On-orbit reconstruction method and system for aerospace electronic system based on FPGA

An electronic system and aerospace technology, applied in the field of on-orbit reconfiguration of aerospace electronic systems, can solve problems such as inability to change hardware functions, high cost of single machine production and high cost of single task execution, and solidification of electronic systems and entire star functions, so as to improve performance and Reliability, the effect of improving autonomous health management and on-orbit maintenance capabilities

Pending Publication Date: 2021-08-27
XIAN MICROELECTRONICS TECH INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Cannot change hardware function
This makes the electronic system and the entire star function solidified and single
The hardware design is highly customized and cannot be used universally, and the production cost of a single machine and the execution cost of a single task are high

Method used

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  • On-orbit reconstruction method and system for aerospace electronic system based on FPGA
  • On-orbit reconstruction method and system for aerospace electronic system based on FPGA

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Embodiment Construction

[0039] The present invention will be further described below in conjunction with the accompanying drawings.

[0040] see figure 1 , an FPGA-based on-orbit reconfiguration system for aerospace electronic systems, is characterized in that it includes an antifuse FPGA-based main control communication protocol analysis module, refresh chip protocol conversion and control module, CPU routing software and loading control module, telemetry Acquisition and framing module, CPU software operation monitoring module, communication module, etc. And the SRAM type FPGA refresh chip outside the FPGA, FLASH memory, etc.

[0041] The main control communication and protocol analysis module is realized by FPGA, mainly interfaces with the main control unit, and receives from the main control unit: target FPGA start, stop, refresh, programming commands, compatible with CPU software, FPGA configuration file FLASH erasure, programming, and readback verification commands, as well as commands such as...

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Abstract

The invention discloses an on-orbit reconstruction method and system for an aerospace electronic system based on FPGA. The method is based on an FPGA technology and can realize software and FPGA on-orbit reconstruction functions of the aerospace electronic system. The method plays a key role in astronavigation electronic system on-orbit fault restoration, and relieving of the influence of the universe space single event effect (SEE) on astronavigation electronic equipment such as satellites. The autonomous health management and on-orbit maintenance capabilities of the aerospace electronic system are fundamentally improved. And on-orbit autonomous configuration, self-test, autonomous repair and maintenance can be realized. Therefore, the system performance and reliability are greatly improved.

Description

technical field [0001] The invention belongs to the field of on-orbit upgrade maintenance and control, and in particular relates to an FPGA-based on-orbit reconfiguration method and system for an aerospace electronic system. Background technique [0002] As the functions of aerospace systems become more and more complex, more and more functions are implemented by FPGA, which puts forward higher requirements for system on-orbit reconstruction, on-orbit maintenance, mission upgrade and health management. With the continuous deepening and upgrading of the on-orbit application of aerospace systems, there is an urgent need for a technology that can systematically and comprehensively upgrade software and reconfigure FPGA on-orbit to achieve iterative upgrades of applications. [0003] Traditional satellites, spacecraft and other system functions are highly customized, and on-orbit maintenance is generally achieved through application software. The hardware function cannot be chan...

Claims

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Application Information

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IPC IPC(8): G06F15/78
CPCG06F15/7871Y02D10/00
Inventor 佘星星路海全马屹巍闫博
Owner XIAN MICROELECTRONICS TECH INST
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