Evolutionary control mode analysis
Evolutionary control mode analysis
The control configuration design problem is to find appropriate sets of closed - and/or open-loop controls to meet the desired specification including performance, complexity and economic considerations whilst the choice of the final controller configuration is determined by analysis of the acceptable control models. This paper has considered an approach to the problem of control mode analysis based on the use of multiobjective evolutionary algorithms for the search and optimization of suitable control configurations. The proposed method differs from currently available techniques in that it allows a number of potential configurations to be identified and compared with one another, highlighting both the positive and negative aspects of each individual scheme, in a single framework - hopefully realizing a more informed and efficient design process. As aero-engines become more complex and greater numbers of parameters become controllable and measurable, the need for such tools will increase.
Chipperfield, A.J.
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Betteridge, H.C.
9b5ae06d-8806-4162-acab-b7efab2e5bc2
Fleming, P.J.
2264e51b-cddd-4db4-ae8d-7f970564bb0e
18 February 1997
Chipperfield, A.J.
524269cd-5f30-4356-92d4-891c14c09340
Betteridge, H.C.
9b5ae06d-8806-4162-acab-b7efab2e5bc2
Fleming, P.J.
2264e51b-cddd-4db4-ae8d-7f970564bb0e
Chipperfield, A.J., Betteridge, H.C. and Fleming, P.J.
(1997)
Evolutionary control mode analysis.
In IEE Colloquium (Digest).
Record type:
Conference or Workshop Item
(Paper)
Abstract
The control configuration design problem is to find appropriate sets of closed - and/or open-loop controls to meet the desired specification including performance, complexity and economic considerations whilst the choice of the final controller configuration is determined by analysis of the acceptable control models. This paper has considered an approach to the problem of control mode analysis based on the use of multiobjective evolutionary algorithms for the search and optimization of suitable control configurations. The proposed method differs from currently available techniques in that it allows a number of potential configurations to be identified and compared with one another, highlighting both the positive and negative aspects of each individual scheme, in a single framework - hopefully realizing a more informed and efficient design process. As aero-engines become more complex and greater numbers of parameters become controllable and measurable, the need for such tools will increase.
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Published date: 18 February 1997
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Local EPrints ID: 470244
URI: http://eprints.soton.ac.uk/id/eprint/470244
PURE UUID: a278017f-eda2-46fe-9b35-37f16d247f4a
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Date deposited: 05 Oct 2022 16:33
Last modified: 23 Feb 2023 02:45
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Author:
H.C. Betteridge
Author:
P.J. Fleming
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