Abstract
AbstractThis paper presents a control design trade study related to robust and adaptive control methods for an autonomous aerial platform representative of the Boeing / USAF X-45A Joint Unmanned Combat Air System (J-UCAS). Control architectures and methodologies selected for this study include a robust baseline augmented by a direct adaptive model reference controller with various recently developed modifications. Specifically, inner-loop flight control design using robust adaptive methods is performed, and closed-loop system tracking performance is demonstrated in simulation environment.
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