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Data transmission method for dual redundant systems based on high-speed serial buses

A high-speed serial bus, system data technology, applied in the direction of data exchange, transmission system, bus network, etc. through path configuration, can solve problems such as inability to exchange data, slow data exchange, and inability to achieve cross control with dual redundancy

Inactive Publication Date: 2018-10-02
XIAN AVIATION COMPUTING TECH RES INST OF AVIATION IND CORP OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The traditional data transmission set between dual redundancy, the general data interaction is slow, requires processor intervention, cannot be completed independently, all data cannot be interacted in real time, and cross control cannot be realized between dual redundancy, etc.

Method used

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  • Data transmission method for dual redundant systems based on high-speed serial buses

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Embodiment Construction

[0011] According to the requirements of the electromechanical subsystem, in the data transmission method of the dual redundancy system based on the high-speed serial bus, real-time data transmission between the dual redundancy is set, the data transmission speed is fast, the data transmission package is large, and the data between the dual channels can be forwarded independently , At the same time, when any channel fails, the data transmission method of the dual redundancy system with cross control can be completed, and the method can well complete the data transmission function between the dual redundancy systems.

[0012] In the data transmission method of the dual-redundancy system based on the high-speed serial bus, the characteristics of the high-speed serial bus data packet are used to encode the data of each packet in the system. The encoded information includes: data source, data destination , the length of the data, the data verification status, the health status of th...

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Abstract

The invention belongs to a practical technology in the field of an airborne electromechanical management subsystem and is mainly applied to design and implementation of dual redundant systems in airborne equipment. The data transmission method for the dual redundant systems is simple, the dual redundant systems are cross-linked through high-speed buses, all data can be transmitted in real time, data received by the system are autonomously transmitted to the opposite channel while being received, and the data to be transmitted by the systems are mutually transmitted in real time through a datatransmission module between the two channels, thereby ensuring real-time update of the data between the dual redundant systems. When individual signal failures occur in a single channel, each channelis enabled to obtain complete correct data through data integration between the two channels; when functional component failures occurs in a single channel, data calculation is completed by the normalchannel through failure isolation; and when the process of a single channel fails, the opposite channel can complete system functions through cross data control.

Description

1 technical field [0001] This technology is a technology in the field of airborne electromechanical management subsystems, and is mainly used in the design and implementation of dual redundancy systems in airborne equipment. 2 background technology [0002] One of the important components of the aircraft electromechanical system is the electromechanical management subsystem, whose reliability directly affects the safety of the electromechanical system and even the entire aircraft. In the context of this demand, the electromechanical management subsystem is required to have high safety and reliability. sex. Due to the further improvement of the comprehensiveness of the electromechanical management subsystem, the electromechanical management subsystem integrates braking, power supply and other systems that have high safety requirements, which requires real-time and complete data transmission between the dual redundancy of the electromechanical management subsystem and autonom...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04L12/40H04L12/24
CPCH04L12/40182H04L41/0663
Inventor 陈奎呼明亮王永国闫稳於二军邓道杰
Owner XIAN AVIATION COMPUTING TECH RES INST OF AVIATION IND CORP OF CHINA