Adaptive sliding mode control for missile guidance law

Xiangyang Wu; Shihua Bi; Zheng Zhu; Weinan Wu

doi:10.1109/ChiCC.2014.6896757

Adaptive sliding mode control for missile guidance law

Xiangyang Wu^*, Shihua Bi, Zheng Zhu, Weinan Wu

^*Corresponding author for this work

School of Aerospace Engineering

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

1 Citation (Scopus)

Abstract

The problem of missile interception is investigated in this paper. Sliding mode controllers are proposed for the design of guidance laws. Specially, the control design consists of the estimation of the target acceleration by adaptive scheme and thus it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.

Original language	English
Title of host publication	Proceedings of the 33rd Chinese Control Conference, CCC 2014
Editors	Shengyuan Xu, Qianchuan Zhao
Publisher	IEEE Computer Society
Pages	960-965
Number of pages	6
ISBN (Electronic)	9789881563842
DOIs	https://doi.org/10.1109/ChiCC.2014.6896757
Publication status	Published - 11 Sept 2014
Event	Proceedings of the 33rd Chinese Control Conference, CCC 2014 - Nanjing, China Duration: 28 Jul 2014 → 30 Jul 2014

Publication series

Name	Proceedings of the 33rd Chinese Control Conference, CCC 2014
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	Proceedings of the 33rd Chinese Control Conference, CCC 2014
Country/Territory	China
City	Nanjing
Period	28/07/14 → 30/07/14

Keywords

Adaptive control
Guidance law
Sliding mode control

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10.1109/ChiCC.2014.6896757

Cite this

Wu, X., Bi, S., Zhu, Z., & Wu, W. (2014). Adaptive sliding mode control for missile guidance law. In S. Xu, & Q. Zhao (Eds.), Proceedings of the 33rd Chinese Control Conference, CCC 2014 (pp. 960-965). Article 6896757 (Proceedings of the 33rd Chinese Control Conference, CCC 2014). IEEE Computer Society. https://doi.org/10.1109/ChiCC.2014.6896757

@inproceedings{7860d153fd364e919a5ebcb7a28a3655,

title = "Adaptive sliding mode control for missile guidance law",

abstract = "The problem of missile interception is investigated in this paper. Sliding mode controllers are proposed for the design of guidance laws. Specially, the control design consists of the estimation of the target acceleration by adaptive scheme and thus it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.",

keywords = "Adaptive control, Guidance law, Sliding mode control",

author = "Xiangyang Wu and Shihua Bi and Zheng Zhu and Weinan Wu",

note = "Publisher Copyright: {\textcopyright} 2014 TCCT, CAA.; Proceedings of the 33rd Chinese Control Conference, CCC 2014 ; Conference date: 28-07-2014 Through 30-07-2014",

year = "2014",

month = sep,

day = "11",

doi = "10.1109/ChiCC.2014.6896757",

language = "English",

series = "Proceedings of the 33rd Chinese Control Conference, CCC 2014",

publisher = "IEEE Computer Society",

pages = "960--965",

editor = "Shengyuan Xu and Qianchuan Zhao",

booktitle = "Proceedings of the 33rd Chinese Control Conference, CCC 2014",

address = "United States",

}

Wu, X, Bi, S, Zhu, Z & Wu, W 2014, Adaptive sliding mode control for missile guidance law. in S Xu & Q Zhao (eds), Proceedings of the 33rd Chinese Control Conference, CCC 2014., 6896757, Proceedings of the 33rd Chinese Control Conference, CCC 2014, IEEE Computer Society, pp. 960-965, Proceedings of the 33rd Chinese Control Conference, CCC 2014, Nanjing, China, 28/07/14. https://doi.org/10.1109/ChiCC.2014.6896757

Adaptive sliding mode control for missile guidance law. / Wu, Xiangyang; Bi, Shihua; Zhu, Zheng et al.
Proceedings of the 33rd Chinese Control Conference, CCC 2014. ed. / Shengyuan Xu; Qianchuan Zhao. IEEE Computer Society, 2014. p. 960-965 6896757 (Proceedings of the 33rd Chinese Control Conference, CCC 2014).

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

TY - GEN

T1 - Adaptive sliding mode control for missile guidance law

AU - Wu, Xiangyang

AU - Bi, Shihua

AU - Zhu, Zheng

AU - Wu, Weinan

PY - 2014/9/11

Y1 - 2014/9/11

N2 - The problem of missile interception is investigated in this paper. Sliding mode controllers are proposed for the design of guidance laws. Specially, the control design consists of the estimation of the target acceleration by adaptive scheme and thus it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.

AB - The problem of missile interception is investigated in this paper. Sliding mode controllers are proposed for the design of guidance laws. Specially, the control design consists of the estimation of the target acceleration by adaptive scheme and thus it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.

KW - Adaptive control

KW - Guidance law

KW - Sliding mode control

UR - http://www.scopus.com/inward/record.url?scp=84907943819&partnerID=8YFLogxK

U2 - 10.1109/ChiCC.2014.6896757

DO - 10.1109/ChiCC.2014.6896757

M3 - Conference contribution

AN - SCOPUS:84907943819

T3 - Proceedings of the 33rd Chinese Control Conference, CCC 2014

SP - 960

EP - 965

BT - Proceedings of the 33rd Chinese Control Conference, CCC 2014

A2 - Xu, Shengyuan

A2 - Zhao, Qianchuan

PB - IEEE Computer Society

T2 - Proceedings of the 33rd Chinese Control Conference, CCC 2014

Y2 - 28 July 2014 through 30 July 2014

ER -

Adaptive sliding mode control for missile guidance law

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Keywords

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