Architectural optimisation of distributed control systems for aero gas turbine engines using genetic algorithms

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Standard

Architectural optimisation of distributed control systems for aero gas turbine engines using genetic algorithms. / Bourne, Duncan; Dixon, Roger; Horne, Alex.

47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011. 2011.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Harvard

Bourne, D, Dixon, R & Horne, A 2011, Architectural optimisation of distributed control systems for aero gas turbine engines using genetic algorithms. in 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011. 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011, San Diego, CA, United States, 31/07/11.

APA

Bourne, D., Dixon, R., & Horne, A. (2011). Architectural optimisation of distributed control systems for aero gas turbine engines using genetic algorithms. In 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011

Vancouver

Bourne D, Dixon R, Horne A. Architectural optimisation of distributed control systems for aero gas turbine engines using genetic algorithms. In 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011. 2011

Author

Bourne, Duncan ; Dixon, Roger ; Horne, Alex. / Architectural optimisation of distributed control systems for aero gas turbine engines using genetic algorithms. 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011. 2011.

Bibtex

@inproceedings{b567a9b8610d4e348bf8f24825bb15b3,
title = "Architectural optimisation of distributed control systems for aero gas turbine engines using genetic algorithms",
abstract = "The design of distributed control systems (DCSs) for large, civil gas turbine engines is an inherently difficult architectural challenge. To date, the majority of research into DCSs has focused on the contributing technologies and high temperature electronics rather than the architecture of the system itself. This paper proposes a method for the architectural design of distributed systems using a genetic algorithm to generate, evaluate and refine designs. The method is presented along with results proving the concept.",
author = "Duncan Bourne and Roger Dixon and Alex Horne",
year = "2011",
month = dec,
day = "1",
language = "English",
isbn = "9781600869495",
booktitle = "47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011",
note = "47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 ; Conference date: 31-07-2011 Through 03-08-2011",

}

RIS

TY - GEN

T1 - Architectural optimisation of distributed control systems for aero gas turbine engines using genetic algorithms

AU - Bourne, Duncan

AU - Dixon, Roger

AU - Horne, Alex

PY - 2011/12/1

Y1 - 2011/12/1

N2 - The design of distributed control systems (DCSs) for large, civil gas turbine engines is an inherently difficult architectural challenge. To date, the majority of research into DCSs has focused on the contributing technologies and high temperature electronics rather than the architecture of the system itself. This paper proposes a method for the architectural design of distributed systems using a genetic algorithm to generate, evaluate and refine designs. The method is presented along with results proving the concept.

AB - The design of distributed control systems (DCSs) for large, civil gas turbine engines is an inherently difficult architectural challenge. To date, the majority of research into DCSs has focused on the contributing technologies and high temperature electronics rather than the architecture of the system itself. This paper proposes a method for the architectural design of distributed systems using a genetic algorithm to generate, evaluate and refine designs. The method is presented along with results proving the concept.

UR - http://www.scopus.com/inward/record.url?scp=84880652889&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84880652889

SN - 9781600869495

BT - 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011

T2 - 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011

Y2 - 31 July 2011 through 3 August 2011

ER -