Integrated robust dynamic inversion design of missile guidance and control Based on nonlinear disturbance observer

Yanjun Shu; Shuo Tang

doi:10.1109/IHMSC.2012.106

Integrated robust dynamic inversion design of missile guidance and control Based on nonlinear disturbance observer

Yanjun Shu, Shuo Tang

航天学院

Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

5 引用（Scopus）

摘要

A robust dynamic inversion control law based on nonlinear disturbance observer is proposed for the integrated guidance and control of missile. Firstly the pitch channel of integrated guidance and control model was established. According to this model, a robust nonlinear integrated guidance and control law was designed by adopting dynamic inversion approach. Then, a nonlinear disturbance observer is employed to estimate the unknown compound disturbance and compensate them. Based on the Lyapunov stability theorem, we proved that all signals of the composite closed-loop are uniformly ultimately bounded. Finally, Simulation results demonstrate the effectiveness of the control scheme.

源语言	英语
主期刊名	Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012
页	42-45
页数	4
DOI	https://doi.org/10.1109/IHMSC.2012.106
出版状态	已出版 - 2012
活动	2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012 - Nanchang, Jiangxi, 中国期限: 26 8月 2012 → 27 8月 2012

出版系列

姓名	Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012
卷	2

会议

会议	2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012
国家/地区	中国
市	Nanchang, Jiangxi
时期	26/08/12 → 27/08/12

访问文件

10.1109/IHMSC.2012.106

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链接到 Scopus 的出版物

引用此

Shu, Y., & Tang, S. (2012). Integrated robust dynamic inversion design of missile guidance and control Based on nonlinear disturbance observer. 在 Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012 (页码 42-45). 文章 6305720 (Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012; 卷 2). https://doi.org/10.1109/IHMSC.2012.106

Shu, Yanjun ; Tang, Shuo. / Integrated robust dynamic inversion design of missile guidance and control Based on nonlinear disturbance observer. Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012. 2012. 页码 42-45 (Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012).

@inproceedings{49d914ce4a8a4d19beee22a13f5ed7ec,

title = "Integrated robust dynamic inversion design of missile guidance and control Based on nonlinear disturbance observer",

abstract = "A robust dynamic inversion control law based on nonlinear disturbance observer is proposed for the integrated guidance and control of missile. Firstly the pitch channel of integrated guidance and control model was established. According to this model, a robust nonlinear integrated guidance and control law was designed by adopting dynamic inversion approach. Then, a nonlinear disturbance observer is employed to estimate the unknown compound disturbance and compensate them. Based on the Lyapunov stability theorem, we proved that all signals of the composite closed-loop are uniformly ultimately bounded. Finally, Simulation results demonstrate the effectiveness of the control scheme.",

keywords = "Integrated guidance and control, Nonlinear disturbance observer, Robust dynamic inversion",

author = "Yanjun Shu and Shuo Tang",

year = "2012",

doi = "10.1109/IHMSC.2012.106",

language = "英语",

isbn = "9780769547213",

series = "Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012",

pages = "42--45",

booktitle = "Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012",

note = "2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012 ; Conference date: 26-08-2012 Through 27-08-2012",

}

Shu, Y & Tang, S 2012, Integrated robust dynamic inversion design of missile guidance and control Based on nonlinear disturbance observer. 在 Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012., 6305720, Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012, 卷 2, 页码 42-45, 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012, Nanchang, Jiangxi, 中国, 26/08/12. https://doi.org/10.1109/IHMSC.2012.106

Integrated robust dynamic inversion design of missile guidance and control Based on nonlinear disturbance observer. / Shu, Yanjun; Tang, Shuo.
Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012. 2012. 页码 42-45 6305720 (Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012; 卷 2).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - Integrated robust dynamic inversion design of missile guidance and control Based on nonlinear disturbance observer

AU - Shu, Yanjun

AU - Tang, Shuo

PY - 2012

Y1 - 2012

N2 - A robust dynamic inversion control law based on nonlinear disturbance observer is proposed for the integrated guidance and control of missile. Firstly the pitch channel of integrated guidance and control model was established. According to this model, a robust nonlinear integrated guidance and control law was designed by adopting dynamic inversion approach. Then, a nonlinear disturbance observer is employed to estimate the unknown compound disturbance and compensate them. Based on the Lyapunov stability theorem, we proved that all signals of the composite closed-loop are uniformly ultimately bounded. Finally, Simulation results demonstrate the effectiveness of the control scheme.

AB - A robust dynamic inversion control law based on nonlinear disturbance observer is proposed for the integrated guidance and control of missile. Firstly the pitch channel of integrated guidance and control model was established. According to this model, a robust nonlinear integrated guidance and control law was designed by adopting dynamic inversion approach. Then, a nonlinear disturbance observer is employed to estimate the unknown compound disturbance and compensate them. Based on the Lyapunov stability theorem, we proved that all signals of the composite closed-loop are uniformly ultimately bounded. Finally, Simulation results demonstrate the effectiveness of the control scheme.

KW - Integrated guidance and control

KW - Nonlinear disturbance observer

KW - Robust dynamic inversion

UR - http://www.scopus.com/inward/record.url?scp=84868090435&partnerID=8YFLogxK

U2 - 10.1109/IHMSC.2012.106

DO - 10.1109/IHMSC.2012.106

M3 - 会议稿件

AN - SCOPUS:84868090435

SN - 9780769547213

T3 - Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012

SP - 42

EP - 45

BT - Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012

T2 - 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012

Y2 - 26 August 2012 through 27 August 2012

ER -

Shu Y, Tang S. Integrated robust dynamic inversion design of missile guidance and control Based on nonlinear disturbance observer. 在 Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012. 2012. 页码 42-45. 6305720. (Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012). doi: 10.1109/IHMSC.2012.106

Integrated robust dynamic inversion design of missile guidance and control Based on nonlinear disturbance observer

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