Attitude Tracking Control for Hypersonic Flight Vehicles Based on Sliding Mode Observers

Bairui Xiong; Yu Wang; Chenliang Wang; Jianzhong Qiao

doi:10.1109/CAC53003.2021.9728509

Attitude Tracking Control for Hypersonic Flight Vehicles Based on Sliding Mode Observers

Bairui Xiong
, Yu Wang^*
, Chenliang Wang
, Jianzhong Qiao

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

1 Scopus citations

Abstract

In this paper, a novel backstepping control scheme based on sliding mode observers is proposed for the attitude system of a hypersonic flight vehicle. By employing sliding mode observers, the estimations of the disturbances and extra dynamics are guaranteed to converge to their exact values in finite time. The control scheme is designed through backstepping approach, which benefits for compensating the mismatched disturbances. Then the Lyapunov stability analysis is given to prove that the closed-loop system which contains the observers, the controller and the vehicle is asymptotically stable with attitude states converging to reference signals. Simulation results are provided to demonstrate the effectiveness of the proposed control method.

Original language	English
Title of host publication	Proceeding - 2021 China Automation Congress, CAC 2021
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	2027-2033
Number of pages	7
ISBN (Electronic)	9781665426473
DOIs	https://doi.org/10.1109/CAC53003.2021.9728509
State	Published - 2021
Event	2021 China Automation Congress, CAC 2021 - Beijing, China Duration: 22 Oct 2021 → 24 Oct 2021

Publication series

Name	Proceeding - 2021 China Automation Congress, CAC 2021

Conference

Conference	2021 China Automation Congress, CAC 2021
Country/Territory	China
City	Beijing
Period	22/10/21 → 24/10/21

Keywords

attitude control
backstepping design
hypersonic flight vehicle
sliding mode observer

Access to Document

10.1109/CAC53003.2021.9728509

Cite this

Xiong, B., Wang, Y., Wang, C., & Qiao, J. (2021). Attitude Tracking Control for Hypersonic Flight Vehicles Based on Sliding Mode Observers. In Proceeding - 2021 China Automation Congress, CAC 2021 (pp. 2027-2033). (Proceeding - 2021 China Automation Congress, CAC 2021). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CAC53003.2021.9728509

@inproceedings{9f684a9f26794c6595737015d81f2996,

title = "Attitude Tracking Control for Hypersonic Flight Vehicles Based on Sliding Mode Observers",

abstract = "In this paper, a novel backstepping control scheme based on sliding mode observers is proposed for the attitude system of a hypersonic flight vehicle. By employing sliding mode observers, the estimations of the disturbances and extra dynamics are guaranteed to converge to their exact values in finite time. The control scheme is designed through backstepping approach, which benefits for compensating the mismatched disturbances. Then the Lyapunov stability analysis is given to prove that the closed-loop system which contains the observers, the controller and the vehicle is asymptotically stable with attitude states converging to reference signals. Simulation results are provided to demonstrate the effectiveness of the proposed control method.",

keywords = "attitude control, backstepping design, hypersonic flight vehicle, sliding mode observer",

author = "Bairui Xiong and Yu Wang and Chenliang Wang and Jianzhong Qiao",

note = "Publisher Copyright: {\textcopyright} 2021 IEEE; 2021 China Automation Congress, CAC 2021 ; Conference date: 22-10-2021 Through 24-10-2021",

year = "2021",

doi = "10.1109/CAC53003.2021.9728509",

language = "英语",

series = "Proceeding - 2021 China Automation Congress, CAC 2021",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "2027--2033",

booktitle = "Proceeding - 2021 China Automation Congress, CAC 2021",

address = "美国",

}

Xiong, B, Wang, Y, Wang, C & Qiao, J 2021, Attitude Tracking Control for Hypersonic Flight Vehicles Based on Sliding Mode Observers. in Proceeding - 2021 China Automation Congress, CAC 2021. Proceeding - 2021 China Automation Congress, CAC 2021, Institute of Electrical and Electronics Engineers Inc., pp. 2027-2033, 2021 China Automation Congress, CAC 2021, Beijing, China, 22/10/21. https://doi.org/10.1109/CAC53003.2021.9728509

Attitude Tracking Control for Hypersonic Flight Vehicles Based on Sliding Mode Observers. / Xiong, Bairui; Wang, Yu; Wang, Chenliang et al.
Proceeding - 2021 China Automation Congress, CAC 2021. Institute of Electrical and Electronics Engineers Inc., 2021. p. 2027-2033 (Proceeding - 2021 China Automation Congress, CAC 2021).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Attitude Tracking Control for Hypersonic Flight Vehicles Based on Sliding Mode Observers

AU - Xiong, Bairui

AU - Wang, Yu

AU - Wang, Chenliang

AU - Qiao, Jianzhong

PY - 2021

Y1 - 2021

N2 - In this paper, a novel backstepping control scheme based on sliding mode observers is proposed for the attitude system of a hypersonic flight vehicle. By employing sliding mode observers, the estimations of the disturbances and extra dynamics are guaranteed to converge to their exact values in finite time. The control scheme is designed through backstepping approach, which benefits for compensating the mismatched disturbances. Then the Lyapunov stability analysis is given to prove that the closed-loop system which contains the observers, the controller and the vehicle is asymptotically stable with attitude states converging to reference signals. Simulation results are provided to demonstrate the effectiveness of the proposed control method.

AB - In this paper, a novel backstepping control scheme based on sliding mode observers is proposed for the attitude system of a hypersonic flight vehicle. By employing sliding mode observers, the estimations of the disturbances and extra dynamics are guaranteed to converge to their exact values in finite time. The control scheme is designed through backstepping approach, which benefits for compensating the mismatched disturbances. Then the Lyapunov stability analysis is given to prove that the closed-loop system which contains the observers, the controller and the vehicle is asymptotically stable with attitude states converging to reference signals. Simulation results are provided to demonstrate the effectiveness of the proposed control method.

KW - attitude control

KW - backstepping design

KW - hypersonic flight vehicle

KW - sliding mode observer

UR - https://www.scopus.com/pages/publications/85128071936

U2 - 10.1109/CAC53003.2021.9728509

DO - 10.1109/CAC53003.2021.9728509

M3 - 会议稿件

AN - SCOPUS:85128071936

T3 - Proceeding - 2021 China Automation Congress, CAC 2021

SP - 2027

EP - 2033

BT - Proceeding - 2021 China Automation Congress, CAC 2021

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2021 China Automation Congress, CAC 2021

Y2 - 22 October 2021 through 24 October 2021

ER -

Attitude Tracking Control for Hypersonic Flight Vehicles Based on Sliding Mode Observers

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