Keyword-driven airborne software automatic test method and system

An automated testing, keyword-driven technology, applied in software testing/debugging, electrical digital data processing, error detection/correction, etc., can solve the problems of less attention in automated testing, improve the level of test automation, shorten the test cycle, The effect of improving reusability

Inactive Publication Date: 2017-04-26
CHINA HELICOPTER RES & DEV INST
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0009] Existing airborne software testing mainly focuses on testing methods, secu

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  • Keyword-driven airborne software automatic test method and system
  • Keyword-driven airborne software automatic test method and system
  • Keyword-driven airborne software automatic test method and system

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Embodiment Construction

[0038] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention provides a keyword-driven airborne software automatic test method and system, and belongs to the field of aviation airborne software test. The method comprises the following steps: extracting a function keyword according to the design scheme of each subsystem of an avionics system, constructing logic input and output of each subsystem according to the function keyword, and meanwhile constructing a logic function of each interface keyword according to an interface control file of the avionics system; constructing a case script comprising a step of quoting the logic input and output of the corresponding subsystem and the logic function of the corresponding interface keyword according to case demands, a step executing the case and a step of judging a case result; and judging whether the airborne software satisfies the design demands according to the case result. By adoption of the test method, the reusability of the test script is improved, and the formation of test assets is facilitated; the cost of regression test is reduced, the test period of the whole process is shortened, the consistency of the test process is guaranteed, and the automation level of the test is improved.

Description

technical field [0001] The invention belongs to the field of aviation airborne software testing, and in particular relates to a keyword-driven airborne software automatic testing method and system. Background technique [0002] Helicopter onboard software has become a key element in aircraft development, playing an increasingly important role in safe flight, information perception, and mission execution. With the continuous increase of software scale and complexity, how to ensure the quality of airborne software and meet the requirements has become an important issue in the development of aircraft. [0003] Software testing is currently the most important means to ensure the quality of software development. Through engineering design, implementation and maintenance of test software, the quality of tested software is measured and improved; emphasis is placed on early testing, independent testing, throughout the software life cycle and covering all user needs Wait. The initi...

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Application Information

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IPC IPC(8): G06F11/36
CPCG06F11/3688
Inventor 孟浩
Owner CHINA HELICOPTER RES & DEV INST
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