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《Measurement & Control Technology》 2008-02
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LabWindows/CVI-Based UAV Fuel Assembly Test System Development

WANG Rui1,LEI Jin-kui2(1.College of Electronics and Information,Northwestern Polytechnical University,Xi'an 710072,China;2.The 365th Institute,Northwestern Polytechnical University,Xi'an 710072,China)  
The UAV fuel assembly system for the design and test research which is based on the virtual instrument technology is stated,and the entire process of the test system structure and working principle is also described.LabWindows/CVI7.0 is used as the test system software development platform,and CompactPCI system structure is selected as a hardware-based program.The result of test shows that the UAV fuel assembly system which is based on the virtual instrument technology can meet the requirements of engineering and test technology.
【CateGory Index】: TP274;TP391.9
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