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

School of Astronautics

Northwestern Polytechnical University Xian

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

5 Scopus citations

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.

Original language	English
Title of host publication	Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012
Pages	42-45
Number of pages	4
DOIs	https://doi.org/10.1109/IHMSC.2012.106
State	Published - 2012
Event	2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012 - Nanchang, Jiangxi, China Duration: 26 Aug 2012 → 27 Aug 2012

Publication series

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

Conference

Conference	2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012
Country/Territory	China
City	Nanchang, Jiangxi
Period	26/08/12 → 27/08/12

Keywords

Integrated guidance and control
Nonlinear disturbance observer
Robust dynamic inversion

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10.1109/IHMSC.2012.106

Cite this

Shu, Y., & Tang, S. (2012). Integrated robust dynamic inversion design of missile guidance and control Based on nonlinear disturbance observer. In Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012 (pp. 42-45). Article 6305720 (Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012; Vol. 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. pp. 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. in 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, vol. 2, pp. 42-45, 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012, Nanchang, Jiangxi, China, 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. p. 42-45 6305720 (Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012; Vol. 2).

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

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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

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DO - 10.1109/IHMSC.2012.106

M3 - 会议稿件

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SN - 9780769547213

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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

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Shu Y, Tang S. Integrated robust dynamic inversion design of missile guidance and control Based on nonlinear disturbance observer. In Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012. 2012. p. 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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