the STS-1 SPE is an 87 byte column x 9 row structure. The very first column within the STS-1 SPE consists of some overhead bytes which are known as the "Path Overhead" (or POH) bytes. The remaining portions of the STS-1 SPE is available for "user" data. The Byte Structure of the STS-1 SPE is presented below in Figure 42.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
FIGURE 42. ILLUSTRATION OF THE BYTE STRUCTURE OF THE STS-1 SPE
87 Bytes 1 Byte 86 Bytes
9 Rows
J1 B3 C2 G1 F2 H4 Z3 Z4 Z5
Payload (or User) Data
In general, the role/purpose of the POH bytes is to fulfill the following functions.
* To support error detection within the STS-1 SPE * To support the transmission of various alarm conditions such as RDI-P (Path - Remote Defect Indicator) and
REI-P (Path - Remote Error Indicator)
* To support the transmission and reception of "Path Trace" Messages
The role of the POH bytes is beyond the scope of this data sheet and will not be discussed any further. 8.2.1.2
Mapping DS3 data into an STS-1 SPE
Now that we have defined the STS-1 SPE, we can now describe how a DS3 signal is mapped into an STS-1 SPE. As mentioned above, the STS-1 SPE is basically an 87 byte column x 9 row structure of data. The very first byte column (e.g., in all 9 bytes) consists of the POH (Path Overhead) bytes. All of the remaining bytes within the STS-1 SPE is simply referred to as "user" or "payload" data because this is the portion of the STS-1 signal that is used to transport "user data" from one end of the SONET network to the other. Telcordia GR-253CORE specifies the approach that one must use to asynchronously map DS3 data into an STS-1 SPE. In short, this approach is presented below in Figure 43.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER FIGURE 43. AN ILLUSTRATION OF TELCORDIA GR-253-CORE'S RECOMMENDATION ON HOW MAP DS3 DATA INTO AN STS-1 SPE
*
For DS3 Mapping, the STS-1 SPE has the following structure.
87 bytes R R R R R R R R R R R R R R R R R R C1 C1 C1 C1 C1 C1 C1 C1 C1 25I 25I 25I 25I 25I 25I 25I 25I 25I R R R R R R R R R C2 C2 C2 C2 C2 C2 C2 C2 C2 I I I I I I I I I 25I 25I 25I 25I 25I 25I 25I 25I 25I
i = DS3 data
R R R R R R R R R
C3 C3 C3 C3 C3 C3 C3 C3 C3
I I I I I I I I I
25I 25I 25I 25I 25I 25I 25I 25I 25I
POH
I = [i, i, i, i, i, i, i, i] R = [r, r, r, r, r, r, r, r] C1 = [r, r, c, i, i, i, i, i] C2 = [c, c, r, r, r, r, r, r] C3 = [c, c, r, r, o, o, r, s]
Fixed Stuff
r = fixed stuff bit c = stuff control bit s = stuff opportunity bit o = overhead communications channel bit
Figure 43 was copied directly out of Telcordia GR-253-CORE. However, this figure can be simplified and redrawn as depicted below in Figure 44. FIGURE 44. A SIMPLIFIED "BIT-ORIENTED" VERSION OF TELCORDIA GR-253-CORE'S RECOMMENDATION ON HOW TO MAP DS3 DATA INTO AN STS-1 SPE
18r 18r 18r 18r 18r 18r 18r 18r 18r
c c c c c c c c c
205i 205i 205i 205i 205i 205i 205i 205i 205i
16r 16r 16r 16r 16r 16r 16r 16r 16r
2c 2c 2c 2c 2c 2c 2c 2c 2c
6r 6r 6r 6r 6r 6r 6r 6r 6r
208i 208i 208i 208i 208i 208i 208i 208i 208i
16r 16r 16r 16r 16r 16r 16r 16r 16r
2c 2c 2c 2c 2c 2c 2c 2c 2c
2r 2r 2r 2r 2r 2r 2r 2r 2r
2o 2o 2o 2o 2o 2o 2o 2o 2o
1r 1r 1r 1r 1r 1r 1r 1r 1r
s s s s s s s s s
208i 208i 208i 208i 208i 208i 208i 208i 208i
POH
r c i s
- Fixed Stuff Bits - Stuff Control/Indicator Bits - DS3 Data Bits - Stuff Opportunity Bits
o
- Overhead Communication Bits
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Figure 44 presents an alternative illustration of Telcordia GR-253-CORE's recommendation on how to asynchronously map DS3 data into an STS-1 SPE. In this case, the STS-1 SPE bit-format is expressed purely in the form of "bit-types" and "numbers of bits within each of these types of bits". If one studies this figure closely he/she will notice that this is the same "87 byte column x 9 row" structure that we have been talking about when defining the STS-1 SPE. However, in this figure, the "user-data" field is now defined and is said to consist of five (5) different types of bits. Each of these bit-types play a role when asynchronously mapping a DS3 signal into an STS-1 SPE. Each of these types of bits are listed and described below. Fixed Stuff Bits Fixed Stuff bits are simply "space-filler" bits that simply occupy space within the STS-1 SPE. These bit-fields have no functional role other than "space occupation". Telcordia GR-253-CORE does not define any particular value that these bits should be set to. Each of the 9 rows, within the STS-1 SPE will contain 59 of these "fixed stuff" bits. DS3 Data Bits The DS3 Data-Bits are (as its name implies) used to transport the DS3 data-bits within the STS-1 SPE. If the STS-1 SPE is transporting a framed DS3 data-stream, then these DS3 Data bits will carry both the "DS3 payload data" and the "DS3 overhead bits". Each of the 9 rows, within the STS-1 SPE will contain 621 of these "DS3 Data bits". This means that each STS-1 SPE contains 5,589 of these DS3 Data bit-fields. Stuff Opportunity Bits The "Stuff" Opportunity bits will function as either a "stuff" (or junk) bit, or it will carry a DS3 data-bit. The decision as to whether to have a "Stuff Opportunity" bit transport a "DS3 data-bit" or a "stuff" bit depends upon the "timing differences" between the DS3 data that is being mapped into the STS-1 SPE and the timing source that is driving the STS-1 circuitry within the PTE. As will be described later on, these "Stuff Opportunity" Bits play a very important role in "frequency-justifying" the DS3 data that is being mapped into the STS-1 SPE. These "Stuff Opportunity" bits also play a critical role in inducing Intrinsic Jitter and Wander within the DS3 signal (as it is de-mapped by the remote PTE). Each of the 9 rows, within the STS-1 SPE consists of one (1) Stuff Opportunity bit. Hence, there are a total of nine "Stuff Opportunity" bits within each STS-1 SPE. Stuff Control/Indicator Bits Each of the nine (9) rows within the STS-1 SPE contains five (5) Stuff Control/Indicator bits. The purpose of these "Stuff Control/Indicator" bits is to indicate (to the de-mapping PTE) whether the "Stuff Opportunity" bits (that resides in the same row) is a "Stuff" bit or is carrying a DS3 data bit. If all five of these "Stuff Control/Indicator" bits, within a given row are set to "0", then this means that the corresponding "Stuff Opportunity" bit (e.g., the "Stuff Opportunity" bit within the same row) is carrying a DS3 data bit. Conversely, if all five of these "Stuff Control/Indicator" bits, within a given row are set to "1" then this means that the corresponding "Stuff Opportunity" bit is carrying a "stuff" bit. Overhead Communication Bits Telcordia GR-253-CORE permits the user to use these two bits (for each row) as some sort of "Communications" bit. Some Mapper devices, such as the XRT94L43 12-Channel DS3/E3/STS-1 to STS-12/ STM-1 Mapper and the XRT94L33 3-Channel DS3/E3/STS-1 to STS-3/STM-1 Mapper IC (both from Exar Corporation) do permit the user to have access to these bit-fields. However, in general, these particular bits can also be thought of as "Fixed Stuff" bits, that mostly have a "space occupation" function. 8.2.2 DS3 Frequency Offsets and the Use of the "Stuff Opportunity" Bits In order to fully convey the role that the "stuff-opportunity" bits play, when mapping DS3 data into SONET, we will present a detailed discussion of each of the following "Mapping DS3 into STS-1" scenarios.
* The Ideal Case (e.g., with no frequency offsets) * The 44.736Mbps + 1 ppm Case
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* The 44.736MHz - 1ppm Case
Throughout each of these cases, we will discuss how the resulting "bit-stuffing" (that was done when mapping the DS3 signal into SONET) affects the amount of intrinsic jitter and wander that will be present in the DS3 signal, once it is ultimately de-mapped from SONET. 8.2.2.1
The Ideal Case for Mapping DS3 data into an STS-1 Signal (e.g., with no Frequency Offsets)
Let us assume that we are mapping a DS3 signal, which has a bit rate of exactly 44.736Mbps (with no frequency offset) into SONET. Further, let us assume that the SONET circuitry within the PTE is clocked at exactly 51.84MHz (also with no frequency offset), as depicted below. FIGURE 45. A SIMPLE ILLUSTRATION OF A DS3 DATA-STREAM BEING MAPPED INTO AN STS-1 SPE, VIA A PTE
DS3_Data_In
STS-1_Data_Out
PTE PTE
44.736MHz + 0ppm 51.84MHz + 0ppm
Given the above-mentioned assumptions, we can state the following.
