Design and Realization of an Avionics Equipment Testability Model Based on TADS

Article Preview

Abstract:

The testability design becomes one of important works to do during a design process of a system and en equipment. Whereas, the testability labor of current avionics equipments are performed after design and most of its testability results are acquired by manual statistic. In this article, taking an aviation radio’s power supply model for example, a testability model is designed based on TADS and the scientificity and practicability of this model is testified by realizing fault separation by GPTS.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

964-967

Citation:

Online since:

September 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Tian Zhong, SHI Jun-you. Design, analysis and verification for system testability [M]. Beijing: Press of Beijing University of Aeronautics & Astronautics, (2003).

Google Scholar

[2] ZANG Tian-xiang. Testability and Diagnosis Technology of Electric Devices[M]. Beijing: Press of Aeronautics Industry, (1995).

Google Scholar

[3] MIL-STD-2165AN1 Testability Program [S].

Google Scholar

[4] Kang zhong-wei. Study of Testability Design [J]. Micro-computer Information, 2008, 1-157-159.

Google Scholar

[5] Yang zhi-yong, Xu hua-long, Xu ai-qiang. Design of Multiple Fault diagnosis systems [J]. Computer Measurement and Control , 2006, 12 (4): 1616-1619.

Google Scholar