GB/T 39350-2020 in English
VALIDSpace data and information transfer systems—TC (telecommand) space data link protocol
- Issued on:2020-11-19
- Implemented on:2021-06-01
- File Format:PDF
- Delivery:Via email within 5 business days
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| Standard No: | GB/T 39350-2020 |
| Document status: | VALID |
| Title in English: | Space data and information transfer systems—TC (telecommand) space data link protocol |
| Title in Chinese: | 空间数据与信息传输系统 遥控空间数据链路协议 |
| Language: | English |
| File Format: | Electronic (PDF) |
| Delivery: | Via email within 5 business days |
| Issued on: | 2020-11-19 |
| Implemented on: | 2021-06-01 |
| ICS Classification: | 49.140-Space systems and operations |
| Chinese Classification: | V75-Spacecraft telemetering and remote sensing system |
| Professional Classification: | GB-National Standard |
| Related Keywords: | space data
protocol data unit data transmission service small data aggregation virtual channel data field |
| Related Topics: | Inter-assay difference of data
remote spatial data cavity data remote control cavity data space version data link GBT39350 GB/T 39350-2020 data link Information transfer Introverted space and extroverted space Lake spatial data production Agricultural spatial information standards and |
《GB/T 39350-2020空间数据与信息传输系统 遥控空间数据链路协议》由TC425(全国宇航技术及其应用标准化技术委员会)归口,TC425SC3(全国宇航技术及其应用标准化技术委员会空间数据与信息传输分会)执行,主管部门为国家标准化管理委员会。
Introduction
1. Core architecture and technical features of the protocol
This standard corresponds to the data link layer of the OSI model and adopts a variable-length PDU transmission mechanism. The key features include:
- Service data unit segment assembly: Supports large data segment transmission and small data aggregation
- Virtual channel (VC) multiplexing: 6-bit VCID enables multiple services to share the physical channel
- Security protocol support: Optional SDLS provides encryption and authentication (the security header and tail are up to 1017 bytes)
2. Service classification and data transmission
| Service type | Reliability | SDU format | Typical application |
|---|---|---|---|
| Class A | High reliability (automatic retransmission) | Packet/MAP_SDU | Key command transmission |
| Class B | Basic transmission | Custom data unit | Spacecraft recovery operation |
Note: MAPP service supports multiple versions of packets and distinguishes user data by PVN (packet version number)
III. Detailed explanation of protocol data unit
7.2 Remote control transmission frame structure
Key field definition:
- Leading header (5 bytes): including TFVN(00), SCID(10bit), VCID(6bit)
- Data field (1019 bytes): supports segment header (optional) to implement MAP segmentation
- FECF (2 bytes): CRC-16 checksum, polynomial X16+X12+X5+1
Typical application scenarios:
In deep space exploration missions, the upper limit of the number of retransmissions is set through the COP management service, and reliable transmission in long-delay environments is achieved in combination with CLCW (communication link control word).
IV. Technology Evolution and Implementation Recommendations
9.1 Management Parameter Configuration
Key Parameter Examples:
- Physical channel: maximum frame length 1024 bytes, SCID set dynamic configuration
- Virtual channel: frame sequence number 8bit cycle, CLCW report rate ≥1Hz
- MAP channel: segmentation permission flag, MAP_ID range 0-63
10.5 SDLS Enhanced Security
Security implementation requires synchronous configuration:
- Virtual channel level: security header/tail length independent setting
- Class D frames are exclusively protected, and Class C frames are distinguished by control flags (1bit)

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