* The DS3 data-stream has a bit-rate of exactly 44.736Mbps * The PTE will create 8000 STS-1 SPE's per second * In order to properly map a DS3 data-stream into an STS-1 data-stream, then each STS-1 SPE must carry
(44.736Mbps/8000 =) 5592 DS3 data bits. Is there a Problem? According to Figure 44, each STS-1 SPE only contains 5589 bits that are specifically designated for "DS3 data bits". In this case, each STS-1 SPE appears to be three bits "short". No there is a Simple Solution No, earlier we mentioned that each STS-1 SPE consists of nine (9) "Stuff Opportunity" bits. Therefore, these three additional bits (for DS3 data) are obtained by using three of these "Stuff Opportunity" bits. As a consequence, three (3) of these nine (9) "Stuff Opportunity" bits, within each STS-1 SPE, will carry DS3 databits. The remaining six (6) "Stuff Opportunity" bits will typically function as "stuff" bits. In summary, for the "Ideal Case"; where there is no frequency offset between the DS3 and the STS-1 bit-rates, once this DS3 data-stream has been mapped into the STS-1 data-stream, then each and every STS-1 SPE will have the following "Stuff Opportunity" bit utilization. 3 "Stuff Opportunity" bits will carry DS3 data bits. 6 "Stuff Opportunity" bits will function as "stuff" bits In this case, this DS3 signal (which has now been mapped into STS-1) will be transported across the SONET network. As this STS-1 signal arrives at the "Destination PTE", this PTE will extract (or de-map) this DS3 datastream from each incoming STS-1 SPE. Now since each and every STS-1 SPE contains exactly 5592 DS3 data bits; then the bit rate of this DS3 signal will be exactly 44.736Mbps (such as it was when it was mapped into SONET, at the "Source" PTE).
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As a consequence, no "Mapping/De-Mapping" Jitter or Wander is induced in the "Ideal Case". 8.2.2.2
The 44.736Mbps + 1ppm Case
The "above example" was a very ideal case. In reality, there are going to be frequency offsets in both the DS3 and STS-1 signals. For instance Bellcore GR-499-CORE mandates that a DS3 signal have a bit rate of 44.736Mbps 20ppm. Hence, the bit-rate of a "Bellcore" compliant DS3 signal can vary from the exact correct frequency for DS3 by as much of 20ppm in either direction. Similarly, many SONET applications mandate that SONET equipment use at least a "Stratum 3" level clock as its timing source. This requirement mandates that an STS-1 signal must have a bit rate that is in the range of 51.84 4.6ppm. To make matters worse, there are also provisions for SONET equipment to use (what is referred to as) a "SONET Minimum Clock" (SMC) as its timing source. In this case, an STS-1 signal can have a bit-rate in the range of 51.84Mbps 20ppm. In order to convey the impact that frequency offsets (in either the DS3 or STS-1 signal) will impose on the bitstuffing behavior, and the resulting bit-rate, intrinsic jitter and wander within the DS3 signal that is being transported across the SONET network; let us assume that a DS3 signal, with a bit-rate of 44.736Mbps + 1ppm is being mapped into an STS-1 signal with a bit-rate of 51.84Mbps + 0ppm. In this case, the following things will occur.
* In general, most of the STS-1 SPE's will each transport 5592 DS3 data bits. * However, within a "one-second" period, a DS3 signal that has a bit-rate of 44.736Mbps + 1 ppm will deliver
approximately 44.7 additional bits (over and above that of a DS3 signal with a bit-rate of 44.736Mbps + 0 ppm). This means that this particular signal will need to "negative-stuff" or map in an additional DS3 data bit every (1/44.736 =) 22.35ms. In other words, this additional DS3 data bit will need to be mapped into about one in every (22.35ms * 8000 =) 178.8 STS-1 SPEs in order to avoid dropping any DS3 data-bits. What does this mean at the "Source" PTE? All of this means that as the "Source" PTE maps this DS3 signal, with a data rate of 44.736Mbps + 1ppm into an STS-1 signal, most of the resulting "outbound" STS-1 SPEs will transport 5592 DS3 data bits (e.g., 3 Stuff Opportunity bits will be carrying DS3 data bits, the remaining 6 Stuff Opportunity bits are "stuff" bits, as in the "Ideal" case). However, in approximately one out of 178.8 "outbound" STS-1 SPEs, there will be a need to insert an additional DS3 data bit within this STS-1 SPE. Whenever this occurs, then (for these particular STS1 SPEs) the SPE will be carrying 5593 DS3 data bits (e.g., 4 Stuff Opportunity bits will be carrying DS3 data bits, the remaining 5 Stuff Opportunity bits are "stuff" bits). Figure 46 presents an illustration of the STS-1 SPE traffic that will be generated by the "Source" PTE, during this condition. FIGURE 46. AN ILLUSTRATION OF THE STS-1 SPE TRAFFIC THAT WILL BE GENERATED BY THE "SOURCE" PTE, WHEN MAPPING IN A DS3 SIGNAL THAT HAS A BIT RATE OF 44.736MBPS + 1PPM, INTO AN STS-1 SIGNAL
Extra DS3 Data Bit Stuffed Here
SPE # N 5592 5592 DS3 Data DS3 Data Bits Bits
SPE # N+1 5592 5592 DS3 Data DS3 Data Bits Bits
SPE # N+177 5592 5592 DS3 Data DS3 Data Bits Bits 5593 5593 DS3 Data DS3 Data Bits Bits
SPE # N+179 5592 5592 DS3 Data DS3 Data Bits Bits
Source Source PTE PTE
SPE # N+178
44.736Mbps + 1ppm
STS-1 SPE Data Stream
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER What does this mean at the "Destination" PTE? In this case, this DS3 signal (which has now been mapped into an STS-1 data-stream) will be transported across the SONET network. As this STS-1 signal arrives at the "Destination" PTE, this PTE will extract (or demap) this DS3 data from each incoming STS-1 SPE. Now, in this case most (e.g., 177/178.8) of the incoming STS-1 SPEs will contain 5592 DS3 data-bits. Therefore, the nominal data rate of the DS3 signal being demapped from SONET will be 44.736Mbps. However, in approximately 1 out of every 178 incoming STS-1 SPEs, the SPE will carry 5593 DS3 data-bits. This means that (during these times) the data rate of the demapped DS3 signal will have an instantaneous frequency that is greater than 44.736Mbps. These "excursion" of the de-mapped DS3 data-rate, from the nominal DS3 frequency can be viewed as occurrences of "mapping/ de-mapping" jitter. Since each of these "bit-stuffing" events involve the insertion of one DS3 data bit, we can say that the amplitude of this "mapping/de-mapping" jitter is approximately 1UI-pp. From this point on, we will be referring to this type of jitter (e.g., that which is induced by the mapping and de-mapping process) as "demapping" jitter. Since this occurrence of "de-mapping" jitter is periodic and occurs once every 22.35ms, we can state that this jitter has a frequency of 44.7Hz. 8.2.2.3
The 44.736Mbps - 1ppm Case
In this case, let us assume that a DS3 signal, with a bit-rate of 44.736Mbps - 1ppm is being mapped into an STS-1 signal with a bit-rate of 51.84Mbps + 0ppm. In this case, the following this will occur.
* In general, most of the STS-1 SPEs will each transport 5592 DS3 data bits. * However, within a "one-second" period a DS3 signal that has a bit-rate of 44.736Mbps - 1ppm will deliver
approximately 45 too few bits below that of a DS3 signal with a bit-rate of 44.736Mbps + 0ppm. This means that this particular signal will need to "positive-stuff" or exclude a DS3 data bit from mapping every (1/44.736) = 22.35ms. In other words, we will need to avoid mapping this DS3 data-bit about one in every (22.35ms*8000) = 178.8 STS-1 SPEs. What does this mean at the "Source" PTE? All of this means that as the "Source" PTE maps this DS3 signal, with a data rate of 44.736Mbps - 1ppm into an STS-1 signal, most of the resulting "outbound" STS-1 SPEs will transport 5592 DS3 data bits (e.g., 3 Stuff Opportunity bits will be carrying DS3 data bits, the remaining 6 Stuff Opportunity bits are "stuff" bits). However, in approximately one out of 178.8 "outbound" STS-1 SPEs, there will be a need for a "positive-stuffing" event. Whenever these "positive-stuffing" events occur then (for these particular STS-1 SPEs) the SPE will carry only 5591 DS3 data bits (e.g., in this case, only 2 Stuff Opportunity bits will be carrying DS3 data-bits, and the remaining 7 Stuff Opportunity bits are "stuff" bits). Figure 47 presents an illustration of the STS-1 SPE traffic that will be generated by the "Source" PTE, during this condition.
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FIGURE 47. AN ILLUSTRATION OF THE STS-1 SPE TRAFFIC THAT WILL BE GENERATED BY THE SOURCE PTE, WHEN DS3 SIGNAL THAT HAS A BIT RATE OF 44.736MBPS - 1PPM, INTO AN STS-1 SIGNAL
MAPPING A
DS3 Data Bit Excluded Here
SPE # N 5592 5592 DS3 Data DS3 Data Bits Bits
SPE # N+1 5592 5592 DS3 Data DS3 Data Bits Bits
SPE # N+177 5592 5592 DS3 Data DS3 Data Bits Bits 5591 5591 DS3 Data DS3 Data Bits Bits
SPE # N+179 5592 5592 DS3 Data DS3 Data Bits Bits
Source Source PTE PTE
SPE # N+178
44.736Mbps - 1ppm
STS-1 SPE Data Stream
What does this mean at the Destination PTE? In this case, this DS3 signal (which has now been mapped into an STS-1 data-stream) will be transported across the SONET network. As this STS-1 signal arrives at the "Destination" PTE, this PTE will extract (or demap) this DS3 data from each incoming STS-1 SPE. Now, in this case, most (e.g., 177/178.8) of the incoming STS-1 SPEs will contain 5592 DS3 data-bits. Therefore, the nominal data rate of the DS3 signal being demapped from SONET will be 44.736Mbps. However, in approximately 1 out of every 178 incoming STS-1 SPEs, the SPE will carry only 5591 DS3 data bits. This means that (during these times) the data rate of the demapped DS3 signal will have an instantaneous frequency that is less than 44.736Mbps. These "excursions" of the de-mapped DS3 data-rate, from the nominal DS3 frequency can be viewed as occurrences of mapping/demapping jitter with an amplitude of approximately 1UI-pp. Since this occurrence of "de-mapping" jitter is periodic and occurs once every 22.35ms, we can state that this jitter has a frequency of 44.7Hz. We talked about De-Mapping Jitter, What about De-Mapping Wander? The Telcordia and Bellcore specifications define "Wander" as "Jitter with a frequency of less than 10Hz". Based upon this definition, the DS3 signal (that is being transported by SONET) will cease to contain jitter and will now contain "Wander", whenever the frequency offset of the DS3 signal being mapped into SONET is less than 0.2ppm. 8.3
Jitter/Wander due to Pointer Adjustments
In the previous section, we described how a DS3 signal is asynchronously-mapped into SONET, and we also defined "Mapping/De-mapping" jitter. In this section, we will describe how occurrences within the SONET network will induce jitter/wander within the DS3 signal that is being transported across the SONET network. In order to accomplish this, we will discuss the following topics in detail.
