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GB/T 43670-2024 English PDF

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GB/T 43670-2024EnglishRFQ ASK 3 days [Need to translate] Space data and information transfer systems - SpaceFibre data bus communication protocol on spacecraft Valid GB/T 43670-2024

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Basic data

Standard ID GB/T 43670-2024 (GB/T43670-2024)
Description (Translated English) Space data and information transfer systems - SpaceFibre data bus communication protocol on spacecraft
Sector / Industry National Standard (Recommended)
Classification of Chinese Standard V75
Classification of International Standard 49.140
Word Count Estimation 138,123
Date of Issue 2024-03-15
Date of Implementation 2024-07-01
Issuing agency(ies) State Administration for Market Regulation, China National Standardization Administration

GB/T 43670-2024: Space data and information transfer systems - SpaceFibre data bus communication protocol on spacecraft


---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
ICS 49.140 CCSV75 National Standards of People's Republic of China Space data and information transmission system Spacecraft SpaceFibre bus communication protocol Released on 2024-03-15 2024-07-01 Implementation State Administration for Market Regulation The National Standardization Administration issued

Table of Contents

Preface V 1 Scope 1 2 Normative references 1 3 Terms and Definitions 1 4 Abbreviations 4 5 General Principles 4 5.1 Protocol Stack 4 5.2 Topology 6 6 Business Definition 6 6.1 Business Description 6 6.2 Network layer services 7 6.3 Data Link Layer Services 7 6.4 Physical layer services 8 6.5 Management Information Base Services 8 7 Format Definition 8 7.1 8B/10B Encoding and Decoding 8 7.2 Control Word 11 7.3 Character 23 7.4 Frame Format 24 7.5 Data Packet Format 26 7.6 Control Word and Frame Priority 27 7.7 K code summary table 28 7.8 Summary table of control characters 28 8 Physical Layer Protocol 29 8.1 Physical layer functions 29 8.2 Serialization 30 9 Data Link Layer Protocol 31 9.1 Channel Sublayer Protocol 31 9.2 Multichannel Sublayer Protocol 44 9.3 Link Control Sublayer Protocol 55 10 Network Layer Protocol 79 10.1 Network Layer Functions 79 10.2 SpaceFibre Network 80 10.3 Virtual Network 81 10.4 Link 83 10.5 Sending Data Packets 83 10.6 Receiving Data Packets 83 10.7 Routing Switch 84 10.8 Packet Addressing 87 10.9 Group Adaptive Routing 89 10.10 Packet Multicast 89 10.11 Broadcast Message 89 10.12 SpaceFibre Node 90 10.13 SpaceFibre Unit 91 11 Management Information Base92 11.1 Management Information Base Function 92 11.2 Network Management 92 11.3 Configuration Parameters 92 11.4 Status parameters 95 12 Reliability Design 96 12.1 Service Quality Assurance Mechanism 96 12.2 FDIR Mechanism 97 Appendix A (Informative) SpaceFibre bus physical layer design reference 98 Appendix B (Normative) SpaceFibre Bus Communication Protocol Business Interface 120 Appendix C (Informative) SpaceFibre bus communication protocol CRC check code calculation 129 References 131 Figure 1 Schematic diagram of SpaceFibre bus protocol stack 5 Figure 2 SpaceFibre bus simplest network diagram 6 Figure 3 Schematic diagram of SpaceFibre bus complex network 6 Figure 4 Schematic diagram of D/K character representation of 8B/10B coding symbols 9 Figure 5 Padding character 24 at the end of the packet Figure 6 Padding characters 24 at the beginning and end of a packet Figure 7 Single channel data frame structure 25 Figure 8 Idle frame structure 26 Figure 9 Broadcast frame structure 26 Figure 10 SpaceFibre data packet format 27 Figure 11 Physical layer interface 30 Figure 12 Channel sublayer interface 32 of a single channel link Figure 13 Connection interface between multi-channel and channel sublayer 33 Figure 14 Channel initialization state machine 34 Figure 15 Receive synchronization state machine 43 Figure 16 Multi-channel sublayer interface 45 Figure 17 Multi-channel link with different number of channels at both ends 45 Figure 18 Words forming row 46 on a multi-channel link Figure 19.Data expansion on a multi-channel link 47 Figure 20 PAD control word padding in multi-channel links 47 Figure 21 Row alignment of multi-channel links 49 Figure 22 Alignment state machine 51 Figure 23 Multi-channel link with unidirectional channels 53 Figure 24 Link Control Sublayer Interface 56 Figure 25 Scrambler/Descrambler 64 Figure 26 Scrambling example of a short data frame 64 Figure 27 Idle frame scrambling effect 65 Figure 28 Bit order in 16-bit CRC calculation 67 Figure 29 Bit order in 8-bit CRC calculation 68 Figure 30 Receive Error State Machine 72 Figure 31 Data word recognition state machine 74 Figure 32 Link reset state machine 77 Figure 33 Network layer interface relationship 80 Figure 34 SpaceFibre network composition 81 Figure 35 Relationship of virtual networks 83 Figure 36 Composition of SpaceFibre routing switch 85 Figure 37 SpaceFibre node components and node instantiation 91 Figure 38 Components and instantiations of a SpaceFibre unit 92 Figure A.1 Schematic diagram of the electrical physical layer unidirectional structure 98 Figure A.2 Serial output signal 101 Figure A.3 Serial output test circuit 102 Figure A.4 Serial Eye Diagram Template 102 Figure A.5 Serial input signal 103 Figure A.6 Schematic diagram of a single channel of a flight cable assembly 106 Figure A.7 Flight connector adapter protector 107 Figure A.8 Schematic diagram of single channel connection of EGSE cable assembly 109 Figure A.9 Schematic diagram of EGSE to flight adapter cable assembly 110 Figure A.10 Unidirectional optical fiber physical layer structure composition 110 Figure A.11 Unidirectional optical fiber physical layer structure using active optical fiber 111 Figure A.12 Electrical-optical eye diagram template for 1Gbit/s~5Gbit/s transmitter 112 Figure A.13 Electrical-optical eye diagram template for 1Gbit/s~10Gbit/s transmitter 113 Figure A.14 A flying optical cable assembly comprising one channel 116 Figure A.15 Flying cable assembly containing multiple channels 117 Figure A.16 Flying cable assembly for asymmetric links 117 Figure A.17 Active optical cable assembly for flight 119 Figure C.1 CRC checksum calculation example for data frame 129 Figure C.2 Calculation example of CRC checksum for broadcast frame and FCT 130 Table 1 5B/6B encoding table (lower 5 bits encoding of 8-bit data) 10 Table 2 3B/4B encoding table (high 3 bits encoding of 8-bit data) 11 Table 3 Channel control word 11 Table 4 Multi-channel control word 16 Table 5 Data frame control word 17 Table 6 Flow Control Word 20 Table 7 Error recovery control word 21 Table 8 Receive error indication control word 23 Table 9 SpaceFibre standard character 23 Table 10 Fill control character 24 Table 11 K code summary table 28 Table 12 Summary of control character symbols 28 Table 13 Priority values of different QoS types60 Table 14 Routing switch address 85 Table 15 SpaceFibre configuration parameters 93 Table 16 SpaceFibre status parameters 95 Table A.1 Summary of control characters 99 Table A.2 1Gbit/s~3.125Gbit/s serial eye diagram template spacing 99 Table A.3 3.125Gbit/s~6.25Gbit/s serial eye diagram template spacing 100 Table A.4 Driver and receiver characteristics for 1 Gbit/s to 3.125 Gbit/s 100 Table A.5 Driver and receiver characteristics for 3.125 Gbit/s to 6.25 Gbit/s 101 Table A.6 Flight cable assembly connector contact terminal connection relationship 106 Table A.7 Flight connector adapter protector connector contact termination 107 Table A.8 EGSE cable assembly connector contact terminal connection relationship 109 Table A.9 EGSE to flight adapter cable assembly connector contact terminal connection relationship 109 Table A.10 Electro-optical characteristics of 1Gbit/s~5Gbit/s transmitter 112 Table A.11 Electro-optical characteristics of 1Gbit/s~10Gbit/s transmitter 113 Table A.12 Electro-optical characteristics of 1Gbit/s~5Gbit/s receiver 114 Table A.13 Electro-optical characteristics of 1Gbit/s~10Gbit/s receiver 115 Table A.14 Connector contact connection relationship for each SpaceFibre channel in the flying cable assembly 116 Table A.15 Signals per SpaceFibre channel in the Flying Active Optical Cable Assembly connector 118 Table A.16 Connector contact relationship for each SpaceFibre channel in a flying active optical cable assembly 119

