Finite Time Convergence Cooperative Guidance Law for Non-maneuvering Moving Targets

Wenjie Zhang; Baogang Lu; Qunli Xia

doi:10.1109/ICUS48101.2019.8996078

Finite Time Convergence Cooperative Guidance Law for Non-maneuvering Moving Targets

Wenjie Zhang, Baogang Lu, Qunli Xia

宇航学院

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

1 引用（Scopus）

摘要

A consensus theory-based distributed cooperative guidance law is proposed for multi-missile intercepting a non-maneuvering moving target in this paper. The model is built on the three-dimensional plane. The designed control method consists of three parts: the part along the line of sight (LOS) guarantees salvo attacks of all missiles, the other two part perpendicular to the LOS in vertical and lateral plane ensure the zero LOS angular rates to achieve accurate interceptions. By applying the Lyapunov stability theorem, convergences of all missiles¶ time-to-go (TGO) are verified. Digital simulations prove the accuracy of the designed multi-missile cooperative control method.

源语言	英语
主期刊名	Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019
出版商	Institute of Electrical and Electronics Engineers Inc.
页	7-12
页数	6
ISBN（电子版）	9781728137926
DOI	https://doi.org/10.1109/ICUS48101.2019.8996078
出版状态	已出版 - 10月 2019
活动	2019 IEEE International Conference on Unmanned Systems, ICUS 2019 - Beijing, 中国期限: 17 10月 2019 → 19 10月 2019

出版系列

姓名	Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019

会议

会议	2019 IEEE International Conference on Unmanned Systems, ICUS 2019
国家/地区	中国
市	Beijing
时期	17/10/19 → 19/10/19

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10.1109/ICUS48101.2019.8996078

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链接到 Scopus 的出版物

引用此

Zhang, W., Lu, B., & Xia, Q. (2019). Finite Time Convergence Cooperative Guidance Law for Non-maneuvering Moving Targets. 在 Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019 (页码 7-12). 文章 8996078 (Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICUS48101.2019.8996078

Zhang, Wenjie ; Lu, Baogang ; Xia, Qunli. / Finite Time Convergence Cooperative Guidance Law for Non-maneuvering Moving Targets. Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019. Institute of Electrical and Electronics Engineers Inc., 2019. 页码 7-12 (Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019).

@inproceedings{219b2050a3dc4a4ead57ae5362371584,

title = "Finite Time Convergence Cooperative Guidance Law for Non-maneuvering Moving Targets",

abstract = "A consensus theory-based distributed cooperative guidance law is proposed for multi-missile intercepting a non-maneuvering moving target in this paper. The model is built on the three-dimensional plane. The designed control method consists of three parts: the part along the line of sight (LOS) guarantees salvo attacks of all missiles, the other two part perpendicular to the LOS in vertical and lateral plane ensure the zero LOS angular rates to achieve accurate interceptions. By applying the Lyapunov stability theorem, convergences of all missiles¶ time-to-go (TGO) are verified. Digital simulations prove the accuracy of the designed multi-missile cooperative control method.",

keywords = "Lyapunov stability, Multi-missile, consensus theory, cooperative control, finite time convergence",

author = "Wenjie Zhang and Baogang Lu and Qunli Xia",

note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 2019 IEEE International Conference on Unmanned Systems, ICUS 2019 ; Conference date: 17-10-2019 Through 19-10-2019",

year = "2019",

month = oct,

doi = "10.1109/ICUS48101.2019.8996078",

language = "English",

series = "Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019",

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

pages = "7--12",

booktitle = "Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019",

address = "United States",

}

Zhang, W, Lu, B & Xia, Q 2019, Finite Time Convergence Cooperative Guidance Law for Non-maneuvering Moving Targets. 在 Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019., 8996078, Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019, Institute of Electrical and Electronics Engineers Inc., 页码 7-12, 2019 IEEE International Conference on Unmanned Systems, ICUS 2019, Beijing, 中国, 17/10/19. https://doi.org/10.1109/ICUS48101.2019.8996078

Finite Time Convergence Cooperative Guidance Law for Non-maneuvering Moving Targets. / Zhang, Wenjie; Lu, Baogang; Xia, Qunli.
Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019. Institute of Electrical and Electronics Engineers Inc., 2019. 页码 7-12 8996078 (Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - Finite Time Convergence Cooperative Guidance Law for Non-maneuvering Moving Targets

AU - Zhang, Wenjie

AU - Lu, Baogang

AU - Xia, Qunli

PY - 2019/10

Y1 - 2019/10

N2 - A consensus theory-based distributed cooperative guidance law is proposed for multi-missile intercepting a non-maneuvering moving target in this paper. The model is built on the three-dimensional plane. The designed control method consists of three parts: the part along the line of sight (LOS) guarantees salvo attacks of all missiles, the other two part perpendicular to the LOS in vertical and lateral plane ensure the zero LOS angular rates to achieve accurate interceptions. By applying the Lyapunov stability theorem, convergences of all missiles¶ time-to-go (TGO) are verified. Digital simulations prove the accuracy of the designed multi-missile cooperative control method.

AB - A consensus theory-based distributed cooperative guidance law is proposed for multi-missile intercepting a non-maneuvering moving target in this paper. The model is built on the three-dimensional plane. The designed control method consists of three parts: the part along the line of sight (LOS) guarantees salvo attacks of all missiles, the other two part perpendicular to the LOS in vertical and lateral plane ensure the zero LOS angular rates to achieve accurate interceptions. By applying the Lyapunov stability theorem, convergences of all missiles¶ time-to-go (TGO) are verified. Digital simulations prove the accuracy of the designed multi-missile cooperative control method.

KW - Lyapunov stability

KW - Multi-missile

KW - consensus theory

KW - cooperative control

KW - finite time convergence

UR - http://www.scopus.com/inward/record.url?scp=85080933025&partnerID=8YFLogxK

U2 - 10.1109/ICUS48101.2019.8996078

DO - 10.1109/ICUS48101.2019.8996078

M3 - Conference contribution

AN - SCOPUS:85080933025

T3 - Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019

SP - 7

EP - 12

BT - Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2019 IEEE International Conference on Unmanned Systems, ICUS 2019

Y2 - 17 October 2019 through 19 October 2019

ER -

Zhang W, Lu B, Xia Q. Finite Time Convergence Cooperative Guidance Law for Non-maneuvering Moving Targets. 在 Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019. Institute of Electrical and Electronics Engineers Inc. 2019. 页码 7-12. 8996078. (Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019). doi: 10.1109/ICUS48101.2019.8996078

Finite Time Convergence Cooperative Guidance Law for Non-maneuvering Moving Targets

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