Lightweight visual satellite testing program design system and method

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...

AI Technical Summary

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 traditional test mode. Standardized and error-prone problems, while greatly improving the efficiency of test program design and the standardization level of the design process, at the same time, it has realized the controllable and credible management of the entire life cycle of the test program in the AIT stage of the whole star

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