Adaptive sliding mode back-stepping control for hypersonic flight vehicle with state constraints and unmodeled disturbances

Fei Ma; Yunjie Wu; Xiaocen Liu; Bohao Li; Xiaodong Liu

doi:10.1109/ICCA51439.2020.9264516

Adaptive sliding mode back-stepping control for hypersonic flight vehicle with state constraints and unmodeled disturbances

Fei Ma
, Yunjie Wu
, Xiaocen Liu
, Bohao Li
, Xiaodong Liu

自动化科学与电气工程学院

Beihang University
Science and Technology on Aircraft Control Laboratory
Beijing Aerospace Automatic Control Institute

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

5 引用（Scopus）

摘要

This study presents a finite-time adaptive sliding mode back-stepping controller (FASMBC) for hypersonic flight vehicle (HFV), where the state constraints and unmodeled disturbances are considered. Firstly, the longitudinal model of HFV is decomposed into altitude subsystem and velocity subsystem. Then, sliding mode control and back-stepping logic based on barrier Lyapunov function are merged to design the robust controller for each subsystem. Besides, the adaptive strategy is applied to estimate the unmodeled disturbances. A tracking differentiator is introduced to avoid the explosion of terms problem involved in traditional back-stepping control. Finally, the simulation results is provided to illustrate the effectiveness of the proposed control scheme.

源语言	英语
主期刊名	2020 IEEE 16th International Conference on Control and Automation, ICCA 2020
出版商	IEEE Computer Society
页	1547-1552
页数	6
ISBN（电子版）	9781728190938
DOI	https://doi.org/10.1109/ICCA51439.2020.9264516
出版状态	已出版 - 9 10月 2020
活动	16th IEEE International Conference on Control and Automation, ICCA 2020 - Virtual, Sapporo, Hokkaido, 日本期限: 9 10月 2020 → 11 10月 2020

出版系列

姓名	IEEE International Conference on Control and Automation, ICCA
卷	2020-October
ISSN（印刷版）	1948-3449
ISSN（电子版）	1948-3457

会议

会议	16th IEEE International Conference on Control and Automation, ICCA 2020
国家/地区	日本
市	Virtual, Sapporo, Hokkaido
时期	9/10/20 → 11/10/20

访问文件

10.1109/ICCA51439.2020.9264516

其它文件与链接

链接到 Scopus 的出版物

引用此

Ma, F., Wu, Y., Liu, X., Li, B., & Liu, X. (2020). Adaptive sliding mode back-stepping control for hypersonic flight vehicle with state constraints and unmodeled disturbances. 在 2020 IEEE 16th International Conference on Control and Automation, ICCA 2020 (页码 1547-1552). 文章 9264516 (IEEE International Conference on Control and Automation, ICCA; 卷 2020-October). IEEE Computer Society. https://doi.org/10.1109/ICCA51439.2020.9264516

@inproceedings{e44a7008ea0045f39a39724f53aaad50,

title = "Adaptive sliding mode back-stepping control for hypersonic flight vehicle with state constraints and unmodeled disturbances",

abstract = "This study presents a finite-time adaptive sliding mode back-stepping controller (FASMBC) for hypersonic flight vehicle (HFV), where the state constraints and unmodeled disturbances are considered. Firstly, the longitudinal model of HFV is decomposed into altitude subsystem and velocity subsystem. Then, sliding mode control and back-stepping logic based on barrier Lyapunov function are merged to design the robust controller for each subsystem. Besides, the adaptive strategy is applied to estimate the unmodeled disturbances. A tracking differentiator is introduced to avoid the explosion of terms problem involved in traditional back-stepping control. Finally, the simulation results is provided to illustrate the effectiveness of the proposed control scheme.",

keywords = "Adaptive control, back-stepping control, bar-rier Lyapunov function, hypersonic flight vehicle, sliding mode control",

author = "Fei Ma and Yunjie Wu and Xiaocen Liu and Bohao Li and Xiaodong Liu",

note = "Publisher Copyright: {\textcopyright} 2020 IEEE.; 16th IEEE International Conference on Control and Automation, ICCA 2020 ; Conference date: 09-10-2020 Through 11-10-2020",

year = "2020",

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doi = "10.1109/ICCA51439.2020.9264516",

language = "英语",

series = "IEEE International Conference on Control and Automation, ICCA",

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booktitle = "2020 IEEE 16th International Conference on Control and Automation, ICCA 2020",