* The concept of an STS-1 SPE pointer * The concept of Pointer Adjustments * The causes of Pointer Adjustments * How Pointer Adjustments induce jitter/wander within a DS3 signal being transported by that SONET network.
8.3.1 The Concept of an STS-1 SPE Pointer As mentioned earlier, the STS-1 SPE is not aligned to the STS-1 frame boundaries and is permitted to "float" within the Envelope Capacity. As a consequence, the STS-1 SPE will often times "straddle" across two
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FIGURE 48. AN ILLUSTRATION OF AN STS-1 SPE STRADDLING ACROSS TWO CONSECUTIVE STS-1 FRAMES
TOH
STS-1 FRAME N
STS-1 FRAME N + 1
H1, H2 Bytes
J1 Byte (1st byte of SPE)
J1 Byte (1st byte of next SPE)
SPE can straddle across two STS-1 frames
A PTE that is receiving and terminating an STS-1 data-stream will perform the following tasks.
* It will acquire and maintain STS-1 frame synchronization with the incoming STS-1 data-stream. * Once the PTE has acquired STS-1 frame synchronization, then it will locate the J1 byte (e.g., the very byte
within the very next STS-1 SPE) within the Envelope Capacity by reading out the contents of the H1 and H2 bytes. The H1 and H2 bytes are referred to (in the SONET standards) as the SPE Pointer Bytes. When these two bytes are concatenated together in order to form a 16-bit word (with the H1 byte functioning as the "Most Significant Byte") then the contents of the "lower" 10 bit-fields (within this 16-bit word) reflects the location of the J1 byte within the Envelope Capacity of the incoming STS-1 data-stream. Figure 49 presents an illustration of the bit format of the H1 and H2 bytes, and indicates which bit-fields are used to reflect the location of the J1 byte.
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FIGURE 49. THE BIT-FORMAT OF THE 16-BIT WORD (CONSISTING OF THE H1 AND H2 BYTES) WITH THE 10 BITS, J1 BYTE, DESIGNATED
REFLECTING THE LOCATION OF THE
H1 Byte MSB
H2 Byte LSB
NNNNSSXXXXXXXXXX
10 Bit Pointer Expression
Figure 50 relates the contents within these 10 bits (within the H1 and H2 bytes) to the location of the J1 byte (e.g., the very first byte of the STS-1 SPE) within the Envelope Capacity. FIGURE 50. THE RELATIONSHIP BETWEEN THE CONTENTS OF THE "POINTER BITS" (E.G., THE 10-BIT EXPRESSION WITHIN THE H1 AND H2 BYTES) AND THE LOCATION OF THE J1 BYTE WITHIN THE ENVELOPE CAPACITY OF AN STS1 FRAME
TOH
The Pointer Value "0" is immediately After the H3 byte
A1 B1 D1 H1 B2 D4 D7 D10 S1
A2 E1 D2 H2 K1 D5 D8 D11 M0
C1/J0 F1 D3 H3 K2 D6 D9 D12 E2
522 609 696 0 87 174 261 348 435
523 610 697 1 88 175 262 349 436
******** ** ******** ** ******** ** ******** ** ******** ** ******** ** ******** ** ******** ** ******** **
607 694 781 85 172 259 346 433 520
608 695 782 86 173 260 347 434 521
NOTES: 1. If the content of the "Pointer Bits" is "0x00" then the J1 byte is located immediately after the H3 byte, within the Envelope Capacity. 2. If the contents of the 10-bit expression exceed the value of 0x30F (or 782, in decimal format) then it does not contain a valid pointer value.
8.3.2
Pointer Adjustments within the SONET Network
The word SONET stands for "Synchronous Optical NETwork. This name implies that the entire SONET network is synchronized to a single clock source. However, because the SONET (and SDH) Networks can
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER span thousands of miles, traverse many different pieces of equipments, and even cross International boundaries; in practice, the SONET/SDH network is NOT synchronized to a single clock source. In practice, the SONET/SDH network can be thought of as being divided into numerous "Synchronization Islands". Each of these "Synchronization Islands" will consist of numerous pieces of SONET Terminal Equipment. Each of these pieces of SONET Terminal Equipment will all be synchronized to a single Stratum-1 clock source which is the most accurate clock source within the Synchronization Island. Typically a "Synchronization Island" will consist of a single "Timing Master" equipment along with multiple "Timing Slave" pieces of equipment. This "Timing Master" equipment will be directly connected to the Stratum-1 clock source and will have the responsibility of distributing a very accurate clock signal (that has been derived from the Stratum 1 clock source) to each of the "Timing Slave" pieces of equipment within the "Synchronization Island". The purpose of this is to permit each of the "Timing Slave" pieces of equipment to be "synchronized" with the "Timing Master" equipment, as well as the Stratum 1 Clock source. Typically this "clock distribution" is performed in the form of a BITS (Building Integrated Timing Supply) clock, in which a very precise clock signal is provided to the other pieces of equipment via a T1 or E1 line signal. Many of these "Synchronization Islands" will use a Stratum-1" clock source that is derived from GPS pulses that are received from Satellites that operate at Geo-synchronous orbit. Other "Synchronization Islands" will use a Stratum-1" clock source that is derived from a very precise local atomic clock. As a consequence, different "Synchronization Islands" will use different Stratum 1 clock sources. The up-shot of having these "Synchronization Islands" that use different "Stratum-1 clock" sources, is that the Stratum 1 Clock frequencies, between these "Synchronization Islands" are likely to be slightly different from each other. These "frequencydifferences" within Stratum 1 clock sources will result in "clock-domain changes" as a SONET signal (that is traversing the SONET network) passes from one "Synchronization Island" to another. The following section will describe how these "frequency differences" will cause a phenomenon called "pointer adjustments" to occur in the SONET Network. 8.3.3 Causes of Pointer Adjustments The best way to discuss how pointer adjustment events occur is to consider an STS-1 signal, which is driven by a timing reference of frequency f1; and that this STS-1 signal is being routed to a network equipment (that resides within a different "Synchronization Island") and processes STS-1 data at a frequency of f2.
NOTE: Clearly, both frequencies f1 and f2 are at the STS-1 rate (e.g., 51.84MHz). However, these two frequencies are likely to be slightly different from each other.
Now, since the STS-1 signal (which is of frequency f1) is being routed to the network element (which is operating at frequency f2), the typical design approach for handling "clock-domain" differences is to route this STS-1 signal through a "Slip Buffer" as illustrated below.
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FIGURE 51. AN ILLUSTRATION OF AN STS-1 SIGNAL BEING PROCESSED VIA A SLIP BUFFER
Clock Domain operating At frequency f1
STS-1 Data_IN STS-1 Clock_f1
STS-1 Data_OUT
SLIP BUFFER SLIP BUFFER
STS-1 Clock_f2
Clock Domain operating At Frequency f2.
In the "Slip Buffer, the "input" STS-1 data (labeled "STS-1 Data_IN") is latched into the FIFO, upon a given edge of the corresponding "STS-1 Clock_f1" input clock signal. The STS-1 Data (labeled "STS-1 Data_OUT") is clocked out of the Slip Buffer upon a given edge of the "STS-1 Clock_f2" input clock signal. The behavior of the data, passing through the "Slip Buffer" is now described for each possible relationship between frequencies f1 and f2.
If f1 = f2
If both frequencies, f1 and f2 are exactly equal, then the STS-1 data will be "clocked" into the "Slip Buffer" at exactly the same rate that it is "clocked out". In this case, the "Slip Buffer" will neither fill-up nor become depleted. As a consequence, no pointer-adjustments will occur in this STS-1 data stream. In other words, the STS-1 SPE will remain at a constant location (or offset) within each STS-1 envelope capacity for the duration that this STS-1 signal is supporting this particular service.
If f1 < f2
If frequency f1 is less than f2, then this means that the STS-1 data is being "clocked out" of the "Slip Buffer" at a faster rate than it is being clocked in. In this case, the "Slip Buffer" will eventually become depleted. Whenever this occurs, a typical strategy is to "stuff" (or insert) a "dummy byte" into the data stream. The purpose of stuffing this "dummy byte" is to compensate for the frequency differences between f1 and f2, and attempt to keep the "Slip Buffer, at a somewhat constant fill level.
NOTE: This "dummy byte" does not carry any valuable information (not for the user, nor for the system).
Since this "dummy byte" carries no useful information, it is important that the "Receiving PTE" be notified anytime this "dummy byte" stuffing occurs. This way, the Receiving Terminal can "know" not to treat this "dummy byte" as user data. Byte-Stuffing and Pointer Incrementing in a SONET Network Whenever this "byte-stuffing" occurs then the following other things occur within the STS-1 data stream.