Foreword

This document is in accordance with the provisions of GB/T 1.1-2020 "Guidelines for standardization work Part 1.Structure and drafting rules for standardization documents" Drafting. Please note that some of the contents of this document may involve patents. The issuing organization of this document does not assume the responsibility for identifying patents. This document was proposed and coordinated by the National Technical Committee for Standardization of Aerospace Technology and Its Applications (SAC/TC425). This document was drafted by. Beijing Space Vehicle General Design Department, China Academy of Space Technology, Beijing Institute of Microelectronics Technology, China Aerospace Standardization Research Institute, Xiamen Panchi Technology Research Institute Co., Ltd., State Grid Siji Location Services Co., Ltd., Zhejiang Huilong Chip Technology Co., Ltd. Limited company. The main drafters of this document are. Niu Yuehua, Wang Luyuan, Xu Zhihong, Li Xin, Liu Weiwei, Pang Yalong, Zhao Wenyan, Guo Hehe, Zhan Panpan, Tian Miaomiao, Wu Wei, Li Ke, Wang Wenping, Fei Haidong, Xu Dongyan, Wang Dan, Feng Guoping, Jiang Shuai, Zhang Yi, Guo Jiaxin, Xu Jieli, Zhao Guang, Gu Pilin. Space data and information transmission system Spacecraft SpaceFibre bus communication protocol

1 Scope

This document specifies the spacecraft SpaceFibre bus communication protocol business, data format, physical layer protocol, data link layer protocol, Network layer protocols, management information base, and reliability design. This document applies to the development and use of the SpaceFibre bus and its related equipment in spacecraft.

2 Normative references

The contents of the following documents constitute the essential clauses of this document through normative references in this document. For referenced documents without a date, only the version corresponding to that date applies to this document; for referenced documents without a date, the latest version (including all amendments) applies to This document. GB/T 42041 Aerospace terminology Space data and information transmission

3 Terms and definitions

The terms and definitions defined in GB/T 42041 and the following apply to this document. 3.1 Active Lane An active one-way channel or a two-way channel. 3.2 asymmetric link A link containing multiple channels in which one or more channels are unidirectional channels. 3.3 Available bandwidth availablebandwidth The number of data words and control words sent by all virtual channels in the link since the last update of bandwidth credits. 3.4 bandwidth utilization The percentage of bandwidth allocated to a virtual channel that has been used in the recent period. Note. When the bandwidth credit of a virtual channel reaches the upper or lower threshold, there is no need to calculate bandwidth utilization for a short period of time. 3.5 Bidirectional channel bi-directionallane An active channel for bidirectional information transmission on a link. 3.6 broadcastmessage 8 bytes of application data sent to each node on the network, and an 8-bit broadcast type identifier that indicates the meaning of the application data.