General Test System of Airplane Power Supply Product Based on PC/104 Bus
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TP274 V242

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    Abstract:

    The article introduces a suit of general electric parameter test system of airplane power supply products based on PC/104 bus and virtual instrument technology in detail and the principles of software and hardware realization method are presented. The design principle of this test system is discussed. Finally, combining with the design of the overall system, the design and realization of the test system software under LabVIEW development environment are introduced.

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  • Received:
  • Revised:October 19,2004
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