Robust finite-time sliding mode control of twin rotor MIMO system

被引：2

作者：

Raj, Kaushik ^{[1
]}

Choudhary, Santosh Kumar ^{[2
]}

Muthukumar, Venkatesan ^{[1
]}

机构：

[1] Department of Electrical and Computer Engineering, University of Nevada Las Vegas, Las Vegas,NV,89154, United States

[2] Manipal Institute of Technology, Manipal Academy of Higher Education, Manipal, Karnataka,576104, India

来源：

International Journal of Modelling, Identification and Control | 2020年 / 35卷 / 01期

关键词：

Sliding mode control - MIMO systems - Aircraft control - Nonlinear systems - Stabilization;

D O I：

10.1504/IJMIC.2020.113292

中图分类号：

学科分类号：

摘要：

In this paper, a robust finite-time sliding mode control (SMC) of the twin rotor MIMO system (TRMS) is discussed. This helicopter laboratory model is highly nonlinear in characteristics and coupling dynamics between main and tail rotors. The main purpose of this paper is to investigate finite-time SMC for pitch and yaw angles of TRMS, either for posture stabilisation or trajectory tracking. Moreover, these angles are used commonly to determine the hovering posture of a helicopter. The paper first briefs the dynamical model of TRMS and then it adopts a finite-time SMC technique to achieve the desired trajectory or posture stabilisation. Numerical simulation results are demonstrated and verify the effectiveness of the control technique. © 2020 Inderscience Enterprises Ltd.. All rights reserved.

引用

页码：1 / 8

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