Application of H_∞ Control Problem to the Identification of Pilot's Control Law in Aircraft Attitude Control(ABSTRACTS OF PROCEEDINGS OF THE SCHOOL OF ENGINEERING SERIES J TOKAI UNIVERSITY -2003-2004-)
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概要
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The H_∞, control theory is effective for the performance and stability analyses of a system with uncertain controlled elements. The synthesis of the controller for such uncertain systems is called the H_∞ control problem. We applied a solution method for the H_∞ control problem to the identification of the human pilot as an aircraft controller. Experiments using a flight simulator were also carried out and compared to the derived H_∞ controller. We found that the application of the solution method for the H_∞ control problem has a large possibility of becoming an effective tool for the identification of a human pilot and analysis of the closed-loop system's performance and stability.
著者
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Kobayashi Osamu
Department Of Aeronautics And Astronautics
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Kiritani Minoru
Course Of Aeronautics And Astronautics
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