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ROBUST H_∞ HYBRID OBSERVER-CONTROLLER DESIGN WITH APPLICATION TO ATTITUDE CONTROL OF 2-DOF HELICOPTER

机译:鲁棒H_∞混合观测器 - 控制器设计,适用于2-DOF直升机的姿态控制

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摘要

In this paper, a class of uncertain piecewise affine (PWA) systems, subject to system and measurement external disturbances are studied. The uncertainties are assumed to be norm bounded and the external disturbance signals belong to the L_2 space. The problem of optimizing the system response in the H_∞ sense, by means of a piecewise affine observer-controller, is formulated as an optimization problem subject to a number of constraints in the form of matrix inequalities. The derived constraints are obtained by considering a partially piecewise quadratic Lyapunov function in combination with the general conditions for H_∞ stability. Then the uncertain PWA approximation of the nonlinear attitude dynamics of a simplified helicopter model, subject to system and measurement external disturbances, is presented. The uncertainties arise in the form of the difference between the actual nonlinear dynamics and the PWA approximation. Utilizing the introduced methods, a robust PWA observer-controller is designed and implemented on the simplified nonlinear helicopter model to demonstrate the effectiveness of the proposed observer-controller design method.
机译:本文研究了一类不确定的分段仿射(PWA)系统,受系统和测量外部干扰。假设不确定因素是常态的,外部干扰信号属于L_2空间。通过分段仿射观察者控制器优化H_∞感觉中的系统响应的问题,被制定为经受矩阵不等式形式的许多约束的优化问题。通过考虑局部分段二次Lyapunov函数与H_‖稳定性的一般条件相结合来获得衍生的约束。然后,提出了经过系统和测量外部干扰的简化直升机模型的非线性姿态动态的不确定PWA近似。不确定性以实际非线性动态和PWA近似之间的差异的形式出现。利用介绍的方法,在简化的非线性直升机模型上设计和实现了一种坚固的PWA观察者控制器,以证明所提出的观察者控制器设计方法的有效性。

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