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DSP multi-core data programming method based on 1553B bus

A data and bus technology, which is applied in the field of DSP multi-core data programming based on 1553B bus, can solve the problems of missing sector burning and judging, poor reliability, cumbersome operation, etc., to improve reliability, reduce workload, and improve the operation process. easy effect

Pending Publication Date: 2021-01-05
BEIJING AEROSPACE ERA LASER NAVIGATION TECH CO LTD
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  • Summary
  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] (1) It needs to be operated under the premise that the laser inertial group has not completed the assembly and sealing. After the assembly is completed, the inertial group must be disassembled;
[0006] (2) The construction of the simulation environment requires special equipment and professional DSP designers, and the operation is cumbersome;
[0007] (3) It is necessary to manually compare files offline, which is inefficient
[0009] (1) For different sectors, repeated programming operations are required, and the efficiency is low;
[0010] (2) Due to human negligence, it is easy to cause missed burning and missed judgment of the sector, and the reliability is poor;
[0011] (3) The method of first verifying and then programming cannot avoid errors in the programming process, and the reliability is poor

Method used

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  • DSP multi-core data programming method based on 1553B bus
  • DSP multi-core data programming method based on 1553B bus
  • DSP multi-core data programming method based on 1553B bus

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Embodiment Construction

[0035] In order to better understand the above technical solutions, the technical solutions of the present application will be described in detail below through the accompanying drawings and specific examples. It should be understood that the embodiments of the present application and the specific features in the examples are detailed descriptions of the technical solutions of the present application, and It is not a limitation to the technical solutions of the present application, and the embodiments of the present application and the technical features in the embodiments can be combined without conflict.

[0036] A kind of DSP multi-core data programming method based on 1553B bus provided by the embodiment of the present application will be described in further detail below in conjunction with the accompanying drawings, and the specific implementation may include (such as figure 1 shown):

[0037] (1) Convert the inertial group software or coefficient file that needs to be p...

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Abstract

The invention relates to a DSP (Digital Signal Processor) multi-core data programming method based on a 1553B bus, in particular to a method for performing multi-core data programming operation on a laser inertia measurement unit with a DSP programming module. According to the invention, communication and instruction control with the programming module are realized, and programming upgrading of computer board 03 nuclear inertia measurement unit software, element coefficients, temperature compensation parameters and the like is realized by selecting corresponding BIN files.

Description

technical field [0001] The invention relates to a DSP multi-core data programming method based on a 1553B bus, in particular for performing multi-core data programming operations on a laser inertial group equipped with a DSP programming module. Background technique [0002] After the development of inertial group software enters the stage of operation and maintenance, how to realize the rapid, simple and reliable upgrade of inertial group software is a key issue in the stage of operation and maintenance of inertial group software. In addition to the maintenance and upgrade of the software, the metadata stored in the inertial group also needs to be updated during the maintenance phase. The accuracy of the laser inertial group is affected by its own various error factors, and it needs to be calibrated regularly, and the calibrated zero offset, scale factors, and installation Coefficients such as errors are burned into the inertial computer board. The IMU computer board DSP ne...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F8/61G06F11/10G06F13/42
CPCG06F8/63G06F11/1004G06F13/4282
Inventor 薛靖邦刘晓亮李天军宋腾腾曲丹丹
Owner BEIJING AEROSPACE ERA LASER NAVIGATION TECH CO LTD
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