A low-cost and high-reliability satellite-borne single-machine multi-chip SRAM type FPGA on-orbit reconstruction system and method

A space-borne stand-alone, cost-effective technology, applied in the architecture with a single central processing unit, the generation of response errors, general-purpose stored program computers, etc., can solve problems such as small PROM capacity, achieve small weight, power consumption, volume, and improve flexibility. , low-cost effect

Pending Publication Date: 2019-05-21
XIAN INSTITUE OF SPACE RADIO TECH
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Problems solved by technology

However, the capacity of the PROM is small. For a large-scale SRAM FPGA, mult

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  • A low-cost and high-reliability satellite-borne single-machine multi-chip SRAM type FPGA on-orbit reconstruction system and method
  • A low-cost and high-reliability satellite-borne single-machine multi-chip SRAM type FPGA on-orbit reconstruction system and method
  • A low-cost and high-reliability satellite-borne single-machine multi-chip SRAM type FPGA on-orbit reconstruction system and method

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[0055] The present invention will be described in detail below with reference to the drawings and examples.

[0056] Such as image 3 As shown, the system of the present invention includes a user function configuration data memory FLASH, a reconstruction interface configuration data memory PROM, an on-orbit reconstruction control circuit, an external reconstruction interface circuit and multiple pieces of SRAM FPGAs to be reconstructed;

[0057] Select one piece of SRAM FPGA to be reconstructed as the reconstruction interface FPGA, and build an external reconstruction interface circuit in the reconstruction interface FPGA;

[0058] External reconfiguration interface circuit ( image 3 The external reconstruction interface module in the) is used to receive the reconstructed user function configuration data and reconstruction instructions on the ground, and verify them. If the verification result is correct, the reconstruction configuration data and instructions will be forwarded to the in

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Abstract

The invention discloses a low-cost and high-reliability satellite-borne single-machine multi-chip SRAM type FPGA on-orbit reconstruction system. One chip is selected from a plurality of to-be-reconstructed FPGAs as a reconstruction interface FPGA, and an external reconstruction interface circuit is constructed in the reconstruction interface FPGA; The external reconfiguration interface circuit isused for receiving reconfiguration user function configuration data and a reconfiguration instruction which are injected on the ground, generating a reconfiguration telemetry data packet from the received reconfiguration user function configuration data and the received reconfiguration instruction, sending the reconfiguration telemetry data packet to the on-orbit reconfiguration control circuit, and downloading reconfiguration telemetry information on a satellite to the ground; The reconfiguration interface configuration data memory PROM is used for storing reconfiguration interface function configuration data of the reconfiguration interface FPGA; Wherein different spaces are set in the FLASH and correspond to the FPGAs to be reconstructed respectively, and the FLASH is used for pre-storing original user function configuration data of the FPGAs to be reconstructed or storing reconstructed user function configuration data used during on-orbit reconstruction; The on-orbit reconstructioncontrol circuit is responsible for communication with the reconstruction interface circuit, storage of reconstruction configuration data and loading and refreshing of the FPGA to be reconstructed according to control of a ground remote control instruction.

Description

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Claims

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Application Information

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Owner XIAN INSTITUE OF SPACE RADIO TECH
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