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