Adaptive nonsingular guidance law against maneuvering targets

Zhao Bin; Zhou Jun

doi:10.1109/ICCRE.2018.8376477

Adaptive nonsingular guidance law against maneuvering targets

Zhao Bin, Zhou Jun

School of Astronautics

Northwestern Polytechnical University Xian

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

Abstract

A novel three dimensional adaptive nonsingular guidance law against maneuvering targets is documented. Firstly, the nonlinear state equation is given regarding the target motion as unknown bounded external disturbance. Secondly, a new adaptive law estimating the square of the target acceleration bound is proposed based on which the adaptive nonsingular guidance law is derived, which solve the problem of non-smooth and chattering phenomenon; Thirdly, the finite time convergence of the guidance system is proved by the theory of finite time stability. Finally, simulation results of different target maneuver scenarios indicate that the proposed guidance law can not only ensure the fast convergent speed, but also provide smooth missile acceleration command, which shows its superiority.

Original language	English
Title of host publication	2018 3rd International Conference on Control and Robotics Engineering, ICCRE 2018
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	264-269
Number of pages	6
ISBN (Electronic)	9781538666630
DOIs	https://doi.org/10.1109/ICCRE.2018.8376477
State	Published - 8 Jun 2018
Event	3rd International Conference on Control and Robotics Engineering, ICCRE 2018 - Nagoya, Japan Duration: 20 Apr 2018 → 23 Apr 2018

Publication series

Name	2018 3rd International Conference on Control and Robotics Engineering, ICCRE 2018

Conference

Conference	3rd International Conference on Control and Robotics Engineering, ICCRE 2018
Country/Territory	Japan
City	Nagoya
Period	20/04/18 → 23/04/18

Keywords

adaptive law
finite time convergence
nonsingular
terminal sliding mode

Access to Document

10.1109/ICCRE.2018.8376477

Cite this

Bin, Z., & Jun, Z. (2018). Adaptive nonsingular guidance law against maneuvering targets. In 2018 3rd International Conference on Control and Robotics Engineering, ICCRE 2018 (pp. 264-269). (2018 3rd International Conference on Control and Robotics Engineering, ICCRE 2018). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICCRE.2018.8376477

@inproceedings{7895f529aa324a2a9eb0fb6511e5945b,

title = "Adaptive nonsingular guidance law against maneuvering targets",

abstract = "A novel three dimensional adaptive nonsingular guidance law against maneuvering targets is documented. Firstly, the nonlinear state equation is given regarding the target motion as unknown bounded external disturbance. Secondly, a new adaptive law estimating the square of the target acceleration bound is proposed based on which the adaptive nonsingular guidance law is derived, which solve the problem of non-smooth and chattering phenomenon; Thirdly, the finite time convergence of the guidance system is proved by the theory of finite time stability. Finally, simulation results of different target maneuver scenarios indicate that the proposed guidance law can not only ensure the fast convergent speed, but also provide smooth missile acceleration command, which shows its superiority.",

keywords = "adaptive law, finite time convergence, nonsingular, terminal sliding mode",

author = "Zhao Bin and Zhou Jun",

note = "Publisher Copyright: {\textcopyright} 2018 IEEE.; 3rd International Conference on Control and Robotics Engineering, ICCRE 2018 ; Conference date: 20-04-2018 Through 23-04-2018",

year = "2018",

month = jun,

day = "8",

doi = "10.1109/ICCRE.2018.8376477",

language = "英语",

series = "2018 3rd International Conference on Control and Robotics Engineering, ICCRE 2018",

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

pages = "264--269",

booktitle = "2018 3rd International Conference on Control and Robotics Engineering, ICCRE 2018",

}

Bin, Z & Jun, Z 2018, Adaptive nonsingular guidance law against maneuvering targets. in 2018 3rd International Conference on Control and Robotics Engineering, ICCRE 2018. 2018 3rd International Conference on Control and Robotics Engineering, ICCRE 2018, Institute of Electrical and Electronics Engineers Inc., pp. 264-269, 3rd International Conference on Control and Robotics Engineering, ICCRE 2018, Nagoya, Japan, 20/04/18. https://doi.org/10.1109/ICCRE.2018.8376477

Adaptive nonsingular guidance law against maneuvering targets. / Bin, Zhao; Jun, Zhou.
2018 3rd International Conference on Control and Robotics Engineering, ICCRE 2018. Institute of Electrical and Electronics Engineers Inc., 2018. p. 264-269 (2018 3rd International Conference on Control and Robotics Engineering, ICCRE 2018).

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

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AU - Bin, Zhao

AU - Jun, Zhou

PY - 2018/6/8

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N2 - A novel three dimensional adaptive nonsingular guidance law against maneuvering targets is documented. Firstly, the nonlinear state equation is given regarding the target motion as unknown bounded external disturbance. Secondly, a new adaptive law estimating the square of the target acceleration bound is proposed based on which the adaptive nonsingular guidance law is derived, which solve the problem of non-smooth and chattering phenomenon; Thirdly, the finite time convergence of the guidance system is proved by the theory of finite time stability. Finally, simulation results of different target maneuver scenarios indicate that the proposed guidance law can not only ensure the fast convergent speed, but also provide smooth missile acceleration command, which shows its superiority.

AB - A novel three dimensional adaptive nonsingular guidance law against maneuvering targets is documented. Firstly, the nonlinear state equation is given regarding the target motion as unknown bounded external disturbance. Secondly, a new adaptive law estimating the square of the target acceleration bound is proposed based on which the adaptive nonsingular guidance law is derived, which solve the problem of non-smooth and chattering phenomenon; Thirdly, the finite time convergence of the guidance system is proved by the theory of finite time stability. Finally, simulation results of different target maneuver scenarios indicate that the proposed guidance law can not only ensure the fast convergent speed, but also provide smooth missile acceleration command, which shows its superiority.

KW - adaptive law

KW - finite time convergence

KW - nonsingular

KW - terminal sliding mode

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M3 - 会议稿件

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BT - 2018 3rd International Conference on Control and Robotics Engineering, ICCRE 2018

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 3rd International Conference on Control and Robotics Engineering, ICCRE 2018

Y2 - 20 April 2018 through 23 April 2018

ER -

Adaptive nonsingular guidance law against maneuvering targets

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Publication series

Conference

Keywords

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