Lightweight visual satellite testing program design system and method

A testing program and satellite testing technology, applied in program control devices, visual/graphics programming, software testing/debugging, etc., can solve problems such as error-prone, non-standard version control of test program data, and low efficiency of test program design. Improve design efficiency, efficient test program design and optimization, and achieve the effect of controllable and credible management

Active Publication Date: 2016-04-13
CHINA ACADEMY OF SPACE TECHNOLOGY
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  • Application Information

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Problems solved by technology

[0005] The technical problem of the present invention is: to overcome the deficiencies of the prior art, to provide a light-weight visual satellite test program design system and method, which effectively solves the problem of low efficiency of test program design and insufficient version control of test program data in the tra

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  • Lightweight visual satellite testing program design system and method
  • Lightweight visual satellite testing program design system and method
  • Lightweight visual satellite testing program design system and method

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Embodiment Construction

[0031] Such as figure 1 As shown, a light-weight visual satellite test program design system of the present invention is based on the B / SWeb system MVC architecture design concept, and realizes an intuitive and easy-to-use satellite test program interactive design environment, covering the satellite test program design. all functional elements. Users do not need to install any test program design software on the local machine, and do not need to perform any test design configuration operations. They only need to log in to the system with any general-purpose browser, and then they can call the general functional components of the system through a simple drag operation in the visual interactive design environment. and custom project components to efficiently complete test program design, optimization, approval, test task assignment and test program version control based on a unified data source, thus greatly improving the efficiency of test program design and the standardization...

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Abstract

The invention relates to a lightweight visual satellite testing program design system and method. The lightweight visual satellite testing program design system comprises a uniform data source management module, an authority control module, a custom component module, a universal functional component library module, a test item component library module, a visual testing program design module, a testing program optimization module, a testing program auditing module, a testing program archiving module and a test task distribution module. According to the invention, testing program design efficiency and the standardization level of the design process are greatly improved, and the lightweight visual satellite testing program design system and method are applicable to testing program design of spacecrafts of various types.

Description

technical field [0001] The invention relates to a light-weight visual satellite test program design system and method, which belongs to the technical field of spacecraft automatic testing, and is suitable for comprehensive testing of various spacecraft such as communication satellites, navigation satellites, early warning satellites, remote sensing satellites, and manned spacecraft. . Background technique [0002] Satellite comprehensive testing usually includes three stages: test design, test implementation, and test result evaluation. Test program design is the core content of the test design stage, and the design efficiency and correctness of the test program will directly affect the validity and test cycle of the satellite comprehensive test. [0003] Satellite model, test phase, satellite telemetry parameters, parameter information, remote control instructions, test items, test outline, and test rules are all basic business data necessary for satellite comprehensive te...

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Application Information

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IPC IPC(8): G06F9/44G06F11/36
CPCG06F8/34G06F11/3628
Inventor 刘志飘魏振超温洁
Owner CHINA ACADEMY OF SPACE TECHNOLOGY
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