Robust Flight Control System Design Using H∞ Loop-Shaping and Recessive Trait Crossover Genetic Algorithm | ||||
The International Conference on Electrical Engineering | ||||
Article 38, Volume 7, 7th International Conference on Electrical Engineering ICEENG 2010, May 2010, Page 1-14 PDF (508.7 K) | ||||
Document Type: Original Article | ||||
DOI: 10.21608/iceeng.2010.32990 | ||||
View on SCiNiTO | ||||
Authors | ||||
A. A. El-Mahallawy1; A. A. Madkour1; A. M. Youssef1; H. A. Yousef2; M. I. El-Singaby3 | ||||
1Egyptian Armed Forces. | ||||
2College of Engineering, Alexandria University. | ||||
3College of Engineering & Technology, Alexandria. | ||||
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. | ||||
Keywords | ||||
Recessive Trait Crossover Genetic Algorithm; H∞ Loop-Shaping; Flight simulations; Control augmentation system | ||||
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