Abstract
A multi-stage design approach that uses a multiobjective genetic algorithm as the framework for optimization and multiobjective preference articulation, and an H_infty loop-shaping technique are used to design controllers for a gas turbine engine. A non-linear model is used to assess performance of the controller. Because the computational load of applying multiobjective genetic algorithm to this control strategy is very high, a neural network and response surface models are used in order to speed up the design process within the framework of a multiobjective genetic algorithm. The final designs are checked using the original non-linear model.
Original language | English |
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Pages (from-to) | 392-401 |
Number of pages | 10 |
Journal | Applied Soft Computing Journal |
Volume | 8 |
Issue number | 1 |
DOIs | |
Publication status | Published - 2008 Jan |
Keywords
- H_infty control
- Multiobjective genetic algorithms
- Neural networks
- Optimization
- Variable complexity modelling
ASJC Scopus subject areas
- Software
- Computer Science Applications
- Artificial Intelligence