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Reseach Article

Fuzzy Assisted PI Controller with Anti-reset wind up for Regulating Pressure in a Hypersonic Wind Tunnel

Published on None 2011 by Rini Jones S.B, Dr. P.Poongodi, Binu L.S
Artificial Intelligence Techniques - Novel Approaches & Practical Applications
Foundation of Computer Science USA
AIT - Number 2
None 2011
Authors: Rini Jones S.B, Dr. P.Poongodi, Binu L.S
db0ac59d-403b-4fdb-859e-d5d1f6831f90

Rini Jones S.B, Dr. P.Poongodi, Binu L.S . Fuzzy Assisted PI Controller with Anti-reset wind up for Regulating Pressure in a Hypersonic Wind Tunnel. Artificial Intelligence Techniques - Novel Approaches & Practical Applications. AIT, 2 (None 2011), 7-11.

@article{
author = { Rini Jones S.B, Dr. P.Poongodi, Binu L.S },
title = { Fuzzy Assisted PI Controller with Anti-reset wind up for Regulating Pressure in a Hypersonic Wind Tunnel },
journal = { Artificial Intelligence Techniques - Novel Approaches & Practical Applications },
issue_date = { None 2011 },
volume = { AIT },
number = { 2 },
month = { None },
year = { 2011 },
issn = 0975-8887,
pages = { 7-11 },
numpages = 5,
url = { /specialissues/ait/number2/2829-210/ },
publisher = {Foundation of Computer Science (FCS), NY, USA},
address = {New York, USA}
}
%0 Special Issue Article
%1 Artificial Intelligence Techniques - Novel Approaches & Practical Applications
%A Rini Jones S.B
%A Dr. P.Poongodi
%A Binu L.S
%T Fuzzy Assisted PI Controller with Anti-reset wind up for Regulating Pressure in a Hypersonic Wind Tunnel
%J Artificial Intelligence Techniques - Novel Approaches & Practical Applications
%@ 0975-8887
%V AIT
%N 2
%P 7-11
%D 2011
%I International Journal of Computer Applications
Abstract

Wind tunnels are being used to study the aerodynamic properties of race cars, fighter planes etc. It allows us to make a reusable prototype and test it in the tunnel. Hypersonic wind tunnels operate at hypersonic speeds ie, with a mach number greater than 6. For doing experiments, it is necessary to maintain a constant pressure in the settling chamber of the tunnel so that we get the desired Mach number and mass flow rate through the nozzle. Here, a fuzzy assisted PI control system incorporating anti reset wind up is developed for regulating the pressure and hence a constant mass flow rate in the hypersonic intermittent blow down type wind tunnel and the results obtained are analised

References
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Index Terms

Computer Science
Information Sciences

Keywords

Hypersonic wind tunnel anti reset windup fuzzy assisted PI controller fuzzy assisted PI controller