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A spacecraft uses sram type fpga dual-port ram anti-single event flip reinforcement device

An anti-single event and reinforcement device technology, applied in the field of aerospace electronics, can solve the problems of real-time processing of multiple additional storage resources, inability to cover BlockRAM, lack of anti-single event flipping means, etc., to improve anti-single event capability and avoid data duplication Effect of mold error and memory overhead reduction

Active Publication Date: 2021-04-13
BEIJING INST OF SPACECRAFT SYST ENG
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AI Technical Summary

Problems solved by technology

[0006] First of all, the overhead of three-mode redundancy for the FPGA internal BlockRAM is huge, it takes up a lot of additional storage resources, and the real-time processing is not strong; moreover, the long-term flip accumulation also increases the possibility of data errors caused by the flipping of two of the three modes;
[0007] Secondly, the refresh mechanism only refreshes the resources inside the FPGA except BlockRAM and RAM interconnection, and cannot cover BlockRAM
Therefore, when a single event flip occurs in the long-term in-orbit RAM area data, the refresh mechanism cannot be corrected
[0008] Therefore, there is still a lack of effective anti-single event flipping means for BlockRAM for long-term important data storage

Method used

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  • A spacecraft uses sram type fpga dual-port ram anti-single event flip reinforcement device

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Embodiment Construction

[0032] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0033] like figure 1 As shown, a spacecraft using SRAM type FPGA dual-port RAM anti-single event reversal hardening device provided by the present invention includes a dual-port RAM module, a first EDAC encoder, a first EDAC decoder and an arbitration refresher.

[0034] 1. Dual-port RAM module as physical data storage

[0035] The dual-port RAM module includes two sets of completely independent ports, namely the first port and the second port, each port includes data lines, address lines, read enable control lines and write enable control lines; among them, user data passes through the first port One port writes and reads the dual-port RAM module; the arbitration refresher reads the user data stored in the dual-port RAM module through the second port and writes it into the dual-port RAM module again without affecting the data written by the...

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Abstract

The invention relates to an anti-single event reversal reinforcement device using SRAM-type FPGA dual-port RAM for a spacecraft, belonging to the technical field of aerospace electronics. The anti-single event reversal hardening device includes a dual-port RAM module and an arbitration refresher. The dual-port RAM module includes two sets of completely independent ports, namely the first port and the second port, and each port includes a data line and an address line. , read enable control line and write enable control line; wherein, user data is written into and read out of the dual-port RAM module through the first port; The user data stored in the dual-port RAM module is read out and written into the dual-port RAM again, thereby refreshing the dual-port RAM. The invention solves the difficult problem of anti-single-event flipping reinforcement of the BlockRAM inside the SRAM type FPGA of the spacecraft.

Description

technical field [0001] The invention belongs to the technical field of aerospace electronics, and relates to an anti-single-event flipping reinforcing device using SRAM-type FPGA dual-port RAM for spacecraft. Background technique [0002] SRAM-type FPGAs are widely used in the design of spacecraft electronic systems. At present, the anti-radiation hardening of traditional SRAM FPGA adopts the three-mode redundancy plus scrubbing mechanism to improve reliability. E.g: [0003] In the article "SRAM Type FPGA Anti-Single Event Flipping Design for Aerospace" (Spacecraft Environmental Engineering, Vol. Part of the anti-single event flipping design scheme adopts general-purpose self-correcting macros. This solution is achieved through internal BlockRAM triple-mode redundancy. [0004] Patent CN201610939803.2 is named as a RAM data reliability reinforcement device and method based on SRAM FPGA, which describes the use of Hsiao codes as error correction codes to realize the enco...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G11C11/413
CPCG11C11/413
Inventor 冯国平徐勇周东曾连连庞波韩庆龙陶涛张溢牛跃华李柯汪路元禹霁阳
Owner BEIJING INST OF SPACECRAFT SYST ENG
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