During the STS-1 frame that contains the "Byte-Stuffing" event
a. The "stuff-byte" will be inserted into the byte position immediately after the H3 byte. This insertion of the "dummy byte" immediately after the H3 byte position will cause the J1 byte (and in-turn, the rest of the SPE) to be "byte-shifted" away from the H3 byte. As a consequence, the offset between the H3 byte position and the STS-1 SPE will now have been increased by 1 byte. b. The "Transmitting" Network Equipment will notify the remote terminal of this byte-stuffing event, by inverting certain bits within the "pointer word" (within the H1 and H2 bytes) that are referred to as "I" bits.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER Figure 52 presents an illustration of the bit-format within the 16-bit word (consist of the H1 and H2 bytes) with the "I" bits designated. FIGURE 52. AN ILLUSTRATION OF THE BIT FORMAT WITHIN THE 16-BIT WORD (CONSISTING OF THE H1 AND H2 BYTES) WITH THE "I" BITS DESIGNATED
H1 Byte MSB
H2 Byte LSB
NNNNSS ID ID ID I D ID
10 Bit Pointer Expression
NOTE: At this time the "I" bits are inverted in order to denote that an "incrementing" pointer adjustment event is currently occurring.
During the STS-1 frame that follows the "Byte-Stuffing" event
The "I" bits (within the "pointer-word") will be set back to their normal value; and the contents of the H1 and H2 bytes will be incremented by "1".
If f1 > f2
If frequency f1 is greater than f2, then this means that the STS-1 data is being clocked into the "Slip Buffer" at a faster rate than is being clocked out. In this case, the "Slip Buffer" will start to fill up. Whenever this occurs, a typical strategy is to delete (e.g., negative-stuff) a byte from the Slip Buffer. The purpose of this "negativestuffing" is to compensate for the frequency differences between f1 and f2; and to attempt to keep the "Slip Buffer" at a somewhat constant fill-level.
NOTE: This byte, which is being "un-stuffed" does carry valuable information for the user (e.g., this byte is typically a payload byte). Therefore, whenever this negative stuffing occurs, two things must happen.
a. The "negative-stuffed" byte must not be simply discarded. In other words, it must somehow also be transmitted to the remote PTE with the remainder of the SPE data. b. The remote PTE must be notified of the occurrence of these "negative-stuffing" events. Further, the remote PTE must know where to obtain this "negative-stuffed" byte. Negative-Stuffing and Pointer-Decrementing in a SONET Network Whenever this "byte negative-stuffing" occurs then the following other things occur within the STS-1 datastream.
During the STS-1 frame that contains the "Negative Byte-Stuffing" Event
a. The "Negative-Stuffed" byte will be inserted into the H3 byte position. Whenever an SPE data byte is inserted into the H3 byte position (which is ordinarily an unused byte), the number of bytes that will exist between the H3 byte and the J1 byte within the very next SPE will be reduced by 1 byte. As a consequence, in this case, the J1 byte (and in-turn, the rest of the SPE) will now be "byte-shifted" towards the H3 byte position. b. The "Transmitting" Network Element will notify the remote terminal of this "negative-stuff" event by inverting certain bits within the "pointer word" (within the H1 and H2 bytes) that are referred to as "D" bits.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
Figure 53 presents an illustration of the bit format within the 16-bit word (consisting of the H1 and H2 bytes) with the "D" bits designated. FIGURE 53. AN ILLUSTRATION OF THE BIT-FORMAT WITHIN THE 16-BIT WORD (CONSISTING OF THE H1 AND H2 "D" BITS DESIGNATED
BYTES) WITH THE
H1 Byte MSB
H2 Byte LSB
NNNNSS ID ID ID I D ID
10 Bit Pointer Expression
NOTE: At this time the "D" bits are inverted in order to denote that a "decrementing" pointer adjustment event is currently occurring.
During the STS-1 frame that follows the "Negative Byte-Stuffing" Event The "D" bits (within the pointer-word) will be set back to their normal value; and the contents of the H1 and H2 bytes will be decremented by one.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 8.3.4 Why are we talking about Pointer Adjustments?
The overall SONET network consists of numerous "Synchronization Islands". As a consequence, whenever a SONET signal is being transmitted from one "Synchronization Island" to another; that SONET signal will undergo a "clock domain" change as it traverses the network. This clock domain change will result in periodic pointer-adjustments occurring within this SONET signal. Depending upon the direction of this "clock-domain" shift that the SONET signal experiences, there will either be periodic "incrementing" pointer-adjustment events or periodic "decrementing" pointer-adjustment events within this SONET signal. Regardless of whether a given SONET signal is experiencing incrementing or decrementing pointer adjustment events, each pointer adjustment event will result in an abrupt 8-bit shift in the position of the SPE within the STS-1 data-stream. If this STS-1 signal is transporting an "asynchronously-mapped" DS3 signal; then this 8-bit shift in the location of the SPE (within the STS-1 signal) will result in approximately 8UIpp of jitter within the asynchronously-mapped DS3 signal, as it is de-mapped from SONET. In "Section 8.5, A Review of the Category I Intrinsic Jitter Requirements (per Telcordia GR-253-CORE) for DS3 applications" on page 106 we will discuss the "Category I Intrinsic Jitter Requirements (for DS3 Applications) per Telcordia GR-253CORE. However, for now we will simply state that this 8UIpp of intrinsic jitter far exceeds these "intrinsic jitter" requirements. In summary, pointer-adjustments events are a "fact of life" within the SONET/SDH network. Further, pointeradjustment events, within a SONET signal that is transporting an asynchronously-mapped DS3 signal, will impose a significant impact on the Intrinsic Jitter and Wander within that DS3 signal as it is de-mapped from SONET. 8.4
Clock Gapping Jitter
In most applications (in which the LIU will be used in a SONET De-Sync Application) the user will typically interface the LIU to a Mapper Device in the manner as presented below in Figure 54. FIGURE 54. ILLUSTRATION OF THE TYPICAL APPLICATIONS FOR THE LIU IN A SONET DE-SYNC APPLICATION
De-Mapped (Gapped) DS3 Data and Clock
TPDATA_n input pin
STS-N Signal
DS3 to STS-N DS3 to STS-N Mapper/ Mapper/ Demapper Demapper IC IC
LIU LIU
TCLK_n input
In this application, the Mapper IC will have the responsibility of receiving an STS-N signal (from the SONET Network) and performing all of the following operations on this STS-N signal.
* Byte-de-interleaving this incoming STS-N signal into N STS-1 signals * Terminating each of these STS-1 signals * Extracting (or de-mapping) the DS3 signal(s) from the SPEs within each of these terminated STS-1 signals.
In this application, these Mapper devices can be thought of as multi-channel devices. For example, an STS-3 Mapper can be viewed as a 3-Channel DS3/STS-1 to STS-3 Mapper IC. Similarly, an STS-12 Mapper can be
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
viewed as a 12-Channel DS3/STS-1 to STS-12 Mapper IC. Continuing on with this line of thought, if a Mapper IC is configured to receive an STS-N signal, and (from this STS-N signal) de-map and output N DS3 signals (towards the DS3 facility), then it will typically do so in the following manner.
* In many cases, the Mapper IC will output this DS3 signal, using both a "Data-Signal" and a "Clock-Signal".
In many cases, the Mapper IC will output the contents of an entire STS-1 data-stream via the Data-Signal.
* However, as the Mapper IC output this STS-1 data-stream, it will typically supply clock pulses (via the ClockSignal output) coincident to whenever a DS3 bit is being output via the Data-Signal. In this case, the Mapper IC will NOT supply a clock pulse coincident to when a TOH, POH, or any "non-DS3 data-bit" is being output via the "Data-Signal". Now, since the Mapper IC will output the entire STS-1 data stream (via the Data-Signal), the output ClockSignal will be of the form such that it has a period of 19.3ns (e.g., a 51.84MHz clock signal). However, the Mapper IC will still generate approximately 44,736,000 clock pulses during any given one second period. Hence, the clock signal that is output from the Mapper IC will be a horribly gapped 44.736MHz clock signal. One can view such a clock signal as being a very-jittery 44.736MHz clock signal. This jitter that exists within the "Clock-Signal" is referred to as "Clock-Gapping" Jitter. A more detailed discussion on how the user must handle this type of jitter is presented in "Section 8.8.2, Recommendations on Pre-Processing the Gapped Clocks (from the Mapper/ASIC Device) prior to routing this DS3 Clock and Data-Signals to the Transmit Inputs of the LIU" on page 117. 8.5
A Review of the Category I Intrinsic Jitter Requirements (per Telcordia GR-253-CORE) for DS3 applications
The "Category I Intrinsic Jitter Requirements" per Telcordia GR-253-CORE (for DS3 applications) mandates that the user perform a large series of tests against certain specified "Scenarios". These "Scenarios" and their corresponding requirements is summarized in Table 46, below. TABLE 46: SUMMARY OF "CATEGORY I INTRINSIC JITTER REQUIREMENT PER TELCORDIA GR-253-CORE, FOR DS3
APPLICATIONS
SCENARIO DESCRIPTION DS3 De-Mapping Jitter Single Pointer Adjustment
SCENARIO NUMBER
TELCORDIA GR-253-CORE CATEGORY I INTRINSIC JITTER REQUIREMENTS 0.4UI-pp
COMMENTS
Includes effects of De-Mapping and Clock Gapping Jitter
A1
0.3UI-pp + Ao
Includes effects of Jitter from Clock-Gapping, De-Mapping and Pointer Adjustments.NOTE: Ao is the amount of intrinsic jitter that was measured during the "DS3 DeMapping Jitter" phase of the Test. Includes effects of Jitter from Clock-Gapping, De-Mapping and Pointer Adjustments. Includes effects of Jitter from Clock-Gapping, De-Mapping and Pointer Adjustments. Includes effects of Jitter from Clock-Gapping, De-Mapping and Pointer Adjustments. Includes effects of Jitter from Clock-Gapping, De-Mapping and Pointer Adjustments. Includes effects of Jitter from Clock-Gapping, De-Mapping and Pointer Adjustments. Includes effects of Jitter from Clock-Gapping, De-Mapping and Pointer Adjustments.
