Command filtered adaptive control for integrated missile guidance and autopilot with terminal angular constraint

Xiaoling Liang; Ning Wang; Yancheng Liu; Shuailin Lv; Bin Xu

doi:10.1109/WCICA.2016.7578525

Command filtered adaptive control for integrated missile guidance and autopilot with terminal angular constraint

Xiaoling Liang
, Ning Wang
, Yancheng Liu
, Shuailin Lv
, Bin Xu

School of Automation

Dalian Maritime University

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

1 Scopus citations

Abstract

For homing missiles considering terminal angular constraint, integrated design of guidance and control utilizing adaptive command filtered backstepping is studied in this paper. The proposed control scheme guarantees not only the stability of the missile dynamics with state constraints but also the interception performance with a desired terminal attitude angle. An adaptive law is introduced to compensate unknown uncertainties in the varying-time system. Simulation results are further presented to show the effectiveness and performance of the proposed approach.

Original language	English
Title of host publication	Proceedings of the 2016 12th World Congress on Intelligent Control and Automation, WCICA 2016
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	715-720
Number of pages	6
ISBN (Electronic)	9781467384148
DOIs	https://doi.org/10.1109/WCICA.2016.7578525
State	Published - 27 Sep 2016
Event	12th World Congress on Intelligent Control and Automation, WCICA 2016 - Guilin, China Duration: 12 Jun 2016 → 15 Jun 2016

Publication series

Name	Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
Volume	2016-September

Conference

Conference	12th World Congress on Intelligent Control and Automation, WCICA 2016
Country/Territory	China
City	Guilin
Period	12/06/16 → 15/06/16

Access to Document

10.1109/WCICA.2016.7578525

Cite this

Liang, X., Wang, N., Liu, Y., Lv, S., & Xu, B. (2016). Command filtered adaptive control for integrated missile guidance and autopilot with terminal angular constraint. In Proceedings of the 2016 12th World Congress on Intelligent Control and Automation, WCICA 2016 (pp. 715-720). Article 7578525 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA); Vol. 2016-September). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/WCICA.2016.7578525

Liang, Xiaoling ; Wang, Ning ; Liu, Yancheng et al. / Command filtered adaptive control for integrated missile guidance and autopilot with terminal angular constraint. Proceedings of the 2016 12th World Congress on Intelligent Control and Automation, WCICA 2016. Institute of Electrical and Electronics Engineers Inc., 2016. pp. 715-720 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA)).

@inproceedings{f145013228c34104a1bf0fd67da5490f,

title = "Command filtered adaptive control for integrated missile guidance and autopilot with terminal angular constraint",

abstract = "For homing missiles considering terminal angular constraint, integrated design of guidance and control utilizing adaptive command filtered backstepping is studied in this paper. The proposed control scheme guarantees not only the stability of the missile dynamics with state constraints but also the interception performance with a desired terminal attitude angle. An adaptive law is introduced to compensate unknown uncertainties in the varying-time system. Simulation results are further presented to show the effectiveness and performance of the proposed approach.",

author = "Xiaoling Liang and Ning Wang and Yancheng Liu and Shuailin Lv and Bin Xu",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 12th World Congress on Intelligent Control and Automation, WCICA 2016 ; Conference date: 12-06-2016 Through 15-06-2016",

year = "2016",

month = sep,

day = "27",

doi = "10.1109/WCICA.2016.7578525",

language = "英语",

series = "Proceedings of the World Congress on Intelligent Control and Automation (WCICA)",

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

pages = "715--720",

booktitle = "Proceedings of the 2016 12th World Congress on Intelligent Control and Automation, WCICA 2016",

}

Liang, X, Wang, N, Liu, Y, Lv, S & Xu, B 2016, Command filtered adaptive control for integrated missile guidance and autopilot with terminal angular constraint. in Proceedings of the 2016 12th World Congress on Intelligent Control and Automation, WCICA 2016., 7578525, Proceedings of the World Congress on Intelligent Control and Automation (WCICA), vol. 2016-September, Institute of Electrical and Electronics Engineers Inc., pp. 715-720, 12th World Congress on Intelligent Control and Automation, WCICA 2016, Guilin, China, 12/06/16. https://doi.org/10.1109/WCICA.2016.7578525

Command filtered adaptive control for integrated missile guidance and autopilot with terminal angular constraint. / Liang, Xiaoling; Wang, Ning; Liu, Yancheng et al.
Proceedings of the 2016 12th World Congress on Intelligent Control and Automation, WCICA 2016. Institute of Electrical and Electronics Engineers Inc., 2016. p. 715-720 7578525 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA); Vol. 2016-September).

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

TY - GEN

T1 - Command filtered adaptive control for integrated missile guidance and autopilot with terminal angular constraint

AU - Liang, Xiaoling

AU - Wang, Ning

AU - Liu, Yancheng

AU - Lv, Shuailin

AU - Xu, Bin

PY - 2016/9/27

Y1 - 2016/9/27

N2 - For homing missiles considering terminal angular constraint, integrated design of guidance and control utilizing adaptive command filtered backstepping is studied in this paper. The proposed control scheme guarantees not only the stability of the missile dynamics with state constraints but also the interception performance with a desired terminal attitude angle. An adaptive law is introduced to compensate unknown uncertainties in the varying-time system. Simulation results are further presented to show the effectiveness and performance of the proposed approach.

AB - For homing missiles considering terminal angular constraint, integrated design of guidance and control utilizing adaptive command filtered backstepping is studied in this paper. The proposed control scheme guarantees not only the stability of the missile dynamics with state constraints but also the interception performance with a desired terminal attitude angle. An adaptive law is introduced to compensate unknown uncertainties in the varying-time system. Simulation results are further presented to show the effectiveness and performance of the proposed approach.

UR - https://www.scopus.com/pages/publications/84991699766

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DO - 10.1109/WCICA.2016.7578525

M3 - 会议稿件

AN - SCOPUS:84991699766

T3 - Proceedings of the World Congress on Intelligent Control and Automation (WCICA)

SP - 715

EP - 720

BT - Proceedings of the 2016 12th World Congress on Intelligent Control and Automation, WCICA 2016

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 12th World Congress on Intelligent Control and Automation, WCICA 2016

Y2 - 12 June 2016 through 15 June 2016

ER -

Liang X, Wang N, Liu Y, Lv S, Xu B. Command filtered adaptive control for integrated missile guidance and autopilot with terminal angular constraint. In Proceedings of the 2016 12th World Congress on Intelligent Control and Automation, WCICA 2016. Institute of Electrical and Electronics Engineers Inc. 2016. p. 715-720. 7578525. (Proceedings of the World Congress on Intelligent Control and Automation (WCICA)). doi: 10.1109/WCICA.2016.7578525

Command filtered adaptive control for integrated missile guidance and autopilot with terminal angular constraint

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