High-reliable fault-tolerant system based on bus network

A technology of fault-tolerant system and bus network, applied in the direction of bus network, transmission system, digital transmission system, etc., can solve the problems of low bus bandwidth, computer system failure, and high-speed interactive transmission of data streams, etc., and achieve extensive fault tolerance and transmission The effect of speed increase

A technology of fault-tolerant system and bus network, applied in the direction of bus network, transmission system, digital transmission system, etc., can solve the problems of low bus bandwidth, computer system failure, and high-speed interactive transmission of data streams, etc., and achieve extensive fault tolerance and transmission The effect of speed increase

CN108768754AActive Publication Date: 2018-11-06XIAN MICROELECTRONICS TECH INST

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  • High-reliable fault-tolerant system based on bus network
  • High-reliable fault-tolerant system based on bus network
  • High-reliable fault-tolerant system based on bus network

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Embodiment Construction

[0029] see figure 1 , the present invention is a high-reliability fault-tolerant system based on a bus network. By utilizing the SpaceWire interconnection bus architecture, a higher and wider fault-tolerant capability for a dual-redundancy system is realized with a double-ring topology.

[0030] Including analog IO control module, interface and switching module, airborne flight control and comprehensive computing module, high-performance processing module, digital IO control module, router module, these 6 modules and their dual redundant isomorphic modules, a total of 12 modules, to achieve dual Redundant hot backup.

[0031] Dual redundant homogeneous modules include backup analog IO control module, backup interface and switch module, backup airborne flight control and comprehensive computing module, backup high-performance processing module, backup digital IO control module and backup router module.

[0032] The dual-ring topology based on router interaction is constructed ...

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Abstract

The invention discloses a high-reliable fault-tolerant system based on a bus network. The fault-tolerant system comprises a simulation IO (Input Output) control module, an interface and switching module, an onboard flight control and integrative computation module, a high-performance processing module, a digital IO control module, a router module, and dual-redundancy isomorphic modules corresponding to above six modules; the six modules and the corresponding dual-redundancy isomorphic modules compose four network connections to realize the dual-redundancy hot backup; and thus, the fault-tolerant capacity of the dual-redundancy system is improved through the dual-ring topological structure by using the SpaceWire interconnected bus architecture. Based on a plurality of point-to-point bus interconnected bridge connections, the fault-tolerant system provided by the invention realizes the faster and stronger system fault-tolerant capability by using the dual-ring topological structure.

Description

technical field [0001] The invention belongs to the technical field of embedded system design in aerospace applications, and in particular relates to a highly reliable fault-tolerant system based on a bus network. Background technique [0002] Traditional aerospace high-reliability embedded computers mostly adopt the method of multi-module dual-redundant hot standby, and the system's dual-channel redundant bus mostly uses CAN, 1553, AFDX, etc. Such a dual redundant structure has two obvious disadvantages. First, the system is sensitive to multiple failures. In addition, the traditional space-oriented application buses such as CAN, 1553, and AFDX have low speeds, which cannot meet the requirements of fast and reliable transmission of aerospace product data processing. [0003] With the increasing demand for high reliability and high performance of military aerospace products, aerospace embedded computer products are required to have higher fault tolerance and higher communi...

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Application Information

Patent Timeline
06 Nov 2018
Publication
CN108768754A
IPC
H04L12/24; H04L12/40; H04L12/713; H04L45/586
CPC
H04L12/40195; H04L41/0663; H04L45/586
Inventors
张树刚; 刘彬