Sampled-Data Based Fault-Tolerant Control Design for Uncertain CE151 Helicopter System with Random Delays: Takagi-Sugeno Fuzzy Approach

This study inspects the issue of robust reliable sampled data control (SDC) for a class of Takagi-Sugeno (TS) fuzzy CE151 Helicopter systems with time-varying delays and linear fractional uncertainties. Specifically, both the variation range and the distribution probability of the time delay are con...

Full description

Bibliographic Details
Main Authors: V. Dhanya, A. Arunkumar, Kantapon Chaisena
Format: Article
Language:English
Published: MDPI AG 2022-09-01
Series:Fractal and Fractional
Subjects:
Online Access:https://www.mdpi.com/2504-3110/6/9/498
_version_ 1797488156098953216
author V. Dhanya
A. Arunkumar
Kantapon Chaisena
author_facet V. Dhanya
A. Arunkumar
Kantapon Chaisena
author_sort V. Dhanya
collection DOAJ
description This study inspects the issue of robust reliable sampled data control (SDC) for a class of Takagi-Sugeno (TS) fuzzy CE151 Helicopter systems with time-varying delays and linear fractional uncertainties. Specifically, both the variation range and the distribution probability of the time delay are considered in the control input. The essential aspect of the suggested results in this study is that the time variable delay in the control input is dependent not only on the bound but also on the distribution probability of the time delay. The prime intent of this study is to enhance a state feedback reliable sampled-data controller. By constructing an appropriate Lyapunov-Krasovskii functional (LKF) and employing a linear matrix inequalities (LMIs) approach, a new set of delay-dependent necessary conditions is obtained to ensure the asymptotic stabilisation of a TS fuzzy CE151 Helicopter system with a prescribed mixed <i>H</i><sub>∞</sub> and passivity (M<i>H</i><sub>∞</sub>P) performance index. The acquired results are expressed as LMIs, which are easily addressed using standard optimization algorithms. In addition, an exemplary scenario based on the CE151 helicopter model is presented to demonstrate the less conservative nature of the obtained results as well as the application of the recommended unique design approaches.
first_indexed 2024-03-09T23:59:01Z
format Article
id doaj.art-108e051b3cfb4eaeac1f441ccc29c232
institution Directory Open Access Journal
issn 2504-3110
language English
last_indexed 2024-03-09T23:59:01Z
publishDate 2022-09-01
publisher MDPI AG
record_format Article
series Fractal and Fractional
spelling doaj.art-108e051b3cfb4eaeac1f441ccc29c2322023-11-23T16:19:40ZengMDPI AGFractal and Fractional2504-31102022-09-016949810.3390/fractalfract6090498Sampled-Data Based Fault-Tolerant Control Design for Uncertain CE151 Helicopter System with Random Delays: Takagi-Sugeno Fuzzy ApproachV. Dhanya0A. Arunkumar1Kantapon Chaisena2Electrical Engineering Department, National Taiwan Ocean University, Keelung 202, TaiwanElectrical Engineering Department, National Taiwan Ocean University, Keelung 202, TaiwanDepartment of Mathematics, Faculty of Science and Technology, Phuket Rajabhat University, Phuket 83000, ThailandThis study inspects the issue of robust reliable sampled data control (SDC) for a class of Takagi-Sugeno (TS) fuzzy CE151 Helicopter systems with time-varying delays and linear fractional uncertainties. Specifically, both the variation range and the distribution probability of the time delay are considered in the control input. The essential aspect of the suggested results in this study is that the time variable delay in the control input is dependent not only on the bound but also on the distribution probability of the time delay. The prime intent of this study is to enhance a state feedback reliable sampled-data controller. By constructing an appropriate Lyapunov-Krasovskii functional (LKF) and employing a linear matrix inequalities (LMIs) approach, a new set of delay-dependent necessary conditions is obtained to ensure the asymptotic stabilisation of a TS fuzzy CE151 Helicopter system with a prescribed mixed <i>H</i><sub>∞</sub> and passivity (M<i>H</i><sub>∞</sub>P) performance index. The acquired results are expressed as LMIs, which are easily addressed using standard optimization algorithms. In addition, an exemplary scenario based on the CE151 helicopter model is presented to demonstrate the less conservative nature of the obtained results as well as the application of the recommended unique design approaches.https://www.mdpi.com/2504-3110/6/9/498TS fuzzy CE151 helicopter systemsampled data reliable controlmixed <i>H</i><sub>∞</sub> and passivityLyapunov-Krasovskii functionallinear matrix inequality
spellingShingle V. Dhanya
A. Arunkumar
Kantapon Chaisena
Sampled-Data Based Fault-Tolerant Control Design for Uncertain CE151 Helicopter System with Random Delays: Takagi-Sugeno Fuzzy Approach
Fractal and Fractional
TS fuzzy CE151 helicopter system
sampled data reliable control
mixed <i>H</i><sub>∞</sub> and passivity
Lyapunov-Krasovskii functional
linear matrix inequality
title Sampled-Data Based Fault-Tolerant Control Design for Uncertain CE151 Helicopter System with Random Delays: Takagi-Sugeno Fuzzy Approach
title_full Sampled-Data Based Fault-Tolerant Control Design for Uncertain CE151 Helicopter System with Random Delays: Takagi-Sugeno Fuzzy Approach
title_fullStr Sampled-Data Based Fault-Tolerant Control Design for Uncertain CE151 Helicopter System with Random Delays: Takagi-Sugeno Fuzzy Approach
title_full_unstemmed Sampled-Data Based Fault-Tolerant Control Design for Uncertain CE151 Helicopter System with Random Delays: Takagi-Sugeno Fuzzy Approach
title_short Sampled-Data Based Fault-Tolerant Control Design for Uncertain CE151 Helicopter System with Random Delays: Takagi-Sugeno Fuzzy Approach
title_sort sampled data based fault tolerant control design for uncertain ce151 helicopter system with random delays takagi sugeno fuzzy approach
topic TS fuzzy CE151 helicopter system
sampled data reliable control
mixed <i>H</i><sub>∞</sub> and passivity
Lyapunov-Krasovskii functional
linear matrix inequality
url https://www.mdpi.com/2504-3110/6/9/498
work_keys_str_mv AT vdhanya sampleddatabasedfaulttolerantcontroldesignforuncertaince151helicoptersystemwithrandomdelaystakagisugenofuzzyapproach
AT aarunkumar sampleddatabasedfaulttolerantcontroldesignforuncertaince151helicoptersystemwithrandomdelaystakagisugenofuzzyapproach
AT kantaponchaisena sampleddatabasedfaulttolerantcontroldesignforuncertaince151helicoptersystemwithrandomdelaystakagisugenofuzzyapproach