Pointer Bursts Phase Transients 87-3 Pattern 87-3 Add 87-3 Cancel Continuous Pattern
A2 A3 A4 A5 A5 A4
1.3UI-pp 1.2UI-pp 1.0UI-pp 1.3UI-pp 1.3UI-pp 1.0UI-pp
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER TABLE 46: SUMMARY OF "CATEGORY I INTRINSIC JITTER REQUIREMENT PER TELCORDIA GR-253-CORE, FOR DS3
APPLICATIONS
SCENARIO DESCRIPTION Continuous Add Continuous Cancel
SCENARIO NUMBER A5 A5
TELCORDIA GR-253-CORE CATEGORY I INTRINSIC JITTER REQUIREMENTS 1.3UI-pp 1.3UI-pp
COMMENTS
Includes effects of Jitter from Clock-Gapping, De-Mapping and Pointer Adjustments. Includes effects of Jitter from Clock-Gapping, De-Mapping and Pointer Adjustments.
NOTE: All of these intrinsic jitter measurements are to be performed using a band-pass filter of 10Hz to 400kHz.
Each of the scenarios presented in Table 46, are briefly described below. 8.5.1 DS3 De-Mapping Jitter DS3 De-Mapping Jitter is the amount of Intrinsic Jitter that will be measured within the "Line" or "Facility-side" DS3 signal, (after it has been de-mapped from a SONET signal) without the occurrence of "Pointer Adjustments" within the SONET signal. Telcordia GR-253-CORE requires that the "DS3 De-Mapping" Jitter be less than 0.4UI-pp, when measured over all possible combinations of DS3 and STS-1 frequency offsets. 8.5.2 Single Pointer Adjustment Telcordia GR-253-CORE states that if each pointer adjustment (within a continuous stream of pointer adjustments) is separated from each other by a period of 30 seconds, or more; then they are sufficiently isolated to be considered "Single-Pointer Adjustments". Figure 55 presents an illustration of the "Single Pointer Adjustment" Scenario. FIGURE 55. ILLUSTRATION OF SINGLE POINTER ADJUSTMENT SCENARIO
Pointer Adjustment Events
>30s
Initialization
Cool Down
Measurement Period
Telcordia GR-253-CORE states that the Intrinsic Jitter that is measured (within the DS3 signal) that is ultimately de-mapped from a SONET signal that is experiencing "Single-Pointer Adjustment" events, must NOT exceed the value 0.3UI-pp + Ao.
NOTES: 1. Ao is the amount of Intrinsic Jitter that was measured during the "De-Mapping" Jitter portion of this test. 2. Testing must be performed for both Incrementing and Decrementing Pointer Adjustments.
8.5.3
Pointer Burst
Figure 56 presents an illustration of the "Pointer Burst" Pointer Adjustment Scenario per Telcordia GR-253CORE.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
FIGURE 56. ILLUSTRATION OF BURST OF POINTER ADJUSTMENT SCENARIO
Pointer Adjustment Events
Pointer Adjustment Burst Train
t
0.5ms 0.5ms
>30s
Initialization
Cool Down
Measurement Period
Telcordia GR-253-CORE mandates that the Intrinsic Jitter, within the DS3 signal that is de-mapped from a SONET signal, which is experiencing the "Burst of Pointer Adjustment" scenario, must NOT exceed 1.3UI-pp. 8.5.4 Phase Transients Figure 57 presents an illustration of the "Phase Transients" Pointer Adjustment Scenario per Telcordia GR253-CORE. FIGURE 57. ILLUSTRATION OF "PHASE-TRANSIENT" POINTER ADJUSTMENT SCENARIO
Pointer Adjustment Events
Pointer Adjustment Burst Train
0.5s
0.25s
0.25s
t
>30s
Initialization
Cool Down
Measurement Period
Telcordia GR-253-CORE mandates that the Intrinsic Jitter, within the DS3 signal that is de-mapped from a SONET signal, which is experiencing the "Phase Transient - Pointer Adjustment" scenario must NOT exceed 1.2UI-pp.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER 8.5.5 87-3 Pattern
Figure 58 presents an illustration of the "87-3 Continuous Pattern" Pointer Adjustment Scenario per Telcordia GR-253-CORE. FIGURE 58. AN ILLUSTRATION OF THE 87-3 CONTINUOUS POINTER ADJUSTMENT PATTERN
Repeating 87-3 Pattern (see below)
Pointer Adjustment Events
Initialization
Measurement Period
87-3 Pattern
87 Pointer Adjustment Events
No Pointer Adjustments
T
NOTE: T ranges from 34ms to 10s (Req) T ranges from 7.5ms to 34ms (Obj)
Telcordia GR-253-CORE defines an "87-3 Continuous" Pointer Adjustment pattern, as a repeating sequence of 90 pointer adjustment events. Within this 90 pointer adjustment event, 87 pointer adjustments are actually executed. The remaining 3 pointer adjustments are never executed. The spacing between individual pointer adjustment events (within this scenario) can range from 7.5ms to 10seconds. Telcordia GR-253-CORE mandates that the Intrinsic Jitter, within the DS3 signal that is de-mapped from a SONET signal, which is experiencing the "87-3 Continuous" pattern of Pointer Adjustments, must not exceed 1.0UI-pp. 8.5.6 87-3 Add Figure 59 presents an illustration of the "87-3 Add Pattern" Pointer Adjustment Scenario per Telcordia GR-253CORE.
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FIGURE 59. ILLUSTRATION OF THE 87-3 ADD POINTER ADJUSTMENT PATTERN
Added Pointer Adjustment No Pointer Adjustments 43 Pointer Adjustments 43 Pointer Adjustments
T
t
Telcordia GR-253-CORE defines an "87-3 Add" Pointer Adjustment, as the "87-3 Continuous" Pointer Adjustment pattern, with an additional pointer adjustment inserted, as shown above in Figure 59. Telcordia GR-253-CORE mandates that the Intrinsic Jitter, within the DS3 signal that is de-mapped from a SONET signal, which is experiencing the "87-3 Add" pattern of Pointer Adjustments, must not exceed 1.3UIpp. 8.5.7 87-3 Cancel Figure 60 presents an illustration of the 87-3 Cancel Pattern Pointer Adjustment Scenario per Telcordia GR253-CORE. FIGURE 60. ILLUSTRATION OF 87-3 CANCEL POINTER ADJUSTMENT SCENARIO
86 or 87 Pointer Adjustments
No Pointer Adjustments
T
Cancelled Pointer Adjustment
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER Telcordia GR-253-CORE defines an "87-3 Cancel" Pointer Adjustment, as the "87-3 Continuous" Pointer Adjustment pattern, with an additional pointer adjustment cancelled (or not executed), as shown above in Figure 60. Telcordia GR-253-CORE mandates that the Intrinsic Jitter, within the DS3 signal that is de-mapped from a SONET signal, which is experiencing the "87-3 Cancel" pattern of Pointer Adjustments, must not exceed 1.3UI-pp. 8.5.8 Continuous Pattern Figure 61 presents an illustration of the "Continuous" Pointer Adjustment Scenario per Telcordia GR-253CORE. FIGURE 61. ILLUSTRATION OF CONTINUOUS PERIODIC POINTER ADJUSTMENT SCENARIO
Repeating Continuous Pattern (see below)
Pointer Adjustment Events
Initialization
Measurement Period T
Telcordia GR-253-CORE mandates that the Intrinsic Jitter, within the DS3 signal that is de-mapped from a SONET signal, which is experiencing the "Continuous" pattern of Pointer Adjustments, must not exceed 1.0UIpp. The spacing between individual pointer adjustments (within this scenario) can range from 7.5ms to 10s. 8.5.9 Continuous Add Figure 62 presents an illustration of the "Continuous Add Pattern" Pointer Adjustment Scenario per Telcordia GR-253-CORE.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
FIGURE 62. ILLUSTRATION OF CONTINUOUS-ADD POINTER ADJUSTMENT SCENARIO
Added Pointer Adjustment
Continuous Pointer Adjustments
Continuous Pointer Adjustments
T
t
Telcordia GR-253-CORE defines an "Continuous Add" Pointer Adjustment, as the "Continuous" Pointer Adjustment pattern, with an additional pointer adjustment inserted, as shown above in Figure 62. Telcordia GR-253-CORE mandates that the Intrinsic Jitter, within the DS3 signal that is de-mapped from a SONET signal, which is experiencing the "Continuous Add" pattern of Pointer Adjustments, must not exceed 1.3UI-pp. 8.5.10 Continuous Cancel Figure 63 presents an illustration of the "Continuous Cancel Pattern" Pointer Adjustment Scenario per Telcordia GR-253-CORE. FIGURE 63. ILLUSTRATION OF CONTINUOUS-CANCEL POINTER ADJUSTMENT SCENARIO
Continuous Pointer Adjustments
T
Cancelled Pointer Adjustment
112
XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER Telcordia GR-253-CORE defines a "Continuous Cancel" Pointer Adjustment, as the "Continuous" Pointer Adjustment pattern, with an additional pointer adjustment cancelled (or not executed), as shown above in Figure 63. Telcordia GR-253-CORE mandates that the Intrinsic Jitter, within the DS3 signal that is de-mapped from a SONET signal, which is experiencing the "Continuous Cancel" pattern of Pointer Adjustments, must not exceed 1.3UI-pp. 8.6 8.7
A Review of the DS3 Wander Requirements per ANSI T1.105.03b-1997. A Review of the Intrinsic Jitter and Wander Capabilities of the LIU in a typical system application
Intrinsic Jitter Test results
To be provided in the next revision of this data sheet.
