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FPGA single event upset fault simulation test system and method

A technology of single event flipping and fault simulation, applied in testing/monitoring control systems, general control systems, electrical testing/monitoring, etc., can solve the problem of inability to verify the function of the on-orbit monitoring program, the reservation of the device under test by the accelerator, and the failure to solve the functional verification and other problems, to achieve the effect of intuitive and clear test results, easy debugging and verification, and low test cost

Active Publication Date: 2015-12-16
SHANGHAI RADIO EQUIP RES INST
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  • Application Information

AI Technical Summary

Problems solved by technology

The failure simulation test using the method of heavy particle irradiation on FPGA has the disadvantages of high test cost, accelerator reservation and non-reusable devices under test
However, using the method of fault injection requires the establishment of a complex test system. The object under test is FPGA, which cannot verify the function of the on-orbit monitoring program.
Therefore, none of the above methods solves the problem of implementing functional verification on the hardware platform of FPGA on-orbit monitoring.

Method used

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  • FPGA single event upset fault simulation test system and method
  • FPGA single event upset fault simulation test system and method
  • FPGA single event upset fault simulation test system and method

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Embodiment Construction

[0040] The following combination Figure 1 to Figure 4 , a preferred embodiment of the present invention is described in detail.

[0041] Such as figure 1 As shown, the FPGA single event upset fault simulation test system provided by the present invention includes: configuration file generation comparison module 1; FPGA configuration program on-orbit monitoring platform 2; configuration file injection module 3, which is connected to the configuration file Generate comparison module 1 and FPGA configuration program on-orbit monitoring platform 2; fault analysis module 4, which is connected with said FPGA configuration program on-orbit monitoring platform 2.

[0042] Such as figure 2 As shown, the configuration file generation and comparison module 1 is implemented by a host computer 11 to generate a reference configuration file and a new configuration file, and compare the flipped bits of the two.

[0043]Described configuration file injecting module 3 adopts FPGA download ...

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Abstract

The invention relates to an FPGA single event upset fault simulation test system and method. The method comprises the steps that S1, a reference configuration file and a new configuration file are generated by a configuration file generation and comparison module, and the upset digits of the two files are obtained through comparison; S2, the reference configuration file and the new configuration file are respectively injected into the monitored FPGA in an FPGA configuration program on-orbit monitoring platform via a configuration file injection module, and a frequency division signal is generated; S3, the tested on-orbit monitoring module in the FPGA configuration program on-orbit monitoring platform is started, the upset digits of the reference configuration file and the new configuration file are obtained through comparison, and the file data in the monitored FPGA are refreshed; and S4, an on-orbit monitoring verification result is obtained via a fault analysis module. Accuracy of an FPGA on-orbit monitoring function can be guaranteed; and test coverage is great, cost is low, time consumption is low, realization technical difficulty is low in engineering, and implementation of debugging verification in the early phase of the project is facilitated.

Description

technical field [0001] The invention relates to a test system and method for simulating FPGA single-event flip faults in order to verify the on-orbit monitoring function of FPGA (Field-Programmable Gate Array, Field Programmable Gate Array) in satellite or aircraft load, and belongs to the field of reliability of on-board electronic equipment . Background technique [0002] As the altitude of the flight orbit increases, the electronic equipment in the satellite or aircraft is more susceptible to the impact of high-energy particles, especially when the configuration program inside the FPGA is flipped by a single event, when the number reaches a certain level, the FPGA function will fail. The FPGA on-orbit monitoring periodically monitors whether the FPGA configuration program is flipped and dynamically refreshes the configuration area. It is necessary to simulate a single event flip fault on the ground to verify whether the FPGA on-orbit monitoring is correct. [0003] At pr...

Claims

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Application Information

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IPC IPC(8): G05B23/02
CPCG05B23/0213
Inventor 张衡邹波黄勇高媛衡燕
Owner SHANGHAI RADIO EQUIP RES INST
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