Integrated Guidance and Control for Homing Missiles with Terminal Angular Constraint in Three Dimension Space

Shichao Ma; Aijun Li; Zhigang Wang

doi:10.1109/ICAIIS49377.2020.9194808

Integrated Guidance and Control for Homing Missiles with Terminal Angular Constraint in Three Dimension Space

Shichao Ma, Aijun Li, Zhigang Wang

School of Automation

Northwestern Polytechnical University Xian

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

Abstract

A three dimension integrated guidance and control (3D-IGC) system for homing missiles with terminal angle constraint is designed. Firstly, a nonlinear mathematical model of the homing missile is established. In order to deal with the problem of multiple states regulation of such a nonlinear system, an adaptive multiple sliding surface control methodology is deduced. The frame of 3D-IGC law is accomplished by associating with the backstepping method. The digital simulation results verify that the proposed control law can both satisfy the accuracy of target interception and the constrained conditions of terminal angular. Moreover, it shows strong robustness against parameter uncertainties.

Original language	English
Title of host publication	Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	601-606
Number of pages	6
ISBN (Electronic)	9781728165905
DOIs	https://doi.org/10.1109/ICAIIS49377.2020.9194808
State	Published - Mar 2020
Event	2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020 - Dalian, China Duration: 20 Mar 2020 → 22 Mar 2020

Publication series

Name	Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020

Conference

Conference	2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020
Country/Territory	China
City	Dalian
Period	20/03/20 → 22/03/20

Keywords

3D-IGC
Adaptive multiple sliding surface control
backstepping
terminal angular constraint

Access to Document

10.1109/ICAIIS49377.2020.9194808

Cite this

Ma, S., Li, A., & Wang, Z. (2020). Integrated Guidance and Control for Homing Missiles with Terminal Angular Constraint in Three Dimension Space. In Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020 (pp. 601-606). Article 9194808 (Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICAIIS49377.2020.9194808

Ma, Shichao ; Li, Aijun ; Wang, Zhigang. / Integrated Guidance and Control for Homing Missiles with Terminal Angular Constraint in Three Dimension Space. Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020. Institute of Electrical and Electronics Engineers Inc., 2020. pp. 601-606 (Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020).

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title = "Integrated Guidance and Control for Homing Missiles with Terminal Angular Constraint in Three Dimension Space",

abstract = "A three dimension integrated guidance and control (3D-IGC) system for homing missiles with terminal angle constraint is designed. Firstly, a nonlinear mathematical model of the homing missile is established. In order to deal with the problem of multiple states regulation of such a nonlinear system, an adaptive multiple sliding surface control methodology is deduced. The frame of 3D-IGC law is accomplished by associating with the backstepping method. The digital simulation results verify that the proposed control law can both satisfy the accuracy of target interception and the constrained conditions of terminal angular. Moreover, it shows strong robustness against parameter uncertainties.",

keywords = "3D-IGC, Adaptive multiple sliding surface control, backstepping, terminal angular constraint",

author = "Shichao Ma and Aijun Li and Zhigang Wang",

note = "Publisher Copyright: {\textcopyright} 2020 IEEE.; 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020 ; Conference date: 20-03-2020 Through 22-03-2020",

year = "2020",

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doi = "10.1109/ICAIIS49377.2020.9194808",

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series = "Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020",

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

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Ma, S, Li, A & Wang, Z 2020, Integrated Guidance and Control for Homing Missiles with Terminal Angular Constraint in Three Dimension Space. in Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020., 9194808, Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020, Institute of Electrical and Electronics Engineers Inc., pp. 601-606, 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020, Dalian, China, 20/03/20. https://doi.org/10.1109/ICAIIS49377.2020.9194808

Integrated Guidance and Control for Homing Missiles with Terminal Angular Constraint in Three Dimension Space. / Ma, Shichao; Li, Aijun; Wang, Zhigang.
Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020. Institute of Electrical and Electronics Engineers Inc., 2020. p. 601-606 9194808 (Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020).

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

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N2 - A three dimension integrated guidance and control (3D-IGC) system for homing missiles with terminal angle constraint is designed. Firstly, a nonlinear mathematical model of the homing missile is established. In order to deal with the problem of multiple states regulation of such a nonlinear system, an adaptive multiple sliding surface control methodology is deduced. The frame of 3D-IGC law is accomplished by associating with the backstepping method. The digital simulation results verify that the proposed control law can both satisfy the accuracy of target interception and the constrained conditions of terminal angular. Moreover, it shows strong robustness against parameter uncertainties.

AB - A three dimension integrated guidance and control (3D-IGC) system for homing missiles with terminal angle constraint is designed. Firstly, a nonlinear mathematical model of the homing missile is established. In order to deal with the problem of multiple states regulation of such a nonlinear system, an adaptive multiple sliding surface control methodology is deduced. The frame of 3D-IGC law is accomplished by associating with the backstepping method. The digital simulation results verify that the proposed control law can both satisfy the accuracy of target interception and the constrained conditions of terminal angular. Moreover, it shows strong robustness against parameter uncertainties.

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KW - Adaptive multiple sliding surface control

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Ma S, Li A, Wang Z. Integrated Guidance and Control for Homing Missiles with Terminal Angular Constraint in Three Dimension Space. In Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020. Institute of Electrical and Electronics Engineers Inc. 2020. p. 601-606. 9194808. (Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020). doi: 10.1109/ICAIIS49377.2020.9194808

Integrated Guidance and Control for Homing Missiles with Terminal Angular Constraint in Three Dimension Space

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Keywords

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