A Model Reference Adaptive Sliding Mode Control Method for Aero-Engine

Hongliang Xiao; Huacong Li; Kai Peng; Jia Li

doi:10.1515/tjj-2019-0041

A Model Reference Adaptive Sliding Mode Control Method for Aero-Engine

Hongliang Xiao, Huacong Li, Kai Peng, Jia Li

School of Power and Energy

Research output: Contribution to journal › Article › peer-review

3 Scopus citations

Abstract

In this paper, a model reference adaptive sliding mode control method is proposed for a variable cycle engine (VCE) which is a MIMO system with uncertainties and external disturbances. The reference model is designed based on optimal LQR method to provide ideal reference states. An adaptive sliding mode controller (ASMC) is designed for model reference adaptive control structure, which the adaptive law is derived based on Lyapunov function to estimate the unknown upper bound of uncertainties and external disturbances. Simulation results for VCE demonstrate the performance and fidelity of the proposed method.

Original language	English
Pages (from-to)	491-500
Number of pages	10
Journal	International Journal of Turbo and Jet Engines
Volume	39
Issue number	4
DOIs	https://doi.org/10.1515/tjj-2019-0041
State	Published - 1 Dec 2022

Keywords

adaptive sliding mode control
model reference
multi-variable control
uncertainty

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10.1515/tjj-2019-0041

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title = "A Model Reference Adaptive Sliding Mode Control Method for Aero-Engine",

abstract = "In this paper, a model reference adaptive sliding mode control method is proposed for a variable cycle engine (VCE) which is a MIMO system with uncertainties and external disturbances. The reference model is designed based on optimal LQR method to provide ideal reference states. An adaptive sliding mode controller (ASMC) is designed for model reference adaptive control structure, which the adaptive law is derived based on Lyapunov function to estimate the unknown upper bound of uncertainties and external disturbances. Simulation results for VCE demonstrate the performance and fidelity of the proposed method.",

keywords = "adaptive sliding mode control, model reference, multi-variable control, uncertainty",

author = "Hongliang Xiao and Huacong Li and Kai Peng and Jia Li",

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year = "2022",

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TY - JOUR

T1 - A Model Reference Adaptive Sliding Mode Control Method for Aero-Engine

AU - Xiao, Hongliang

AU - Li, Huacong

AU - Peng, Kai

AU - Li, Jia

PY - 2022/12/1

Y1 - 2022/12/1

N2 - In this paper, a model reference adaptive sliding mode control method is proposed for a variable cycle engine (VCE) which is a MIMO system with uncertainties and external disturbances. The reference model is designed based on optimal LQR method to provide ideal reference states. An adaptive sliding mode controller (ASMC) is designed for model reference adaptive control structure, which the adaptive law is derived based on Lyapunov function to estimate the unknown upper bound of uncertainties and external disturbances. Simulation results for VCE demonstrate the performance and fidelity of the proposed method.

AB - In this paper, a model reference adaptive sliding mode control method is proposed for a variable cycle engine (VCE) which is a MIMO system with uncertainties and external disturbances. The reference model is designed based on optimal LQR method to provide ideal reference states. An adaptive sliding mode controller (ASMC) is designed for model reference adaptive control structure, which the adaptive law is derived based on Lyapunov function to estimate the unknown upper bound of uncertainties and external disturbances. Simulation results for VCE demonstrate the performance and fidelity of the proposed method.

KW - adaptive sliding mode control

KW - model reference

KW - multi-variable control

KW - uncertainty

UR - https://www.scopus.com/pages/publications/105001090228

U2 - 10.1515/tjj-2019-0041

DO - 10.1515/tjj-2019-0041

M3 - 文章

AN - SCOPUS:105001090228

SN - 0334-0082

VL - 39

SP - 491

EP - 500

JO - International Journal of Turbo and Jet Engines

JF - International Journal of Turbo and Jet Engines

IS - 4

ER -

A Model Reference Adaptive Sliding Mode Control Method for Aero-Engine

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