Multi-path transmission data bus redundancy synchronous communication method

A data bus and synchronous communication technology, applied in the direction of electrical digital data processing, inter-program communication, multi-program device, etc., can solve the problems of long recovery time of working status, single point of bus controller interface, etc., and improve reliability and safety effects

Active Publication Date: 2021-03-16
SHANDONG INST OF AEROSPACE ELECTRONICS TECH
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AI Technical Summary

Problems solved by technology

[0008] The multi-channel transmission data bus redundant synchronous communication method described in this application is to solve the problems in the prior art and propose a multi-mode redundant computer The 1553B bus controller interface redundancy method is designed to solve the problem that the existing multi-mode redundant fault-tolerant computer 1553B bus controller interface is single-pointed and the problem of too long working state recovery time when reconfiguration is restored, and can expand the redundancy of various models. redundant fault-tolerant system

Method used

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  • Multi-path transmission data bus redundancy synchronous communication method

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Embodiment 1

[0038] Embodiment 1, the multiplex data bus redundant synchronous communication method described in the present application, adopts such as Figure 4 In the bus interface mode shown, the three-mode redundant computer has three CPUs (that is, three mutually redundant computer modules), of which there is only one master, and the rest are slaves by default when powered on. When it is detected that the current chip fails, the host can choose any of the 3 computer modules at any time.

[0039] Specifically, host switching is realized by rewriting the program instructions of the FPGA.

[0040] The single machine where each CPU is located has an independent bus communication chip, and the working mode of the 1553B bus is configured as BC mode, and all of them are connected to the bus communication network.

[0041] Using the above-mentioned bus interface mode, this application mainly adopts the following three solutions: 1. Only one terminal should control the bus system at any time...

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Abstract

The invention relates to a multi-path transmission data bus redundancy synchronous communication method, in particular to a 1553B bus controller interface redundancy method for a multi-mode redundancycomputer, and aims to solve the problem that the working state recovery time is too long when the 1553B bus controller interface of the existing multi-mode redundancy fault-tolerant computer is subjected to single-point and reconstruction recovery, and can expand redundant fault-tolerant systems of various machine types. A single machine where each CPU is located is provided with an independent bus communication chip, and a 1553B bus working mode is configured to be a BC mode and is accessed to a bus communication network; the communication mechanism comprises that only one terminal is required to control the bus system at any moment, that is, only one active BC is available on the bus at any moment, wherein the minimum unit of the 1553B communication sequence is a message, the instruction word in the message is BC sending, the state word is RT sending, and the message transmission sequence determines that RT feedback is not received if the BC is not sent; wherein the interval time for the RT to respond to the valid instruction words is 4-12 us, the minimum response-free timeout is 14 us, and the RT response starts to be detected 2 us after the BC sends the words.

Description

technical field [0001] The invention relates to a redundant computer-oriented, digital time-division system command-response multi-channel transmission data bus redundant synchronous communication method, which belongs to the technical field of computers and their applications. Background technique [0002] The current triple-mode redundant fault-tolerant computer used in the prior art has a relatively urgent application demand in the field of safety-critical control because of its higher safety performance. In the field of aerospace, the digital time-division system command-response multiplex transmission data bus (MIL-STD-1553B bus, referred to as 1553B) is a widely used electronic system field bus, which has excellent reliability and high transmission speed. Speed ​​and anti-interference ability characteristics. [0003] There are three types of 1553B bus terminals: bus controller, remote terminal and bus monitor. as attached figure 1 As shown, in the 1553B bus control...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F13/374G06F13/40G06F9/54
CPCG06F13/374G06F13/4022G06F9/546Y02D10/00
Inventor 赵亮王勇曹振兴谭沛栾丽焦胜利
Owner SHANDONG INST OF AEROSPACE ELECTRONICS TECH
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