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Robust H_∞ Control of Theodorsen's Lift Model for a Pitching and Plunging Airfoil Using LMI Approach

机译:基于LMI方法的俯仰和俯冲翼型Theodorsen升力模型的鲁棒H_∞控制

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This paper develops a robust H_∞ controller for a pitching and plunging airfoil using the state space representation of Theodorsen's lift model employing the linear matrix inequalities (LMI) method. Both parameter uncertainty and the input disturbances are considered in the model. The existence condition for the robust H_∞ state-feedback controller is obtained using the Lyapunov functional approach. In practical systems, it is difficult to obtain all the states of the model needed for the controller. Thus the observer existence condition is proposed to provide the states' information for the model. Several examples are used to demonstrate the effectiveness of the designed controller and the designed observer.
机译:本文使用基于线性矩阵不等式(LMI)方法的西奥多森升力模型的状态空间表示,开发了一种用于俯仰和俯冲翼型的鲁棒H_∞控制器。模型中同时考虑了参数不确定性和输入干扰。使用Lyapunov函数方法获得了鲁棒H_∞状态反馈控制器的存在条件。在实际系统中,很难获得控制器所需的所有模型状态。因此,提出了观察者的存在条件来为模型提供状态信息。使用几个示例来证明所设计的控制器和所设计的观察者的有效性。

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