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Robust control for a 3-DOF helicopter system based on unknown input observer

机译:基于未知输入观测器的三自由度直升机系统的鲁棒控制

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In this paper, a new robust control method based on an unknown input observer (UIO) is proposed for a benchmark 3-DOF helicopter system to deal with unknown time-varying nonlinear dynamics and disturbances. The objective is to make the helicopter track the given elevation and pitch references. For this purpose, we propose a novel simple UIO to estimate the lumped unknown dynamics, which are then used in the control design as a compensator. By defining the auxiliary filter variables, an invariant manifold is obtained and used to design the UIO. This new estimator needs to set a scalar only and achieves exponential convergence. Then, the proposed control design based on the estimator can achieve accurate output tracking. This control method is applied to a benchmark 3-DOF helicopter to validate the efficacy by simulations and results.
机译:本文针对基准三自由度直升机系统,提出了一种基于未知输入观测器(UIO)的新型鲁棒控制方法,用于处理未知时变非线性动力学和扰动。目的是使直升机跟踪给定的仰角和俯仰基准。为此,我们提出了一种新颖的简单UIO来估算集总未知动态,然后将其用于控制​​设计中作为补偿器。通过定义辅助滤波器变量,可以获得不变的流形,并将其用于设计UIO。这个新的估算器仅需设置一个标量即可实现指数收敛。然后,所提出的基于估计器的控制设计可以实现精确的输出跟踪。此控制方法应用于基准3-DOF直升机,以通过仿真和结果验证功效。

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