基于内部1553B总线的航天器控制系统可测试性框架设计与验证

doi:10.3969/j.issn.1674-1579.2014.02.005

Abstract

Abstract: Design for testability (DFT) is an important approach to improve the manufacturing efficiency and test quality of a system. The hierarchical structure of DFT for AOCS of spacecraft based on 1553B bus architecture is given and the model frame of DFT is built. The technical realization of DFT is also analyzed. The software TEAMS(testability engineering and maintenance system) is used to simulate and evaluate the DFT via an example and the simulation result demonstrates the validity of this method.

Key words: DFT, testability standards, busbased configuration, control system of spacecraft

CLC Number:

WANG Hai-Bo, YUAN Li. Frame Design and Verification of DFT Technique for Control System of Spacecraft Based on 1553B Bus Architecture[J]., 2014, 40(2): 26-30.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2014.02.005

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2014/V40/I2/26

References

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Frame Design and Verification of DFT Technique for Control System of Spacecraft Based on 1553B Bus Architecture

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