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Recessive Trait Crossover Genetic Algorithm Flight Control System Design
A. A. El-Mahallawy,A. A. Madkour,A. M. Yousef,H. A. Yousef,M. I. El-Singaby 제어로봇시스템학회 2008 제어로봇시스템학회 국제학술대회 논문집 Vol.2008 No.10
The requirements, design and simulation of a flight control system for precision tracking task, called pitchrate control augmentation system, is considered. This control system is designed for the F-16 fighter aircraft model using the recessive trait crossover genetic algorithm. The behavior of this controller is compared with that of H¥- mixed sensitivity approach. 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.