Volume 31, Issue 17 pp. 8442-8462
RESEARCH ARTICLE

Reachable set estimation and aperiodic sampled-data controller design for Markovian jump systems

Linqi Wang

Linqi Wang

School of Mathematics Science, Liaocheng University, Liaocheng, China

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Jianwei Xia

Corresponding Author

Jianwei Xia

School of Mathematics Science, Liaocheng University, Liaocheng, China

Correspondence Jianwei Xia, School of Mathematics Science, Liaocheng University, Liaocheng, Shandong 252000, China.

[email protected]

Ju H. Park, Department of Electrical Engineering, Yeungnam University, Kyongsan 38541, Republic of Korea.

[email protected]

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Guoliang Chen

Guoliang Chen

School of Mathematics Science, Liaocheng University, Liaocheng, China

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Ju H. Park

Corresponding Author

Ju H. Park

Department of Electrical Engineering, Yeungnam University, Kyongsan, Republic of Korea

Correspondence Jianwei Xia, School of Mathematics Science, Liaocheng University, Liaocheng, Shandong 252000, China.

[email protected]

Ju H. Park, Department of Electrical Engineering, Yeungnam University, Kyongsan 38541, Republic of Korea.

[email protected]

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Hao Shen

Hao Shen

School of Electrical and Information Engineering, Anhui University of Technology, Maanshan, China

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First published: 22 August 2021
Citations: 7

Funding information: National Natural Science Foundation of China, 61973148; 62003154; National Research Foundation of Korea (NRF) grant funded by the Korea government (MSIT), 2020R1A2B5B02002002

Abstract

In this article, the problem of reachable set estimation (RSE) and aperiodic sampled-data controller design are considered for Markovian jump systems (MJSs) with unit-energy bounded disturbance and unit-peak bounded disturbance inputs. First, by constructing mode-dependent loop-based Lyapunov functional, the linear matrix inequalities method is used to derive sufficient conditions for all states of MJSs under zero initial conditions to be bounded by ellipsoids. Second, RSE is considered in the process of designing the aperiodic sampled-data controller. The objective is that the resulting ellipsoid comprises the reachable set of the closed-loop system. Finally, the effectiveness of these methods is illustrated by the actual aircraft model and simulation results in this article. Furthermore, compared with other articles through numerical comparison, the method provided in this article can obtain less conservative results.

CONFLICT OF INTEREST

We declare that we do not have any commercial or associative interest that represents a conflict of interest in connection with the work submitted.

DATA AVAILABILITY STATEMENT

All data generated or analyzed during this study are included in this published article.

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