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

被引：2
|
作者：
Xiao, Hongliang [1 ]
Li, Huacong [1 ]
Peng, Kai [1 ]
Li, Jia [2 ]
机构：
[1] Northwestern Polytech Univ, Sch Power & Energy, Xian 710072, Peoples R China
[2] Changan Univ, Key Lab Rd Construct Technol & Equipment, Minist Educ, Xian 710064, Peoples R China
来源：
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES | 2022年 / 39卷 / 04期
基金：
中国国家自然科学基金;
关键词：
multi-variable control; model reference; adaptive sliding mode control; uncertainty;
D O I：
10.1515/tjj-2019-0041
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
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.
引用
收藏
页码：491 / 500
页数：10
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