Design and Application of Virtual Instrument Detection System for Aerodynamic Instrument

Ping Zhang; Kun Li; Xiao Shu Sun; Xian Wen Gao

doi:10.4028/www.scientific.net/AMR.508.166

Paper Titles

High-Resolution Ultrasonic Spectroscopy for Crystallization Process
p.146

Development of an Embedded High-Temperature Field Measuring Instrument
p.151

Segregation Diagram of a Mixture of Particles with Different Sizes and Densities
p.155

Deformation Modes for Assemblies of Frictionless Polydisperse Spheres
p.160

Design and Application of Virtual Instrument Detection System for Aerodynamic Instrument
p.166

Simulation Study of Spiral Electrode Capacitance Sensor for Measuring Concentration of Gas-Solid Two-Phase Flow
p.170

Population Balance Modelling and Experimental Validation for Synthesis of TiO₂ Nanoparticles Using Continuous Hydrothermal Process
p.175

An Experimental Study on the Characteristics of Nanoparticles Emission from a Vehicle
p.180

Preparation of Super-Fine Cerium Oxide Using Mechanically Chemical Method
p.184

HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 508Design and Application of Virtual Instrument...

Design and Application of Virtual Instrument Detection System for Aerodynamic Instrument

Abstract:

Aerodynamic instruments are widely used in various kinds of industrial equipment, which have many types and complex structure. The traditional instrument detection methods require replacing a variety of testing equipment frequently. Their testing efficiencies are low and the testing equipments are hard to be integrated together. Virtual instrument technology is a hot detection technology in recent years with high detection accuracy and integration, which has a good solution to the problems of traditional detection methods. First of all, this paper introduces an overall design scheme for the virtual detection system. Secondly, for properties of longer response time, overshoot, and difficulties in establishing precise mathematical model of the pneumatic control system, this paper uses fuzzy PID control method to control the pneumatic output pressure. Finally, the virtual detection system is realized based on LabVIEW software platform. This system is applied to the detection of fixed-wing aircraft aerodynamic instrument, and has satisfactory results.

You might also be interested in these eBooks

Measurement and Control of Granular Materials

View Preview

Info:

Periodical:

Advanced Materials Research (Volume 508)

Pages:

166-169

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.508.166

Citation:

Cite this paper

Online since:

April 2012

Authors:

Ping Zhang, Kun Li, Xiao Shu Sun, Xian Wen Gao

Keywords:

Aerodynamic Instrument, Fuzzy PID, LabVIEW, Virtual Instrument Technology

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Pneumatic principles and calibration[M], BEI Jing: National Defence Industry Press, 1977, pp.1-282.

Google Scholar

[2] Wang Shu-yan, Shi Yu, Feng Zhong-xu. A Method for Controlling a Loading System Based on a Fuzzy PID Controller[J]. Mechanical Science and Technology for Aerospace Engineering, 301 (2011): 166-172.

Google Scholar

[3] A. H. Taner, Virtual Instrumentation: a solution to the problem of design complexity in intelligent instruments[J], Measurement/Control, (1997).

Google Scholar

[4] Stanislaw L, Randzio. Towards a global virtual instrument control and a virtual link between experiment and modeling[J], Thermochimica Acta, 355(2000): 107-133.

Google Scholar

[5] Salvatore Nuccio, Ciro Spataro. Assessment of virtual instruments measurement uncertainty[J], Computer Standards&Interfaces, 23(2001): 39-46.

DOI: 10.1016/s0920-5489(01)00058-7

Google Scholar