Adaptive control for missile systems with parameter uncertainty

Zhiwei Lin; Zheng Zhu; Yuanqing Xia; Shuo Wang

Adaptive control for missile systems with parameter uncertainty

Zhiwei Lin^*, Zheng Zhu, Yuanqing Xia, Shuo Wang

^*Corresponding author for this work

School of Automation

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

5 Citations (Scopus)

Abstract

This paper is devoted to attitude control of a nonlinear missile model. Combining the back-stepping technique, the corresponding sliding mode controller is designed to guarantee the state variables of the closed loop system to converge to the reference state with the help of the adaptive law by estimating the total uncertainties. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

Original language	English
Pages (from-to)	1937-1944
Number of pages	8
Journal	ICIC Express Letters
Volume	4
Issue number	5 B
Publication status	Published - Oct 2010

Keywords

Adaptive control
Back-stepping
Missile attitude Control
Sliding mode control

Cite this

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title = "Adaptive control for missile systems with parameter uncertainty",

abstract = "This paper is devoted to attitude control of a nonlinear missile model. Combining the back-stepping technique, the corresponding sliding mode controller is designed to guarantee the state variables of the closed loop system to converge to the reference state with the help of the adaptive law by estimating the total uncertainties. 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 = "Zhiwei Lin and Zheng Zhu and Yuanqing Xia and Shuo Wang",

year = "2010",

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language = "English",

volume = "4",

pages = "1937--1944",

journal = "ICIC Express Letters",

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TY - JOUR

T1 - Adaptive control for missile systems with parameter uncertainty

AU - Lin, Zhiwei

AU - Zhu, Zheng

AU - Xia, Yuanqing

AU - Wang, Shuo

PY - 2010/10

Y1 - 2010/10

N2 - This paper is devoted to attitude control of a nonlinear missile model. Combining the back-stepping technique, the corresponding sliding mode controller is designed to guarantee the state variables of the closed loop system to converge to the reference state with the help of the adaptive law by estimating the total uncertainties. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

AB - This paper is devoted to attitude control of a nonlinear missile model. Combining the back-stepping technique, the corresponding sliding mode controller is designed to guarantee the state variables of the closed loop system to converge to the reference state with the help of the adaptive law by estimating the total uncertainties. 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 - http://www.scopus.com/inward/record.url?scp=77956930206&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:77956930206

SN - 1881-803X

VL - 4

SP - 1937

EP - 1944

JO - ICIC Express Letters

JF - ICIC Express Letters

IS - 5 B

ER -

Adaptive control for missile systems with parameter uncertainty

Abstract

Keywords

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