Composite continuous anti-disturbance autopilot design for missile system with mismatched disturbances

Xinge Liu; Haibin Sun; Jiayuan Shan

doi:10.1007/978-3-662-48386-2_46

Composite continuous anti-disturbance autopilot design for missile system with mismatched disturbances

Xinge Liu, Haibin Sun^*, Jiayuan Shan

^*Corresponding author for this work

School of Aerospace Engineering

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

Abstract

In this paper, the problem of autopilot design for missile system with mismatched disturbances is considered via a sliding mode control method and finite time disturbance observer. Firstly, a finite time disturbance observer is designed to estimate the mismatched disturbances. Secondly, based on disturbance estimation values and traditional sliding mode surface, a novel sliding mode surface is constructed. Thirdly, a composite continuous anti-disturbance autopilot is developed, which can guarantee system output converge to reference signal. Finally, a simulation result is presented to demonstrate the effectiveness of the proposed scheme.

Original language	English
Title of host publication	Proceedings of the 2015 Chinese Intelligent Systems Conference
Editors	Hongbo Li, Weicun Zhang, Yingmin Jia, Junping Du
Publisher	Springer Verlag
Pages	447-455
Number of pages	9
ISBN (Print)	9783662483848
DOIs	https://doi.org/10.1007/978-3-662-48386-2_46
Publication status	Published - 2016
Event	Chinese Intelligent Systems Conference, CISC 2015 - Yangzhou, China Duration: 1 Jan 2015 → …

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	359
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	Chinese Intelligent Systems Conference, CISC 2015
Country/Territory	China
City	Yangzhou
Period	1/01/15 → …

Keywords

Anti-disturbance autopilot
Finite time disturbance observer
Mismatched disturbances
Missile system
Sliding mode control

Access to Document

10.1007/978-3-662-48386-2_46

Cite this

Liu, X., Sun, H., & Shan, J. (2016). Composite continuous anti-disturbance autopilot design for missile system with mismatched disturbances. In H. Li, W. Zhang, Y. Jia, & J. Du (Eds.), Proceedings of the 2015 Chinese Intelligent Systems Conference (pp. 447-455). (Lecture Notes in Electrical Engineering; Vol. 359). Springer Verlag. https://doi.org/10.1007/978-3-662-48386-2_46

@inproceedings{e02611924ec647f19b196f6ef61b9862,

title = "Composite continuous anti-disturbance autopilot design for missile system with mismatched disturbances",

abstract = "In this paper, the problem of autopilot design for missile system with mismatched disturbances is considered via a sliding mode control method and finite time disturbance observer. Firstly, a finite time disturbance observer is designed to estimate the mismatched disturbances. Secondly, based on disturbance estimation values and traditional sliding mode surface, a novel sliding mode surface is constructed. Thirdly, a composite continuous anti-disturbance autopilot is developed, which can guarantee system output converge to reference signal. Finally, a simulation result is presented to demonstrate the effectiveness of the proposed scheme.",

keywords = "Anti-disturbance autopilot, Finite time disturbance observer, Mismatched disturbances, Missile system, Sliding mode control",

author = "Xinge Liu and Haibin Sun and Jiayuan Shan",

note = "Publisher Copyright: {\textcopyright} Springer-Verlag Berlin Heidelberg 2016.; Chinese Intelligent Systems Conference, CISC 2015 ; Conference date: 01-01-2015",

year = "2016",

doi = "10.1007/978-3-662-48386-2_46",

language = "English",

isbn = "9783662483848",

series = "Lecture Notes in Electrical Engineering",

publisher = "Springer Verlag",

pages = "447--455",

editor = "Hongbo Li and Weicun Zhang and Yingmin Jia and Junping Du",

booktitle = "Proceedings of the 2015 Chinese Intelligent Systems Conference",

address = "Germany",

}

Liu, X, Sun, H & Shan, J 2016, Composite continuous anti-disturbance autopilot design for missile system with mismatched disturbances. in H Li, W Zhang, Y Jia & J Du (eds), Proceedings of the 2015 Chinese Intelligent Systems Conference. Lecture Notes in Electrical Engineering, vol. 359, Springer Verlag, pp. 447-455, Chinese Intelligent Systems Conference, CISC 2015, Yangzhou, China, 1/01/15. https://doi.org/10.1007/978-3-662-48386-2_46

Composite continuous anti-disturbance autopilot design for missile system with mismatched disturbances. / Liu, Xinge; Sun, Haibin; Shan, Jiayuan.
Proceedings of the 2015 Chinese Intelligent Systems Conference. ed. / Hongbo Li; Weicun Zhang; Yingmin Jia; Junping Du. Springer Verlag, 2016. p. 447-455 (Lecture Notes in Electrical Engineering; Vol. 359).

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

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T1 - Composite continuous anti-disturbance autopilot design for missile system with mismatched disturbances

AU - Liu, Xinge

AU - Sun, Haibin

AU - Shan, Jiayuan

N1 - Publisher Copyright: © Springer-Verlag Berlin Heidelberg 2016.

PY - 2016

Y1 - 2016

N2 - In this paper, the problem of autopilot design for missile system with mismatched disturbances is considered via a sliding mode control method and finite time disturbance observer. Firstly, a finite time disturbance observer is designed to estimate the mismatched disturbances. Secondly, based on disturbance estimation values and traditional sliding mode surface, a novel sliding mode surface is constructed. Thirdly, a composite continuous anti-disturbance autopilot is developed, which can guarantee system output converge to reference signal. Finally, a simulation result is presented to demonstrate the effectiveness of the proposed scheme.

AB - In this paper, the problem of autopilot design for missile system with mismatched disturbances is considered via a sliding mode control method and finite time disturbance observer. Firstly, a finite time disturbance observer is designed to estimate the mismatched disturbances. Secondly, based on disturbance estimation values and traditional sliding mode surface, a novel sliding mode surface is constructed. Thirdly, a composite continuous anti-disturbance autopilot is developed, which can guarantee system output converge to reference signal. Finally, a simulation result is presented to demonstrate the effectiveness of the proposed scheme.

KW - Anti-disturbance autopilot

KW - Finite time disturbance observer

KW - Mismatched disturbances

KW - Missile system

KW - Sliding mode control

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U2 - 10.1007/978-3-662-48386-2_46

DO - 10.1007/978-3-662-48386-2_46

M3 - Conference contribution

AN - SCOPUS:84952673052

SN - 9783662483848

T3 - Lecture Notes in Electrical Engineering

SP - 447

EP - 455

BT - Proceedings of the 2015 Chinese Intelligent Systems Conference

A2 - Li, Hongbo

A2 - Zhang, Weicun

A2 - Jia, Yingmin

A2 - Du, Junping

PB - Springer Verlag

T2 - Chinese Intelligent Systems Conference, CISC 2015

Y2 - 1 January 2015

ER -

Composite continuous anti-disturbance autopilot design for missile system with mismatched disturbances

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