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Software and hardware co-processing reconfigurable circuit and self-repairing method thereof

A technology of software and hardware coordination and circuit reconstruction, applied in the architecture with a single central processing unit, electrical digital data processing, digital computer components, etc. The effect of tolerating permanent failures

Pending Publication Date: 2021-12-24
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0009] Purpose of the invention: In order to alleviate the repair power consumption of the reconfigurable module circuit in the FPGA, reduce the time for self-detection of faults, thereby speeding up the speed of self-repair of faults, and at the same time solve the problem of self-repair of permanent faults, the present invention proposes a software-based Reconfigurable circuit structure and self-healing method for hardware co-processing

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  • Software and hardware co-processing reconfigurable circuit and self-repairing method thereof
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  • Software and hardware co-processing reconfigurable circuit and self-repairing method thereof

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Embodiment Construction

[0048] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0049] Such as figure 1 Shown is the schematic diagram of the circuit structure of the present invention, including the logic end and the processor end, the logic end is connected with the processor end through the AXI bus, and the fault signal and the enable signal of the reconfigurable module are all transmitted through the AXI bus; the HWICAP interface is respectively Connect the AXI bus and the logic terminal to realize the transfer of configuration information from the external memory to the configuration memory.

[0050] The logic side consists of an auxiliary selection module and three functionally identical reconfigurable modules. Each reconfigurable module includes three functional modules with the same structure: two dual-mode redundant hot backup functional modules and a cold backup functional module; the dual-mode redunda...

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Abstract

The invention discloses a software and hardware co-processing reconfigurable circuit and a self-repairing method thereof.The circuit comprises a logic end and a processor end, the logic end is connected with the processor end through an AXI bus, and an HWICAP controller is connected with the AXI bus and the logic end; the logic end comprises an auxiliary selection module and three reconfigurable modules with the same function, and the reconfigurable modules transmit fault enable signals to a fault interrupt responder of the processor end through an AXI bus; the auxiliary selection module selects a reconfigurable module which needs to be enabled at present, and shields a reconfigurable module which does not work at present at the same time; and the processor end comprises a fault interruption responder, a fault processor and an error correction result judger. Faults can be quickly positioned through the dual-mode comparison functional module in the logic end reconfigurable module. Meanwhile, fault signals are transmitted to the processor end, the processor end interrupts internal circulating self-detection on the faults by responding to the fault signals, and the self-repairing speed is increased.

Description

technical field [0001] The invention belongs to the design field of reconfigurable hardware fault-tolerant methods, in particular to reconfigurable circuits for software and hardware co-processing and a self-repair method thereof. Background technique [0002] Commercial off-the-shelf SRAM (Static Random-Access Memory) FPGA (Field-Programmable Gate Array Field Programmable Gate Array) due to its low cost, short development cycle, good performance and on-rail reconfiguration, etc. More and more applications in aerospace, railway, automatic driving, medical and other fields. Different from the ground environment, high-energy particle radiation in the space environment poses a fatal threat to electronic systems, and SRAM-type FPGAs are more susceptible to the impact of radiation particles due to the particularity of their technology, and single event effects occur. [0003] Affected by single event effects, faults caused by space radiation effects can be divided into transient...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F15/78
CPCG06F15/7871
Inventor 黄莉莉张砦王涛
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS