一种三自由度直升机模型的状态依赖区域极点配置控制器设计

Ahmet Cagri Arican, Engin Hasan Çopur, G. Inalhan, M. U. Salamci
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引用次数: 0

摘要

对于线性系统,由于极点的位置是唯一的,可以很容易地设计一个状态反馈控制律来保持所有闭环极点在指定的磁盘内。然而,它在非线性系统中的应用并不是那么简单。因此,本文提出了一种新的非线性系统极点配置方法——状态相关区域极点配置方法。该方法产生一种状态相关的反馈控制律,使闭环矩阵的特征值被放置在指定的磁盘上,以达到期望的控制性能特征。在三自由度直升机实验装置上验证了该方法的有效性。为了验证其有效性,将非线性方法的实验结果与线性方法的实验结果进行了比较。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
State Dependent Regional Pole Assignment Controller Design for a 3-DOF Helicopter Model
For linear systems, a state feedback control law can be easily designed to keep all closed-loop poles inside a specified disk since the locations of the poles are unique. However, its application to nonlinear systems is not so simple. Therefore, this paper introduces a new pole placement method, named as State Dependent Regional Pole Assignment, for nonlinear systems. This proposed method produces a state dependent feedback control law, enabling the eigenvalues of the closed-loop matrix to be placed in a specified disk to achieve the desired control performance characteristics. The effectiveness of the method is tested on the 3 DOF Helicopter experimental setup. To verify its effectiveness, the experimental results of the nonlinear method are compared with those of the linear method.
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