Backstepping Sliding Mode Control for Missile Attitude System

Huang Zi-Rui; Wu Yun-Jie; Zuo Jing-Xing; Cheng Ling

doi:10.1109/GNCC42960.2018.9019024

Backstepping Sliding Mode Control for Missile Attitude System

Huang Zi-Rui
, Wu Yun-Jie
, Zuo Jing-Xing
, Cheng Ling

School of Automation Science and Electrical Engineering

Beihang University
Beijing New Aerotropolis

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

1 Scopus citations

Abstract

This paper is devoted to the attitude control of a quaternion described missile model, which is nonlinear in aerodynamics with atmospheric moment uncertainties, inertia uncertainties, bounded disturbances and actuator failures. One backstepping sliding mode controller is designed to guarantee the state variables of the closed-loop system to converge to a small region of the reference states. The variable structure control including sliding mode control has the valuable features of anti-interference and resisting parameter distortion, providing a useful solution for designing control law. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

Original language	English
Title of host publication	2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Publisher	Institute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)	9781538611715
DOIs	https://doi.org/10.1109/GNCC42960.2018.9019024
State	Published - Aug 2018
Event	2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 - Xiamen, China Duration: 10 Aug 2018 → 12 Aug 2018

Publication series

Name	2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

Conference

Conference	2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Country/Territory	China
City	Xiamen
Period	10/08/18 → 12/08/18

Keywords

backstepping
missile attitude control
sliding mode control

Access to Document

10.1109/GNCC42960.2018.9019024

Cite this

Zi-Rui, H., Yun-Jie, W., Jing-Xing, Z., & Ling, C. (2018). Backstepping Sliding Mode Control for Missile Attitude System. In 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 Article 9019024 (2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/GNCC42960.2018.9019024

@inproceedings{de286dfc57424d03a0d2f18b08ee6318,

title = "Backstepping Sliding Mode Control for Missile Attitude System",

abstract = "This paper is devoted to the attitude control of a quaternion described missile model, which is nonlinear in aerodynamics with atmospheric moment uncertainties, inertia uncertainties, bounded disturbances and actuator failures. One backstepping sliding mode controller is designed to guarantee the state variables of the closed-loop system to converge to a small region of the reference states. The variable structure control including sliding mode control has the valuable features of anti-interference and resisting parameter distortion, providing a useful solution for designing control law. Also, simulation results are presented to illustrate the effectiveness of the control strategy.",

keywords = "backstepping, missile attitude control, sliding mode control",

author = "Huang Zi-Rui and Wu Yun-Jie and Zuo Jing-Xing and Cheng Ling",

note = "Publisher Copyright: {\textcopyright} 2018 IEEE.; 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 ; Conference date: 10-08-2018 Through 12-08-2018",

year = "2018",

month = aug,

doi = "10.1109/GNCC42960.2018.9019024",

language = "英语",

series = "2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018",

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

booktitle = "2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018",

address = "美国",

}

Zi-Rui, H, Yun-Jie, W, Jing-Xing, Z & Ling, C 2018, Backstepping Sliding Mode Control for Missile Attitude System. in 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018., 9019024, 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018, Institute of Electrical and Electronics Engineers Inc., 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018, Xiamen, China, 10/08/18. https://doi.org/10.1109/GNCC42960.2018.9019024

Backstepping Sliding Mode Control for Missile Attitude System. / Zi-Rui, Huang; Yun-Jie, Wu; Jing-Xing, Zuo et al.
2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018. Institute of Electrical and Electronics Engineers Inc., 2018. 9019024 (2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018).

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

TY - GEN

T1 - Backstepping Sliding Mode Control for Missile Attitude System

AU - Zi-Rui, Huang

AU - Yun-Jie, Wu

AU - Jing-Xing, Zuo

AU - Ling, Cheng

PY - 2018/8

Y1 - 2018/8

N2 - This paper is devoted to the attitude control of a quaternion described missile model, which is nonlinear in aerodynamics with atmospheric moment uncertainties, inertia uncertainties, bounded disturbances and actuator failures. One backstepping sliding mode controller is designed to guarantee the state variables of the closed-loop system to converge to a small region of the reference states. The variable structure control including sliding mode control has the valuable features of anti-interference and resisting parameter distortion, providing a useful solution for designing control law. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

AB - This paper is devoted to the attitude control of a quaternion described missile model, which is nonlinear in aerodynamics with atmospheric moment uncertainties, inertia uncertainties, bounded disturbances and actuator failures. One backstepping sliding mode controller is designed to guarantee the state variables of the closed-loop system to converge to a small region of the reference states. The variable structure control including sliding mode control has the valuable features of anti-interference and resisting parameter distortion, providing a useful solution for designing control law. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

KW - backstepping

KW - missile attitude control

KW - sliding mode control

UR - https://www.scopus.com/pages/publications/85082475995

U2 - 10.1109/GNCC42960.2018.9019024

DO - 10.1109/GNCC42960.2018.9019024

M3 - 会议稿件

AN - SCOPUS:85082475995

T3 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

BT - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

Y2 - 10 August 2018 through 12 August 2018

ER -

Backstepping Sliding Mode Control for Missile Attitude System

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