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Satellite-borne high-speed data multiplexer system and realizing method thereof

A high-speed data and multiplexer technology, which is applied in the field of spacecraft data transmission system, can solve the problems of low data buffer rate, small burst length, and small buffer capacity, so as to eliminate jitter, reduce the number, and improve the stability of the system degree of effect

Active Publication Date: 2013-02-13
XIAN INSTITUE OF SPACE RADIO TECH
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  • Application Information

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Problems solved by technology

[0011] (1) Only small burst length is supported, and the burst length is fixed ( Figure 5 The t1 time is relatively short, generally less than 16K clock cycles, and for each channel of data, the length of t1 is fixed) multi-source data multiplexing;
[0012] (2) The data cache unit generally chooses off-chip FIFO, off-chip SRAM or on-chip RAM as the buffer, and corresponds to the input source data one by one (each channel of source data corresponds to an off-chip buffer), and the data buffer rate is relatively low. Low, small cache capacity;
[0014] (4) The processing rate is low (generally less than 700Mbps)

Method used

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  • Satellite-borne high-speed data multiplexer system and realizing method thereof
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  • Satellite-borne high-speed data multiplexer system and realizing method thereof

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Embodiment Construction

[0062] Below in conjunction with accompanying drawing and specific implementation the present invention will be described in further detail:

[0063] Such as image 3 As shown, a spaceborne high-speed data multiplexer system of the present invention includes 5 modules such as a data packet module, a data packet module, an SDRAM optimization control module, a virtual channel scheduling module, and a channel coding module, wherein:

[0064] Data grouping module: Receive 30 channels of different types of multi-source data, represented by MSD1, MSD2, ..., MSD30 respectively, and group them according to the transmission priority or the strategy of balancing data volume. Every 6 channels of data are divided into groups 5 groups, followed by Group 1 (MGD1), Group 2 (MGD2), Group 3 (MGD3), Group 4 (MGD4), Group 5 (MGD5); According to the different real-time requirements of the data, the source data with the highest real-time requirements are divided into the first group, and so on, a...

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Abstract

The invention discloses a satellite-borne high-speed data multiplexer system and a realizing method thereof. The system comprises a data grouping module, a data sub-packaging module, an SDRAM (Synchronous Dynamic random access memory) optimal control module, a virtual channel scheduling module and a channel coding module, wherein the data grouping module receives 30 paths of information source data; the 30 paths of information source data are divided into 5 groups according to a transmission priority or a strategy of balanced data volume; the data sub-packaging module is used for splitting and organizing packets in each path of the information source data in the 5 groups so as to form 5 groups of protocol unit data; the SDRAM optimal control module is used for respectively writing 5 groups of protocol unit data into 5 SDRAMs for caching and reading control so as to form 5 groups of virtual channel data; the virtual channel scheduling module is used for performing dynamic scheduling management and multiple connection on the 5 groups of virtual channel data and one group of empty frames so as to be combined to form one path of form type code flow; and the channel coding module is used for isolating the one path of form type code flow from an FIFO (first in and first out) by a local clock, and coding and scrambling the isolated form type code flow so as to form one path of data transmission frame as the output of the data multiplexer system.

Description

technical field [0001] The invention relates to a space-borne high-speed data multiplexer system and a realization method, belonging to the field of spacecraft data transmission systems. Background technique [0002] The theoretical basis of data multiplexing is the concept of virtual channels. Divide a physical channel into multiple logical channels, each logical channel is identified separately and transmits a data flow, each data flow can use different services, a logical channel is a virtual channel. The virtual channel enables one physical space channel to be shared by multiple high-level data streams in a time-division multiplexed manner, so that multiple types of data can be transmitted on one physical channel. [0003] The spaceborne data multiplexer system is responsible for receiving multi-source data in space data transmission, that is, multiple source data of different formats and different rates (compressed visible light data, spectral data, SAR data, reconnais...

Claims

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Application Information

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IPC IPC(8): H04Q11/00
Inventor 李永峰赵妍袁素春张建华
Owner XIAN INSTITUE OF SPACE RADIO TECH
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