基于鲁棒$H_{\infty}$的二自由度直升机PI控制设计:一种LMI方法

2019 International Conference on Range Technology (ICORT) Pub Date : 2019-02-01 DOI:10.1109/ICORT46471.2019.9069662

J. Goyal, Shubham Aggarwal, Sandip Ghosh, S. Kamal

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引用次数: 1

摘要

本文提出了一种鲁棒LMI调谐PI控制器设计，用于真实的二自由度(2-DOF)直升机模型，并在期望区域定位极点。实验结果证明了该设计的有效性。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Robust $H_{\infty}$ Based PI Control Design For 2-DOF Helicopter: An LMI Approach

This work presents a robust LMI tuned PI controller design for the real two degree of freedom (2-DOF) helicopter model with locating poles in a desired region. Experimental results are provided to demonstrate the effectiveness of the proposed design.

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来源期刊

2019 International Conference on Range Technology (ICORT)

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