Sliding Mode Auto - Disturbance Rejection Control of Hypersonic Vehicle under Disturbance

Mingzhi Cheng; Yunjie Wu; Fei Ma

doi:10.16182/j.issn1004731x.joss.201710021

Sliding Mode Auto - Disturbance Rejection Control of Hypersonic Vehicle under Disturbance

Mingzhi Cheng
, Yunjie Wu
, Fei Ma

School of Automation Science and Electrical Engineering

Beihang University
National Key Laboratory of Aircraft Integrated Flight Control

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

6 Scopus citations

Abstract

The strong coupling of the hypersonic vehicle, the high order of the model, and the perturbation of the aerodynamic parameters make it difficult for the general controller to achieve the desired control effect. The self-disturbing tandem technique can well meet the requirements of the high-order model control. The use of sliding mode variable structure technology which is not sensitive to perturbation of parameters can enhance the system immunity. The simulation results show that the control effect is very good.

Original language	English
Pages (from-to)	2391-2396 and 2406
Journal	Xitong Fangzhen Xuebao / Journal of System Simulation
Volume	29
Issue number	10
DOIs	https://doi.org/10.16182/j.issn1004731x.joss.201710021
State	Published - 8 Oct 2017

Keywords

Auto-disturbance-rejection control
High-flying aircraft
Series control
Sliding mode variable structure control

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10.16182/j.issn1004731x.joss.201710021

Cite this

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abstract = "The strong coupling of the hypersonic vehicle, the high order of the model, and the perturbation of the aerodynamic parameters make it difficult for the general controller to achieve the desired control effect. The self-disturbing tandem technique can well meet the requirements of the high-order model control. The use of sliding mode variable structure technology which is not sensitive to perturbation of parameters can enhance the system immunity. The simulation results show that the control effect is very good.",

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AU - Cheng, Mingzhi

AU - Wu, Yunjie

AU - Ma, Fei

PY - 2017/10/8

Y1 - 2017/10/8

N2 - The strong coupling of the hypersonic vehicle, the high order of the model, and the perturbation of the aerodynamic parameters make it difficult for the general controller to achieve the desired control effect. The self-disturbing tandem technique can well meet the requirements of the high-order model control. The use of sliding mode variable structure technology which is not sensitive to perturbation of parameters can enhance the system immunity. The simulation results show that the control effect is very good.

AB - The strong coupling of the hypersonic vehicle, the high order of the model, and the perturbation of the aerodynamic parameters make it difficult for the general controller to achieve the desired control effect. The self-disturbing tandem technique can well meet the requirements of the high-order model control. The use of sliding mode variable structure technology which is not sensitive to perturbation of parameters can enhance the system immunity. The simulation results show that the control effect is very good.

KW - Auto-disturbance-rejection control

KW - High-flying aircraft

KW - Series control

KW - Sliding mode variable structure control

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JF - Xitong Fangzhen Xuebao / Journal of System Simulation

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ER -

Sliding Mode Auto - Disturbance Rejection Control of Hypersonic Vehicle under Disturbance

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Keywords

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