【摘 要】
：
In this study,robust control theory is used to design a robust controller for suppression of transonic limit cycle oscillations induced by aerodynamic nonlinearities.
【机 构】
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Nanjing University of Aeronautics and Astronautics
【出 处】
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The 5th International Conference on Dynamics, Vibration and
论文部分内容阅读
In this study,robust control theory is used to design a robust controller for suppression of transonic limit cycle oscillations induced by aerodynamic nonlinearities.
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