Automatic Test and Fault Diagnosing System of XX Airborne Navigation and Control System

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Abstract:

According to the design and development process of XX Airborne Navigation and Control System, we analyzed the main technology characteristics of design and development for hardware platform, software platform and adapter, and then put forward the realization proposal.

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847-850

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August 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] IEEE Std 993-1 997, IEEE Standard for Test Equipment Description Language( FEDL)[S].

Google Scholar

[2] Chisolm K C, Lisonbee J C. ATLAS Compiler Development[A]. Proceedings of 1999 IEEE AUTOTESTCON[C], SanAntonio: IEEE, 1999. 111-119.

DOI: 10.1109/autest.1999.800365

Google Scholar

[3] Liu Jian, Guo Qiang. A Language Recognizer Generator in the Ada Programming Environment[J]. Journal of Xidian University, 1997, 24(2): 180-186.

Google Scholar

[4] Zheng Qi, Fan Zhongfeng, Liu Jian. The System ofTranstMing Ada 83 to Ada 95[J]. Joumal ofXidian University, 2001, 28(5): 616-620.

Google Scholar

[5] IVI Foundation. IVI-3. 10:IVI MSS Measurement and Stimulus Subsystems Specification, Revision 1. 0[S], (1999).

Google Scholar

[6] IVI Foundation. IVI signal Interface, functional specification, Rev. 0. 3[S], (2000).

Google Scholar