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GB/T 39352-2020Space data and information transfer systems. Proximity space link protocol. Data link layer (English PDF)

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Issued by

State Administration for Market Regulation, China National Standardization Administration

Level / Type

National · Recommended

Issue date

November 19, 2020

Implementation date

June 1, 2021

Scope

GB/T 39352-2020 (Space data and information transfer systems. Proximity space link protocol. Data link layer) is available as an English-translated PDF.

GB/T 39352-2020 — This standard specifies the general rules and protocol data sheet of the data link layer in the adjacent space link protocol of space data and information transmission systems: Meta, data link layer structure, time service, data service operation, communication operating procedures (COP-P) and I/O sub-layer operation: This standard applies to communications between adjacent spacecraft: It is recommended to be used together with GB/T 39354 and GB/T 39353-2020:

Document preview — GB/T 39352-2020

National Standard of the People's Republic of China

ICS
49.140
Classification
V 75

Issued by: State Administration for Market Regulation, China National Standardization Administration

Contents

  • 1 Scope1
  • 2 Normative references1
  • 3 Terms and definitions1
  • 4 Abbreviations3
  • 5 General4
  • 5:1 Bit number convention4
  • 5:2 Information rate agreement5
  • 5:3 Adjacent space link model5
  • 5:4 Basic principles of adjacent space link protocol7
  • 6 Protocol data unit10
  • 6:1 Overview10
  • 6:2 Adjacent space link transmission frame11
  • 7 Data link layer structure18
  • 7:1 Overview18
  • 7:2 Synchronization and coding sublayer20
  • 7:3 Data frame sublayer20
  • 7:4 Media Access Control Sublayer21
  • 7:5 Data Service Sublayer22
  • 7:6 I/O sublayer23
  • 8 Time business25
  • 8:1 Overview25
  • 8:2 Transmission frame time label record25
  • 8:3 Time related process26
  • 8:4 Transmission time to remote node26
  • 9 Data Service Operation27
  • 9:1 Overview27
  • 9:2 Adjacent space link state table28
  • 9:3 Factors and events affecting status36
  • 9:4 State transition table and state transition diagram39
  • 9:5 Physical layer interface51
  • 9:6 Send operation51
  • 9:7 Receive operation52
  • 10 Communication Operating Regulations (COP-P)53
  • 10:1 Overview53
  • 10:2 Sending Procedure (FOP-P)53
  • 10:3 Receiving Procedure (FARM-P)58
  • 11 I/O sublayer operations60
  • 11:1 Overview60
  • 11:2 Send operation60
  • 11:3 Receive operation60
  • Appendix A (informative appendix) Structural changes of this standard compared with ISO 22663:201561
  • Appendix B (informative appendix) The technical differences between this standard and ISO 22663:2015 and the reasons63
  • Appendix C (Normative Appendix) Variable Length Management Protocol Data Field Format64
  • C:1 SPDU Type 1: Command/Report/PLCWSPDU Data Field64
  • C:2 SPDU Type 2: Time Distribution SPDU Data Field77
  • Appendix D (Normative Appendix) Management Information Base Parameters79
  • Appendix E (Normative Appendix) Notice to Spacecraft Controller81
  • Appendix F (Normative Appendix) Security Considerations82
  • F:1 Security background82
  • F:2 Security Concerns82
  • F:3 Potential threats and attack scenarios82
  • F:4 Consequences of not taking safety measures82
  • Figure 1 The convention of bit number5
  • Figure 2 Schematic diagram of the measurement positions of different information rates5
  • Figure 3 Adjacent space link model structure6
  • Figure 4 The relationship between adjacent space link transmission frame and PLTU11
  • Figure 5 Adjacent space link transmission frame structure11
  • Figure 6 Transmission frame header format12
  • Figure 7 U-frame data field structure15
  • Figure 8 PLCW structure diagram17
  • Figure 9 Hierarchical structure of adjacent space link protocol Figure19
  • Figure 10 Configuration of COP-P23
  • Figure 11 Time label record of adjacent space link protocol26
  • Figure 12 Transmission time to remote node27
  • Figure 13 Full duplex mode state transition Figure40
  • Figure 14 Half-duplex mode state transition Figure45
  • Figure 15 Simplex mode state transition Figure46
  • Figure 16 COP-P process54
  • Figure 17 FOP-P state diagram58
  • Figure 18 FARM-P state diagram59
  • Figure C:1 SPDU type 1 data field content64
  • Figure C:2 Set transmitter parameter command65
  • Figure C:3 Set control parameter command68
  • Figure C:4 Set receiver parameter command70
  • Figure C:5 Set V(R) command71
  • Figure C:6 Report request72
  • Figure C:7 Set physical layer extension command73
  • Figure C:8 Source SCID report composition structure77
  • Figure C:9 Type 2 SPDU data field content78
  • Table 1 U-frame data field content category definition13
  • Table 2 Setting of SCID and source/destination identification in the generation stage of transmission frame14
  • Table 3 The relationship between the behavior of the receiving end node and the SCID, source/destination identification14
  • Table 4 Segment header sequence identification15
  • Table 5 Fixed-length SPDU16
  • Table 6 Variable length SPDU18
  • Table 7 Index of adjacent space link data service operations28
  • Table 8 Status unrelated to DUPLEX variables (shared status)28

