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A Boundary Control Method for Suppressing Flexible Wings Vibration of the FMAV

机译:一种抑制FMAV柔性翼振动的边界控制方法

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In this paper, we propose a boundary control strategy for vibration suppression of two flexible wings and a rigid body. As a basic approach, Hamilton's principle is used to ascertain the system dynamic model, which includes governing equations and boundary conditions. Considering the coupled bending and torsional deformations of flexible wings, boundary control force and torque act on the rigid body to regulate unexpected deformations of flexible wings that caused by air flow. Then, we present stability analysis of the closed-loop system through Lyapunov's direct method. Simulations are carried out by using finite difference method. The results illustrate the significant effect of the developed control strategies.
机译:在本文中,我们提出了一种用于振动抑制两个柔性翼的边界控制策略和刚体。作为一种基本方法,汉密尔顿的原理用于确定系统动态模型,包括管理方程和边界条件。考虑到柔性翼的耦合弯曲和扭转变形,边界控制力和扭矩在刚体上的扭矩作用,以调节气流引起的柔性翼的意外变形。然后,我们通过Lyapunov的直接方法呈现闭环系统的稳定性分析。利用有限差分法进行仿真。结果说明了发达的控制策略的显着效果。

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