Adaptive back-stepping sliding mode attitude control of missile systems

Yuanqing Xia; Kunfeng Lu; Zheng Zhu; Mengyin Fu

doi:10.1002/rnc.2952

Adaptive back-stepping sliding mode attitude control of missile systems

Yuanqing Xia^*
, Kunfeng Lu
, Zheng Zhu
, Mengyin Fu

^*Corresponding author for this work

School of Automation

Beijing Institute of Technology

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

53 Citations (Scopus)

Abstract

This paper is devoted to the attitude control of a quaternion missile model, which is nonlinear in aerodynamics with atmospheric moment uncertainties, inertia uncertainties, bounded disturbances and actuator failures. By employing the back-stepping technique, the corresponding 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 with the help of the adaptive law by estimating the total uncertainties, and be chatter-free. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

Original language	English
Pages (from-to)	1699-1717
Number of pages	19
Journal	International Journal of Robust and Nonlinear Control
Volume	23
Issue number	15
DOIs	https://doi.org/10.1002/rnc.2952
Publication status	Published - Oct 2013

Keywords

adaptive control
back-stepping
missile attitude control
sliding mode control

Access to Document

10.1002/rnc.2952

Cite this

@article{52ff04d59ad345b3b0187c8b485a0fba,

title = "Adaptive back-stepping sliding mode attitude control of missile systems",

abstract = "This paper is devoted to the attitude control of a quaternion missile model, which is nonlinear in aerodynamics with atmospheric moment uncertainties, inertia uncertainties, bounded disturbances and actuator failures. By employing the back-stepping technique, the corresponding 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 with the help of the adaptive law by estimating the total uncertainties, and be chatter-free. Also, simulation results are presented to illustrate the effectiveness of the control strategy.",

keywords = "adaptive control, back-stepping, missile attitude control, sliding mode control",

author = "Yuanqing Xia and Kunfeng Lu and Zheng Zhu and Mengyin Fu",

year = "2013",

month = oct,

doi = "10.1002/rnc.2952",

language = "English",

volume = "23",

pages = "1699--1717",

journal = "International Journal of Robust and Nonlinear Control",

issn = "1049-8923",

publisher = "John Wiley and Sons Ltd",

number = "15",

}

TY - JOUR

T1 - Adaptive back-stepping sliding mode attitude control of missile systems

AU - Xia, Yuanqing

AU - Lu, Kunfeng

AU - Zhu, Zheng

AU - Fu, Mengyin

PY - 2013/10

Y1 - 2013/10

N2 - This paper is devoted to the attitude control of a quaternion missile model, which is nonlinear in aerodynamics with atmospheric moment uncertainties, inertia uncertainties, bounded disturbances and actuator failures. By employing the back-stepping technique, the corresponding 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 with the help of the adaptive law by estimating the total uncertainties, and be chatter-free. 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 missile model, which is nonlinear in aerodynamics with atmospheric moment uncertainties, inertia uncertainties, bounded disturbances and actuator failures. By employing the back-stepping technique, the corresponding 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 with the help of the adaptive law by estimating the total uncertainties, and be chatter-free. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

KW - adaptive control

KW - back-stepping

KW - missile attitude control

KW - sliding mode control

UR - https://www.scopus.com/pages/publications/84884905443

U2 - 10.1002/rnc.2952

DO - 10.1002/rnc.2952

M3 - Article

AN - SCOPUS:84884905443

SN - 1049-8923

VL - 23

SP - 1699

EP - 1717

JO - International Journal of Robust and Nonlinear Control

JF - International Journal of Robust and Nonlinear Control

IS - 15

ER -

Adaptive back-stepping sliding mode attitude control of missile systems

Abstract

Keywords

Access to Document

Other files and links

Fingerprint

Cite this