The Intrinsic Jitter and Wander Test results are summarized in this section. 8.7.1 The Intrinsic Jitter Test results for the LIU in DS3 being de-mapped from SONET is summarized below in Table 2. TABLE 47: SUMMARY OF "CATEGORY I INTRINSIC JITTER TEST RESULTS" FOR SONET/DS3 APPLICATIONS
SCENARIO DESCRIPTION DS3 De-Mapping Jitter Single Pointer Adjustment Pointer Bursts Phase Transients 87-3 Pattern 87-3 Add 87-3 Cancel Continuous Pattern Continuous Add Continuous Cancel A1 SCENARIO NUMBER LIU INTRINSIC JITTER TEST RESULTS 0.13UI-pp TELCORDIA GR-253-CORE CATEGORY I INTRINSIC JITTER REQUIREMENTS 0.4UI-pp
0.201UI-pp
0.43UI-pp (e.g. 0.13UI-pp + 0.3UI-pp)
A2 A3 A4 A5 A5 A4
0.582UI-pp 0.526UI-pp 0.790UI-pp 0.926UI-pp 0.885UI-pp 0.497UI-pp
1.3UI-pp 1.2UI-pp 1.0UI-pp 1.3UI-pp 1.3UI-pp 1.0UI-pp
A5 A5
0.598UI-pp 0.589UI-pp
1.3UI-pp 1.3UI-pp
NOTES: 1. A detailed test report on our Test Procedures and Test Results is available and can be obtained by contacting your Exar Sales Representative. 2. These test results were obtained via the LIUs mounted on our XRT94L43 12-Channel DS3/E3/STS-1 Mapper Evaluation Board. 3. These same results apply to SDH/AU-3 Mapping applications.
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8.7.2 8.8 Wander Measurement Test Results Wander Measurement test results will be provided in the next revision of the LIU Data Sheet.
Designing with the LIU
In this section, we will discuss the following topics.
* How to design with and configure the LIU to permit a system to meet the above-mentioned Intrinsic Jitter and
Wander requirements.
* How is the LIU able to meet the above-mentioned requirements? * How does the LIU permits the user to comply with the SONET APS Recovery Time requirements of 50ms
(per Telcordia GR-253-CORE)?
* How should one configure the LIU, if one needs to support "Daisy-Chain" Testing at the end Customer's site?
8.8.1 How to design and configure the LIU to permit a system to meet the above-mentioned Intrinsic Jitter and Wander requirements
As mentioned earlier, in most application (in which the LIU will be used in a SONET De-Sync Application) the user will typically interface the LIU to a Mapper device in the manner as presented below in Figure 64. In this application, the Mapper has the responsibility of receiving a SONET STS-N/OC-N signal and extracting as many as N DS3 signals from this signal. As a given channel within the Mapper IC extracts out a given DS3 signal (from SONET) it will typically be applying a Clock and Data signal to the "Transmit Input" of the LIU IC. Figure 64 presents a simple illustration as to how one channel, within the LIU should be connected to the Mapper IC. FIGURE 64. ILLUSTRATION OF THE LIU BEING CONNECTED TO A MAPPER IC FOR SONET DE-SYNC APPLICATIONS
De-Mapped (Gapped) DS3 Data and Clock
TPDATA_n input pin
STS-N Signal
DS3 to STS-N DS3 to STS-N Mapper/ Mapper/ Demapper Demapper IC IC
LIU LIU
TCLK n input
As mentioned above, the Mapper IC will typically output a Clock and Data signal to the LIU. In many cases, the Mapper IC will output the contents of an entire STS-1 data-stream via the Data Signal to the LIU. However, the Mapper IC typically only supplies a clock pulse via the Clock Signal to the LIU coincident to whenever a DS3 bit is being output via the Data Signal. In this case, the Mapper IC would not supply a clock edge coincident to when a TOH, POH or any non-DS3 data-bit is being output via the Data-Signal. Figure 64 indicates that the Data Signal from the Mapper device should be connected to the TPDATA_n input pin of the LIU IC and that the Clock Signal from the Mapper device should be connected to the TCLK_n input pin of the LIU IC. In this application, the LIU has the following responsibilities.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
* Using a particular clock edge within the "gapped" clock signal (from the Mapper IC) to sample and latch the
value of each DS3 data-bit that is output from the Mapper IC.
* To (through the user of the Jitter Attenuator block) attenuate the jitter within this "DS3 data" and "clock signal"
that is output from the Mapper IC.
* To convert this "smoothed" DS3 data and clock into industry-compliant DS3 pulses, and to output these
pulses onto the line. To configure the LIU to operate in the correct mode for this application, the user must execute the following configuration steps. a. Configure the LIU to operate in the DS3 Mode The user can configure a given channel (within the LIU) to operate in the DS3 Mode, by executing either of the following steps.
* If the LIU has been configured to operate in the Host Mode
The user can accomplish this by setting both Bits 2 (E3_n) and Bits 1 (STS-1/DS3*_n), within each of the "Channel Control Registers" to "0" as depicted below.
CHANNEL CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X06 CHANNEL 1 ADDRESS LOCATION = 0X0E CHANNEL 2 ADDRESS LOCATION = 0X16
BIT 7 Unused R/O 0 R/O 0 BIT 6 BIT 5 PRBS Enable Ch_n R/W 0 BIT 4 RLB_n R/W 0 BIT 3 LLB_n R/W 0 BIT 2 E3_n R/W 0 BIT 1 STS-1/DS3_n R/W 0 BIT 0 SR/DR_n R/W 0
* If the LIU has been configured to operate in the Hardware Mode
The user can accomplish this by pulling all of the following input pins "Low". Pin 76 - E3_0 Pin 94 - E3_1 Pin 85 - E3_2 Pin 72 - STS-1/DS3_0 Pin 98 - STS-1/DS3_1 Pin 81 - STS-1/DS3_2 b. Configure the LIU to operate in the Single-Rail Mode Since the Mapper IC will typically output a single "Data Line" and a "Clock Line" for each DS3 signal that it demaps from the incoming STS-N signal, it is imperative to configure each channel within the LIU to operate in the Single Rail Mode. The user can accomplish this by executing either of the following steps.
* If the LIU has been configured to operate in the Host Mode
The user can accomplish this by setting Bit 0 (SR/DR*), within the each of the "Channel Control" Registers to 1, as illustrated below.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
CHANNEL CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X06 CHANNEL 1 ADDRESS LOCATION = 0X0E CHANNEL 2 ADDRESS LOCATION = 0X16
BIT 7 Unused BIT 6 BIT 5 PRBS Enable Ch_n R/O 0 R/W 0 BIT 4 RLB_n BIT 3 LLB_n BIT 2 E3_n BIT 1 STS-1/ BIT 0 SR/DR_n
DS3_n
R/W 0 R/W 0 R/W 0 R/W 0 R/W 1
R/O 0
* If the LIU has been configured to operate in the Hardware Mode
Then the user should tie pin 65 (SR/DR*) to "High". c. Configure each of the channels within the LIU to operate in the SONET De-Sync Mode The user can accomplish this by executing either of the following steps.
* If the LIU has been configured to operate in the Host Mode.
Then the user should set Bit D2 (JA0) to "0" and Bit D0 (JA1) to "1", within the Jitter Attenuator Control Register, as depicted below. JITTER ATTENUATOR CONTROL REGISTER - (CHANNEL 0 ADDRESS LOCATION = 0X07 CHANNEL 1 ADDRESS LOCATION = 0X0F CHANNEL 2 ADDRESS LOCATION = 0X17
BIT 7 BIT 6 Unused BIT 5 BIT 4 SONET APS Recovery Time DisableCh_n R/O 0 R/W 0 BIT 3 JA RESET Ch_n BIT 2 JA1 Ch_n BIT 1 JA in Tx Path Ch_n BIT 0 JA0 Ch_n
R/O 0
R/O 0
R/W 0
R/W 0
R/W 0
R/W 1
* If the LIU has been configured to operate in the Hardware Mode
Then the user should tie pin 44 (JA0) to a logic "HIGH" and pin 42 (JA1) to a logic "LOW". Once the user accomplishes either of these steps, then the Jitter Attenuator (within the LIU) will be configured to operate with a very narrow bandwidth. d. Configure the Jitter Attenuator (within each of the channels) to operate in the Transmit Direction. The user can accomplish this by executing either the following steps.
* If the LIU has been configured to operate in the Host Mode.
Then the user should be Bit D1 (JATx/JARx*) to "1", within the Jitter Attenuator Control Register, as depicted below.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER JITTER ATTENUATOR CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X07 CHANNEL 1 ADDRESS LOCATION = 0X0F CHANNEL 2 ADDRESS LOCATION = 0X17
BIT 7 BIT 6 Unused BIT 5 BIT 4 SONET APS Recovery Time DisableCh_n R/O 0 R/W 0 BIT 3 JA RESET Ch_n BIT 2 JA1 Ch_n BIT 1 JA in Tx Path Ch_n BIT 0 JA0 Ch_n
R/O 0
R/O 0
R/W 0
R/W 0
R/W 1
R/W 1
* If the LIU has been configured to operate in the Hardware Mode.
Then the user should tie pin 43 (JATx/JARx*) to "1". e. Enable the "SONET APS Recovery Time" Mode Finally, if the user intends to use the LIU in an Application that is required to reacquire proper SONET and DS3 traffic, prior within 50ms of an APS (Automatic Protection Switching) event (per Telcordia GR-253-CORE), then the user should set Bit 4 (SONET APS Recovery Time Disable), within the "Jitter Attenuator Control" Register, to "0" as depicted below. JITTER ATTENUATOR CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X07 CHANNEL 1 ADDRESS LOCATION = 0X0F CHANNEL 2 ADDRESS LOCATION = 0X17
BIT 7 BIT 6 Unused BIT 5 BIT 4 SONET APS Recovery Time DisableCh_n R/O 0 R/W 0 BIT 3 JA RESET Ch_n BIT 2 JA1 Ch_n BIT 1 JA in Tx Path Ch_n BIT 0 JA0 Ch_n
R/O 0
R/O 0
R/W 0
R/W 0
R/W 0
R/W 1
NOTES: 1. The ability to disable the "SONET APS Recovery Time" mode is only available if the LIU is operating in the Host Mode. If the LIU is operating in the "Hardware" Mode, then this "SONET APS Recovery Time Mode" feature will always be enabled. 2. The "SONET APS Recovery Time" mode will be discussed in greater detail in "Section 8.8.3, How does the LIU permit the user to comply with the SONET APS Recovery Time requirements of 50ms (per Telcordia GR-253CORE)?" on page 121.
8.8.2
Recommendations on Pre-Processing the Gapped Clocks (from the Mapper/ASIC Device) prior to routing this DS3 Clock and Data-Signals to the Transmit Inputs of the LIU
In order to minimize the effects of "Clock-Gapping" Jitter within the DS3 signal that is ultimately transmitted to the DS3 Line (or facility), we recommend that some "pre-processing" of the "Data-Signals" and "Clock-Signals" (which are output from the Mapper device) be implemented prior to routing these signals to the "Transmit Inputs" of the LIU. 8.8.2.1
SOME NOTES PRIOR TO STARTING THIS DISCUSSION:
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
Our simulation results indicate that Jitter Attenuator PLL (within the LIU LIU IC) will have no problem handling and processing the "Data-Signal" and "Clock-Signal" from a Mapper IC/ASIC if no pre-processing has been performed on these signals. In order words, our simulation results indicate that the Jitter Attenuator PLL (within the LIU IC) will have no problem handling the "worst-case" of 59 consecutive bits of no clock pulses in the "Clock-Signal (due to the Mapper IC processing the TOH bytes, an Incrementing Pointer-Adjustmentinduced "stuffed-byte", the POH byte, and the two fixed-stuff bytes within the STS-1 SPE, etc), immediately followed be processing clusters of DS3 data-bits (as shown in Figure 44) and still comply with the "Category I Intrinsic Jitter Requirements per Telcordia GR-253-CORE for DS3 applications.
NOTE: If this sort of "pre-processing" is already supported by the Mapper device that you are using, then no further action is required by the user.
8.8.2.2
OUR PRE-PROCESSING RECOMMENDATIONS
For the time-being, we recommend that the customer implement the "pre-processing" of the DS3 "Data-Signal" and "Clock-Signal" as described below. Currently we are aware that some of the Mapper products on the Market do implement this exact "pre-processing" algorithm. However, if the customer is implementing their Mapper Design in an ASIC or FPGA solution, then we strongly recommend that the user implement the necessary logic design to realize the following recommendations. Some time ago, we spent some time, studying (and then later testing our solution with) the PM5342 OC-3 to DS3 Mapper IC from PMC-Sierra. In particular, we wanted to understand the type of "DS3 Clock" and "Data" signal that this DS3 to OC-3 Mapper IC outputs. During this effort, we learned the following. 1. This "DS3 Clock" and "Data" signal, which is output from the Mapper IC consists of two major "repeating" patterns (which we will refer to as "MAJOR PATTERN A" and "MAJOR PATTERN B". The behavior of each of these patterns is presented below.
MAJOR PATTERN A MAJOR PATTERN A consists of two "sub" or minor-patterns, (which we will refer to as "MINOR PATTERN P1 and P2). MINOR PATTERN P1 consists of a string of seven (7) clock pulses, followed by a single gap (no clock pulse). An illustration of MINOR PATTERN P1 is presented below in Figure 65. FIGURE 65. ILLUSTRATION OF MINOR PATTERN P1
Missing Clock Pulse
1
2
3
4
5
6
7
It should be noted that each of these clock pulses has a period of approximately 19.3ns (or has an "instantaneously frequency of 51.84MHz). MINOR Pattern P2 consists of string of five (5) clock pulses, which is also followed by a single gap (no clock pulse). An illustration of Pattern P2 is presented below in Figure 66.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER FIGURE 66. ILLUSTRATION OF MINOR PATTERN P2
Missing Clock Pulse
1
2
3
4
5
HOW MAJOR PATTERN A IS SYNTHESIZED MAJOR PATTERN A is created (by the Mapper IC) by:
* Repeating MINOR PATTERN P1 (e.g., 7 clock pulses, followed by a gap) 63 times. * Upon completion of the 63rd transmission of MINOR PATTERN P1, MINOR PATTERN P2 is transmitted
repeatedly 36 times. Figure 67 presents an illustration which depicts the procedure that is used to synthesize MAJOR PATTERN A FIGURE 67. ILLUSTRATION OF PROCEDURE WHICH IS USED TO SYNTHESIZE MAJOR PATTERN A
Repeats 63 Times MINOR PATTERN P1
Repeats 36 Times MINOR PATTERN P2
Hence, MAJOR PATTERN A consists of "(63 x 7) + (36 x 5)" = 621 clock pulses. These 621 clock pulses were delivered over a period of "(63 x 8) + (36 x 6)" = 720 STS-1 (or 51.84MHz) clock periods. MAJOR PATTERN B MAJOR PATTERN B consists of three sub or minor-patterns (which we will refer to as "MINOR PATTERNS P1, P2 and P3). MINOR PATTERN P1, which is used to partially synthesize MAJOR PATTERN B, is exactly the same "MINOR PATTERN P1" as was presented above in Figure 37. Similarly, the MINOR PATTERN P2, which is also used to partially synthesize MAJOR PATTERN B, is exactly the same "MINOR PATTERN P2" as was presented in Figure 38. MINOR PATTERN P3 (which has yet to be defined) consists of a string of six (6) clock pulses, which contains no gaps. An illustration of MINOR PATTERN P3 is presented below in Figure 68.
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
FIGURE 68. ILLUSTRATION OF MINOR PATTERN P3
1
2
3
4
5
6
HOW MAJOR PATTERN B IS SYNTHESIZED MAJOR PATTERN B is created (by the Mapper IC) by:
* Repeating MINOR PATTERN P1 (e.g., 7 clock pulses, followed by a gap) 63 times. * Upon completion of the 63rd transmission of MINOR PATTERN P1, MINOR PATTERN P2 is transmitted
repeatedly 36 times.
* pon completion of the 35th transmission of MINOR PATTERN P2, MINOR PATTERN P3 is transmitted once.
Figure 69 presents an illustration which depicts the procedure that is used to synthesize MAJOR PATTERN B. FIGURE 69. ILLUSTRATION OF PROCEDURE WHICH IS USED TO SYNTHESIZE PATTERN B
Transmitted 1 Time Repeats 63 Times PATTERN P1 Repeats 35 Times PATTERN P2 PATTERN P3
Hence, MAJOR PATTERN B consists of "(63 x 7) + (35 x 5)" + 6 = 622 clock pulses. These 622 clock pulses were delivered over a period of "(63 x 8) + (35 x 6) + 6 = 720 STS-1 (or 51.84MHz) clock periods. PUTTING THE PATTERNS TOGETHER Finally, the DS3 to OC-N Mapper IC clock output is reproduced by doing the following.
* MAJOR PATTERN A is transmitted two times (repeatedly). * After the second transmission of MAJOR PATTERN A, MAJOR PATTERN B is transmitted once. * Then the whole process repeats.
Throughout the remainder of this document, we will refer to this particular pattern as the "SUPER PATTERN". Figure 70 presents an illustration of this "SUPER PATTERN" which is output via the Mapper IC.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER FIGURE 70. ILLUSTRATION OF THE SUPER PATTERN WHICH IS OUTPUT VIA THE "OC-N TO DS3" MAPPER IC
PATTERN A
PATTERN A
PATTERN B
CROSS-CHECKING OUR DATA
* Each SUPER PATTERN consists of (621 + 621 + 622) = 1864 clock pulses. * The total amount of time, which is required for the "DS3 to OC-N Mapper" IC to transmit this SUPER
PATTERN is (720 + 720 + 720) = 2160 "STS-1" clock periods.
* This amount to a period of (2160/51.84MHz) = 41,667ns. * In a period of 41, 667ns, the LIU (when configured to operate in the DS3 Mode), will output a total (41,667ns
x 44,736,000) = 1864 uniformly spaced DS3 clock pulses.
* Hence, the number of clock pulses match.
APPLYING THE SUPER PATTERN TO THE LIU Whenever the LIU is configured to operate in a "SONET De-Sync" application, the device will accept a continuous string of the above-defined SUPER PATTERN, via the TCLK input pin (along with the corresponding data). The channel within the LIU (which will be configured to operate in the "DS3" Mode) will output a DS3 line signal (to the DS3 facility) that complies with the "Category I Intrinsic Jitter Requirements per Telcordia GR-253-CORE (for DS3 applications). This scheme is illustrated below in Figure 71. FIGURE 71. SIMPLE ILLUSTRATION OF THE LIU BEING USED IN A SONET DE-SYNCHRONIZER" APPLICATION
De-Mapped (Gapped) DS3 Data and Clock
TPDATA_n input pin
STS-N Signal
DS3 to STS-N DS3 to STS-N Mapper/ Mapper/ Demapper Demapper IC IC
LIU LIU
TCLK_n input
8.8.3
How does the LIU permit the user to comply with the SONET APS Recovery Time requirements of 50ms (per Telcordia GR-253-CORE)?
