Abstract:
The paper presents the lateral acceleration control design of a missile model using the evolution strategy. The non-linear fixed-structure-like controller is represented ...Show MoreMetadata
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Abstract:
The paper presents the lateral acceleration control design of a missile model using the evolution strategy. The non-linear fixed-structure-like controller is represented by the singleton fuzzy model. This allows a variation of shapes of the gain functions to be explored, and subsequent modification is fairly easy. Instead of finding an optimal decomposition of the fuzzy controller, a set of fuzzy rule is unconventionally optimized for the overall gain surfaces that guarantee acceptable performances for the closed-loop system over the whole operating envelope. The simulation results show that the designed fuzzy gain-scheduled controller is a robust tracking controller for all perturbation vertices.
Date of Conference: 08-10 June 2005
Date Added to IEEE Xplore: 01 August 2005
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First Page of the Article