Robust Command Augmentation System Design Using Genetic Methods
نویسندگان
چکیده
This paper describes the use of a genetic search method in the design of a command augmentation system for a high-performance aircraft. A genetic algorithm is used to design H-infinity controllers for the longitudinal and lateral-directional channels. The integral of absolute value of error between actual response and that of an ideal model is used as the fitness criterion. Starting from an initial population of weighting functions, the algorithm generates new functions with the goal of improving the fitness.
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