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Construction method of airborne computer software testing general system

An airborne computer and software testing technology, which is applied in the field of software static testing, unit/integration testing, system testing, and the construction of a general system for airborne computer software testing, which can solve the problems of difficult reliability assurance, high testing costs, and error positioning Long time and other issues, to achieve the effect of ensuring reliability and timeliness, improving standardization, and reducing testing costs

Inactive Publication Date: 2010-09-29
BEIHANG UNIV
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  • Abstract
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  • Claims
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AI Technical Summary

Problems solved by technology

According to the experience of embedded software development abroad in recent years, the reliability of application software developed in this mode is difficult to guarantee, the error positioning time is long, and the post-test cost is high

Method used

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  • Construction method of airborne computer software testing general system
  • Construction method of airborne computer software testing general system
  • Construction method of airborne computer software testing general system

Examples

Experimental program
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Embodiment Construction

[0058] Below in conjunction with accompanying drawing, each part design method in the present invention will be further described:

[0059] The invention is an airborne computer software testing general system, the development environment is based on Tornado2.2, the corresponding target board operating system can be Vxworks5.5 or 6.0, and the upper computer adopts the Windows XP environment. Automated testing tools in the unit / integration testing process can use either Logiscope or C++Test. The specific design steps of the system are as follows:

[0060] Step 1: Write a test plan document and establish a test system

[0061] 1) Write the required business, explain the users and functions, and then formulate the "Test Requirements Analysis" according to the requirements.

[0062] The position of the entire testing process in software system development is as follows: figure 1 As shown, the testing work runs through the whole process of project requirements and design. In "T...

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PUM

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Abstract

The invention relates to a construction method of an airborne computer software testing general system, which comprises five steps: 1, writing a testing plan file and establishing a testing system; 2, carrying out a unit test (static) during code development; 3, carrying out a unit / integration test (dynamic) by an actual operation function module; 4, carrying out a system test after the unit / integration test; and 5, carrying out an acceptance test. The invention provides the airborne computer software testing general system which achieves the testing purpose economically and effectively via establishing a testing system collateral with the code development, and enhances the normalization and reliability of the software system, and the software testing personal can completely and efficiently deploy and execute testing work according to specific needs. The invention has practical value and broad application prospects in the technical field of the airborne computer software test.

Description

technical field [0001] The invention relates to a construction method of a general system for airborne computer software testing, belongs to the technical field of airborne computer software testing, and specifically relates to software static testing, unit / integration testing, system testing, and the like. Background technique [0002] Airborne computer software belongs to the field of embedded software. In recent years, due to the gradual enhancement of software functions and the gradual expansion of scale, the demand for testing has become increasingly apparent, and it is developing towards standardization and systematization. According to the principles of software engineering, the airborne computer software testing process can be divided into two parts: static testing and dynamic testing. Static testing is mainly to check the programming format and structure of the software after the codes of each functional module of the flight control software are written. Dynamic te...

Claims

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Application Information

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IPC IPC(8): G06F11/36
Inventor 郑泽伟胡轶之祝明
Owner BEIHANG UNIV
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