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Space information system based on SpaceVPX standard

A space information and standard technology, applied in the aerospace field, can solve problems such as poor applicability, insufficient standardization of the system, and lack of reliability design for aerospace applications, and achieve the effect of wide applicability

Active Publication Date: 2019-08-23
SHANGHAI AEROSPACE COMP TECH INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, the above patents are all proposed based on the VITA65 (OpenVPX) or VITA46 standard, lack of reliability design for aerospace applications, making the whole system not standardized enough and poor in applicability

Method used

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  • Space information system based on SpaceVPX standard
  • Space information system based on SpaceVPX standard
  • Space information system based on SpaceVPX standard

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Embodiment Construction

[0030] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0031] figure 1 For the structure diagram of the spatial information system based on the SpaceVPX standard provided by the present invention, see figure 1 , The SpaceVPX architecture strengthens the system reliability management on the basis of the OpenVPX architecture, introduces the bottom layer management module of the system, and maintains the characteristics of multi-protocol switching of the VPX architecture. The interconnection between SpaceVPX modules can be through Serial RapidIO, PCI-E, Ethern...

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Abstract

The invention provides a space information system based on a SpaceVPX standard, which comprises an information plane, a system management module, a main control module, an exchange module and a function module which are in communication connection with one another, and is characterized in that the information plane is used for providing different data exchange topology networks according to the data transmission rate among internal modules of the system; the system management module is used for providing a management strategy of each module in the system and a communication protocol among themodules; the main control module is used for limiting and controlling each module to execute a corresponding task; the exchange module is used for limiting an interaction relationship among the modules; and the function modules are used for limiting the functions of all the modules. Therefore, the spatial information system aiming at the SpaceVPX standard can be constructed, so that the whole system is more standardized, and the applicability is wider.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a space information system based on the SpaceVPX standard. Background technique [0002] The space information system is a space electronic platform integrating platform management, data storage, information processing and other functions. Improving the performance and reliability of the space information system and promoting the modularization of the space information system are current research hotspots. Among the currently known VPX information system platforms, the platform designs are ground applications based on OpenVPX, such as patents CN205389239U, CN105488566A, CN104243174A, etc; In the functional design of the whole machine. [0003] However, the above patents are all proposed based on the VITA65 (OpenVPX) or VITA46 standard, which lacks reliability design for aerospace applications, making the entire system not standardized enough and poor in applicability. Conte...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04L12/40H04L12/24
CPCH04L12/40H04L12/40176H04L41/044H04L41/0893
Inventor 王冠雄邱源田文波曹旭民朱秋菊徐文彬
Owner SHANGHAI AEROSPACE COMP TECH INST
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