Design of a Virtual Automatic Test System of the Missile Autopilot

Gui Fang Cai

doi:10.4028/www.scientific.net/AMM.543-547.1377

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 543-547Design of a Virtual Automatic Test System of the...

Design of a Virtual Automatic Test System of the Missile Autopilot

Abstract:

To improve the test speed and efficiency, a virtual automatic test system of missile autopilot is designed. The inbuilt computer is used as the core of the system; the modularization instrument bus standard which composed of the PXI card, the programmable instrument and other advanced test techniques is adopted. The automation test device hardware facility is used in the virtual automatic test system; the pilot mechanism fault analysis software is developed, so the faults of the missile autopilot can be located faster and more accurate. The virtual automatic test system can be used to test the current parameters, special capability and the function of the electronic parts among the missile weapon system.

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Periodical:

Applied Mechanics and Materials (Volumes 543-547)

Pages:

1377-1380

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.543-547.1377

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Cite this paper

Online since:

March 2014

Authors:

Gui Fang Cai*

Keywords:

Artificial Neural Network (ANN), Fault Diagnosis, Fault Isolation, Feedback, Flight Control System

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* - Corresponding Author

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DOI: 10.1109/3477.938255

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