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Space laboratory information system based on advanced in-orbit data processing method

A data processing and information system technology, applied in the electrical field of spacecraft, can solve problems such as lack of spacecraft, complex bus architecture, data multiplexing, storage design difficulties, etc., to achieve unified management, efficient transmission, and improve channel utilization Effect

Active Publication Date: 2018-08-14
BEIJING SPACE TECH RES & TEST CENT
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The above shows that the data formats and transmission rates from different data sources are different. No other domestic spacecraft has such a large number of data sources and such a complex bus architecture, which brings difficulties to the design of data multiplexing and storage.

Method used

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  • Space laboratory information system based on advanced in-orbit data processing method
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  • Space laboratory information system based on advanced in-orbit data processing method

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Embodiment Construction

[0054] The description of the embodiments in this specification should be combined with the corresponding drawings, and the drawings should be regarded as a part of the complete specification. In the drawings, the shapes or thicknesses of the embodiments may be exaggerated and marked for simplification or convenience. Furthermore, the parts of each structure in the drawings will be described separately. It should be noted that the elements that are not shown in the drawings or described in words are forms known to those of ordinary skill in the art .

[0055] The descriptions of the embodiments here, any references to directions and orientations are just for convenience of description, and should not be construed as any limitation to the protection scope of the present invention. The following descriptions of the preferred embodiments involve combinations of features, which may exist independently or in combination, and the present invention is not particularly limited to the...

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Abstract

The invention relates to a space laboratory information system based on an advanced in-orbit data processing method. The telemetering, instruction and communication functions are realized through a data information system based on a 1553B bus, and the high-speed data transmission is realized through a high-speed data transmission system based on AOS. The space laboratory information system based on the advanced in-orbit data processing method disclosed by the invention can support a manned spacecraft to accomplish all in-orbit functions.

Description

technical field [0001] The invention relates to the electrical field of spacecraft, relates to the design of a manned spacecraft information system, in particular to a manned spacecraft information system based on an advanced on-orbit data processing method. Background technique [0002] With the continuous development of space technology, the scientific tasks of spacecraft flight are becoming more and more heavy, and the amount of data is increasing. The TG-1 space laboratory has many types of data sources, a large amount of bus data, and multiple output channels, which are reflected in: [0003] 1) The data transmitted by the space laboratory includes engineering telemetry, digital tube telemetry, video and voice, scientific experiment data, and application system data. [0004] 2) The data sources of the space laboratory include 2 sets of 1553B bus with a total of 26 terminals, 1 set of docking 1553B bus with a total of 2 terminals, and 1 set of 1394 bus with a total of 5...

Claims

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Application Information

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IPC IPC(8): H04B7/185
CPCH04B7/18504H04B7/18506
Inventor 杨宏何宇张璐刘宏泰梁克刘岩张森徐晓光田庄丁凯
Owner BEIJING SPACE TECH RES & TEST CENT
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