Telcordia GR-253-CORE, Section 5.3.3.3 mandates that the "APS Completion" (or Recovery) time be 50ms or less. Many of our customers interpret this particular requirement as follows. "From the instant that an APS is initiated on a high-speed SONET signal, all lower-speed SONET traffic (which is being transported via this "high-speed" SONET signal) must be fully restored within 50ms. Similarly, if the "high-speed" SONET signal is transporting some PDH signals (such as DS1 or DS3, etc.), then those entities
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
that are responsible for acquiring and maintaining DS1 or DS3 frame synchronization (with these DS1 or DS3 data-streams that have been de-mapped from SONET) must have re-acquired DS1 or DS3 frame synchronization within 50ms" after APS has been initiated." The LIU was designed such that the DS3 signals that it receives from a SONET Mapper device and processes will comply with the Category I Intrinsic Jitter requirements per Telcordia GR-253-CORE. Reference 1 documents some APS Recovery Time testing, which was performed to verify that the Jitter Attenuator blocks (within the LIU) device that permit it to comply with the Category I Intrinsic Jitter Requirements (for DS3 Applications) per Telcordia GR-253-CORE, do not cause it to fail to comply with the "APS Completion Time" requirements per Section 5.3.3.3 of Telcordia GR-253-CORE. However, Table 3 presents a summary of some APS Recovery Time requirements that were documented within this test report. Table 3, TABLE 48: MEASURED APS RECOVERY TIME AS A FUNCTION OF DS3 PPM OFFSET
DS3 PPM OFFSET (PER W&G ANT-20SE) -99 ppm -40ppm -30 ppm -20 ppm -10 ppm 0 ppm +10 ppm +20 ppm +30 ppm +40 ppm +99 ppm MEASURED APS RECOVERY TIME (PER LOGIC ANALYZER) 1.25ms 1.54ms 1.34ms 1.49ms 1.30ms 1.89ms 1.21ms 1.64ms 1.32ms 1.25ms 1.35ms
NOTE: The APS Completion (or Recovery) time requirement is 50ms.
Configuring the LIU to be able to comply with the SONET APS Recovery Time Requirements of 50ms Quite simply, the user can configure a given Jitter Attenuator block (associated with a given channel) to (1) comply with the "APS Completion Time" requirements per Telcordia GR-253-CORE, and (2) also comply with the "Category I Intrinsic Jitter Requirements per Telcordia GR-253-CORE (for DS3 applications) by making sure that Bit 4 (SONET APS Recovery Time Disable Ch_n), within the Jitter Attenuator Control Register is set to "0" as depicted below. JITTER ATTENUATOR CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X07 CHANNEL 1 ADDRESS LOCATION = 0X0F CHANNEL 2 ADDRESS LOCATION = 0X17
BIT 7 BIT 6 Unused BIT 5 BIT 4 SONET APS Recovery Time Disable Ch_n BIT 3 JA RESET Ch_n BIT 2 JA1 Ch_n BIT 1 JA in Tx Path Ch_n BIT 0 JA0 Ch_n
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER JITTER ATTENUATOR CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X07 CHANNEL 1 ADDRESS LOCATION = 0X0F CHANNEL 2 ADDRESS LOCATION = 0X17
BIT 7 R/O 0 BIT 6 R/O 0 BIT 5 R/O 0 BIT 4 R/W 0 BIT 3 R/W 0 BIT 2 R/W 0 BIT 1 R/W 1 BIT 0 R/W 1
NOTE: The user can only disable the "SONET APS Recovery Time Mode" if the LIU is operating in the Host Mode. If the user is operating the LIU in the Hardware Mode, then the user will have NO ability to disable the "SONET APS Recovery Time Mode" feature.
8.8.4
How should one configure the LIU, if one needs to support "Daisy-Chain" Testing at the end Customer's site?
Daisy-Chain testing is emerging as a new requirements that many of our customers are imposing on our SONET Mapper and LIU products. Many System Designer/Manufacturers are finding out that whenever their end-customers that are evaluating and testing out their systems (in order to determine if they wish to move forward and start purchasing this equipment in volume) are routinely demanding that they be able to test out these systems with a single piece of test equipment. This means that the end-customer would like to take a single piece of DS3 or STS-1 test equipment and (with this test equipment) snake the DS3 or STS-1 traffic (that this test equipment will generate) through many or (preferably all) channels within the system. For example, we have had request from our customers that (on a system that supports OC-192) our silicon be able to support this DS3 or STS-1 traffic snaking through the 192 DS3 or STS-1 ports within this system. After extensive testing, we have determined that the best approach to complying with test "Daisy-Chain" Testing requirements, is to configure the Jitter Attenuator blocks (within each of the Channels within the LIU) into the "32-Bit" Mode. The user can configure the Jitter Attenuator block (within a given channel of the LIU) to operate in this mode by settings in the table below. JITTER ATTENUATOR CONTROL REGISTER - CHANNEL 0 ADDRESS LOCATION = 0X07 CHANNEL 1 ADDRESS LOCATION = 0X0F CHANNEL 2 ADDRESS LOCATION = 0X17
BIT 7 BIT 6 Unused BIT 5 BIT 4 SONET APS Recovery Time Disable Ch_n R/O 0 R/W 0 BIT 3 JA RESET Ch_n BIT 2 JA1 Ch_n BIT 1 JA in Tx Path Ch_n BIT 0 JA0 Ch_n
R/O 0
R/O 0
R/W 0
R/W 1
R/W 1
R/W 0
REFERENCES 1. TEST REPORT - AUTOMATIC PROTECTION SWITCHING (APS) RECOVERY TIME TESTING WITH THE XRT94L43 DS3/E3/STS-1 TO STS-12 MAPPER IC - Revision C Silicon
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
9.0 ELECTRICAL CHARACTERISTICS TABLE 49: ABSOLUTE MAXIMUM RATINGS
SYMBOL
PARAMETER Supply Voltage Input Voltage at any Pin Input current at any pin Storage Temperature Ambient Operating Temperature Thermal Resistance
MIN
MAX
UNITS
COMMENTS
VDD VIN IIN STEMP ATEMP Theta JA
-0.5 -0.5
6.0 5.5 100
V V mA
0 0 0
Note 1 Note 1 Note 1 Note 1 linear airflow 0 ft./min linear air flow 0ft/min (See Note 3 below)
-65 -40
150 85 23
C C
C/W
MLEVL
Exposure to Moisture
5
level
EIA/JEDEC JESD22-A112-A
ESD
ESD Rating
2000
V
Note 2
NOTES: 1. Exposure to or operating near the Min or Max values for extended period may cause permanent failure and impair reliability of the device. 2. ESD testing method is per MIL-STD-883D,M-3015.7 3. With Linear Air flow of 200 ft/min, reduce Theta JA by 20%, Theta JC is unchanged.
TABLE 50: DC ELECTRICAL CHARACTERISTICS:
SYMBOL
PARAMETER Digital Supply Voltage Analog Supply Voltage Supply current requirements Power Dissipation Input Low Voltage Input High Voltage Output Low Voltage, IOUT = - 4mA Output High Voltage, IOUT = 4 mA Input Leakage Current1 Input Capacitance Load Capacitance
MIN.
TYP.
MAX.
UNITS
DVDD AVDD ICC PDD VIL VIH VOL VOH IL CI CL
3.135 3.135
3.3 3.3 TBD TBD
3.465 3.465 TBD TBD 0.8
V V mA W V V V V
2.0
5.5 0.4
2.4 10 10 10
A pF pF
NOTES: 1. Not applicable for pins with pull-up or pull-down resistors. 2. The Digital inputs are TTL 5V compliant.
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XRT75R12D PRELIMINARY REV. P1.0.1 TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER
ORDERING INFORMATION
PART NUMBER XRT75R12DIB PACKAGE 420 TBGA OPERATING TEMPERATURE RANGE -40C to +85C
PACKAGE DIMENSIONS 420 Tape Ball Grid Array (35 mm x 35 mm, TBGA)
Rev. 1.00
26 25
24 23
22 21
20 19
18 17
16 15
14 13
12 11
10 9
8 7
6 5
4 3
2 1 A
A1 FEATURE/MARK
B C D E F G H J K L M
D
D1
N P R T U V W Y AA AB AC AD AE AF
e D1 D
(A1 corner feature is mfger option)
SYMBOL A A1 A2 D D1 b e P
INCHES MIN MAX 0.051 0.067 0.020 0.028 0.031 0.039 1.370 1.386 1.5000 BSC 0.024 0.035 0.0500 BSC 0.006 0.012
MILLIMETERS MIN MAX 1.30 1.70 0.50 0.70 0.80 1.00 34.80 35.20 38.10 BSC 0.60 0.90 1.27 BSC 0.15 0.30
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PRELIMINARY XRT75R12D TWELVE CHANNEL E3/DS3/STS-1 LINE INTERFACE UNIT WITH SONET DESYNCHRONIZER REV. P1.0.1
REVISIONS
REVISION P1.0.0 P1.0.1 DATE 09/22/03 10/30/03 Original Added Pull-Up resistor information for RDY and INT. COMMENTS
NOTICE
EXAR Corporation reserves the right to make changes to the products contained in this publication in order to improve design, performance or reliability. EXAR Corporation assumes no responsibility for the use of any circuits described herein, conveys no license under any patent or other right, and makes no representation that the circuits are free of patent infringement. Charts and schedules contained here in are only for illustration purposes and may vary depending upon a user's specific application. While the information in this publication has been carefully checked; no responsibility, however, is assumed for inaccuracies. EXAR Corporation does not recommend the use of any of its products in life support applications where the failure or malfunction of the product can reasonably be expected to cause failure of the life support system or to significantly affect its safety or effectiveness. Products are not authorized for use in such applications unless EXAR Corporation receives, in writing, assurances to its satisfaction that: (a) the risk of injury or damage has been minimized; (b) the user assumes all such risks; (c) potential liability of EXAR Corporation is adequately protected under the circumstances. Copyright 2003 EXAR Corporation Datasheet October 2003. Reproduction, in part or whole, without the prior written consent of EXAR Corporation is prohibited.
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