Consensus Based Cooperative Guidance with a Leader

Yadong Chen; Lan Wei; Jianan Wang; Chunyan Wang; Dandan Wang; Jiayuan Shan; Ming Xin

doi:10.1109/ICCA51439.2020.9264457

Consensus Based Cooperative Guidance with a Leader

Yadong Chen, Lan Wei, Jianan Wang, Chunyan Wang, Dandan Wang, Jiayuan Shan, Ming Xin

School of Aerospace Engineering

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

1 Citation (Scopus)

Abstract

A cooperative guidance law for missile group with a leader is proposed in this paper. Cooperative guidance is divided into state cooperation stage and Proportional Navigation Guidance (PNG) stage with suppressed guidance command jump at switch point. State cooperation is achieved through cooperative state tracking of a leader missile, where the dynamic of guidance is linerized by adding two auxiliary state variables and a linear cooperative tracking algorithm is adopted. PNG is adopted to accomplish the cooperative impact, because state cooperation stage can not guide missiles to realize the final impact. In the linezrized guidance model, guidance command will be singular when leading angle tends to zero, which is necessary in the terminal stage of guidance.

Original language	English
Title of host publication	2020 IEEE 16th International Conference on Control and Automation, ICCA 2020
Publisher	IEEE Computer Society
Pages	442-446
Number of pages	5
ISBN (Electronic)	9781728190938
DOIs	https://doi.org/10.1109/ICCA51439.2020.9264457
Publication status	Published - 9 Oct 2020
Event	16th IEEE International Conference on Control and Automation, ICCA 2020 - Virtual, Sapporo, Hokkaido, Japan Duration: 9 Oct 2020 → 11 Oct 2020

Publication series

Name	IEEE International Conference on Control and Automation, ICCA
Volume	2020-October
ISSN (Print)	1948-3449
ISSN (Electronic)	1948-3457

Conference

Conference	16th IEEE International Conference on Control and Automation, ICCA 2020
Country/Territory	Japan
City	Virtual, Sapporo, Hokkaido
Period	9/10/20 → 11/10/20

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10.1109/ICCA51439.2020.9264457

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Chen, Y., Wei, L., Wang, J., Wang, C., Wang, D., Shan, J., & Xin, M. (2020). Consensus Based Cooperative Guidance with a Leader. In 2020 IEEE 16th International Conference on Control and Automation, ICCA 2020 (pp. 442-446). Article 9264457 (IEEE International Conference on Control and Automation, ICCA; Vol. 2020-October). IEEE Computer Society. https://doi.org/10.1109/ICCA51439.2020.9264457

@inproceedings{f99570dd05014d148133b3b853febca5,

title = "Consensus Based Cooperative Guidance with a Leader",

abstract = "A cooperative guidance law for missile group with a leader is proposed in this paper. Cooperative guidance is divided into state cooperation stage and Proportional Navigation Guidance (PNG) stage with suppressed guidance command jump at switch point. State cooperation is achieved through cooperative state tracking of a leader missile, where the dynamic of guidance is linerized by adding two auxiliary state variables and a linear cooperative tracking algorithm is adopted. PNG is adopted to accomplish the cooperative impact, because state cooperation stage can not guide missiles to realize the final impact. In the linezrized guidance model, guidance command will be singular when leading angle tends to zero, which is necessary in the terminal stage of guidance.",

author = "Yadong Chen and Lan Wei and Jianan Wang and Chunyan Wang and Dandan Wang and Jiayuan Shan and Ming Xin",

note = "Publisher Copyright: {\textcopyright} 2020 IEEE.; 16th IEEE International Conference on Control and Automation, ICCA 2020 ; Conference date: 09-10-2020 Through 11-10-2020",

year = "2020",

month = oct,

day = "9",

doi = "10.1109/ICCA51439.2020.9264457",

language = "English",

series = "IEEE International Conference on Control and Automation, ICCA",

publisher = "IEEE Computer Society",

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booktitle = "2020 IEEE 16th International Conference on Control and Automation, ICCA 2020",

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}

Chen, Y, Wei, L, Wang, J, Wang, C, Wang, D, Shan, J & Xin, M 2020, Consensus Based Cooperative Guidance with a Leader. in 2020 IEEE 16th International Conference on Control and Automation, ICCA 2020., 9264457, IEEE International Conference on Control and Automation, ICCA, vol. 2020-October, IEEE Computer Society, pp. 442-446, 16th IEEE International Conference on Control and Automation, ICCA 2020, Virtual, Sapporo, Hokkaido, Japan, 9/10/20. https://doi.org/10.1109/ICCA51439.2020.9264457

Consensus Based Cooperative Guidance with a Leader. / Chen, Yadong; Wei, Lan; Wang, Jianan et al.
2020 IEEE 16th International Conference on Control and Automation, ICCA 2020. IEEE Computer Society, 2020. p. 442-446 9264457 (IEEE International Conference on Control and Automation, ICCA; Vol. 2020-October).

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

TY - GEN

T1 - Consensus Based Cooperative Guidance with a Leader

AU - Chen, Yadong

AU - Wei, Lan

AU - Wang, Jianan

AU - Wang, Chunyan

AU - Wang, Dandan

AU - Shan, Jiayuan

AU - Xin, Ming

PY - 2020/10/9

Y1 - 2020/10/9

N2 - A cooperative guidance law for missile group with a leader is proposed in this paper. Cooperative guidance is divided into state cooperation stage and Proportional Navigation Guidance (PNG) stage with suppressed guidance command jump at switch point. State cooperation is achieved through cooperative state tracking of a leader missile, where the dynamic of guidance is linerized by adding two auxiliary state variables and a linear cooperative tracking algorithm is adopted. PNG is adopted to accomplish the cooperative impact, because state cooperation stage can not guide missiles to realize the final impact. In the linezrized guidance model, guidance command will be singular when leading angle tends to zero, which is necessary in the terminal stage of guidance.

AB - A cooperative guidance law for missile group with a leader is proposed in this paper. Cooperative guidance is divided into state cooperation stage and Proportional Navigation Guidance (PNG) stage with suppressed guidance command jump at switch point. State cooperation is achieved through cooperative state tracking of a leader missile, where the dynamic of guidance is linerized by adding two auxiliary state variables and a linear cooperative tracking algorithm is adopted. PNG is adopted to accomplish the cooperative impact, because state cooperation stage can not guide missiles to realize the final impact. In the linezrized guidance model, guidance command will be singular when leading angle tends to zero, which is necessary in the terminal stage of guidance.

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DO - 10.1109/ICCA51439.2020.9264457

M3 - Conference contribution

AN - SCOPUS:85098092356

T3 - IEEE International Conference on Control and Automation, ICCA

SP - 442

EP - 446

BT - 2020 IEEE 16th International Conference on Control and Automation, ICCA 2020

PB - IEEE Computer Society

T2 - 16th IEEE International Conference on Control and Automation, ICCA 2020

Y2 - 9 October 2020 through 11 October 2020

ER -

Consensus Based Cooperative Guidance with a Leader

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