Abstract
A proposed approach to robust controller design is introduced. This approach combines the recessive trait crossover genetic algorithm with the loop-shaping design procedure using H∞ synthesis. The requirements, design and simulation of a flight control system for precision tracking task are considered. The proposed method is applied to design a control system for the F-16 fighter aircraft model. The flight simulations reveal that the desired performance objectives are achieved and that the controller provides acceptable performance in spite of modeling errors and plant parameter variations.
Original language | English |
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Pages (from-to) | 169-174 |
Number of pages | 6 |
Journal | Expert Systems with Applications |
Volume | 38 |
Issue number | 1 |
DOIs | |
Publication status | Published - Jan 2011 |
Keywords
- Control augmentation system
- Flight simulations
- H loop-shaping
- Recessive trait crossover genetic algorithm
ASJC Scopus subject areas
- General Engineering
- Computer Science Applications
- Artificial Intelligence