Foreword

This standard was drafted in accordance with the rules given in GB/T 1:1-2009:

This standard uses the redrafting method to modify and adopt ISO 22663:2015 "Space Data and Information Transmission System Proximity-1 Space Link Agreement"

Discussion on the Data Link Layer:

Compared with ISO 22663:2015, this standard has many adjustments in structure: Appendix A lists this standard and ISO 22663:2015:

The chapter number comparison list:

Compared with ISO 22663:2015, there are technical differences between this standard, and the clauses involved in these differences have been passed on the outer margins:

The vertical single line (︱) is marked, and a list of the corresponding technical differences and their reasons is given in Appendix B:

This standard also made the following editorial changes:

---Modified the standard name: the original name "spatial data and information transmission system adjacent-1 space link protocol data link layer"

Changed to "Space Data and Information Transmission System Adjacent Space Link Protocol Data Link Layer";

--- Deleted part of the document structure and references in Chapter 1 of ISO 22663:2015;

--- Deleted Appendix F of ISO 22663:2015 "NASA Mars Survey Program:2001 Orbiter Close Space Link

ability";

--- Deleted Appendix G of ISO 22663:2015 "NASA Mars Reconnaissance Orbiter:2005 Neighboring Space Link Capability";

--- Deleted Appendix H "References" of ISO 22663:2015;

---Delete ISO 22663:2015 Appendix J "Proximity-1 Data Format Hierarchy":

This standard was proposed and managed by the National Aerospace Technology and Application Standardization Technical Committee (SAC/TC425):

Drafting organizations of this standard: Beijing Space Vehicle General Design Department, Beijing Institute of Control Engineering, Anhui China Institute of Standardization

Co:, Ltd:, China Aerospace Standardization Institute:

1 Scope

This standard specifies the general rules and protocol data sheet of the data link layer in the adjacent space link protocol of space data and information transmission systems:

Meta, data link layer structure, time service, data service operation, communication operating procedures (COP-P) and I/O sub-layer operation:

This standard applies to communications between adjacent spacecraft: It is recommended to be used together with GB/T 39354 and GB/T 39353-2020:

2 Normative references

The following documents are indispensable for the application of this document: For dated reference documents, only the dated version applies to this article

Pieces: For undated references, the latest version (including all amendments) applies to this document:

GB/T 39353-2020 Space Data and Information Transmission System Neighboring Space Link Protocol Synchronization and Coding Sublayer

(ISO 21459:2015, MOD)

GB/T 39354 Spatial Data and Information Transmission System Adjacent Space Link Protocol Physical Layer (GB/T 39354-2020,

ISO 21460:2015, MOD)

GB/T 39355 Spatial Data and Information Transmission System Time Code Format (GB/T 39355-2020, ISO 11104:2011,

MOD)

3 Terms and definitions

The following terms and definitions apply to this document:

3:1

Spacelink

A communication link between a spacecraft and the corresponding ground system or between two spacecraft:

Note: A space link contains one or more unidirectional or bidirectional physical channels:

3:2

Proximity space linkproximityspacelink

Proximity linkproximitylink

It is a communication link for direct communication between spacecraft in the distance range of 1m to 100000km:

Used for communication links between the main spacecraft and the auxiliary spacecraft:

Note: Short-distance, two-way, fixed or mobile radio frequency links are mainly used to carry out between detectors, landers, patrol devices, orbital constellations, and orbital repeaters:

Communication has the characteristics of small delay, medium signal energy (not weak signal), independent conversation and short time:

3:3

Asynchronous datalink

A data link composed of variable length and not necessarily continuous transmission PLTU:

3:4

Caller caler

The initiator of the adjacent space link establishment process and the management subject of the session negotiation process:

......
This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — all pages — is available in the English PDF.

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