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A df file verification method based on arinc661

A verification method and file technology, applied in the field of DF file verification based on ARINC661, can solve problems such as difficulty in ensuring the accuracy and repeatability of results, low efficiency, difficult analysis and verification, etc., to ensure development progress and development efficiency, Reduce the time to analyze the cause of the problem and improve the test efficiency

Active Publication Date: 2017-03-22
江苏锐天智能科技股份有限公司
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AI Technical Summary

Problems solved by technology

[0008] Binary format DF is difficult to analyze and verify in a conventional way, usually with the help of special tools to verify; XML format DF can be analyzed, usually only the format can be checked, and the verification of logical content is usually based on walkthrough, but This method is not intuitive, not efficient, and it is difficult to guarantee the accuracy and repeatability of the results
[0009] In terms of verifying the validity of DF files, there is currently a lack of comprehensive and dynamic verification tools for DF files in the aviation field

Method used

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  • A df file verification method based on arinc661
  • A df file verification method based on arinc661
  • A df file verification method based on arinc661

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Embodiment Construction

[0028] The present invention will be specifically introduced below in conjunction with the accompanying drawings and specific embodiments.

[0029] The present invention is applied to the initial stage of DF definition, that is, the DF is verified through the simulation of the UA interface, and the problems of the DF file are found and corrected as much as possible, so that the later test can focus on the UA logic. To a large extent, it reduces the difficulty for developers and testers to locate problems, improves the efficiency of testing, and reduces the cost of development and testing.

[0030] refer to image 3 As shown, the present invention can be implemented using python scripting language, and the software system generated by using this technology can dynamically display the communication information between CDS and UA by providing static analysis of DF files, and dynamically modify parameters according to operator needs Attributes to meet the needs of DF file verific...

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Abstract

The invention discloses a DF file verification method based on the ARINC661. The DF file verification method based on the ARINC661 is characterized by comprising the following steps that firstly, a DF file is led in, information of the DF file is read and stored in a unified global variable, after the DF file is led in successively, data are analyzed and displayed according to a logical hierarchical structure, and attribute values and types of all parts are displayed in rows; secondly, a CDS server is started; thirdly, dynamic verification is performed on the DF file; fourthly, a test scrip of the Python format is automatically generated according to attributes of the corresponding parts of a DF and based on the ARINC661 protocol specifications, an execution environment and management are provided, original manual operation is converted into a script file to be stored, and therefore the verification process can be repeated. According to the DF file verification method based on the ARINC661, time in analyzing question reasons can be reduced, more emphasis of project testing can be put on logical functions, and therefore the development progress and the development efficiency of a whole project are ensured.

Description

technical field [0001] The invention relates to a DF file verification method, in particular to an ARINC661-based DF file verification method. Background technique [0002] With the increasing degree of integration of avionics and the continuous improvement of human-computer interaction requirements, as well as the different interfaces of electronic devices provided by aviation manufacturers, ARINC has developed a comprehensive solution for the aircraft cockpit display system CDS (Cockpit Display System, aircraft cockpit display system) to the user system. The UA (User Application, user system) interface defines the specification ARINC661, which has been used by airlines such as Airbus (A380, A400), Boeing (787), and has gradually become an industry standard after continuous revision. [0003] ARINC661 aims to standardize the definition of cockpit display system CDS and the communication between CDS and user system UA. In a specific implementation manner, a definition file ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F11/22H04L29/06
Inventor 夏高明兰积钱詹海明汤挺薛郝
Owner 江苏锐天智能科技股份有限公司
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