DocumentCode :
2164500
Title :
Systems integration using evolutionary algorithms
Author :
Chipperfield, A.J. ; Fleming, P.J.
Author_Institution :
Sheffield Univ., UK
Volume :
1
fYear :
1996
fDate :
2-5 Sept. 1996
Firstpage :
705
Abstract :
This paper describes an approach to the systems integration problem using multiobjective genetic algorithms. An architecture for evolutionary systems integration is presented and the component parts discussed. An example of an aircraft gas turbine engine control system design problem is shown demonstrating aspects of the proposed architecture that allow many design objectives from different disciplines to be considered in parallel. Potential closed-loop control configurations are evaluated and compared against one another within an optimization framework. As a result of this analysis, it is shown how informed decisions may be made regarding the nature of the control employed, acceptable performance margins and elements of the engine design.
Keywords :
aerospace engines; aircraft control; closed loop systems; control system synthesis; gas turbines; genetic algorithms; performance index; aircraft; closed-loop control; evolutionary algorithms; gas turbine engine control system; multiobjective genetic algorithms; optimization; performance margins; systems integration;
fLanguage :
English
Publisher :
iet
Conference_Titel :
Control '96, UKACC International Conference on (Conf. Publ. No. 427)
ISSN :
0537-9989
Print_ISBN :
0-85296-668-7
Type :
conf
DOI :
10.1049/cp:19960637
Filename :
651465
Link To Document :
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