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A reconfigurable computer module set for measurement, launch and control based on fpga

A computer module, measurement and control technology, applied in the direction of computer control, simulator, program control, etc., can solve the problems of costing research and development funds and investment, and the reuse rate of hardware resources cannot be effectively improved and increased, and achieves strong flexibility and flexibility. Expansion effect

Active Publication Date: 2022-03-04
BEIJING INST OF ELECTRONICS SYST ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, various types of aircraft are showing a trend of diversification and complexity, and the supporting test, launch and control equipment mostly adopts the development model of special equipment, and no generalized and scalable architecture is adopted in the hardware development process. And the number is increasing day by day, which consumes a lot of research and development funds and investment, and at the same time prolongs the equipment development cycle, and the reuse rate of hardware resources cannot be effectively improved, and cannot meet the application requirements of diversified and rapid development of future aircraft types.

Method used

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  • A reconfigurable computer module set for measurement, launch and control based on fpga
  • A reconfigurable computer module set for measurement, launch and control based on fpga

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Embodiment Construction

[0034] In order to illustrate the present invention more clearly, the present invention will be further described below in conjunction with preferred embodiments and accompanying drawings. Similar parts in the figures are denoted by the same reference numerals. Those skilled in the art should understand that the content specifically described below is illustrative rather than restrictive, and should not limit the protection scope of the present invention.

[0035] Such as figure 1 and 2 Shown, a kind of FPGA-based reconfigurable measurement and control computer module set, this module set includes:

[0036] At least one FPGA core control module is used to bridge the data information flow between modules and run the top-level control logic;

[0037] At least one power module is used to provide power for all modules in the module group, and a DC or AC power input interface is provided on the outer panel of the power module, and the power module is also provided with a switch ...

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Abstract

The invention discloses an FPGA-based reconfigurable measuring, launching and controlling computer module group, comprising: an FPGA core control module, used to bridge the data information flow between modules; a power supply module, used to provide power for each module in the module group; The backplane module or cable network is used to provide data information flow channels and power supply interfaces for each module; the peripheral function module is used to realize the specific functions of the module group; the extended operating system motherboard is used to expand the visual graphical interface , providing the data information flow in the computer module group for users to view, and to monitor and intervene the control logic in real time. The reconfigured and integrated aircraft measurement, launch and control computer equipment of the present invention has strong flexibility and scalability, and has the advantages of miniaturization and integration, and can meet the equipment application requirements of short cycle, low cost and high reliability.

Description

technical field [0001] The invention relates to the fields of ground testing and launch control. More specifically, it relates to a FPGA-based reconfigurable computer module set for measuring, launching and controlling. Background technique [0002] Ground test and launch control equipment, as important maintenance equipment for modern aircraft equipment, is an important part of aircraft products that are frequently used, have complex working environments, and require extremely high reliability. The integrity of its test and launch control functions is directly related to reliability. The health status of the entire life cycle of the aircraft determines the ability of the aircraft to complete the mission. [0003] At present, various types of aircraft are showing a trend of diversification and complexity, and the supporting test, launch and control equipment mostly adopts the development model of special equipment, and no generalized and scalable architecture is adopted in ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B19/042
CPCG05B19/0423G05B2219/25257
Inventor 李正天程鹏赵伯阳张润东王玉姣赵明范颖豪
Owner BEIJING INST OF ELECTRONICS SYST ENG