Design and Realization of a Certain Missile Servo Mechanism Test System

Dong Yu Zhang; Xu De Cheng; Bing Xu; Xue Dong Xue; Cheng Peng Jiang

doi:10.4028/www.scientific.net/AMR.466-467.1020

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 466-467Design and Realization of a Certain Missile Servo...

Design and Realization of a Certain Missile Servo Mechanism Test System

Abstract:

To improve the efficiency and precision of missile servo mechanism testing, as the research object, a certain missile servo mechanism was studied in this paper. Based on PC/104 bus and virtual instrument technique, a missile servo mechanism automatic test system was presented, and the design and development on hardware and software of the system was described in detail. The system, which is featured with its simple operation, high precision, high reliability, scalable and portable test software, has been proved to be feasible by the test result.

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Periodical:

Advanced Materials Research (Volumes 466-467)

Pages:

1020-1024

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.466-467.1020

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Online since:

February 2012

Authors:

Dong Yu Zhang, Xu De Cheng, Bing Xu, Xue Dong Xue, Cheng Peng Jiang

Keywords:

Dynamic Test System, LabVIEW, PC/104, Servo Mechanism

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References

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