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}

Ma, F, Wu, Y, Liu, X, Li, B & Liu, X 2020, Adaptive sliding mode back-stepping control for hypersonic flight vehicle with state constraints and unmodeled disturbances. 在 2020 IEEE 16th International Conference on Control and Automation, ICCA 2020., 9264516, IEEE International Conference on Control and Automation, ICCA, 卷 2020-October, IEEE Computer Society, 页码 1547-1552, 16th IEEE International Conference on Control and Automation, ICCA 2020, Virtual, Sapporo, Hokkaido, 日本, 9/10/20. https://doi.org/10.1109/ICCA51439.2020.9264516

Adaptive sliding mode back-stepping control for hypersonic flight vehicle with state constraints and unmodeled disturbances. / Ma, Fei; Wu, Yunjie; Liu, Xiaocen 等.
2020 IEEE 16th International Conference on Control and Automation, ICCA 2020. IEEE Computer Society, 2020. 页码 1547-1552 9264516 (IEEE International Conference on Control and Automation, ICCA; 卷 2020-October).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - Adaptive sliding mode back-stepping control for hypersonic flight vehicle with state constraints and unmodeled disturbances

AU - Ma, Fei

AU - Wu, Yunjie

AU - Liu, Xiaocen

AU - Li, Bohao

AU - Liu, Xiaodong

PY - 2020/10/9

Y1 - 2020/10/9

N2 - This study presents a finite-time adaptive sliding mode back-stepping controller (FASMBC) for hypersonic flight vehicle (HFV), where the state constraints and unmodeled disturbances are considered. Firstly, the longitudinal model of HFV is decomposed into altitude subsystem and velocity subsystem. Then, sliding mode control and back-stepping logic based on barrier Lyapunov function are merged to design the robust controller for each subsystem. Besides, the adaptive strategy is applied to estimate the unmodeled disturbances. A tracking differentiator is introduced to avoid the explosion of terms problem involved in traditional back-stepping control. Finally, the simulation results is provided to illustrate the effectiveness of the proposed control scheme.

AB - This study presents a finite-time adaptive sliding mode back-stepping controller (FASMBC) for hypersonic flight vehicle (HFV), where the state constraints and unmodeled disturbances are considered. Firstly, the longitudinal model of HFV is decomposed into altitude subsystem and velocity subsystem. Then, sliding mode control and back-stepping logic based on barrier Lyapunov function are merged to design the robust controller for each subsystem. Besides, the adaptive strategy is applied to estimate the unmodeled disturbances. A tracking differentiator is introduced to avoid the explosion of terms problem involved in traditional back-stepping control. Finally, the simulation results is provided to illustrate the effectiveness of the proposed control scheme.

KW - Adaptive control

KW - back-stepping control

KW - bar-rier Lyapunov function

KW - hypersonic flight vehicle

KW - sliding mode control

UR - https://www.scopus.com/pages/publications/85098092142

U2 - 10.1109/ICCA51439.2020.9264516

DO - 10.1109/ICCA51439.2020.9264516

M3 - 会议稿件

AN - SCOPUS:85098092142

T3 - IEEE International Conference on Control and Automation, ICCA

SP - 1547

EP - 1552

BT - 2020 IEEE 16th International Conference on Control and Automation, ICCA 2020

PB - IEEE Computer Society

T2 - 16th IEEE International Conference on Control and Automation, ICCA 2020

Y2 - 9 October 2020 through 11 October 2020

ER -

Ma F, Wu Y, Liu X, Li B, Liu X. Adaptive sliding mode back-stepping control for hypersonic flight vehicle with state constraints and unmodeled disturbances. 在 2020 IEEE 16th International Conference on Control and Automation, ICCA 2020. IEEE Computer Society. 2020. 页码 1547-1552. 9264516. (IEEE International Conference on Control and Automation, ICCA). doi: 10.1109/ICCA51439.2020.9264516

Adaptive sliding mode back-stepping control for hypersonic flight vehicle with state constraints and unmodeled disturbances

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